DS9 Document EFTA00618292

CAMP Amnia/mop r4e von' n' 737-72UB3 REVISION 21 S/N 29273 (YG006) VP-BBJ OWNER: PICTON II LTD. OPERATOR: PICTON II LTD. ADDRESS: C/O JET AVIATION ADDRESS: C/O JET AVIATION GENEVA AIRPORT CH-1215 GENEVA AIRPORT CH-1215 PHONE: PHONE: FAX: FAX: ANALYST: DENNIS RUFFINI EMAIL: WWW.CANIPSYSTEMS.COM lr) PLEASE RECORD CHANGES TO ADDRESS, LAST ACTUALS (IF ANY) AND FAX THIS SHEET BACK TO CAMP. AIRCRAFT SERIAL/REGNO: 29273 (YG006)/VP-BBJ MODEL: 737-72UB3 REVISION 21 MANUFACTURER: BOEING COMPANY DATES LAST ACTUALS CURRENT ACTUAL INSERVICE DATE: 08-OCT-1999 3753:19 NC HRS as of 30-JUN-2014 NC HRS as of _i_ii 922 AFL as of 30-JUN-2014 AFL as of _i_t 3455:18 APH as of 30-JUN-2014 APH as of _/_/ APU SERIAL/PART: P-5180/3800702-1 MODEL: 131-9B MANUFACTURER: HONEYWELL INSTALLED ON 25-1UN-2010 LAST ACTUALS CURRENT ACTUAL 3001 AR! HRS 3455:18 APU HRS as of 30-JUN-2014 APU HRS as of _/_/ 2487 APUS 2961 APUS as of 30-JUN-2014 APUS as of _/_/ ENGINE NO. 1 SERIAL/PART: 874437/CFM56-7827/53 MODEL: CFM56-7627/63 MANUFACTURER: CFM INTERNATIONAL S.A. INSTALLED ON 05-MAY-2011 LAST ACTUALS CURRENT ACTUAL 3556:48 ENG. HRS 3525:36 NC HRS 3753:19 ENG. HRS as of 30-JUN-2014 ENG. HRS as of _/_/ 821 ENC 886 ENC as of 30-JUN-2014 ENC as of _/_/ ENGINE NO. 2 SERIAL/PART: 874438/CFM56-7827/B3 MODEL: CFM56-7627/63 MANUFACTURER: CFM INTERNATIONAL S.A. INSTALLED ON 08-OCT-1999 LAST ACTUALS CURRENT ACTUAL 44 ENG. HRS 44 NC HRS 3753:19 ENG. HRS as of 30-JUN-2014 ENG. HRS as of _/_/ 15 ENC 886 ENC as of 30-JUN-2014 ENC as of _i_t BOEING AND BM ME TRADEMARKS OF THE BOEING COMPANY 05-AUG-2014 AD/Service Information Report CAMP SYSTEMS 1 Of 748 EFTA00618292 CAMP AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC COM M-7200-02-01189 EROS CREW OXYGEN MASK. COMMUNIQUE MOS - Is) COM M-7200-02-01290 INSPECT ENGINE STRUT AFT FAIRING FOR WATER ACCUMULATION. COMMUNIQUE MOS AFL 4000 (s) COM M-7200-03-00936 VISUAL INSPECTION FORWARD GRAY WATER DRAIN MAST FOR POSSIBLE FATIGUE CRACKS. COMMUNIQUE MOS 500 (s) MC 737-21-1149 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 SUPERSEDED FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R01 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R02 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R03 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R04 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R05 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 2 Of 748 @ Camp Systems EFTA00618293 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC MC 737-21-1149 R06 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R07 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 ROB AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R09 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 RIO AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FR0M 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R11 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FR0M 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R12 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FR0M 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R13 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FR0M 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R14 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 3 Of 748 @ Camp Systems EFTA00618294 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC MC 737-21-1149 R15 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 RI6 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 RI8 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R19 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R20 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R21 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R22 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-21-1149 R23 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE CABIN ALTITUDE FROM 8000 FEET TO 6500 FEET AT 41.000 FEET FLIGHT ALTITUDE. MASTER CHANGE MOS MC 737-24-1196 RI ELECTRICAL POWER- STANDBY POWER SYSTEM - CHANGE THE ELECTRICAL POWER SYSTEM TO PROVIDE 60 SUPERSEDED MINUTES OF STANDBY POWER FOR THE AIRPLANE BASIC STANDBY LOADS IN UEU OF THE 30 MINUTES (SUPERSEDED BY MC 737-24-1196 R2). MASTER CHANGE MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 4 Of 748 @ Camp Systems EFTA00618295 CAMP fin. thermiewlqi AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC MC 737-32-1478 SB -AP737-34-01 SB 01930-38-1 LANDING GEAR - MAIN LANDING GEAR BRAKE - REPLACEMENT OF HONEYWELL STANDARD STEEL BRAKES WITH SUPERSEDED HONEYWELL HIGH CAPACITY STEEL BRAKES (SUPERSEDED BY MC 737-32-1478 RI ). MASTER CHANGE . SERVICE BULLETIN . SERVICE BULLETIN MOS MOS MOS - Is) - (s) 19-DEC-2000 SB 1153154-47-06 R1 ENVIRONMENTAL CONTROL - NITROGEN GENERATION SYSTEM CONTROLLER (NGSC)- OXYGEN SENSOR INTERFACE CHANGE. MODIFICATION OF PN 1153154-4. PN 1153154-5. AND PN 1153154-6. SERVICE BULLETIN MOS 03-FEB-2014 SB 233A3202-28-01 P5-2 FUEL CONTROL MODULE ASSEMBLY MODIFICATION. SERVICE BULLETIN MOS 03-MAY-2001 - (s) SB 233A3202-28-01 R1 P5-2 FUEL CONTROL MODULE ASSEMBLY MODIFICATION. SERVICE BULLETIN MOS SB 233A3202-28-02 - Is) DISTRIBUTION - P5-2 FUEL SYSTEM MODULE - PW ASSEMBLY CIRCUIT BOARD REPLACEMENT. SERVICE BULLETIN MOS SB 233A3202-28-02R1 DISTRIBUTION - P5-2 FUEL SYSTEM MODULE - PW ASSEMBLY CIRCUIT BOARD REPLACEMENT. SERVICE BULLETIN MOS 28-FEB-2002 SB 233A3202-28-03 FUEL - DISTRIBUTION - P5-2 CONTROL SYSTEM MODULE ASSEMBLY- CENTER FUEL TANK BOOST PUMP AUTO SHOTOFF MODIFICATION.. SERVICE BULLETIN MOS I2-JAN-2006 SB 233A3205-24-01 GENERATOR DRIVE AND STANDBY POWER MODULE ASSEMBLY CHANGE. SERVICE BULLETIN MOS 26-JUL-2001 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 5 Of 748 @ Camp Systems EFTA00618296 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 233A3209-31-01 14-NOV-2CO2 SB 2344-5320-100 SB 28-01 SB 28-01 R2 SB 285A1010-27.04 28-JUN-2001 SB 285A1600-32-01 11-MAY-2CCO MODIFICATION OF THE P5-3 FLIGHT CONTROLS MODULE. SERVICE BULLETIN MOS SERVICE BULLETIN MOS (s) x-RAY INSPECTION CRANE HYDRO-AIRE. SERVICE BULLETIN MOS (s) x-RAY INSPECTION CRANE HYDRO-AIRE. SERVICE BULLETIN MOS AFL ELEVATOR AND TAB STALL MANAGEMENT YAW DAMPER SOFTWARE CHANGE - COMPONENT. SERVICE BULLETIN MOS PROXIMITY SENSOR ELECTRONIC UNIT - UPGRADE FROM -2 TO -3 CONFIGURATION. SERVICE BULLETIN MOS COMPLIED WITH SB 285A1600-32-02 25-JUL-2001 PROXIMITY SWITCH ELECTRONICS UNIT CHANGE - COMPONENT. SERVICE BULLETIN MOS SB 285A1840-24-02 MODIFICATION OF THE P5-13 ELECTRIC METERS. BATTERY AND GALLEY POWER MODULE ASSEMBLY. SERVICE BULLETIN MOS 28-AUG-2CO3 SB 285W0024-23-03 Fti CABIN ATTENDANT HANDSET I FLIGHT DECK HANDSET SHELL REPLACEMENT. SERVICE BULLETIN MOS 25-JUL-2001 . SB 321444636.1904 PNEUMATIC - HIGH STAGE VALVE - REWORK THE HIGH STAGE VALVE. PN 3214446-4. SERIES 6 OR PN 3214146-4. CUSTOMER SERIES 7 TO PN 3214446-4. SERIES 8 (CHANGE MOD 9). SERVICE BULLETIN CONVENIENCE MOS 25-JUL-2013 ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 6 Of 748 Camp Systems EFTA00618297 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 3214552-36-1899 R1 PNEUMATIC - PRESSURE REGULATOR AND SHUTOFF VALVE- REWORK PRESSURE REGULATOR AND SHUTOFF RECOMMENDED VALVE. PN 32145524. SERIES 1 TO PN 3214552-6. MOD 1. SERVICE BULLETIN MOS 05-AUG-2013 SB 3214552-36-1905 PNEUMATIC - PRESSURE REGULATOR AND SHUTOFF VALVE- REWORK THE PRESSURE REGULATOR AND SHUTOFF CUSTOMER VALVE. PN 3214552-5. SERIES 5 TO PN 3214552-5. SERIES 6 (CHANGE MOD 5) AND PN 3214552-6. SERIES 1 AND CONVENIENCE SERIES 2 TO PN 3214552-6. SERIES 3 (CHANGE MOD 2). SERVICE BULLETIN MOS 26-JUL-2013 SB 3215618-30-1895 ICE AND RAIN PROTECTION- NOSE COWL ANTI-ICE VALVE- REWORK THE NOSE COWL ANTI-ICE VALVE PN 3215618-4 SUPERSEDED TO PN 3215618-5 (SUPERSEDED BY SB 3215618-30-1895 R1). SERVICE BULLETIN MOS SB 3215618-30-1895 R1 ICE AND RAIN PROTECTION- NOSE COWL ANTI-ICE VALVE- REWORK THE NOSE COWL ANTI-ICE VALVE. PN SUPERSEDED 3215618-4 TO PN 3215618-5 (SUPERSEDED BY SB 3215618-30-1895 R2). SERVICE BULLETIN MOS SB 3215618-30-1895 R2 ICE AND RAIN PROTECTION- NOSE COWL ANTI-ICE VALVE- REWORK THE NOSE COWL ANTI-ICE VALVE. PN OPTIONAL 3215618-4 TO PN 3215618-5. SERVICE BULLETIN MOS 24-JAN-2014 SB 417A6110-23-01 ATTENDANT PANEL INTEGRATED HANDSET CONTROLLER REPLACEMENT. SERVICE BULLETIN MOS 31-MAY-2001 SB 504443-25-01R3 AF1SAFE - INSPECTION OF RESTRAINT SYSTEM END RELEASE BUCKLE. SERVICE BULLETIN NOT APPLICABLE - TO PN NOT INSTALLED ON AIRCRAFT. MOS 18-AUG-2006 2633:50 AFL 633 SB 65-52801-49-08 AUXILIARY POWER CONTROL UNIT ASSEMBLY MODIFICATION, SERVICE BULLETIN MOS - (s) SB 65C16237-32-02 LANDING GEAR, SERVICE BULLETIN MOS 28-MAR-2002 - Is) SB 72-000 COMPLIANCE AND INTERCHANGEABILITY STATEMENTS USED IN CFM56-78 SERVICE BULLETINS. SERVICE BULLETIN MOS - Is) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 7 Of 748 @ Camp Systems EFTA00618298 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 734-16100-52-2 RI 18-MAR-2005 SB 737-00-1009 I4-APR-20 I DOORS - AIRSTAIR DOOR LATCH LINEAR ACTUATOR - MODIFY ACTUATOR FROM PM 734-16100-01 TO PIN 734-16103-02. SERVICE BULLETIN MOS AFL 12-N0V-2010 3477:55 848 ADMINISTRATIVE - GENERAL - AIRCRAFT GENERAL- DAMAGE TOLERANCE INSPECTION DATA - MASTER CHANGE RECOMMENDED MODIFICATIONS. SERVICE BULLETIN MOS SB 737-11-1076 PLACARDS AND MARKINGS - EXTERIOR PLACARDS AND MARKINGS - NACELLE AND POWER PLANT - THRUST RECOMMENDED REVERSER MAINTENANCE WARNING PLACARD INSTALLATION. SERVICE BULLETIN MOS 06-MAY-1999 - (s) SB 737-11-1077 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] RI). SERVICE BULLETIN MOS SB 737-11-1077 RI PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R2). SERVICE BULLETIN MOS SB 737-11-1077 RIO PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R11), SERVICE BULLETIN MOS SB 737-11-1077 R11 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R12). SERVICE BULLETIN MOS SB 737-11-1077 R12 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R13). SERVICE BULLETIN MOS SB 737-11-1077 R13 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R14). SERVICE BULLETIN MOS COMPUED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 8 Of 748 @ Camp Systems EFTA00618299 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-11-1077 R14 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SI3 [SSN REDACTED] R15). SERVICE BULLETIN MOS SB 737-11-1077 R15 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R16). SERVICE BULLETIN MOS SB 737-11-1077 R16 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R17). SERVICE BULLETIN MOS SB 737-11-1077 R17 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R18). SERVICE BULLETIN MOS 58 [SSN REDACTED] R18 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R19). SERVICE BULLETIN MOS 58 [SSN REDACTED] R19 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R20). SERVICE BULLETIN MOS 58 [SSN REDACTED] R2 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R3). SERVICE BULLETIN MOS SB 737-11-1077 R20 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R21). SERVICE BULLETIN MOS SB 737-11-1077 R21 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R22). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 9 Of 748 @ Camp Systems EFTA00618300 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-11-1077 R22 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SI3 [SSN REDACTED] R23). SERVICE BULLETIN MOS SB 737-11-1077 R23 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R24). SERVICE BULLETIN MOS SB 737-11-1077 R24 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R25). SERVICE BULLETIN MOS SB 737-11-1077 R25 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R26). SERVICE BULLETIN MOS 58 [SSN REDACTED] R26 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R27). SERVICE BULLETIN MOS 58 [SSN REDACTED] R27 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R28). SERVICE BULLETIN MOS 58 [SSN REDACTED] R28 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R29). SERVICE BULLETIN MOS SB 737-11-1077 R29 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R30). SERVICE BULLETIN MOS SB 737-11-1077 R3 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R4). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 10 Of 748 @ Camp Systems EFTA00618301 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-11-1077 R30 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SI3 [SSN REDACTED] R31). SERVICE BULLETIN MOS SB 737-11-1077 R31 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R32). SERVICE BULLETIN MOS SB 737-11-1077 R32 PLACARDS AND MARKINGS - INTERIOR PLACARDS - CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R33). SERVICE BULLETIN MOS SB 737-11-1077 R33 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R34). SERVICE BULLETIN MOS 58 [SSN REDACTED] R34 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R35). SERVICE BULLETIN MOS 58 [SSN REDACTED] R35 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R36). SERVICE BULLETIN MOS 58 [SSN REDACTED] R36 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R37). SERVICE BULLETIN MOS SB 737-11-1077 R37 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R38). SERVICE BULLETIN MOS SB 737-11-1077 R38 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R39). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 11 Of 748 @ Camp Systems EFTA00618302 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-11-1077 R39 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R40). SERVICE BULLETIN MOS SB 737-11-1077 R4 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 RS). SERVICE BULLETIN MOS SB 737-11-1077 R40 PLACARDS AND MARKINGS - INTERIOR PLACARDS - CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R41). SERVICE BULLETIN MOS SB 737-11-1077 R41 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R42). SERVICE BULLETIN MOS 58 [SSN REDACTED] R42 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R43). SERVICE BULLETIN MOS 58 [SSN REDACTED] R43 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R44). SERVICE BULLETIN MOS 58 [SSN REDACTED] R44 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R45). SERVICE BULLETIN MOS SB 737-11-1077 R45 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R46). SERVICE BULLETIN MOS SB 737-11-1077 R46 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R47), SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 12 Of 748 @ Camp Systems EFTA00618303 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-11-1077 R47 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SI3 [SSN REDACTED] R48). SERVICE BULLETIN MOS SB 737-11-1077 R48 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R49). SERVICE BULLETIN MOS SB 737-11-1077 R49 PLACARDS AND MARKINGS - INTERIOR PLACARDS - CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R50). SERVICE BULLETIN MOS SB 737-11-1077 RS PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R6). SERVICE BULLETIN MOS 58 [SSN REDACTED] R50 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R51). SERVICE BULLETIN MOS 58 [SSN REDACTED] R51 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R52). SERVICE BULLETIN MOS 58 [SSN REDACTED] R52 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R53). SERVICE BULLETIN MOS SB 737-11-1077 R53 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R54). SERVICE BULLETIN MOS SB 737-11-1077 R54 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R55), SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 13 Of 748 @ Camp Systems EFTA00618304 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-11-1077 R55 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SI3 [SSN REDACTED] R56). SERVICE BULLETIN MOS SB 737-11-1077 R56 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R57), SERVICE BULLETIN MOS SB 737-11-1077 R57 PLACARDS AND MARKINGS - INTERIOR PLACARDS - CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R58). SERVICE BULLETIN MOS SB 737-11-1077 R58 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R59). SERVICE BULLETIN MOS 58 [SSN REDACTED] R59 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R60). SERVICE BULLETIN MOS 58 [SSN REDACTED] R6 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R7). SERVICE BULLETIN MOS 58 [SSN REDACTED] R60 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R61). SERVICE BULLETIN MOS SB 737-11-1077 R61 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R62). SERVICE BULLETIN MOS SB 737-11-1077 R62 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R63), SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 14 Of 748 @ Camp Systems EFTA00618305 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-11-1077 R63 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SI3 [SSN REDACTED] R64). SERVICE BULLETIN MOS SB 737-11-1077 R64 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R65). SERVICE BULLETIN MOS SB 737-11-1077 R65 PLACARDS AND MARKINGS - INTERIOR PLACARDS - CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R66). SERVICE BULLETIN MOS SB 737-11-1077 R66 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R67). SERVICE BULLETIN MOS 58 [SSN REDACTED] R67 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R68). SERVICE BULLETIN MOS 58 [SSN REDACTED] R68 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY S8 [SSN REDACTED] R69). SERVICE BULLETIN MOS 58 [SSN REDACTED] R69 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R70). SERVICE BULLETIN MOS SB 737-11-1077 R7 PLACARDS AND MARKINGS - INTERIOR PLACARDS- CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R8). SERVICE BULLETIN MOS SB 737-11-1077 R8 PLACARDS AND MARKINGS - INTERIOR PLACARDS - CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 R9). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 15 Of 748 @ Camp Systems EFTA00618306 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YO006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-11-1077 R9 SB 737-11-1125 23-SEP-2004 PLACARDS AND MARKINGS - INTERIOR PLACARDS - CHANGE PLACARD INSTALLATION FOR MAXIMUM TAKEOFF SUPERSEDED WEIGHT (SUPERSEDED BY SB 737-11-1077 RIO). SERVICE BULLETIN MOS PLACARDS AND MARKINGS - EXTERIOR PLACARDS AND MARKINGS - APPLICATION OF EXTERIOR DECORATIVE PAINT RECOMMENDED SYSTEM ON LEFT SIDE AND RIGHT SIDE WINGS. SERVICE BULLETIN MOS SB 737-11-1129 PLACARDS AND MARKINGS - EXTERIOR PLACARDS AND MARKINGS - FORWARD AIRSTAIRDECAL INSTALLATION. SERVICE BULLETIN MOS CO (5) 11-NOV-2CO1 SB 737-11-1129 RI PLACARDS AND MARKINGS - EXTERIOR PLACARDS AND MARKINGS - FORWARD AIRSTAIR DECAL INSTALLATION. SERVICE BULLETIN 11-NOV-2C04 SB 737-11-1156 22-MAR-2007 MOS • SB 737-11-1156R1 PLACARD AND MARKINGS - FLIGHT DECK - CHANGE CONTROL COLUMN CHECKLIST PLACARDS. SERVICE BULLETIN COMPLIED WITH - lAw THE AD MOS 22-AUG-2C08 I6-APR-2008 3260:48 AFL 782 SB 737-11-1179 PLACARDS AND MARKINGS - INTERIOR PLACARDS - ALTERNATE MAXIMUM TAKEOFF WEIGHT PLACARD SUPERSEDED INSTALLATION (SUPERSEDED BY SB 737-11-1179 RI ). SERVICE BULLETIN MOS SB 737-11-1179 R1 PLACARDS AND MARKINGS - INTERIOR PLACARDS - ALTERNATE MAXIMUM TAKEOFF WEIGHT PLACARD SUPERSEDED INSTALLATION (SUPERSEDED BY SB 737-11-1179 R2). SERVICE BULLETIN MOS SB 737-11-1179 R2 PLACARDS AND MARKINGS - INTERIOR PLACARDS - ALTERNATE MAXIMUM TAKEOFF WEIGHT PLACARD RECOMMENDED INSTALLATION. SERVICE BULLETIN MOS 21-DEC-2010 MOS CO (5) PLACARD AND MARKINGS - FLIGHT DECK - CHANGE CONTROL COLUMN CHECKLIST PLACARDS. SERVICE BULLETIN ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time 16 Of 748 LI Camp Systems EFTA00618307 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-11-1201 13-JUL-2010 PLACARDS AND MARKINGS - CARGO COMPARTMENT PLACARDS - FORWARD AND AFT CARGO COMPARTMENTS - RECOMMENDED REPLACEMENT OF LOAD LIMIT PLACARDS. SERVICE BULLETIN MOS SB 737-11-1202 13-JUL-2010 PLACARDS AND MARKINGS - CARGO COMPARTMENT PI WARDS - FORWARD AND AFT CARGO COMPARTMENTS - REPLACEMENT OF LOAD LIMIT PLACARDS. SERVICE BULLETIN MOS RECOMMENDED SB 737-11-1207 PLACARDS AND MARKINGS - INTERIOR PLACARDS- REMOVAL OF AIRCRAFT FROM ALTERNATE WEIGHT PROGRAM SUPERSEDED AND CHANGE MAXIMUM TAKEOFF WEIGHT FROM 143.000 POUNDS! 60.863 KILOGRAMS TO 134.000 POUNDS! 60.781 KILOGRAMS (SUPERSEDED BY S/3 [SSN REDACTED] R1). SERVICE BULLETIN MOS 58 [SSN REDACTED] PLACARDS AND MARKINGS - INTERIOR PLACARDS- INSTALLATION OF ALTERNATE MAXIMUM TAKEOFF WEIGHT RECOMMENDED PLACARD AND INCREASE OF MAXIMUM TAKEOFF WEIGHT. SERVICE BULLETIN MOS 14-JAN-2011 58 737-11AI109 PLACARDS AND MARKINGS - INTERIOR PLACARDS- INSTALLATION OF IN-FLIGHT SPEEDBRAKE USAGE LIMITATION SUPERSEDED NOT APPLICABLE - NO ACTION REQUIRED MARKER. SERVICE BULLETIN MOS 22-AUG-2003 28-MAR-2002 - (s) 1342 AFL 351 SB 737-11A1109 R1 PLACARDS AND MARKINGS - INTERIOR PLACARDS- INSTALLATION OF IN-FLIGHT SPEEDBRAKE USAGE LIMITATION RECOMMENDED MARKER. SERVICE BULLETIN MOS 16-JAN-2004 58 [SSN REDACTED] AIR CONDITIONING - DISTRIBUTION - FLIGHT COMPARTMENT CONDITIONED AIR DISTRIBUTION - REPLACE DUCT RECOMMENDED TAPE JOINTS WITH SLEEVES AND CLAMPS. SERVICE BULLETIN MOS 12-APR-2001 - (6) 58 [SSN REDACTED] RI AIR CONDITIONING - DISTRIBUTION - FLIGHT COMPARTMENT CONDITIONED AIR DISTRIBUTION - REPLACE DUCT RECOMMENDED TAPE JOINTS WITH SLEEVES AND CLAMPS. SERVICE BULLETIN MOS 07-MAY-2009 58 [SSN REDACTED] AIR CONDITIONING - MAIN AIR DISTRIBUTION - REPLACEMENT OF BULKHEAD FLEX SEAL CLAMP ON ENVIROMENTAL RECOMMENDED CONTROL SYSTEMS SUPPLY DUCTS. SERVICE BULLETIN MOS 23-AUG-2001 - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 17 Of 748 @ Camp Systems EFTA00618308 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-21-1127 RI 27-JUN-2002 SB 737-21-1135 12-DEC-2007 AIR CONDITIONING - MAIN AIR DISTRIBUTION - REPLACEMENT OF BULKHEAD FLEX SEAL CLAMP ON ENVIROMENTAL RECOMMENDED CONTROL SYSTEMS SUPPLY DUCTS. SERVICE BULLETIN MOS - (s) AIR CONDITIONING - PRESSURIZATION CONTROL - PRESSURIZATION CONTROL SYSTEM - CHANGE OF THE CABIN PRESSURE CONTROL SYSTEM FOR 750 FEET PER MINUTE RATE OF DESCENT DURING A CARGO COMPARTMENT SMOKE EVENT SERVICE BULLETIN. SERVICE BULLETIN MOS 72 (s) 58 [SSN REDACTED] RI AIR CONDITIONING - PRESSURIZATION CONTROL- PRESSURIZATION CONTROL SYSTEM - CHANGE OF THE CABIN PRESSURE CONTROL SYSTEM FOR 750 FEET PER MINUTE RATE OF DESCENT DURING A CARGO COMPARTMENT SMOKE EVENT. SERVICE BULLETIN MOS 72 (5) I3-NOV-2008 SB 737-21-1144 I4-APR-2005 AIR CONDITIONING - PASSENGER CABIN CONDITIONED AIR DUSTRIBUTION SYSTEM - TRANSITION DUCT RECOMMENDED ASSEMBLIES AND SIDEWALL RISER DUCTS REPLACEMENT. SERVICE BULLETIN MOS SB 737-21-1148 AIR CONDITIONING - PACK FLOW CONTROL AND PACK COOLING SYSTEM - RAM AIR INLET SYSTEM COMPONENTS RECOMMENDED INSPECTIION AND REPLACEMENT. SERVICE BULLETIN MOS 28-JUL-2005 SB 737-21-1148 RI AIR CONDITIONING - PACK FLOW CONTROL AND PACK COOLING SYSTEM - RAM AIR INLET SYSTEM COMPONENTS INSPECTIION AND REPLACEMENT. SERVICE BULLETIN MOS 26-JAN-2006 SB 737-21-1148 R2 AIR CONDITIONING - PACK FLOW CONTROL AND PACK COOLING SYSTEM - RAM AIR INLET SYSTEM COMPONENTS INSPECTION AND REPLACEMENT.. SERVICE BULLETIN MOS 27-JUL-2006 SB 737-21-1148 R3 02-NOV-2006 58 [SSN REDACTED] R4 22-AUG-2007 AIR CONDITIONING - PACK FLOW CONTROL AND PACK COOLING SYSTEM - RAM AIR INLET SYSTEM COMPONENTS INSPECTION AND REPLACEMENT.. SERVICE BULLETIN MOS AIR CONDITIONING - PACK FLOW CONTROL AND PACK COOLING SYSTEM - RAM AIR INLET SYSTEM COMPONENTS INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 18 Of 748 @ Camp Systems EFTA00618309 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-21-1148 R5 06-MAY-2008 AIR CONDITIONING - PACK FLOW CONTROL AND PACK COOLING SYSTEM - RAM MR INLET SYSTEM COMPONENTS INSPECTION AND REPLACEMENT.. SERVICE BULLETIN MOS SB 737-21-1148 R6 AIR CONDITIONING - PACK FLOW CONTROL AND PACK COOLING SYSTEM - RAM AIR INLET SYSTEM COMPONENTS INSPECTION AND REPLACEMENT. . SERVICE BULLETIN I I -SEP-2008 MOS SB 737-21-1148 R7 AIR CONDITIONING - PACK FLOW CONTROL AND PACK COOLING SYSTEM - RAM AIR INLET SYSTEM COMPONENTS RECOMMENDED INSPECTION AND REPLACEMENT.. SERVICE BULLETIN MOS 21 -JAN-2010 SB 737-21-1155 AIR CONDITIONING - EQUIPMENT COOLING SYSTEM - EQUIPMENT COOLING DUCT INSPECTION AND TAPE INSTALLATION TO PREVENT A RUB CONDITION. SERVICE BULLETIN MOS SB I0-NOV-2005 [SSN REDACTED] R1 22-DEC-2005 AIR CONDITIONING - EQUIPMENT COOLING SYSTEM - EQUIPMENT COOLING DUCT INSPECTION AND TAPE INSTALLATION TO PREVENT A RUB CONDITION. SERVICE BULLETIN MOS SB 737-21-1155 R2 AIR CONDITIONING - EQUIPMENT COOLING SYSTEM - EQUIPMENT COOLING DUCT INSPECTION AND TAPE INSTALLATION TO PREVENT A RUB CONDITION. SERVICE BULLETIN MOS 20-JUL-2006 SB 737-21-1155 R3 AIR CONDITIONING - EQUIPMENT COOLING SYSTEM - EQUIPMENT COOLING DUCT INSPECTION AND TAPE INSTALLATION TO PREVENT A RUB CONDITION. SERVICE BULLETIN MOS 25-MAR-2008 SB 737-21-1155 R4 AIR CONDITIONING - EQUIPMENT COOLING SYSTEM - EQUIPMENT COOLING DUCT INSPECTIONAND TAPE RECOMMENDED INSTALLATION TO PREVENT A RUB CONDITION. SERVICE BULLETIN MOS 24-SEP-2009 SB 737-21-1163 AIR CONDITIONING - PRESSURIZATION CONTROL - PRESSURIZATION CONTROL SYSTEM - CHANGE OF THE CABIN PRESSURE CONTROLLERS FOR 750 FEET PER MINUTE RATE OF DESCENT DURING A CARGO COMPARTMENT SMOKE EVENT. SERVICE BULLETIN MOS 72 (s) 2-DEC-2007 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 19 Of 748 @ Camp Systems EFTA00618310 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-21-1163 RI AIR CONDITIONING - PRESSURIZATION CONTROL- PRESSURIZATION CONTROL SYSTEM - CHANGE OF THE CABIN RECOMMENDED PRESSURE CONTROLLERS FOR 750 FEET PER MINUTE RATE OF DESCENT DURING A CARGO COMPARTMENT SMOKE EVENT. SERVICE BULLETIN MOS 72 (0) 17-DEC-2009 SB 737-21-1165 AIR CONDITIONING - CABIN PRESSURE INDICATION AND WARNING SYSTEM- REDUNDANT PRESSURE SWITCH SUPERSEDED INSTALLATION (SUPERSEDED BY S8 [SSN REDACTED] RI). SERVICE BULLETIN MOS SB 737-21-1165 RI AIR CONDITIONING - CABIN PRESSURE INDICATION AND WARNING SYSTEM - REDUNDANT PRESSURE SWITCH SUPERSEDED INSTALLATION (SUPERSEDED BY S8 [SSN REDACTED] R2). SERVICE BULLETIN MOS - Is) SB 737-21-1165 R2 AIR CONDITIONING - CABIN PRESSURE INDICATION AND WARNING SYSTEM - REDUNDANT PRESSURE SWITCH SUPERSEDED INSTALLATION (SUPERSEDED BY S8 [SSN REDACTED] R3). SERVICE BULLETIN MOS SB 737-21-1165 R3 AIR CONDITIONING - CABIN PRESSURE INDICATION AND WARNING SYSTEM - REDUNDANT PRESSURE SWITCH RECOMMENDED INSTALLATION. SERVICE BULLETIN MOS 72 (5) 07-NOV-2012 SB 737-21-1170 AIR CONDITIONING - PACK FLOW CONTROL AND PACK COOLING SYSTEM- REPLACEMENT OF SHAFT ASSEMBLIES RECOMMENDED AND LINK ARM ASSEMBLIES TO INCREASE THE CLEARANCE FOR THE RAM AIR INLET ACTUATORS. SERVICE BULLETIN MOS 23-SEP-2010 SB 737-21-1177 AIR CONDITIONING - PRESSURIZATION CONTROL SYSTEM - CHANGE OF THE POWER SOURCE TO THE RECOMMENDED PRESSURIZATION SYSTEM CIRCUIT BREAKER. SERVICE BULLETIN MOS 06-JAN-2011 SB 737-21-1178 AIR CONDITIONING - FUGHT COMPARTMENT CONDITIONED AIR DISTRIBUTION - CHANGE OF THE DUCTS AND RECOMMENDED PLENUMS TO REDUCE NOISE. SERVICE BULLETIN MOS I9-AUG-2013 SB 737-21A1139 AIR CONDITIONING - DISTRIBUTION - INSTALLATION OF THE INSULATION AND TAPE ON THE OVERHEAD DUCTS AND SUPERSEDED PLENUMS (SUPERSEDED BY 737-21A1139 R1). SERVICE BULLETIN MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 20 Of 748 @ Camp Systems EFTA00618311 COMP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-21A1I39 RI 28-AUG-2003 AIR CONDITIONING - DISTRIBUTION - INSTALLATION OF THE INSULATION AND TAPE ON THE OVERHEAD DUCTS AND RECOMMENDED PLENUMS. SERVICE BULLETIN MOS SB 737-22-1137 AUTOFLIGHT - AUTOTHROTTLE SYSTEM- ACTIVATION OF FLIGHT MANAGEMENT COMPUTER TRANSITION ALTITUDE RECOMMENDED SELECTION. SERVICE BULLETIN MOS 25-MAY-2000 - (s) SB 737-22-1140 AUTO FLIGHT - AUTOPILOT - AUTOPILOT OPERATION WITH ONE IRU INOPERATIVE RETROFIT, SERVICE BULLETIN RECOMMENDED MOS I5-JUN-2060 - (s) SB 737-22-1153 AUTO FLIGHT - AUTOPILOT - INSTALLATION OF RED NON-DIMMABLE 'AUTOLAND* WARNING LIGHTS. SERVICE RECOMMENDED NOT APPLICABLE - BY EFFECTIVITY - BULLETIN MOS 01-NOV-2001 SB 737-22-1154 AUTO FLIGHT - AUTOPILOT - OPTION/PROGRAM PIN CHANGES TO ACTIVATE FLIGHT CONTROL COMPUTER IMPROVEMENTS, SERVICE BULLETIN MOS 24-JAN-2002 - (s) SB 737-22-1154 RI AUTO FLIGHT - AUTOPILOT - OPTION/PROGRAM PIN CHANGES TO ACTIVATE FLIGHT CONTROL COMPUTER RECOMMENDED IMPROVEMENTS. SERVICE BULLETIN MOS I2-SEP-2002 SB 737-22-1213 AUTOFLIGHT - YAW DAMPER SYSTEM - DELETION OF A YAW DAMPER INDICATOR (SUPERSEDED BY S8737-22-1213 SUPERSEDED Ft1). SERVICE BULLETIN MOS SB 737-22-1213 RI AUTOFLIGHT - YAW DAMPER SYSTEM - DELETION OF A YAW DAMPER INDICATOR. SERVICE BULLETIN RECOMMENDED MOS I2-APR-20 I I SB 737-22-1216 AUTOFLIGHT - DIGITAL FLIGHT CONTROL SYSTEM- FLIGHT CONTROL COMPUTER DIP SWITCH CHANGE. SERVICE RECOMMENDED BULLETIN RECOMMENDED I6-AUG-2010 SB 737-22-1223 25-JAN-2011 MOS AUTOFLIGHT - AUTOPILOT - INSTALLATION OF LATERAL NAVIGATION MODE AS THE DEFAULT ROLL MODE FOR RECOMMENDED GO-AROUND IN LIEU OF TRACK HOLD FOR A MISSED APPROACH. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (0-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 21 Of 748 @ Camp Systems EFTA00618312 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-22A1164 AUTOFLIGHT - DIGITAL FLIGHT CONTROL SYSTEM - FLIGHT CONTROL COMPUTER OPERATIONAL PROGRAM SOFTWARE INSTALLATION - P2.0. SERVICE BULLETIN NOT APPLICABLE MOS 28-APR-2006 20-MAY-2004 - (s) 2606:18 AFL 626 SB 737-22A1211 AUTOFLIGHT - DIGITAL FLIGHT CONTROL SYSTEM - RIGHT CONTROL COMPUTER SOFTWARE CHANGE. SERVICE RECOMMENDED NOT APPLICABLE - BY AIRCRAFT SERIAL BULLETIN NUMBER DAYS 09-AUG-2010 13-APR-2010 3448:31 AFL 841 SB 737-22A1215 AUTOFLIGHT - AUTOTHROTTLE SYSTEM - AUTOTHROTTLE COMPUTER REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 36 (EFF) 22-NOV-2016 22-NOV-20I3 SB 737-22A1224 AUTOFLIGHT - DIGITAL FLIGHT CONTROL SYSTEM - RIGHT CONTROL COMPUTER SOFTWARE CHANGE. SERVICE RECOMMENDED NOT APPLICABLE - N/A BY PN INSTALLED. BULLETIN REFER AD 2012-21-08. MOS I6-NOV-2012 I8-MAY-2012 3670:04 AFL 890 SB 737-23-1135 PASSENGER ADDRESS AND ENTERTAINMENT - ATTENDANT PANEL REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 31-MAY-2001 - (s) SB 737-23-1139 COMMUNICATIONS - PASSENGER ADDRESS AND ENTERTAINMENT. SERVICE BULLETIN RECOMMENDED MOS 08-FEB-2001 - (s) SB 737-23-1139 RI INSTALATION OF THE PASSENGER ADDRESS AMPLIFIER AND IN-FLIGHT ENTERTAINMENT AUDIO CIRCUT BREAKERS. RECOMMENDED SERVICE BULLETIN MOS 03-JUL-2002 - (s) SB 737-23-1172 HF FERRY FLIGHT KIT INSTALLATION/REMOVAL (SUPERSEDED BY SB 737-23-1172 R1). SERVICE BULLETIN MOS SB 737-23-1172 RI HIGH FREQUENCY (HF) COMMUNICATIONS SYSTEM - HF FERRY FLIGHT KIT INSTALLATION/REMOVAL (SUPERSEDED BY SB 737-23-1172 R2). SERVICE BULLETIN MOS SUPERSEDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 22 Of 748 @ Camp Systems EFTA00618313 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-23-1172 R2 01-MAY-2012 SB 737-23-1200 AUDIO SELECTOR PANEL RELOCATION. SERVICE BULLETIN RECOMMENDED COMMUNICATIONS - HIGH FREQUENCY (HF) COMMUNICATIONS SYSTEM - HF FERRY FLIGHT KIT INSTALLATION:REMOVAL. SERVICE BULLETIN MOS RECOMMENDED MOS 01-NOV-2001 • 1.51 SB 737-23-1208 29-SEP-2005 COMMUNICATIONS AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING SYSTEM (ACARS) - DATA BUS WIRE CHANGES. SERVICE BULLETIN MOS RECOMMENDED SB 737-23-1266 COMMUNICATIONS - IRIDIUM ANTENNA - INSTALLATION (SUPERSEDED BY SB 737-23-1266 R1). SERVICE BULLETIN SUPERSEDED MOS SB 737-23-1266 RI COMMUNICATIONS - IRIDIUM ANTENNA - INSTALLATION (SUPERSEDED BY SB 737-23-1266 R2) SUPERSEDED . SERVICE BULLETIN MOS SB 737-23-1266 R2 COMMUNICATIONS - IRIDIUM ANTENNA - INSTALLATION (SUPERSEDED BY SB 737-23-1266 R3). SERVICE BULLETIN SUPERSEDED MOS SB 737-23-1266 R3 COMMUNICATIONS - IRIDIUM ANTENNA - INSTALLATION. SERVICE BULLETIN RECOMMENDED C6-JAN-2011 MOS • SB 737-23-1336 1341AY-2010 SB 737-23-1337 C6-AUG-2010 SB 737-23-1342 30-NOV-2010 COMMUNICATIONS - EMERGENCY LOCATOR TRANSMITTER - INSTALLATION OF A GROUND WIRE. SERVICE BULLETIN MOS • COMMUNICATIONS - AUDIO VISUAL MONITORING - COCKPIT DOOR SURVEILLANCE SYSTEM WIRE BUNDLE CHANGE. RECOMMENDED SERVICE BULLETIN MOS COMMUNICATIONS - LAV Al CONNECTOR MATE-WITH TAPE - CHANGE. SERVICE BULLETIN MOS RECOMMENDED ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 23 Of 748 Camp Systems EFTA00618314 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-23-1343 COMMUNICATION - HIGH FREQUENCY COMMUNICATION SYSTEM - INSTALL WIRES BETWEEN THE VERY HIGH RECOMMENDED FREQUENCY TRANSCEIVER 3 AND THE COMMUNICATION MANAGEMENT UNIT OF THE AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING SYSTEM. SERVICE BULLETIN MOS 10-JAN-2011 SB 737-23-1397 COMMUNICATIONS - CABIN INTERPHONE SYSTEM - IN-LINE FILTER INSTALLATION, SERVICE BULLETIN RECOMMENDED 06-DEC-2013 SB 737-23-1403 COMMUNICATIONS - SATELLITE COMMUNICATIONS SYSTEM- SATELLITE DATA UNIT REPLACEMENT AND AIR DATA RECOMMENDED INERTIAL REFERENCE UNIT OUTPUT BUS WIRING CHANGES. SERVICE BULLETIN MOS 07-FEB-2013 SB 737-23-1410 04-APR-2013 58 [SSN REDACTED] 18-OCT-2013 MOS - Is) COMMUNICATIONS - EMERGENCY EVACUATION SYSTEM - ERRONEOUS ACTIVATION OF CABIN CALL LIGHT IN FLIGHT RECOMMENDED COMPARTMENT CORRECTIVE WIRING CHANGES. SERVICE BULLETIN MOS COMMUNICATIONS - AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING SYSTEM (AGARS) - COMMUNICATIONS MANAGEMENT UNIT (CMU) WIRING CHANGE - INSTALL WIRING BETWEEN AGARS CMU AND ENGINE RUNNING SWITCHES. SERVICE BULLETIN MOS RECOMMENDED SB 737-23-1423 COMMUNICATIONS - VOICE RECORDER SYSTEM - INSTALLATION OF THE NEW L-3 COCKPIT VOICE RECORDER (CVR) RECOMMENDED CONTROL PANEL. SERVICE BULLETIN MOS 04-FEB-2014 SB 737-23-1429 COMMUNICATIONS - VOICE RECORDER SYSTEM - INSTALLATION OF THE COCKPIT VOICE RECORDER INDEPENDENT RECOMMENDED POWER SUPPLY (RIPS) AND THE RIPS-COMPATIBLE MANUAL ON/AUTO OFF SWITCH OPTION. SERVICE BULLETIN MOS 13-MAR-2014 SB 737-23A1170 COMMUNICATIONS - VHF-1 AND VHF-2 ANTENNA INTERCHANGE (SUPERSEDED BY SB 737-23A1170 R1). SERVICE SUPERSEDED COMPUED WITH BULLETIN MOS 10-AUG-2000 27-APR-2000 SB 737-23A1170 R1 COMMUNICATIONS - VHF-1 AND VHF-2 ANTENNA INTERCHANGE (SUPERSEDED BY SB 737-23A1170 R2). SERVICE SUPERSEDED BULLETIN MOS 27-JUL-2000 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 24 Of 748 @ Camp Systems EFTA00618315 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-23AI170 RI PART VHF-1 AND VHF-2 ANTENNA INTERCHANGE. SERVICE BULLETIN MOS 27-JUL-2000 SB 737-23A1170 RI PART COMMUNICATIONS - VHF-I AND VHF-2 ANTENNA INTERCHANGE. SERVICE BULLETIN MOS 27-JUL-2000 SB 737-23A1170 R2 COMMUNICATIONS - VHF-I AND VHF-2 ANTENNA INTERCHANGE, SERVICE BULLETIN MOS 02-MAR-2006 I4-SEP-2000 2509:38 RECOMMENDED RECOMMENDED RECOMMENDED COMPLIED WITH - REF: PART I PART II DUE 4000 HRS AFL 609 SB 737-23A1170 R2 PART COMMUNICATIONS - VHF-1 AND VHF-2 ANTENNA INTERCHANGE. SERVICE BULLETIN RECOMMENDED COMPLIED WITH DAYS 10 (s) 02-MAR-2006 I4-SEP-2000 2509:38 AFL 609 SB 737-23A1170 R2 PART COMMUNICATIONS - VHF-I AND VHF-2 ANTENNA INTERCHANGE, SERVICE BULLETIN RECOMMENDED II MOS I4-SEP-2000 4000 4000 4000 SB 737-24-1126 AILERON CONTROL SYSTEM - WIRING BUNDLE SHIELD OVERBRAID INSTALLATION FOR EMI PROTECTION, SERVICE RECOMMENDED BULLETIN MOS 0 I -AUG-2002 - (s) SB 737-24-1126 RI AILERON CONTROL SYSTEM - WIRING BUNDLE SHIELD OVERBRAID INSTALLATION FOR EMI PROTECTION. SERVICE RECOMMENDED BULLETIN MOS I4-NOV-2002 - (s) SB 737-24-1128 POWER DISTRIBUTION PANEL. SERVICE BULLETIN RECOMMENDED NOT APPLICABLE- TERMINATED PCW MOS 18-AUG-2006 28-APR-1999 2633:50 AFL 633 SB 737-24-1132 ELECTRICAL POWER- DC GENERATION. SERVICE BULLETIN RECOMMENDED MOS 08-JUN-2000 - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 25 Of 748 @ Camp Systems EFTA00618316 COMP Astant.frn• thernand up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-24-1134 22-JUN-2000 STANDBY POWER SYSTEM. SERVICE BULLETIN MOS - (s) SB 737-24-1135 NO.1 AIR TRAFFIC CONTROL SYSTEM. SERVICE BULLETIN MOS 27-APR-2000 - RECOMMENDED RECOMMENDED SB 737-24-1147 20-NOV-2003 INSTALLATION OF THE INFLIGHT ENTERTAINMENT SYSTEM CIRCUIT BREAKER. RELAYS AND WIRING. SERVICE BULLETIN MOS 60 (s) 58 [SSN REDACTED] RI ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTION - INSTALLATION OF THE INFLIGHT ENTERTAINMENT SYSTEM CIRCUIT BREAKER. RELAYS AND WIRING. SERVICE BULLETIN MOS 60 (s) 01-MAR-2007 SB 737-24-1147 R2 ELECTRICAL LOAD DISTRIBUTION - INSTALLATION OF THE INFLIGHT RECOMMENDED ENTERTAINMENT SYSTEM CIRCUIT BREAKER. RELAYS AND WIRING. SERVICE BULLETIN MOS 60 (s) 30-JUL-2009 SB 737-24-1149 CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS (SUPERSEDED BY 737-24-1149 RI), SERVICE SUPERSEDED BULLETIN 01-JAN-2000 DAYS SB 737-24-1109 RI CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL (SUPERSEDED BY SUPERSEDED 737-24-1149 R2). SERVICE BULLETIN MOS 01-JAN-2000 SB 737-24-1149 R2 CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL (SUPERSEDED BY SUPERSEDED 737-24-1149 R3) . SERVICE BULLETIN MOS 01-JAN-2000 SB 737-24-1149 R3 ELECTRICAL POWER - GENERAL - CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS IN THE MAIN SUPERSEDED WHEEL WELL (SUPERSEDED BY 737-24-1149 R4) . SERVICE BULLETIN MOS 01-JAN-2000 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 26 Of 748 @ Camp Systems EFTA00618317 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-24-1149 R4 07-AUG-2007 SB 737-24-1154 01-MAY-2003 SB 737-24-1155 ELECTRICAL POWER - GENERAL - CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL SERVICE BULLETIN MOS 24 (s) GUARD INSTALLATION FOR THE CIRCUIT BREAKERS FOR THE OVERWING DOOR FLIGHT LOCKS. SERVICE BULLETIN RECOMMENDED MOS STANDBY POWER CONTROL UNIT (SPCU) TRAY BRACE AND TRAY STIFFENER ASSEMBLY INSTALLATION.. SERVICE RECOMMENDED BULLETIN 26-FEB-2004 MOS SB 737-24-1155 RI STANDBY POWER CONTROL UNIT (SPCU) TRAY BRACE AND TRAY STIFFENER ASSEMBLY INSTALLATION. SERVICE RECOMMENDED BULLETIN MOS 16-DEC-2004 SB 737-24-1155 R2 ELECTRICAL POWER- STANDBY POWER CONTROL UNIT (SPCU) TRAY BRACE AND TRAY STIFFENER ASSEMBLY INSTALLATION. SERVICE BULLETIN MOS 08-SEP-2005 SB 737-24-1155 R3 ELECTRICAL POWER - STANDBY POWER CONTROL UNIT (SPCU) TRAY BRACE AND TRAY STIFFENER ASSEMBLY INSTALLATION. SERVICE BULLETIN MOS 23-MAR-2006 SB 737-24-1157 INSTALLATION OF CLAMPS BETWEEN THE WIRE BUNDLES AND THE HYDRAULIC TUBES IN THE LEFT MAIN LANDING RECOMMENDED GEAR WHEEL WELL SERVICE BULLETIN MOS I4-AUG-2003 SB 737-24-1161 ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTION - INSTALLATION OF PROTECTION GUARDS ON THE P6 AND RECOMMENDED P18 LOAD CONTROL PANELS. SERVICE BULLETIN MOS 24-MAR-2005 SB 737-24-1161 RI ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTION - INSTALLATION OF PROTECTION GUARDS ON THE P6 AND P18 LOAD CONTROL PANELS. SERVICE BULLETIN MOS 17-NOV-2005 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 27 Of 748 @ Camp Systems EFTA00618318 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-24-1161 R2 24-JAN-2008 SB 737-24-1162 02-JUN-2005 ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTION - INSTALLATION OF PROTECTION GUARDS ON THE P6 AND P18 LOAD CONTROL PANELS. SERVICE BULLETIN MOS ELECTRICAL POWER - AC GENERATION SYSTEM - STA 1088 BULKHEAD CATERPILLAR GROMMET. INSPECTION AND INSTALLATION. SERVICE BULLETIN MOS SB 737-24-1165 ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL AND REPLACEMENT OF THE STATIC INVERTER MODULE. SERVICE BULLETIN MOS 42 (s) 28-APR-2005 NOT APPLICABLE SB 737-24-1165 RI ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL AND REPLACEMENT OF THE STATIC INVERTER COMPLIED WITH MODULE. SERVICE BULLETIN MOS 29-AUG-2011 20-OCT-2005 (s) 3533:32 AFL 863 SB 737-24-1167 ELECTRICAL POWER - GENERAL - REPLACEMENT OF ANTISKID SYSTEM ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELLS. SERVICE BULLETIN MOS CE-APR-2006 SB 737-24-1167 RI 13-NOv-2608 ELECTRICAL POWER - GENERAL - REPLACEMENT OF ANTISKID SYSTEM ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELLS. SERVICE BULLETIN MOS SB 737-24-1169 ELECTRICAL POWER - INSPECTION FOR MISSING FILLET SEAL ON RECEPTACLES IN MAIN LANDING GEAR WHEEL WELLS. SERVICE BULLETIN MOS 24 (s) 15-DEC-2006 SB 737-24-1169 R1 CE-AUG-2007 SB 737-24-1169 R2 09-APR-2008 ELECTRICAL POWER - INSPECTION FOR MISSING FILLET SEAL ON RECEPTACLES IN MAIN LANDING GEAR WHEEL WELLS. SERVICE BULLETIN MOS 24 (s) ELECTRICAL POWER - INSPECTION FOR MISSING FILLET SEAL ON RECEPTACLES IN MAIN LANDING GEAR WHEEL WELLS. SERVICE BULLETIN MOS 22-AUG-2608 -(s) 3260:48 AFL 782 RECOMMENDED COMPLIED WITH ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 28 Of 748 1' Camp System s EFTA00618319 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 [SSN REDACTED] 26-MAR-2007 SB 737-24-1171 RI 02-JUL-2007 SB 737-24-1171 R2 I8-SEP-2007 SB 737-24-1171 R3 08-MAY-2008 SB 737-24-1171 R4 30-OCT-2008 SB 737-24-1172 I6-MAY-2008 ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTION - INSPECTION. REPAIR AND INSTALLATION OF PROTECTIVE SLEEVE ON WIRE BUNDLE W0018 IN THE FLIGHT COMPARTMENT. SERVICE BULLETIN MOS 24 (s) ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTION - INSPECTION. REPAIR AND INSTALLATION OF PROTECTIVE SLEEVE ON WIRE BUNDLE W0018 IN THE FLIGHT COMPARTMENT. SERVICE BULLETIN MOS 24 (s) ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTION - INSPECTION. REPAIR AND INSTALLATION OF PROTECTIVE SLEEVE ON WIRE BUNDLE W0018 IN THE RIGHT COMPARTMENT. SERVICE BULLETIN MOS 24 (s) ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTION - INSPECTION. REPAIR AND INSTALLATION OF PROTECTIVE SLEEVE ON WIRE BUNDLE W0018 IN THE RIGHT COMPARTMENT. SERVICE BULLETIN MOS 24 (s) ELECTRICAL LOAD DISTRIBUTION - INSPECTION. REPAIR AND INSTALLATION OF PROTECTIVE SLEEVE ON WIRE BUNDLE W0018 IN THE RIGHT COMPARTMENT. SERVICE BULLETIN MOS 24 (s) ELECTRICAL - ELECTRICAL POWER - INSPECTION AND REPAIR OF ELECTRICAL BONDING RESISTANCE AT THE WING-TO-BODY FEED THROUGH RECEPTACLES. SERVICE BULLETIN MOS SB 737-24-1172 RI INSPECTION AND REPAIR OF ELECTRICAL BONDING RESISTANCE AT THE WING-TO-BODY FEED THROUGH RECOMMENDED RECEPTACLES. SERVICE BULLETIN MOS 18-NOV-2009 SB 737-24-1172 RI TABLE REPAIR INSPECTION AND REPAIR OF ELECTRICAL BONDING RESISTANCE AT THE WING-TO-BODY FEED THROUGH RECOMMENDED 1 (A) RECEPTACLES. SERVICE BULLETIN AS GIVEN IN ACCOMPLISHMENT INSTRUCTIONS OPTION 1 MOS 72 (s) 18-NOV-2009 SB 737-24-1172 RI TABLE INSPECTION INSPECTION AND REPAIR OF ELECTRICAL BONDING RESISTANCE AT THE WING-TO-BODY FEED RECOMMENDED 1 (B) THROUGH RECEPTACLES. SERVICE BULLETIN OF ELECTRICAL BONDING AS GIVEN IN ACCOMPLISHMENT INSTRUCTIONS OPTION 2 MOS 24 (s) 18-NOV-2009 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 29 Of 748 @ Camp Systems EFTA00618320 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-24-1172 TABLE 1 REPAIR ELECTRICAL - ELECTRICAL POWER - INSPECTION AND REPAIR OF ELECTRICAL BONDING RESISTANCE (A) AT THE WING-TO-BODY FEED THROUGH RECEPTACLES. SERVICE BULLETIN AS GIVEN IN ACCOMPLISHMENT INSTRUCTIONS OPTION 1 MOS 72 (s) 16-MAY-2008 58 [SSN REDACTED] TABLE 1 INSPECTION ELECTRICAL - ELECTRICAL POWER - INSPECTION AND REPAIR OF ELECTRICAL BONDING RESISTANCE (8) AT THE WING-TO-BODY FEED THROUGH RECEPTACLES. SERVICE BULLETIN OF ELECTRICAL BONDING AS GIVEN IN ACCOMPLISHMENT INSTRUCTIONS OPTION 2 MOS 24 (s) 16-MAY-2008 SB 737-24-1173 07-NOV-2007 SB 737-24-1173 RI 27-MAR-2008 SB 737-24-1173 R2 23-APR-2009 ELECTRICAL - ELECTRICAL POWER - REPLACEMENT OF WIRE SUPPORT BRACKET AND INSPECTION OF THE ROD END PLATES ON THE RUDDER FEEL AND CENTERING UNIT. SERVICE BULLETIN MOS 72 (s) ELECTRICAL - ELECTRICAL POWER - REPLACEMENT OF WIRE SUPPORT BRACKET AND INSPECTION OF THE ROD END PLATES ON THE RUDDER FEEL AND CENTERING UNIT. SERVICE BULLETIN MOS 72 (s) REPLACEMENT OF WIRE SUPPORT BRACKET AND INSPECTION OF THE ROD END PLATES ON THE RUDDER FEEL AND CENTERING UNIT. SERVICE BULLETIN MOS 72 (s) SB 737-24-1176 ELECTRICAL POWER- AC GENERATION SYSTEM - RE-PIN WIRES AT TWO WING-TO-STRUT ELECTRICAL CONNECTORS AT EACH ENGINE STRUT BRACKET. SERVICE BULLETIN MOS 21-FEB-2008 SB 737-24-1176 RI 22-APR-2008 SB 737-24-1176 R2 06-NOV-2008 SB 737-24-1176 R3 18-DEC-2008 ELECTRICAL POWER - AC GENERATION SYSTEM - RE-PIN WIRES AT TWO WING-TO-STRUT ELECTRICAL CONNECTORS AT EACH ENGINE STRUT BRACKET. SERVICE BULLETIN MOS AC GENERATION SYSTEM - RE-PIN WIRES AT TWO WING-TO-STRUT ELECTRICAL CONNECTORS AT EACH ENGINE STRUT BRACKET. SERVICE BULLETIN MOS AC GENERATION SYSTEM - INSPECTION AND RE-PIN WIRES AT TWO WING-TO-STRUT ELECTRICAL CONNECTORS AT EACH ENGINE STRUT BRACKET. SERVICE BULLETIN MOS RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 30 Of 748 @ Camp Systems EFTA00618321 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-24-1182 20-JAN-2009 INSPECTION AND CHANGE WIRE BUNDLE ROUTING TO PREVENT CONTACT WITH MAIN BATTERY CHARGER. SERVICE BULLETIN MOS SB 737-24-1194 ELECTRICAL POWER - MEDICAL OUTLET SYSTEM- MEDICAL FREQUENCY CONVERTER SUB-TRAY CHANGE. SERVICE RECOMMENDED BULLETIN MOS 14-SEP-2011 SB 737-24-1203 ELECTRICAL POWER- AC EXTERNAL POWER- CHANGE OF THE EXTERNAL POWER RECEPTACLE CONTACTS. RECOMMENDED SERVICE BULLETIN MOS 02-DEC-2013 SB 737-24-1205 ELECTRICAL POWER- STANDBY POWER SYSTEM - REPLACEMENT OF THE M9 STATIC INVERTER TERMINAL LUGS.. RECOMMENDED SERVICE BULLETIN MOS 25-MAR-2014 SB SB 737-24-1206 03-APR-2014 737-24A1141 R1 23-DEC-2004 ELECTRICAL POWER - GENERAL - E8-1 SHELF ASSEMBLY - VINYL MARKER REPLACEMENT. SERVICE BULLETIN MOS PS OVERHEAD PANEL - BRACKET REPLACEMENT AND WIRE INSTALLATION. SERVICE BULLETIN MOS 24 (s) RECOMMENDED - REF: R2 SB 737-24A1141 R2 ELECTRICAL POWER - GENERAL - PS OVERHEAD PANEL - BRACKET REPLACEMENT AND WIRE INSTALLATION. COMPUED WITH SERVICE BULLETIN MOS 18-AUG-2006 01-DEC-2005 -Is) 2633:50 AFL 633 SB 737-24A1141 R3 ELECTRICAL POWER - GENERAL - PS OVERHEAD PANEL - BRACKET REPLACEMENT AND COMPUED WITH - IAW THE AD R2 ALREADY CM WIRE INSTALLATION REVISION. SERVICE BULLETIN GVBBJ122. AUG 18. 2006. MOS 02-DEC-2009 20-FEB-2008 -Is) 3402:19 AFL 824 SB 737-24A1148 CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL (SUPERSEDED BY SUPERSEDED COMPUED WITH - INSPECTED AND CLEANED 737-24A1148 R1). SERVICE BULLETIN CONNECTORS MOS 13-AUG-2004 06-DEC-2001 -(s) 1785:06 AFL 446 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 31 Of 748 @ Camp Systems EFTA00618322 COMP Astant.frn• thernand up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-24A1148 RI CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL. SERVICE BULLETIN MOS 12 (s) 03-JUL-2013 3723:21 1O-JUL-2003 AFL 908 SB 737-24A1150 INSPECTION OF THE POWER SUPPLY VOLTAGE TO THE CAPTAINS PITOT HEATER. SERVICE BULLETIN DAYS 60 (s) 27-AUG-2002 I I -DEC-2002 1057:48 SB 737-24M193 SB 737-25-1373 24-JUL-I 999 SB 737-25-1376 30-JUL-2009 SB 737-25-1378 08-APR-1999 SB 737-25-1378 RI I2-JAN-2001 SB 737-25-1403 04-MAY-2000 SB 737-25-1403 RI 29-NOV-2001 SB 737-25-1404 25-MAY-2000 AFL 271 ELECTRICAL POWER-AC GENERATOR DRIVE SYSTEM- INCORRECT ELECTRICAL BOND ON GROUND BRACKET FOR LEFT ENGINE GENERATOR. SERVICE BULLETIN MOS OVERHEAD STOWAGE BIN DOOR. SERVICE BULLETIN MOS - (s) LAVATORY COMPARTMENT - CHANGE TO AFT CLEVIS SYSTEM AND AFT WALL ON LAVATORY A. SERVICE BULLETIN MOS CHANGE ESCAPE SLIDE INSTALLATION. SERVICE BULLETIN MOS . SERVICE BULLETIN MOS - (s) - DOOR-MOUNTED ESCAPE SYSTEM, SERVICE BULLETIN MOS - (s) DOOR MOUNTED ESCAPE SYSTEM - INFLATION CYLINDER TRIGGER HOUSING COVER INSTALLATION. SERVICE BULLETIN MOS ESCAPE SLIDE LATCH ASSEMBLY. SERVICE BULLETIN MOS - (s) RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED COMPUED WITH - LAW. AD 2005-18-23 NOT APPLICABLE - BY EFFECTIVITY 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 32 Of 748 @ Camp Systems EFTA00618323 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-25-1404 RI EMERGENCY - DOOR-MOUNTED ESCAPE SYSTEM - LATCH ASSEMBLY MODIFICATION (SUPERSEDED BY SB SUPERSEDED 737-25-1404 R2). SERVICE BULLETIN MOS - (s) SB 737-25-1404 R2 EQUIPMENT/FURNISHINGS - EMERGENCY - DOOR-MOUNTED ESCAPE SYSTEM - LATCH ASSEMBLY MODIFICATION. RECOMMENDED SERVICE BULLETIN MOS 36 (s) 25-MAY-2000 SB 737-25-1439 R3 EQUIPMENT/FURNISHINGS-BUFFET/,ALLEY- GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT. SERVICE BULLETIN MOS II -NOV-2004 SB 737-25-1440 REPLACEMENT OF SPARE BULB STOWAGE ASSEMBLY, SERVICE BULLETIN RECOMMENDED 06-DEC-2001 SB 737-25-1447 I8-OCT-2001 SB 737-25-1449 08-NOV-2001 SB 737-25-1449 RI 0I-AUG-2002 SB 737-25-1475 26-NOV-2002 SB 737-25-1477 I4-NOV-2002 SB 737-25-1477 RI 28-AUG-2003 MOS - (s) INSTALL SECOND OBSERVERS STATION, SERVICE BULLETIN MOS - (s) AFT CARGO COMPARTMENT - REPLACE INSULATION SUPPORT TRAYS. SERVICE BULLETIN MOS - (s) REPLACE INSLUATION SUPPORT TRAYS. SERVICE BULLETIN MOS REPLACE TRIGGER HOUSING ON SLIDE REGULATOR VALVE. SERVICE BULLETIN MOS WINDOW NUMBER FOUR SUNSHADE INSTALLATION. SERVICE BULLETIN MOS - (s) WINDOW NUMBER FOUR SUNSHADE INSTALLATION. SERVICE BULLETIN MOS RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 33 Of 748 @ Camp Systems EFTA00618324 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-25-1491 23-APR-2007 SB 737-25-1491 RI 23-APR-2007 SB 737-25-1493 EQUIPMENT/FURNISHINGS - EMERGENCY - DOOR MOUNTED ESCAPE SYSTEM - CHANGE EVACUATION SLIDE INFLATION VALVE REGULATOR. SERVICE BULLETIN MOS 09-AUG-2010 3148:31 AFL PA EMERGENCY - DOOR MOUNTED ESCAPE SYSTEM - CHANGE EVACUATION SLIDE INFLATION VALVE REGULATOR. SERVICE BULLETIN MOS C9-AUG-2010 3448:31 AFL 841 EQUIPMENT/FURNISHINGS- INSULATION BLANKET - MOISTURE REDUCTION OF INSULATION BLANKETS AT THE AUTOMATIC OVERWING EXIT DOORS. SERVICE BULLETIN MOS COMPLIED WITH - PREVIOUSLY RECOMMENDED COMPLIED WITH - PREVIOUSLY 737-25-1491 SLIDE PN INSTALLED: 5A3086-301 02-MAY-2007 SB 737-25-1493 RI INSULATION BLANKET - MOISTURE REDUCTION OF INSULATION RECOMMENDED BLANKETS AT THE AUTOMATIC OVERWING EXIT DOORS. SERVICE BULLETIN MOS 28-JUL-2009 SB 737-25-1523 EQUIPMENT/FURNISHINGS- FORWARD GALLEY DOOR DOORWAY HEADER PANEL - INSTALLATION OF ATTENDANT SUPERSEDED SERVICE UNIT (SUPERSEDED BY SB 737-25.1523 RI ). SERVICE BULLETIN MOS SB 737-25-1523 RI EQUIPMENT/FURNISHINGS- FORWARD GALLEY DOOR DOORWAY HEADER PANEL - INSTALLATION OF ATTENDANT RECOMMENDED SERVICE UNIT. SERVICE BULLETIN MOS 27-JAN-2011 SB 737-25-1543 EQUIPMENT l FURNISHINGS - FLIGHT COMPARTMENT AND FORWARD CARGO COMPARTMENT - FLIGHT DECK NOISE RECOMMENDED REDUCTION CHANGE. SERVICE BULLETIN MOS 09-N0v-2012 SB 737-25-1544 04-OCT-2000 SB 737-25-1544 RI PASSENGER CABIN PARTITIONS AND COMPARTMENTS - SUPPORT FITTING ASSEMBLY AIR CONDITIONING EXTRUSIONS REPLACEMENT. SERVICE BULLETIN MOS 72 (s) AFL 36000 EQUIPMENT/FURNISHING - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - SUPPORT FITTING ASSEMBLY SUPERSEDED AIR CONDITIONING EXTRUSIONS REPLACEMENT (SUPERSEDED BY SB SB 737-25-1544 R2). SERVICE BULLETIN MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time 34 Of 748 '2 Camp Systems EFTA00618325 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-25-1544 R2 23-MAR-2011 EQUIPMENT/FURNISHING - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - SUPPORT FITTING ASSEMBLY AIR CONDITIONING EXTRUSIONS REPLACEMENT. SERVICE BULLETIN MOS 72 (s) RECOMMENDED SB 737-25-1545 EQUIPMENT AND FURNISHINGS - PASSENGER COMPARTMENT - MODIFICATION OF THE OXYGEN ACTIVATION SUPERSEDED NOT APPLICABLE - PER PN NOT INSTALLED MECHANISM WITHIN THE PASSENGER SERVICE UNITS (SUPERSEDED BY SB 737-25-1545 R1). SERVICE BULLETIN MOS 24-AUG-2007 - (s) 2968:28 AFL 699 SB 737-25-1545 RI EQUIPMENT AND FURNISHINGS - PASSENGER COMPARTMENT - MODIFICATION OF THE OXYGEN ACTIVATION SUPERSEDED NOT APPLICABLE - PER PN NOT INSTALLED MECHANISM WITHIN THE PASSENGER SERVICE UNITS (SUPERSEDED BY SB 737-25-1545 R2). SERVICE BULLETIN MOS 24-AUG-2007 - (s) 2968:28 AFL 699 SB 737-25-1545 R2 EQUIPMENT AND FURNISHINGS - PASSENGER COMPARTMENT - MODIFICATION OF THE OXYGEN ACTIVATION RECOMMENDED MECHANISM WITHIN THE PASSENGER SERVICE UNITS. SERVICE BULLETIN MOS 60 (s) 02-MAY-2007 SB 737-25-1593 EQUIPMENT/FURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - INSTALL OVERHEAD STOWAGE BIN DURABILITY PATCH. SERVICE BULLETIN MOS I2-MAR-2008 SB 737-25-1602 SB 737-25-1602 RI I0-DEC-2010 SB 737-25-1617 I I -JUN-2009 SB 737-25-1617 RI 09-NOV-2009 AUTOMATIC OVERWING EXIT DOOR SURROUND STRUCTURE - CHANGE UPPER AND LOWER DOOR SILLS (SUPERSEDED BY SB 737-25-1602 RI). SERVICE BULLETIN MOS SUPERSEDED EQUIPMENT/FURNISHINGS - AUTOMATIC OVERWING EXIT DOOR SURROUND STRUCTURE - CHANGE UPPER AND RECOMMENDED LOWER DOOR SILLS. SERVICE BULLETIN MOS CUP HOLDERS INSTALLATION CHANGE. SERVICE BULLETIN MOS FLIGHT COMPARTMENT - CUP HOLDERS INSTALLATION CHANGE. SERVICE BULLETIN MOS RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 35 Of 748 @ Camp Systems EFTA00618326 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-25-1636 21-MAY-2010 SB 737-25-1639 EQUIPMENT/FURNISHINGS - PASSENGER SEATS - EMERGENCY EXIT DOOR - ARMREST INSTALLATION. SERVICE BULLETIN MOS EQUIPMENT AND FURNISHINGS - PASSENGER COMPARTMENT - INTERIOR RECONFIGURATION - CHANGE FROM 167 RECOMMENDED PASSENGER DUAL CLASS CONFIGURATION TO 176 PASSENGER SINGLE CLASS CONFIGURATION WITH PANASONIC IN-FLIGHT ENTERTAINMENT (SUPERSEDED BY SB 737-25-1639 R1). SERVICE BULLETIN MOS 09-DEC-2010 SB 737-25-1601 EQUIPMENT / FURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - CENTER OVERHEAD SUPERSEDED NOT APPLICABLE - BY EFFECTIVITY STOWAGE BOX WITH LIFERAFT PROVISIONS - 9G TIE ROD ATTACHMENT CHANGE (SUPERSEDED BY S8 [SSN REDACTED] R1). SERVICE BULLETIN MOS SB 737-25-1601 RI EQUIPMENT 7 FURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - CENTER OVERHEAD SUPERSEDED STOWAGE BOX WITH LIFERAFT PROVISIONS - 9G TIE ROD ATTACHMENT CHANGE (SUPERSEDED BY SB 737-25-1601 R2). SERVICE BULLETIN MOS SB 737-25-1601 R2 EQUIPMENT 7 FURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - CENTER OVERHEAD RECOMMENDED STOWAGE BOX WITH LIFERAFT PROVISIONS - 9G TIE ROD ATTACHMENT CHANGE. SERVICE BULLETIN MOS 60 (s) I3-MAY-2011 SB 737-25-1602 EQUIPMENT FURNISHINGS - PASSENGER AND CABIN ATTENDANT ACCOMMODATIONS SAM250 SLIDE COVER RECOMMENDED ASSEMBLY FOR HBL3330 ELECTRICAL OUTLET - CHANGE. SERVICE BULLETIN MOS 22-FEB-20 II SB 737-25-1603 EQUIPMENT/FURNISHINGS - ESCAPE SLIDES. SNAPS AND LANYARDS - CARGO DOOR. PERSONNEL SAFETY NET REPLACEMENT. SERVICE BULLETIN MOS SB 737-25-1605 I I -MAY-2012 EQUIPMENT/FURNISHINGS - PASSENGER CABIN FLOORS - SECTIONS 44 - CHANGE SOUND DAMPING MATERIALS OF RECOMMENDED FLOOR PANELS. SERVICE BULLETIN MOS 12 (s) SB 737-25-1606 EQUIPMENT FURNISHINGS - POWER DISTRIBUTION PANEL P92- CIRCUIT BREAKER C0912. INOP COLLAR AND LABEL RECOMMENDED INSTALLATION. SERVICE BULLETIN MOS 02-AUG-20I2 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 36 Of 748 @ Camp Systems EFTA00618327 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-25-1647 EQUIPMENT FURNISHINGS - PASSENGER SEATS - PALLETIZED SEAT PALLET LATCH REPLACEMENT. SERVICE BULLETIN MOS RECOMMENDED 12-OCT-201 I SB 737-25-1648 EQUIPMENTIFURNISHINGS-BUFFETIGALLEY. GALLEY NUMBER 2. FOLDING TROLLEY INSTALLATION. SERVICE RECOMMENDED BULLETIN 13-MAY-2011 MOS SB 737-25-1651 EOUIPMENTIFURNISHINGS - PASSENGER CABIN LININGS AND PANELS - RIGHT SIDE SIDEWALL AND LITERATURE RECOMMENDED POCKET REPLACEMENT. SERVICE BULLETIN 15-AUG-2011 MOS SB 737-25-1654 EQUIPMENTIFURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - BOEING SKY INTERIOR RECOMMENDED OVERHEAD STOWAGE BINS. INSTALLATION OF FASTER DEPLOYING BIN RATE CONTROLS FOR THE FORWARD AND AFT. LEFT AND RIGHT TERMINATION BINS (SUPERSEDED BY SB 737-25-1654 R1). SERVICE BULLETIN 24-JUL-2012 MOS SB 737-25-1654 RI EOUIPMENTIFURNiSHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - BOEING SKY INTERIOR RECOMMENDED OVERHEAD STOWAGE BINS. INSTALLATION OF FASTER DEPLOYING BIN RATE CONTROLS FOR THE FORWARD AND AFT. LEFT AND RIGHT TERMINATION BINS. SERVICE BULLETIN 07-MAR-2013 MOS SB 737-25-1660 EOUIPMENTIFURNISHINGS- ELECTRICAL EQUIPMENT RACK MOISTURE SHROUD - CHANGE (SUPERSEDED BY SB SUPERSEDED 737-25-1660 RI). SERVICE BULLETIN MOS SB 737-25-1660 RI EQUIPNIENTIFURNIS11INGS- ELECTRICAL EQUIPMENT RACK MOISTURE SHROUD - CHANGE. SERVICE BULLETIN RECOMMENDED 26-SEP-2012 MOS SB 737-25-1661 EQUIPMENT r FURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - OUTBOARD STOWAGE RECOMMENDED CLOSET - REPLACEMENT OF FORWARD LEFT FULL HEIGHT CLOSET DOOR ASSEMBLIES. SERVICE BULLETIN MOS 16-OCT-2012 SB 737-25-1663 EQUIPMENTFURNiSHINGS - WINDOW SHADE AND REVEAL ASSEMBLY - BOEING SKY INTERIOR AUTOMATIC SUPERSEDED OVERWING EXIT DOOR WINDOW SHADE AND REVEAL ASSEMBLY REPLACEMENT (SUPERSEDED BY SB 737-25-1663 R1). SERVICE BULLETIN MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CAN (EBT)-Estimated Base Time 37 Of 748 Camp Systems EFTA00618328 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-25-1663 RI EQUIPMENT/FURNISHINGS - WINDOW SHADE AND REVEAL ASSEMBLY - BOEING SKY INTERIOR AUTOMATIC SUPERSEDED OVERWING EXIT DOOR WINDOW SHADE. REVEAL ASSEMBLY. AND INSULATION BLANKET REPLACEMENT (SUPERSEDED BY SB 737-25-1663 R2). SERVICE BULLETIN MOS SB 737-25-1663 R2 EQUIPMENT/FURNISHINGS - WINDOW SHADE AND REVEAL ASSEMBLY - BOEING SKY INTERIOR AUTOMATIC RECOMMENDED OVERWING EXIT DOOR WINDOW SHADE. REVEAL ASSEMBLY. AND INSULATION BLANKET REPLACEMENT. SERVICE BULLETIN MOS 02-DEC-2013 SB 737-25-1665 EQUIPMENT/FURNISHINGS - PASSENGER CABIN LININGS AND PANELS - CHANGE OVERWING EMERGENCY EXIT RECOMMENDED DOOR MOUNTED ARMREST PADS (SUPERSEDED BY SB 737-25-1665 R1). SERVICE BULLETIN MOS 24-APR-20I2 SB 737-25-1665 RI EQUIPMENT/FURNISHINGS - PASSENGER CABIN LININGS AND PANELS - CHANGE OVERWING EMERGENCY EXIT SUPERSEDED DOOR MOUNTED ARMREST PADS (SUPERSEDED BY SB 737-25-1665 R2). SERVICE BULLETIN MOS SB 737-25-1665 R2 EQUIPMENT/FURNISHINGS - PASSENGER CABIN LININGS AND PANELS - CHANGE OVERWING EMERGENCY EXIT NOT APPLICABLE DOOR MOUNTED ARMREST PADS (REPLACED BY SB 737-25-1663 R2). SERVICE BULLETIN MOS 03-DEC-2013 SB 737-25-1667 EQUIPMENT 7 FURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - PARTITIONS - PLACARD RECOMMENDED REMOVAL NO CHILDREN THIS ROW. SERVICE BULLETIN MOS I5-AUG-2012 SB 737-25-1668 02-AUG-20I2 SB 737-25-1671 23-MAR-2012 SB 737-25-1672 29-MAR-2013 EQUIPMENT/FURNISHINGS - CABIN ATTENDANT STATIONS- REPLACEMENT OF FORWARD ATTENDANT CONTROL RECOMMENDED PANEL AND SHROUD FOR IMPROVED RELIABILITY - BOEING SKY INTERIOR AIRPLANES. SERVICE BULLETIN MOS EQUIPMENT/FURNISHINGS - PASSENGER CABIN LININGS AND PANELS - SIDEWALL PANEL ASSEMBLY - RECOMMENDED REPLACEMENT OF SIDEWALL PANEL ASSEMBLY AT GALLEY 2 INTERFACE. SERVICE BULLETIN MOS EQUIPMENT/FURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - INSTALL MEGAPHONES IN THE RECOMMENDED BOEING SKY INTERIOR LEFT FORWARD AND AFT TERMINATION OVERHEAD STOWAGE BINS. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 38 Of 748 @ Camp Systems EFTA00618329 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-25-1677 EQUIPMENT FURNISHINGS - ATTENDANT SEATS AND PANELS - ATTENDANT PANEL ASSEMBLY -REPLACEMENT, RECOMMENDED SERVICE BULLETIN 04-DEC-2012 MOS SB 737-25-1678 EQUIPMENT! FURNISHINGS - AFT. LEFT SIDE PRIVACY CURTAIN - ENCLOSURE INSTALLATION (SUPERSEDED BY SB SUPERSEDED 737-25-1678 RI), SERVICE BULLETIN MOS SB 737-25-1678 RI EQUIPMENT FURNISHINGS - AFT. LEFT SIDE PRIVACY CURTAIN- ENCLOSURE INSTALLATION. SERVICE BULLETIN OPERATORS DISCRETION MOS 26-AUG-20I3 SB 737-25-1679 EQUIPMENT/FURNISHINGS - PASSENGER SEAT - MOVE THE PASSENGER SEATS. CHANGE CARPETS. SERVICE RECOMMENDED BULLETIN IS-MAR-2013 SB 737-25-1680 08-MAR-2013 SB 737-25-1681 21-SEP-2012 MOS EQUIPMENT FURNISHINGS - PASSENGER CABIN LININGS AND PANELS- WINDOW SHADE AND REVEAL ASSEMBLY - RECOMMENDED CHANGE THE WINDOW SHADES. SERVICE BULLETIN MOS EQUIPMENT/FURNISHING- PASSENGER CABIN UNING AND PANELS - SIDEWALL PANEL ASSEMBLY - CHANGE RECOMMENDED MEDICAL OUTLET PLACARD. SERVICE BULLETIN MOS SB 737-25-1682 EQUIPMENT FURNISHINGS - PASSENGER CABIN LININGS AND PANELS- WINDOW SHADE AND REVEAL ASSEMBLY - RECOMMENDED CHANGE THE WINDOW SHADES. SERVICE BULLETIN MOS 25-MAR-2013 SB 737-25-1680 EQUIPMENT/FURNISHINGS- PASSENGER COMPARTMENT - BOEING SKY INTERIOR OVERWING EXIT DOOR LINER RECOMMENDED REPLACEMENT. SERVICE BULLETIN MOS 14-MAY-2013 SB 737-25-1685 EQUIPMENT/FURNISHINGS- PASSENGER CABIN LININGS AND PANELS - INSTALLATION OF ALUMINUM FOIL TAPE ON RECOMMENDED BACK SIDE OF SIDEWALL PANELS. SERVICE BULLETIN MOS Of-MAR-2013 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 39 Of 748 @ Camp Systems EFTA00618330 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-25-1689 EQUIPMENT / FURNISHINGS - LAVATORIES - MODULAR LAVATORY A- REPLACE LAVATORY A THRESHOLD LIGHT SUPERSEDED WITH STRIKE PLATE (SUPERSEDED BY SB 737-25-1689 R1). SERVICE BULLETIN MOS SB 737-25-1689 RI EQUIPMENT! FURNISHINGS - LAVATORIES - MODULAR LAVATORY A- REPLACE LAVATORY A THRESHOLD LIGHT RECOMMENDED WITH STRIKE PLATE. SERVICE BULLETIN MOS 09-JUL-2014 - (s) SB 737-25-1691 EQUIPMENT/FURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - BOEING SKY INTERIOR OPERATORS OVERHEAD STOWAGE BINS - INSPECTION AND CHANGE OF THE THRESHOLD TRIM ASSEMBLY. SERVICE BULLETIN DISCRETION MOS 04-SEP-2013 SB 737-25-1693 EQUIPMENT / FURNISHINGS - PARTITIONS - REPLACEMENT OF JOGGLED CLASS DWIDERS. SERVICE BULLETIN RECOMMENDED MOS 28-JUN-20I3 SB 737-25-1702 EQUIPMENT/FURNISHINGS - DETACHABLE EMERGENCY EQUIPMENT - AFT RIGHT SIDE TERMINATION STOWAGE BIN RECOMMENDED CHANGE PORTABLE OXYGEN BOTTLES INSTALLATION. SERVICE BULLETIN MOS 23-JUN-20I4 - (s) SB 737-25-1703 EQUIPMENT! FURNISHINGS- PASSENGER COMPARTMENT- PASSENGER SERVICE UNIT - REPLACE 12 MINUTE RECOMMENDED OXYGEN GENERATORS WITH 22 MINUTE OXYGEN GENERATORS. SERVICE BULLETIN MOS 06-DEC-2013 SB 737-25-1706 EQUIPMENT/FURNISHINGS- PASSENGER COMPARTMENT - SIDEWALL - AFT EMERGENCY EXIT. AUTOMATIC RECOMMENDED OVERWING (AOE) EXIT DOOR - LEFT AND RIGHT SIDE. SEAT INTRUSION CONTROL BLOCK INSTALLATION. SERVICE BULLETIN I3-JUN-2014 MOS SB 737-25A1372 FLIGHT COMPUTER FWD INSTRUMENT PANEL ACCESS PANEL FASTENER INTERFERENCE. SERVICE BULLETIN MOS 20-MAY-1999 - (s) SB 737-25A1383 RI RUDDER PEDAL COVER FASTENER INTERFERENCE. SERVICE BULLETIN RECOMMENDED COMPUED WITH MOS 13-SEP-1999 02-DEC-1999 -(s) SB 737-25A1626 EQUIPMENT/FURNISHINGS- ELECTRICAL EQUIPMENT RACK MOISTURE SHROUD - LIQUID CONTAMINATION RECOMMENDED PROTECTION IMPROVEMENTS ON THE E5 ELECTRONIC RACK DRIPSHIELD EQUIPMENT. SERVICE BULLETIN MOS 60 (EFF) 25-MAR-2015 25-MAR-2015 25-MAR-2010 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 40 Of 748 @ Camp Systems EFTA00618331 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-26-1112 06-DEC-2001 SB 737-26-1112 RI CORROSION PROTECTION OF THE FENWAL CONNECTORS. SERVICE BULLETIN 06-FEB-2003 CORROSION PROTECTION OF THE FENWAL CONNECTORS. SERVICE BULLETIN MOS 6(s) (EFF) MOS 6 (s) SB 737-26-1121 FIRE PROTECTION - LOWER CARGO COMPARTMENT SMOKE DETECTION - INSTALLATION OF FORWARD CARGO SUPERSEDED COMPARTMENT SMOKE PENETRATION SEALING PROVISIONS (SUPERSEDED BY 737-26-1121 R1). SERVICE BULLETIN MOS 13-DEC-2007 - Is) + SB 737-26-1121 RI FIRE PROTECTION - LOWER CARGO COMPARTMENT SMOKE DETECTION - INSTALLATION OF FORWARD CARGO RECOMMENDED COMPARTMENT SMOKE PENETRATION SEALING PROVISIONS. SERVICE BULLETIN MOS 72 (s) I3-DEC-2007 SB 737-26-1122 FIRE PROTECTION- LOWER CARGO COMPARTMENT SMOKE DETECTION- FORWARD CARGO COMPARTMENT SMOKE SUPERSEDED PENETRATION ELECTRICAL CHANGES (SUPERSEDED BY 737-26-1122 R1). SERVICE BULLETIN MOS I3-DEC-2007 - (s) SB 737-26-1122 RI I3-AUG-2009 SB 737-26-1123 I8-JAN-2005 SB 737-26-1123 RI 21-MAR-2005 LOWER CARGO COMPARTMENT SMOKE DETECTION- FORWARD CARGO COMPARTMENT SMOKE PENETRATION ELECTRICAL CHANGES. SERVICE BULLETIN MOS 72 (s) REPLACEMENT OF THE LEFT AND RIGHT ENGINE CORE FIRE DETECTION HARNESSES. SERVICE BULLETIN MOS FIRE PROTECTION - ENGINE FIRE DETECTION - REPLACEMENT OF THE LEFT AND RIGHT ENGINE CORE FIRE DETECTION HARNESSES. SERVICE BULLETIN MOS SB 737-26-1123 R2 FIRE PROTECTION - ENGINE FIRE DETECTION - REPLACEMENT OF THE LEFT AND RIGHT ENGINE CORE FIRE DETECTION HARNESSES. SERVICE BULLETIN MOS I6-AUG-2007 SB 737-26-1123 R3 28-FEB-2008 FIRE PROTECTION - ENGINE FIRE DETECTION - REPLACEMENT OF THE LEFT AND RIGHT ENGINE CORE FIRE DETECTION HARNESSES. SERVICE BULLETIN MOS RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 41 Of 748 @ Camp Systems EFTA00618332 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-26-1123 R4 20-AUG-2008 ENGINE FIRE DETECTION - REPLACEMENT OF THE LEFT AND RIGHT ENGINE CORE FIRE DETECTION HARNESSES. SERVICE BULLETIN MOS SB 737-26-1123 RS ENGINE FIRE DETECTION - REPLACEMENT OF THE LEFT AND RIGHT ENGINE CORE FIRE DETECTION HARNESSES SUPERSEDED (SUPERSEDED BY 737-26-1123 R6), SERVICE BULLETIN MOS 27-APR-2009 SB 737-26-1123 Re FIRE PROTECTION - ENGINE FIRE DETECTION - REPLACEMENT OF THE LEFT AND RIGHT ENGINE CORE FIRE SUPERSEDED DETECTION HARNESSES (SUPERSEDED BY SB 737-26-1123 R7). SERVICE BULLETIN MOS SB 737-26-1124 FIRE PROTECTION- WHEEL WELL. WING AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM- MAIN WHEEL WELL CONNECTOR CORROSION PREVENTION. SERVICE BULLETIN MOS 72-JAN-2006 SB 737-26-1131 FIRE PROTECTION- WHEEL WELL. WING. AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM- DUCT LEAK SUPERSEDED OVERHEAT DETECTOR SUPPORT INSTALLATION (SUPERSEDED BY SB 737-26-1131 R1). SERVICE BULLETIN MOS 58 [SSN REDACTED] RI FIRE PROTECTION - WHEEL WELL. WING. AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM - DUCT LEAK RECOMMENDED OVERHEAT DETECTOR SUPPORT INSTALLATION. SERVICE BULLETIN MOS 14-OCT-2011 58 [SSN REDACTED] FIRE PROTECTION -CARGO FIRE EXTINGUISHING SYSTEM - INSTALLATION OF SECOND FIRE BOTTLE FOR SUPERSEDED EXTENDED RANGE TWIN ENGINE OPERATIONS (SUPERSEDED BY SB 737-26-1133 R1). SERVICE BULLETIN MOS SB 737-26A1099 ENGINE FIRE EXTINGUISHING BOTTLES. SERVICE BULLETIN RECOMMENDED DAYS 90 (s) 17-JAN-2001 01-NOV-2000 634 AFL 175 SB 737-26A1108 RI ENGINES AND CARGO COMPARTMENT FIRE EXTINGUISHING BOTTLE HOSES INSPECTION AND REPLACEMENT. RECOMMENDED SERVICE BULLETIN MOS 12 (s) 27-JUN-2002 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 42 Of 748 @ Camp Systems EFTA00618333 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-26A1109 ENGINES. APU AND CARGO COMPARTMENT FIRE EXTINGUISHING BOTTLE HOSES AND WING-TO-STRUT ENGINE RECOMMENDED NOT APPLICABLE - BY EFFECTIVITY FUEL SUPPLY HOSES INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS 15-NOV-2001 - (s) SB 737-26A1109 R1 ENGINES. APU AND CARGO COMPARTMENT FIRE EXTINGUISHING BOTTLE HOSES AND WING-TO-STRUT ENGINE RECOMMENDED NOT APPLICABLE - BY EFFECTIVITY FUEL SUPPLY HOSES INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS 18 (s) 07-NOV-2002 SB 737-26A1109 R2 ENGINES. APU AND CARGO COMPARTMENT FIRE EXTINGUISHING BOTTLE HOSES AND WING-TO-STRUT ENGINE NOT APPLICABLE - BY SERIAL NUMBER FUEL SUPPLY HOSES INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS 30-NOV-2005 15-NOV-2001 -(s) 2338:24 AFL 573 SB 737-26A1109 R3 ENTINGUISHING - ENGINES. APU AND CARGO COMPARTMENT FIRE EXTINGUISHING BOTTLE HOSES AND COMPUED WITH - NO REWORK REQUIRED WING-TO-STRUT ENGINE FUEL SUPPLY HOSES INSPECTION AND REPLACEMENT. SERVICE BULLETIN FOUND S8 737-26A1109 R2 ALREADY COMPUED WITH AS NOT APPLICABLE 30-NOV-2005 (2338:24 HRS. 573 CYC) REF WO GUBBJ111-0202 MOS 05-APR-2007 29-SEP-2005 2871:09 AFL 676 SB 737-26A1118 FIRE PROTECTION-ENGINE FIRE EXTINGUISHING BOTTLES-GROUNDS INSPECTION/CHECK. SERVICE BULLETIN RECOMMENDED DAYS 90 (5) I7-OCT-2002 SB 737-26A1118 R1 FIRE PROTECTION-ENGINE FIRE EXTINGUISHING BOTTLES-GROUNDS INSPECTION/CHECK. SERVICE BULLETIN RECOMMENDED NOT APPLICABLE - BY VARIABLE NUMBER. MOS 22-DEC-2004 08-APR-2004 1951:36 AFL 476 SB 737-26A1137 FIRE PROTECTION -CARGO BAY SMOKE DETECTION - EQUIPMENT COOLING SYSTEM SMOKE CLEARANCE MODE RECOMMENDED OPERATIONAL TEST FOR CARGO SMOKE PROTECTION. SERVICE BULLETIN MOS 22-MAY-2014 - (s) SB 737-26A1137 TABLE PERFORM FIRE PROTECTION- CARGO BAY SMOKE DETECTION - EQUIPMENT COOLING SYSTEM SMOKE RECOMMENDED 1.1 CNF 1 CLEARANCE MODE OPERATIONAL TEST FOR CARGO SMOKE PROTECTION. SERVICE BULLETIN A SMOKE CLEARANCE MODE - OPERATIONAL TEST (GROUP I. CONFIGURATION I AIRPLANES) MOS SI (s) 22-MAY-20I4 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 43 Of 748 @ Camp Systems EFTA00618334 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-26A1137 TABLE PERFORM FIRE PROTECTION - CARGO BAY SMOKE DETECTION - EQUIPMENT COOLING SYSTEM SMOKE 1.2 CNF 2 CLEARANCE MODE OPERATIONAL TEST FOR CARGO SMOKE PROTECTION. SERVICE BULLETIN A SMOKE CLEARANCE MODE - OPERATIONAL TEST (GROUP 1. CONFIGURATION 2. GROUP 2 AND GROUP 3 AIRPLANES) MOS - (s) SB 737-26A1137 TABLE PERFORM FIRE PROTECTION - CARGO BAY SMOKE DETECTION - EQUIPMENT COOLING SYSTEM SMOKE 1.3 CLEARANCE MODE OPERATIONAL TEST FOR CARGO SMOKE PROTECTION. SERVICE BULLETIN A SYSTEM FAULT ISOLATION (IF THE SMOKE CLEARANCE MODE - OPERATIONAL TEST RESULT IS NOT SATISFACTORY) MOS 22-MAY-2014 SB 737-27-1210 28-OCT-1999 BF/F (s) HORIZ STAB-REPLACEMENT OF STAB TRIM ACTUATOR. SERVICE BULLETIN MOS - (s) 22-AUG-2008 3260:48 AFL 782 SB 737-27-1210 RI HORIZONTAL STABILIZER REPLACEMENT OF STABILIZER TRIM ACTUATOR. SERVICE BULLETIN MOS 22-AUG-2008 01 -JUN-2000 4500 (s) 3260:48 RECOMMENDED AFL 782 SB 737-27-1215 FLIGHT CONTROLS- ELEVATOR AND TAB- INSTALLATION OF A 10-SECOND DELAY FOR THE RIGHT ELEVATOR RECOMMENDED ANTI-BALANCE TAB, SERVICE BULLETIN MOS 01-APR-1999 -(s) SB 737-27-1215 RI FLIGHT CONTROLS - ELEVATOR TAB - INSTALLATION OF A 10-SECOND DELAY.RIGHT ELEVATOR ANTI-BALANCE RECOMMENDED TAB. SERVICE BULLETIN MOS 07-DEC-2000 - (s) COMPUED WITH COMPUED WITH - IAW THE 58 SB 737-27-1224 AILERON 8 AILERON TRIM CONTROL SYSTEM. SERVICE BULLETIN RECOMMENDED COMPLIED WITH -Cm MOS 19-JAN-2000 21-OCT-1999 3200 (s) S8 [SSN REDACTED] ELEVATOR AND TAB CONTROL SYSTEM TEST, SERVICE BULLETIN MOS 28-FEB-2002 - (s) S8 [SSN REDACTED] MAIN WHEEL WELL AFT BULKHEAD STANDBY SHUT-OFF VALVE GROUND WIRE INSTALLATION MODIFICATION. RECOMMENDED SERVICE BULLETIN 10-MAY-2001 MOS 18 (s) 6000 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 44 Of 748 @ Camp Systems EFTA00618335 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27-1242 29-MAR-2001 SB 737-27-1242 RI 28-SEP-2002 SB 737-27-1244 I4-JUN-2001 MOS - (s) SB 737-27-1247 RI WIRE PROVISIONS FOR RUDDEER SYSTEM ENHANCEMENT. SERVICE BULLETIN RECOMMENDED COMPUED WITH - IAW THE 58 REV.1 N/A FOR AIRCRAFT REV 00 ALREADY CAN. MOS 13-AUG-2007 25-JUL-2002 - (s) 1785:05 AFL 446 SB 737-27-1247 R2 RUDDER AND RUDDER TRIM CONTROL SYSTEM - WIRE PROVISIONS FOR RECOMMENDED RUDDER SYSTEM ENHANCEMENT. SERVICE BULLETIN MOS 26-NOV-2008 - SB 737-27-1248 FLIGHT CONTROLS - ELEVATOR PITOT-STATIC SYSTEM - TURN THE PITOT PROBE DOWN. SERVICE BULLETIN FLIGHT CONTROLS - LIFT AUGMENTING - LEADING EDGE - CRUISE DEPRESSURIZATION VALVE MODIFICATION. SERVICE BULLETIN MOS - (s) UFT AUGMENTING - LEADING EDGE - CRUISE DEPRESSURIZATION. SERVICE BULLETIN MOS - (s) ELEVATOR FEEL COMPUTER. SERVICE BULLETIN RECOMMENDED RECOMMENDED RECOMMENDED 24-JAN-2002 SB 737-27-1251 II-JUL-2002 SB 737-27-1251 RI 27-FEB-2003 SB 737-27-1253 02-JAN-2003 SB 737-27-1253 RI 27-MAR-2003 MOS - (s) STALL MANAGEMENT YAW DAMPER (SMYD)-REPLACEMENT. SERVICE BULLETIN MOS - (s) STALL MANAGEMENT YAW DAMPERS(SMYD) REPLACEMENT. SERVICE BULLETIN MOS INSTALLATION OF AN ENHANCED RUDDER CONTROL SYSTEM. SERVICE BULLETIN MOS INSTALLATION OF AN ENHANCED RUDDER CONTROL SYSTEM. SERVICE BULLETIN MOS RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 45 Of 748 @ Camp Systems EFTA00618336 flP Megnand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27-1253 R2 07-OCT-2004 INSTALLATION OF AN ENHANCED RUDDER CONTROL SYSTEM (RSEP). SERVICE BULLETIN MOS RECOMMENDED SB 737-27-1253 R3 FLIGHT CONTROLS - RUDDER AND RUDDER TRIM CONTROL SYSTEM - INSTALLATION OF AN ENHANCED RUDDER COMPLIED WITH - IAW THE SB CONTROL SYSTEM (RSEP). SERVICE BULLETIN MOS 22-AUG-2008 12-MAY-2086 - (s) 3260:48 AFL 782 SB 737-27-1253 R4 RUDDER AND RUDDER TRIM CONTROL SYSTEM - INSTALLATION OF AN RECOMMENDED ENHANCED RUDDER CONTROL SYSTEM (RSEP) - TEST. SERVICE BULLETIN MOS 07-MAY-2009 SB 737-27-1254 FLIGHT CONTROLS-CONTROL CABLE ASSEMBLIES WITH "LOW ZINC' COATING (SUPERSEDED BY 737-27-1254 RI ). SUPERSEDED SERVICE BULLETIN 31-OCT-2002 MOS - (s) SB 737-27-1254 E. 1 INSPECT FLIGHT CONTROLS-CONTROL CABLE ASSEMBLIES WITH 'LOW ZINC' COATING (SUPERSEDED BY RECOMMENDED 737-27-1254 RI). SERVICE BULLETIN UNPROTECTED CONTROL CABLE ASSEMBLIES WITH 'LOW ZINC' COATING MOS RECURRING 31-OCT-2002 SB 737-27-1254 E. 2 INSPECT FLIGHT CONTROLS-CONTROL CABLE ASSEMBLIES WITH 'LOW ZINC' COATING (SUPERSEDED BY RECOMMENDED 737-27-1254 RI). SERVICE BULLETIN PROTECTED CONTROL CABLE ASSEMBLIES WITH 'LOW ZINC' COATING MOS RECURRING 31-OCT-2002 SB 737-27-1254 RI CONTROL CABLE ASSEMBLIES WITH LOW ZINC COATING-INSPECTION AND REPLACEMENT (SUPERSEDED BY SUPERSEDED 737-27-1254 R2). SERVICE BULLETIN MOS 14-APR-2003 SB 737-27-1254 RI E.1 INSPECT CONTROL CABLE ASSEMBLIES WITH LOW ZINC COATING-INSPECTION AND REPLACEMENT (SUPERSEDED RECOMMENDED BY 737-27-1254 R2), SERVICE BULLETIN UNPROTECTED CONTROL CABLE ASSEMBLIES WITH 'LOW ZINC' COATING MOS RECURRING 14-APR-2003 S8 [SSN REDACTED] RI E. 2 INSPECT CONTROL CABLE ASSEMBLIES WITH LOW ZINC COATING-INSPECTION AND REPLACEMENT (SUPERSEDED RECOMMENDED BY 737-27-1254 R2), SERVICE BULLETIN PROTECTED CONTROL CABLE ASSEMBLIES WITH 'LOW ZINC' COATING MOS RECURRING 14-APR-2003 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks *-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 46 Of 748 @Camp Systems EFTA00618337 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB SB 737-27-1254 RI E 3 I 7-APR-2003 [SSN REDACTED] R2 02-JUL-2008 REPLACE CONTROL CABLE ASSEMBLIES WITH LOW ZINC COATING-INSPECTION AND REPLACEMENT (SUPERSEDED BY 737-27-1254 R2). SERVICE BULLETIN CONTROL CABLE ASSEMBLIES MOS 24 (5) CONTROL CABLE ASSEMBLIES WITH LOW ZINC COATING - INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS SB 737-27-1254 R2 El INSPECT CONTROL CABLE ASSEMBLIES WITH LOW ZINC COATING- INSPECTION AND REPLACEMENT. SERVICE BULLETIN UNPROTECTED CONTROL CABLE ASSEMBLIES WITH 'LOW ZINC COATING MOS 9 (s) 02-JUL-2008 S8 [SSN REDACTED] R2 E2 INSPECT CONTROL CABLE ASSEMBLIES WITH LOW ZINC COATING- INSPECTION AND REPLACEMENT. SERVICE BULLETIN PROTECTED CONTROL CABLE ASSEMBLIES WITH 'LOW ZINC' COATING MOS 12 (s) 02-JUL-2008 SB 737-27-1254 R2 E3 REPLACE CONTROL CABLE ASSEMBLIES WITH LOW ZINC COATING - INSPECTION AND REPLACEMENT. SERVICE BULLETIN CONTROL CABLE ASSEMBLIES MOS 24 (s) 02-JUL-2008 SB 737-27-1262 RUDDER AND RUDDER TRIM CONTROL SYSTEM-REPLACEMENT OF THE P5-3 PANEL (RSEP).. SERVICE BULLETIN RECOMMENDED COMPLIED WITH - PREVIOUSLY 19-DEC-2002 SB 737-27-1262 RI 07-MAY-2009 SB 737-27-1268 12-OCT-2006 MOS - Is) 22-AUG-2008 3260:48 AFL 782 RUDDER AND RUDDER TRIM CONTROL SYSTEM- REPLACEMENT OF THE P5-3 PANEL (RSEP). SERVICE BULLETIN MOS FLIGHT CONTROLS - HORIZONTAL STABLIZER TRIM CONTROL SYSTEM - STABLIZER TRIM AND LIMIT SWITCHES WIRE BUNDLE PROTECTION. SERVICE BULLETIN MOS SB 737-27-1268 RI HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - STABILIZER TRIM AND UNIT SWITCHES WIRE BUNDLE PROTECTION. SERVICE BULLETIN MOS 29-AUG-2011 26-MAR-2009 3533:32 AFL 863 RECOMMENDED - INFORMATION REF TO RI RECOMMENDED COMPUED WITH - GROUP I A/C WIRE BUNDLES INSPECTED. IAW S8737-27-1268 RI FIGURE 1. GROUP 2 NC WIRE BUNDLES INSPECTED IAW SB 737-27-1268 RI FIGURE 2.. IAW S8 [SSN REDACTED] RI FIGURE 3 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 47 Of 748 @ Camp Systems EFTA00618338 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 [SSN REDACTED] 02-OCT-2003 RUDDER FEEL AND CENTERING UNIT-CAM ROLLER BOLT TO FLANGE CLEARANCE-INSPECTION AND REWORK. SERVICE BULLETIN MOS SB 737-27-1273 FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - AILERON BALANCE TAB FREEPLAY CHECK AND LUBRICATION. SERVICE BULLETIN 29-SEP-2005 MOS 24-AUG-2007 2968:28 RECOMMENDED COMPLIED WITH AFL 699 SB 737-27-1273 PART 1 FLIGHT CONTROLS -AILERON AND AILERON TRIM CONTROL SYSTEM - AILERON BALANCE TAB FREEPLAY CHECK COMPLIED WITH AND LUBRICATION. SERVICE BULLETIN MOS 24 (5) 24-AUG-2007 29-SEP-2005 8000 2968:28 AFL 699 SB 737-27-1273 PART 2 FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - AILERON BALANCE TAB FREEPLAY CHECK COMPLIED WITH AND LUBRICATION. SERVICE BULLETIN MOS 12 (s) 24-AUG-2007 29-SEP-2005 4000 2968:28 AFL 699 SB 737-27-1273 RI FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - AILERON BALANCE TAB FREEPLAY CHECK COMPLIED WITH AND LUBRICATION. SERVICE BULLETIN MOS 24-AUG-2007 79-DEC-2006 2968:28 AFL 699 SB 737-27-1273 RI PART FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - AILERON BALANCE TAB FREEPLAY CHECK COMPLIED WITH 1 AND LUBRICATION. SERVICE BULLETIN MOS 24 (5) 24-AUG-2007 19-DEC-2006 8000 2968:28 AFL 699 SB 737-27-1273 RI PART FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - AILERON BALANCE TAB FREEPLAY CHECK COMPLIED WITH 2 AND LUBRICATION. SERVICE BULLETIN MOS 12 (5) 24-AUG-2007 19-DEC-2006 4000 2968:28 AFL 699 SB 737-27-1273 R2 FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - AILERON BALANCE TAB FREEPLAY CHECK AND LUBRICATION. SERVICE BULLETIN MOS 03-JUL-2013 23-APR-2007 3723:21 AFL 908 COMPLIED WITH - IA.W. AD 2006-21-01 PART 1 AND PART 2 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time ,i6 Of 748 @ Camp Systems EFTA00618339 COMP Astant.frar• Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27-1273 R2 PART 1 23-APR-2007 SB 737-27-1273 R2 PART 2 23-APR-2007 SB 737-27-1282 15-MAR-2007 SB 737-27-1282 RI 14-JUN-2010 FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - AILERON BALANCE TAB FREEPLAY CHECK AND LUBRICATION. SERVICE BULLETIN MOS 24 (5) 8000 AFL 03-JUL-2013 3723:21 908 FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - AILERON BALANCE TAB FREEPLAY CHECK AND LUBRICATION. SERVICE BULLETIN MOS 12 (s) 03-JUL-2013 4000 3723:21 AFL 908 FLIGHT CONTROLS - RUDDER AND RUDDER TRIM CONTROL SYSTEM - WIRE BUNDLE W443 AND LEFT FORWARD SUPERSEDED RUDDER QUADRANT CLEARANCE INSPECTION (SUPERSEDED BY 737-27-1282 R1). SERVICE BULLETIN MOS - (s) FLIGHT CONTROLS - RUDDER AND RUDDER TRIM CONTROL SYSTEM- WIRE BUNDLE W443 AND LEFT FORWARD RECOMMENDED RUDDER QUADRANT CLEARANCE INSPECTION. SERVICE BULLETIN MOS 60 (s) SB 737-27-1284 FLIGHT CONTROLS - ELEVATOR AND TAB - LEFT AND RIGHT ELEVATOR TAB PUSHRODS REPLACEMENT. SERVICE BULLETIN MOS 48 (s) 28-NOV-2007 COMPUED WITH - LAW. AD 2006-21-01 PART I COMPUED WITH - IA.W. AD 2006-21-01 PART 2 SB 737-27-1284 RI ELEVATOR AND TAB- LEFT AND RIGHT ELEVATOR TAB PUSHRODS COMPUED WITH REPLACEMENT. SERVICE BULLETIN MOS 29-AUG-2011 28-NOV-2007 - (s) 3533:32 AFL 863 SB 737-27-1289 737 STABILIZER TAKEOFF WARNING SWITCHES - TEST OF THE TAKEOFF WARNING INDICATION. SERVICE BULLETIN RECOMMENDED COMPUED WITH DAYS 29-AUG-2011 RECURRING 07-APR-2010 750 3533:32 4283:32 SB 737-27-1290 AFL 863 TRAILING EDGE FLAP SYSTEM - FLAP UMIT SWITCH AND FLAP LANDING WARNING SWITCH REPLACEMENT (SUPERSEDED BY SB 737-27-1290 RI), SERVICE BULLETIN MOS SUPERSEDED SB 737-27-1290 RI FLIGHT CONTROLS - TRAILING EDGE FLAP SYSTEM - FLAPS UP LIMIT SWITCH AND FLAP LANDING WARNING LIMIT SUPERSEDED SWITCH REPLACEMENT (SUPERSEDED BY SB 737-27-1290 RZ. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 49 Of 748 @ Camp Systems EFTA00618340 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27-1290 R2 14-OCT-2011 FLIGHT CONTROLS - TRAILING EDGE FLAP SYSTEM - FLAPS UP AND FLAP LANDING WARNING LIMIT SWITCH REPLACEMENT. SERVICE BULLETIN MOS RECOMMENDED SB 737-27-1290 R3 FLIGHT CONTROLS - TRAILING EDGE FLAP SYSTEM - FLAPS UP AND FLAP LANDING WARNING LIMIT SWITCH RECOMMENDED 10-APR-2012 REPLACEMENT. SERVICE BULLETIN MOS SB 737-27-1290 R4 FLIGHT CONTROLS - TRAILING EDGE FLAP SYSTEM - FLAPS UP AND FLAP LANDING WARNING LIMIT SWITCH RECOMMENDED 28-NOV-2012 REPLACEMENT. SERVICE BULLETIN MOS SB 737-27-1291 LEADING EDGE FLAP AND SLAT CONTROL SYSTEM - LEADING EDGE SLATS- TITANIUM PROXIMITY SENSOR SUPERSEDED PROVISIONAL INSTALLATION (SUPERSEDED BY SB 737-27-1291 R1). SERVICE BULLETIN MOS SB 737-27-1291 RI LEADING EDGE FLAP AND SLAT CONTROL SYSTEM - LEADING EDGE SLATS- TITANIUM PROXIMITY SENSOR RECOMMENDED 18-N0V-2010 PROVISIONAL INSTALLATION. SERVICE BULLETIN MOS SB 737-27-1298 FLIGHT CONTROLS - CENTRAL WARNING SYSTEM - SPEEDBRAKE TAKEOFF WARNING SWITCH. 5651 - INSPECTION RECOMMENDED 18-AUG-2010 AND REPLACEMENT. SERVICE BULLETIN MOS SB 737-27-1300 SB 737-27-1300 RI SB 737-27-1303 21-JUN-2012 FLIGHT CONTROLS - ELEVATOR AND TAB - ELEVATOR TAB CONTROL MECHANISM - AFT ATTACH LUG MODIFICATION SUPERSEDED (SUPERSEDED BY S8 [SSN REDACTED] RI). SERVICE BULLETIN MOS - (s) FLIGHT CONTROLS - ELEVATOR AND TAB - ELEVATOR TAB CONTROL MECHANISM - AFT ATTACH LUG MODIFICATION. SERVICE BULLETIN MOS FLIGHT CONTROLS- FLIGHT SPOILER CONTROL SYSTEM- LEFT AND RIGHT WING FLIGHT SPOILERS SHORT FIELD RECOMMENDED PERFORMANCE POWER CONTROL UNIT REPLACEMENT. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 50 Of 748 @ Camp Systems EFTA00618341 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27A1219 11 -SEP-I998 FLAP/SLAT ELECTRONICS UNIT. SERVICE BULLETIN MOS - (s) RECOMMENDED SB 737-27A1222 MAIN RUDDER POWER CONTROL UNIT (SUPERSEDED BY SB 737-27A1222 RI). SERVICE BULLETIN SUPERSEDED COMPUED WITH-CM MOS 13-SEP-1999 - (s) SB 737-27A1222 RI MAIN RUDDER POWER CONTROL UNIT. SERVICE BULLETIN RECOMMENDED COMPUED WITH MOS 13-SEP-1999 28-JAN-I999 - (s) SB 737-27A1228 TRAILING EDGE FLAP AND HORIZONTAL STABILIZER TRIM SYSTEMS (SUPERSEDED BY SB 737-27A1228 R1). SERVICE SUPERSEDED COMPUED WITH BULLETIN MOS 13-SEP-1999 - (s) SB 737-27A1228 RI TRAILING EDGE FLAP AND HORIZONTAL STABILIZER TRIM SYSTEMS (SUPERSEDED BY SI3 737-27A1228 R2). SERVICE SUPERSEDED COMPUED WITH - CM BULLETIN MOS 13-SEP-1999 - (s) SB 737-27A1228 R2 TRAILING EDGE FLAP AND HORIZONTAL STABILIZER TRIM SYSTEMS (SUPERSEDED BY SI3 737-27A1228 R3). SERVICE SUPERSEDED BULLETIN MOS - (s) SB 737-27A1228 R3 TRAILING EDGE FLAP AND HORIZONTAL STABILIZER TRIM SYSTEMS. SERVICE BULLETIN RECOMMENDED COMPUED WITH MOS 13-SEP-1999 18-NOV-1999 300(s) 23:30 AFL 21 SB 737-27A1234 ELEVATOR-PCU RETENTION BRACKET AND BOLT (SUPERSEDED BY SB 737-27A1234 R1). SERVICE BULLETIN SUPERSEDED MOS - (s) SB 737-27A1234 RI ELEVATOR-PCU RETENTION BRACKET AND BOLT. SERVICE BULLETIN RECOMMENDED DAYS 7 (s) 22-NOV-2001 10-AUG-2000 854:54 AFL 225 SB 737-27A1239 FLIGHT CONTROLS - RUDDER AND RUDDER TRIM CONTROL SYSTEM - RELOCATION OF WIRE BUNDLES AWAY FROM RECOMMENDED COMPUED WITH - IAW THE SB THE RUDDER FEEL AND CENTERING UNIT. SERVICE BULLETIN MOS 22-AUG-2008 11 -JAN-2001 -(s) 3260:48 AFL 782 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 51 Of 748 @ Camp Systems EFTA00618342 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27A1245 SB 737-27AI245 RI EXCESSIVE FREEPLAY IN THE TAB CONTROL (SUPERSEDED BY SB 737-27A1245 R1). SERVICE BULLETIN MOS - Is) 26-APR-2001 EXCESSIVE FREEPLAY IN THE TAB CONTROL (SUPERSEDED BY SB 737-27A1245 R2) . SERVICE BULLETIN MOS - Is) SUPERSEDED COMPUED WITH - CM SUPERSEDED SB 737-27A1245 R2 EXCESSIVE FREEPLAY IN THE TAB CONTROL. SERVICE BULLETIN RECOMMENDED MOS 02-AUG-2002 - Is) SB 737-27A1259 RUDDER FEEL AND CENTERING UNIT - INSPECTION AND REPLACEMENT OF SPRING ASSEMBLY. SERVICE BULLETIN RECOMMENDED 30-MAY-2002 - Is) MOS SB 737-27A1259 PART A INSPECT/REPLACE RUDDER FEEL AND CENTERING UNIT - INSPECTION AND REPLACEMENT OF SPRING ASSEMBLY. RECOMMENDED SERVICE BULLETIN SPRING ASEMBLY DAYS 10 (s) 30-MAY-2002 SB 737-27A1259 PART 8 INSPECT/REPLACE RUDDER FEEL AND CENTERING UNIT - INSPECTION AND REPLACEMENT OF SPRING ASSEMBLY. RECOMMENDED SERVICE BULLETIN SPRING ASSEMBLY DAYS 90 (s) 30-MAY-2002 SB 737-27A1259 RI RUDDER FEEL AND CENTERING UNIT - INSPECTION AND REPLACEMENT OF SPRING ASSEMBLY. SERVICE BULLETIN RECOMMENDED MOS 19-DEC-2002 SB 737-27A1259 RI PART INSPECT RUDDER FEEL AND CENTERING UNIT - INSPECTION AND REPLACEMENT OF SPRING ASSEMBLY. SERVICE RECOMMENDED A BULLETIN DAYS 10 (s) 19-DEC-2002 SB 737-27A1259 RI PART REPLACE RUDDER FEEL AND CENTERING UNIT - INSPECTION AND REPLACEMENT OF SPRING ASSEMBLY. SERVICE RECOMMENDED 8 BULLETIN DAYS 90 (s) 19-DEC-2002 SB 737-27A1260 REPLACEMENT OF COMPENSATORS. SERVICE BULLETIN DAYS 180(s) 07-OCT-2002 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 52 Of 748 @ Camp Systems EFTA00618343 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27A1271 SB 737-27A1271 R1 ELEVATOR INPUT TORQUE TUBE MODIFICATION (SUPERSEDED BY SB 737-27A1271 R1). SERVICE BULLETIN MOS 22-AUG-2008 3260:48 AFL 782 FLIGHT CONTROLS - ELEVATOR AND TAB - ELEVATOR INPUT TORQUE TUBE - MODIFICATION. SERVICE BULLETIN MOS SB 737-27A1277 FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL NUT INSPECTION. LUBRICATION AND REPAIR/OVEFtHAUL. SERVICE BULLETIN MOS 24-AUG-2007 2968:28 AFL 699 SB 737-27A1277 PAC 1 (1) DETAILED INSPECTION FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL NUT INSPECTION. LUBRICATION AND REPAIR/OVERHAUL. SERVICE BULLETIN MOS 24 (s) 24-AUG-2007 27 -JUL-2005 2000 2968:28 AFL 699 SB 737-27A1277 PAC 1 (2) LUBRICATE FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM- BALLSCREW AND BALL NUT INSPECTION. LUBRICATION AND REPAIR/OVERHAUL. SERVICE BULLETIN MOS 12 (s) 24-AUG-2007 27 -JUL-2005 1600 2968:28 AFL 699 SB 737-27A1277 PAC 2 REPLACE FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL NUT INSPECTION. LUBRICATION AND REPAIR/OVERHAUL. SERVICE BULLETIN BALL NUT TUBE RETAINERS MOS 27 -JUL-2005 25000 (s) SUPERSEDED COMPUED WITH - IAW THE SB COMPUED WITH - PREVIOUSLY 737-27A1271 COMPUED WITH - PAC 1(1) INSPECTION - NEX DUE 151AUG/2099 - 9368HRS / PAC 1(2) LUBRICATION NEXT DUE 15/AUG/2008 - 4568 HRS / HSTA REPLACEMENT DUE 25.0000 AFUCYC TO BE ACCOMPLISHED IN REV 1 OF THIS SB COMPUED WITH - PAC 1(1) INSPECTION - NEX DUE 15/AUG/2C09 - 9368HRS IN REV.1 COMPUED WITH - NEXT DUE 15/AUG/2008 - 4568 HRS IN REV 1 OF THIS SB - REF: REV.1 SB 737-27A1277 PAC 3 REPLACE FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL NUT - REF: REV.1 INSPECTION. LUBRICATION AND REPAIR/OVERHAUL. SERVICE BULLETIN HORIZONTAL STABILIZER TRIM ACTUATOR MOS 27 -JUL-2005 25000 (s) SB 737-27A1277 RI FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN 25-JUL-2007 MOS 28-SEP-2009 3378:04 AFL 812 COMPLIED WITH - PAC 1 (1) INSPECTION AND PAC 1 (2) LUBERICATION REFER NEXT TO REV.2 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 53 Of 748 @Camp Systems EFTA00618344 COMP Astant.frar• Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27A1277 RI PAC 1 DETAIL INSPECTION FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL (1) 27-JUL-2007 NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN MOS 24 (s) 28-SEP-2009 6400 3378:04 AFL 812 SB 737-27A1277 RI PAC 1 LUBRICATE FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM- BALLSCREW AND BALL (2) NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN 25-JUL-2007 MOS 12 (s) 28-SEP-2009 1600 3378:04 COMPLIED WITH - REFER NEXT COMPLIANCE IN REV.2 COMPLIED WITH - REFER NEXT COMPLIANCE IN REV.2 AFL 812 SB 737-27A1277 RI PAC 2 REPLACE FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - R0i I cd-REW AND BALL - INFORMATION REFER TO REV2 NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN BALL NUT TUBE RETAINERS MOS 25-JUL-2007 25000 (s) SB 737-27A1277 RI PAC 3 REPLACE FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL COMPLIED WITH - REPLACEMENT PER NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN HORIZONTAL STABILIZER TRIM 737-27-1210/RI PN 251A4510-6 TSO .O'. ACTUATOR UPDATED COMPONENT TASK 27-108-00 WITH THE COMPLETION DATE OF THIS SB. FURTURE TRACKING OF THIS SB WILL BE ACCOMPLISHED PER 27-108-00 MOS 22-AUG-2008 25-JUL-2007 3260:48 AFL 782 SB 737-27A1277 R2 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN MOS 03-JUL-2013 08-JAN-2010 3723:21 AFL 908 SB 737-27A1277 R2 PAC 1 DETAIL INSPECTION HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL (I) NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN MOS 24 (s) 03-JUL-2013 08-JAN-2010 6400 3723:21 AFL 908 SB 737-27A1277 R2 PAC 1 LUBRICATE HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL (2) NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN MOS 12 (s) 03-JUL-2013 08-JAN-2010 1600 3723:21 AFL 908 SB 737-27A1277 R2 PAC 2 REPLACE HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN BALL NUT TUBE RETAINERS MOS 19-DEC-2002 25000 (s) RECOMMENDED COMPLIED WITH - INSPECTION AND LUBRICATION LA.W. AD 2011-27-03 RECOMMENDED COMPLIED WITH - IA.W. AD 2011-27-03 RECOMMENDED COMPLIED WITH - IA.W. AD 2011-27-03 RECOMMENDED - INFO REFERENCE TO AD 2011-27-03 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 54 Of 748 @ Camp Systems EFTA00618345 C O MP Atiant.fran Ad-own/lop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27A1277 R2 PAC 3 REPLACE HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - BALLSCREW AND BALL NUT INSPECTION . LUBRICATION. AND REPAIR/OVERHAUL. SERVICE BULLETIN HORIZONTAL STABILIZER TRIM ACTUATOR MOS 19-DEC-2002 SB 737-27A1279 RUDDER - RUDDER AND RUDDER TRIM CONTROL SYSTEM - MAIN RUDDER POWER CONTROL UNIT INPUT CONTROL RODS AND STANDBY RUDDER POWER CONTROL UNIT INPUT CONTROL ROD - REPLACEMENT. SERVICE BULLETIN MOS 28-OCT-2007 RECOMMENDED - INFORMATION REFERENCE REV.I PREVIOUSLY CW 22-AUG-2008 REPLACEMENT PER 737-27-1210411 PN 251A4510-6 TSO "0'. UPDATED COMPONENT TASK 27-108-00 WITH THE COMPLETION DATE OF THIS Se. FURTURE TRACKING OF THIS SIB WILL BE ACCOMPLISHED PER 27-108-00 NOT APPLICABLE - BY EFFECTIVITY N/A BY LINE NO. SB 737-27A1279 RI MAIN RUDDER POWER CONTROL UNIT INPUT CONTROL RODS AND STANDBY RUDDER POWER CONTROL UNIT INPUT RECOMMENDED NOT APPLICABLE - BY EFFECTIVITY CONTROL ROD - REPLACEMENT. SERVICE BULLETIN YG091-YG096 EFFECTED AIRCRAFT I I -JAN-2010 SB 737-27A1280 25-MAY-2006 S8 737-27A1280 RI 24-MAY-2007 SB 737-27A1280 RI TABLE 1 24-MAY-2007 SB 737-27A1280 RI TABLE 2 16-FEB-2007 MOS RUDDER AND RUDDER TRIM CONTROL SYSTEM - OPERATIONAL TEST OF THE STANDBY HYDRAULIC ACTUATION SYSTEM AND RUDDER MAIN POWER CONTROL UNIT FORCE FIGHT MONITOR TEST - TEST FREQUENCY CHANGE. SERVICE BULLETIN MOS 08-DEC-2006 2785:43 AFL 661 RUDDER AND RUDDER TRIM CONTROL SYSTEM - OPERATIONAL TEST Of THE STANDBY HYDRAULIC ACTUATION SYSTEM AND RUDDER MAIN POWER CONTROL UNIT FORCE FIGHT MONITOR TEST - TEST FREQUENCY CHANGE. SERVICE BULLETIN MOS 22-AUG-2008 3260:48 AFL 782 MONITOR TEST RUDDER AND RUDDER TRIM CONTROL SYSTEM - OPERATIONAL TEST OF THE STANDBY HYDRAULIC ACTUATION SYSTEM AND RUDDER MAIN POWER CONTROL UNIT FORCE FIGHT MONITOR TEST - TEST FREQUENCY CHANGE. SERVICE BULLETIN RUDDER MAIN POWER CONTROL UNIT (PCU) FORCE FLIGHT DAYS 90 (s) OPERATIONAL TEST RUDDER AND RUDDER TRIM CONTROL SYSTEM - OPERATIONAL TEST OF THE STANDBY HYDRAULIC ACTUATION SYSTEM AND RUDDER MAIN POWER CONTROL UNIT FORCE FIGHT MONITOR TEST - TEST FREQUENCY CHANGE. SERVICE BULLETIN OF THE STANDBY HYDRAULIC ACTUATION SYSTEM DAYS 60 (s) NOT APPLICABLE - NO PCU CONTROL RODS PREVIOUSLY CHANGED. COMPUED WITH - IAW THE SB 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 55 Of 748 @ Camp Systems EFTA00618346 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27A1280 TABLE 1 25-MAY-2006 SB 737-27A1280 TABLE 2 25-MAY-2006 MONITOR TEST RUDDER AND RUDDER TRIM CONTROL SYSTEM - OPERATIONAL TEST OF THE STANDBY HYDRAULIC ACTUATION SYSTEM AND RUDDER MAIN POWER CONTROL UNIT FORCE FIGHT MONITOR TEST - TEST FREQUENCY CHANGE. SERVICE BULLETIN RUDDER MAIN POWER CONTROL UNIT (PCU) FORCE FLIGHT DAYS 08-DEC-2006 6000 (s) 2785:43 AFL 661 OPERATIONAL TEST RUDDER AND RUDDER TRIM CONTROL SYSTEM - OPERATIONAL TEST OF THE STANDBY HYDRAULIC ACTUATION SYSTEM AND RUDDER MAIN POWER CONTROL UNIT FORCE FIGHT MONITOR TEST - TEST FREQUENCY CHANGE. SERVICE BULLETIN OF THE STANDBY HYDRAULIC ACTUATION SYSTEM DAYS 08-DEC-2006 500(s) 2785:43 AFL 661 NOT APPLICABLE - NO PCU CONTROL RODS PREVIOUSLY CHANGED. NOT APPLICABLE - NO PCU CONTROL RODS PREVIOUSLY CHANGED. SB SB 737-27A1283 03-APR-2007 737-27A1287 FLIGHT CONTROLS - SPOILER. DRAG DEVICES. AND VARIABLE AERODYNAMIC FAIRINGS - LEFT AND RIGHT WING FLIGHT SPOILERS SHORT FIELD PERFORMANCE ACTUATOR REPLACEMENT. SERVICE BULLETIN MOS 18-OCT-2007 RUDDER FEEL AND CENTERING UNIT - INSPECTION AND REPLACEMENT OF SPRING ASSEMBLY. SERVICE BULLETIN NOT APPLICABLE - BY EFFECTIVITY APPLICABLE TO 737-800 SERIES AIRCRFAT ONLY. - N/A BY LINE NO. MOS 03-NOV-2009 16-APR-2008 3391 AFL 817 SB 737-27A1296 ELAVATOR TAB CONTROL MECHANISM DETAILED INSPECTION (SUPERSEDED BY SB 737-27A1297 R1). SERVICE SUPERSEDED COMPUED WITH - IAW THE AD BULLETIN MOS I9-MAY-2010 3438:54 AFL 835 SB 737-27A1296 R1 FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION (SUPERSEDED BY SB SUPERSEDED 737-27A1297 R1), SERVICE BULLETIN MOS SB 737-27A1297 FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION (SUPERSEDED BY SB SUPERSEDED 737-27A1297 R1), SERVICE BULLETIN MOS SB 737-27A1297 RI FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION (SUPERSEDED BY SB SUPERSEDED 737-27A1297 R2). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 56 Of 748 @ Camp Systems EFTA00618347 COMP Astant.fran 'Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27A1297 RI TABLE 1.03 02-AUG-2010 DETAILED INSPECTION FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION RECOMMENDED COMPLIED WITH (SUPERSEDED BY S8 737-27AI297 R2). SERVICE BULLETIN OF THE LEFT SIDE ELEVATOR TAB CONTROL MECHANISM (GROUP 3) DAYS 180(s) 1800 28-FEB-2011 3525:36 AFL 857 SB 737-27A1297 RI REPLACE FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION (SUPERSEDED BY SB RECOMMENDED TABLE 1.04 737-27A1297 R2). SERVICE BULLETIN THE LEFT SIDE ELEVATOR TAB CONTROL MECHANISM AND DO DETAILED INSPECTION BEFORE AND AFTER INSTALLING IT ( IF ELEVATOR TAB CONTROL MECHANISM IS FOUND TO BE DISCREPANT OR REPLACEMENT ELEVATOR TAB CONTROL MECHANISM IS FOUND TO BE DISCREPANT) MOS BF(F SB 737-27A1297 RI DETAILED INSPECTION FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION RECOMMENDED COMPLIED WITH TABLE 2.03 (SUPERSEDED BY 58 737-27A1297 R2). SERVICE BULLETIN OF THE RIGHT SIDE ELEVATOR TAB CONTROL MECHANISM (GROUP 3) DAYS 180 (5) 28-FEB-2011 02-AUG-2010 1800 3525:36 AFL 857 SB 737-27A1297 RI REPLACE FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION (SUPERSEDED 8Y SB RECOMMENDED TABLE 2.04 737-27A1297 R2). SERVICE BULLETIN THE RIGHT SIDE ELEVATOR TAB CONTROL MECHANISM AND DO DETAILED INSPECTION BEFORE AND AFTER INSTALLING IT ( IF ELEVATOR TAB CONTROL MECHANISM IS FOUND TO BE DISCREPANT OR REPLACEMENT ELEVATOR TAB CONTROL MECHANISM IS FOUND TO BE DISCREPANT) MOS BF(F SB 737-27A1297 R2 FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION. SERVICE BULLETIN RECOMMENDED MOS 16-APR-2012 SB 737-27A1297 R2 DETAILED INSPECTION FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION. RECOMMENDED TABLE (1) SERVICE BULLETIN OF THE LEFT SIDE ELEVATOR TAB CONTROL MECHANISM MOS RECURRING 1800 (EFF) 5325:36 M SB 737-27A1297 R2 DETAILED INSPECTION FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION. RECOMMENDED TABLE (2) SERVICE BULLETIN OF THE RIGHT SIDE ELEVATOR TAB CONTROL MECHANISM MOS RECURRING 1800 (EFF) 5325:36 M SB 737-27A1299 FLIGHT CONTROLS- ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION AND BEARING RETAINER SUPERSEDED INSTALLATION (SUPERSEDED BY SI3 737-27A1299 R1). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 57 Of 748 @ Camp Systems EFTA00618348 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-27A1299 RI 16-APR-20I2 SB 737-27A1299 RI TABLE 1 SB 737-27A1299 RI TABLE 2 INSP FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION AND BEARING RETAINER INSTALLATION. SERVICE BULLETIN MOS (EFF) RECOMMENDED DETAILED INSPECTION FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION AND RECOMMENDED BEARING RETAINER INSTALLATION. SERVICE BULLETIN THE ELEVATOR TAB CONTROL MECHANISM ALL AIRPLANES AND REPORT ALL INITIAL INSPECTION RESULTS AND DATE OF BEARING RETAINER INSTALLATION TO BOEING DAYS 30 (s) DETAILED INSPECTION FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION AND RECOMMENDED BEARING RETAINER INSTALLATION. SERVICE BULLETIN OF THE BEARING RETAINERS AND THE ELEVATOR TAB CONTROL MECHANISM WITH BEARING RETAINERS INSTALLED. MOS 890 (s) AFL 40O SB 737-27A1299 RI REPORT FLIGHT CONTROLS - ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION AND BEARING RECOMMENDED TABLE 2 REPORT RETAINER INSTALLATION. SERVICE BULLETIN ALL DISCREPANT MECHANISM FINDINGS FROM REPEAT INSPECTIONS TO BOEING INCLUDING WHICH REPEAT THE FAILED INSPECTION OCCURRED FOR ALL AIRPLANES: AFTER THE DETAILED INSPECTION DAYS 30 (s) SB 737-28-1152 P5-2 FUEL CONTROL MODULE REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 03-MAY-2001 - (s) SB 737-28-1155 CENTER FUEL TANK SCAVENGE SYSTEM, SERVICE BULLETIN MOS 19-OCT-2000 SB 737-28-1160 SPARE VALVE DUAL WIRE VERIFICATION TEST. SERVICE BULLETIN RECOMMENDED MOS 05-JUN-2000 - (s) SB 737-28-1160 RI ENGINE FUEL FEED SYSTEM, SERVICE BULLETIN RECOMMENDED MOS 6(s) 31-AUG-2001 26-OCT-2000 793:18 SB 737-28-1172 AFL 212 INTEGRAL FUEL TANKS - ALIGNMENT OF CENTER TANK BOOST PUMP INLETS AND FUEL PUMP ALIGNMENT BRACKETRY. SERVICE BULLETIN MOS 18-APR-2002 - (s) RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 58 Of 748 @ Camp Systems EFTA00618349 C O MP Atiant.fran Ad-own/lop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-28-1172 RI FUEL - STORAGE - INTEGRAL FUEL TANKS - ALIGNMENT OF CENTER TANK BOOST PUMP INLETS AND FUEL PUMP ALIGNMENT BRACKETRY. SERVICE BULLETIN MOS 04-JUN-2007 SB 737-28-1173 APU FUEL FEED LINE SHROUD. INSPECTION FOR ADEQUATE CLEARANCE AND REPAIR. SERVICE BULLETIN MOS 17-JAN-2002 - SB 737-28-1173 RI APU FUEL FEED LINE SHROUD. INSPECTION FOR ADEQUATE CLEARANCE AND REPAIR. SERVICE BULLETIN MOS 04-NOV-2004 SB 737-28-1173 R2 FUEL SYSTEM - DISTRIBUTION - APU FUEL FEED LINE SHROUD. INSPECTION FOR ADEQUATE CLEARANCE AND REPAIR. SERVICE BULLETIN MOS 23-FEB-2006 RECOMMENDED SB 737-28-1179 P5-2 FUEL SYSTEM MODULE REMOVAL AND REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 27-AUG-2002 31-JAN-2002 1057:50 SB 737-28-1179 RI 28-FEB-2002 SB 737-28-1179 R2 02-DEC-2004 SB 737-28-1190 16-JAN-2003 AFL 271 P5-2 FUEL SYSTEM MODULE REMOVAL AND REPLACEMENT. SERVICE BULLETIN MOS - (s) P5-2 FUEL SYSTEM MODULE REMOVAL AND REPLACEMENT. SERVICE BULLETIN MOS RECOMMENDED FUEL-FUEL QUANTITY INDICATING SYSTEM (FQIS)-CENTER FUEL TANK WIRE SUPPORT BRACKET REPLACEMENT. RECOMMENDED SERVICE BULLETIN MOS 18(s) SB 737-28-1190 RI FUEL-FUEL QUANTITY INDICATING SYSTEM (FQIS)-CENTER FUEL TANK WIRE SUPPORT BRACKET REPLACEMENT. COMPLIED WITH SERVICE BULLETIN MOS 18-AUG-2006 27-MAR-2003 - (s) 2633:50 AFL 633 SB 737-28-1194 RELOCATION OF CONNECTOR PINS. SERVICE BULLETIN RECOMMENDED MOS 20-FEB-2003 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 59 Of 748 @ Camp Systems EFTA00618350 COMP Jm. tMrrnM•O AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: O5-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-28-1194 RI 37 -JUL-2003 RELOCATION OF CONNECTOR PINS AT WING(BODY CONNECTORS. SERVICE BULLETIN MOS SB 737-28-1194 R2 RELOCATION OF CONNECTOR PINS AT VYING/BODY CONNECTORS. SERVICE BULLETIN MOS 08-JAN-2004 SB 737-28-1194 R3 FUEL - FUEL BOOST PUMP - RELOCATION OF CONNECTOR PINS AT VYING/BODY CONNECTORS. SERVICE BULLETIN MOS I8-SEP-2007 RECOMMENDED RECOMMENDED SB 737-28-1199 ENGINE FUEL SHUTOFF VALVE WIRE AND CONDUIT ASSEMBLY REPLACEMENT. SERVICE BULLETIN COMPUED WITH 09-SEP-2004 MOS I8-AUG-2006 - (s) 2633:50 AFL 633 SB 737-28-1199 RI FUEL - ENGINE FUEL FEED SYSTEM - ENGINE FUEL SHOUTOFF VALVE WIRE AND CONDUIT ASSEMBLY COMPUED WITH REPLACEMENT. SERVICE BULLETIN MOS 18-AUG-2086 15-DEC-2005 - (s) 2633:50 AFL 633 SB 737-28-1199 R2 FUEL - ENGINE FUEL FEED SYSTEM - ENGINE FUEL SHUTOFF VALVE WIRE AND CONDUIT ASSEMBLY REPLACEMENT. SERVICE BULLETIN MOS 36 (s) I 7-JUL-2006 SB 737-28-1200 INSPECTION FOR WIRE CHAFING BEHIND P15 REFUEL PANEL. SERVICE BULLETIN COMPUED WITH - NO CHAFING FOUND MOS 24(s) 0I -JUN-2007 I0JUL-2003 2955:24 AFL 691 SB 737-28-1200 RI FUEL - PRESSURE FUELING SYSTEM - INSPECTION FOR WIRE CHAFING BEHIND P15 REFUEL PANEL. SERVICE COMPUED WITH - NO CHAFING FOUND BULLETIN MOS 01-JUN-2007 28-JUL-2005 - (s) 2955:24 AFL 691 SB 737-28-1209 FUEL - INDICATING - WING CENTER TANK WIRE BUNDLES INSTALLATION CHANGE (SUPERSEDED BY SB 737-28-1209 SUPERSEDED COMPLIED WITH R1). SERVICE BULLETIN MOS I8-AUG-2006 -(s) 2633:50 AFL 633 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 60 Of 7,18 @ Camp Systems EFTA00618351 COMP Moan Aim thernand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-28-1209 RI FUEL - INDICATING - WING CENTER TANK WIRE BUNDLES INSTALLATION CHANGE. SERVICE BULLETIN MOS 60 (s) 21-DEC-2005 58 [SSN REDACTED] FUEL - DISTRIBUTION - ENGINE FUEL FEED SYSTEM - INSPECTION/REPA1R OF THE ELECTRICAL BOND BETWEEN THE BULKHEAD FITTING AND THE WING FRONT SPAR. SERVICE BULLETIN MOS 22-AUG-2008 I2-JAN-2006 - (s) 3260:48 AFL 782 SB 737-28-1225 RI FUEL - DISTRIBUTION - ENGINE FUEL FEED SYSTEM -INSPECTION/REPAIR OF THE ELECTRICAL BOND BETWEEN THE BULKHEAD FITTING AND THE WING FRONT SPAR. SERVICE BULLETIN 30-OCT-2006 MOS 22-AUG-2008 -(s) 3260:48 AFL 782 SB 737-28-1251 FUEL - BOOST PUMP CONTROL RELAY - GROUND MODULE INSPECTION AND REPLACEMENT IF NECESSARY. SERVICE BULLETIN DAYS 90 (s) 20-OCT-2005 SB 737-28-1251 RI FUEL - ENGINE FUEL FEED SYSTEM - GROUND MODULE INSPECTION AND REPLACEMENT. SERVICE BULLETIN DAYS 90 (s) 27-APR-2006 RECOMMENDED NOT APPLICABLE - REF: TO R1 COMPUED WITH - IAW THE SB - INFORMATION REF COMPLIANCE OF 737-28-1257 - INFORMATION REF COMPLIANCE OF 737-28-1257 SB 737-28-1251 R2 FUEL - ENGINE FUEL FEED SYSTEM - GROUND MODULE INSPECTION AND REPLACEMENT. SERVICE BULLETIN - INFORMATION REF COMPLIANCE OF 737-28-1257 DAYS 90 (s) 26-OCT-2006 SB 737-28-1257 FUEL - ENGINE FUEL FEED SYSTEM - BOOST PUMP CONTROL RELAY GROUND LOCATION CHANGE. SERVICE COMPLIED WITH BULLETIN MOS I4-FEB-2008 26-FEB-2007 -(s) 3151:22 AFL 746 58 [SSN REDACTED] RI FUEL - ENGINE FUEL FEED SYSTEM - BOOST PUMP CONTROL RELAY GROUND LOCATION CHANGE. SERVICE COMPUED WITH BULLETIN MOS 14-FEB-2008 28-NOV-2007 - (s) 3151:22 AFL 746 SB 737-28-1272 ENGINE FUEL FEED SYSTEM - MAIN TANKS ENGINE FUEL SPAR VALVE BODY REPLACEMENT (SUPERSEDED BY SB SUPERSEDED 737-28-1272 RI), SERVICE BULLETIN MOS 29-AUG-2011 3533:32 AFL 863 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time @ Camp Systems 61 Of 748 EFTA00618352 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-28-1272 RI FUEL - ENGINE FUEL FEED SYSTEM - MAIN TANKS ENGINE FUEL SPAR VALVE BODY REPLACEMENT. SERVICE BULLETIN MOS 60 (s) RECOMMENDED 18-FEB-2010 SB 737-28-1283 FUEL QUANTITY INDICATING SYSTEM - FUEL QUANTITY PROCESSOR UNIT REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 11-FEB-2009 SB 737-28-1303 FUEL - GENERAL - LEFT ENVIRONMENTAL CONTROL SYSTEMS BAY WIRE CLAMP - INSPECTION AND REPLACEMENT. RECOMMENDED SERVICE BULLETIN 26-APR-2012 MOS 60 (s) SB 737-28-1312 FUEL - GENERAL - LEFT AND RIGHT ENVIRONMENTAL CONTROL SYSTEMS BAY WIRE CLAMP - INSPECTION AND SUPERSEDED REPLACEMENT (SUPERSEDED BY SB 737-28-1312 R1). SERVICE BULLETIN MOS (EFF) SB 737-28-1312 RI FUEL - GENERAL - LEFT AND RIGHT ENVIRONMENTAL CONTROL SYSTEMS BAY WIRE CLAMP - INSPECTION AND RECOMMENDED REPLACEMENT. SERVICE BULLETIN MOS 19-APR-2013 58 [SSN REDACTED] FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. RECOMMENDED SERVICE BULLETIN MOS 03-APR-2014 SB 737-28-1318 TABLE 1.1 DO FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN A MAINTENANCE RECORDS CHECK TO SEE IF ANY OF THE FOUR FUEL VALVE ADAPTER SHAFT ASSEMBLIES HAVE A SERIAL NUMBER THAT IS SPECIFIED IN APPENDIX A (ALL AIRPLANES) MOS SB 737-28-1318 TABLE 12 FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. RECOMMENDED SERVICE BULLETIN NO MORE WORK IS NECESSARY IF CONDITION 1: ALL FUEL VALVE ADAPTER SHAFT ASSEMBLIES THAT DO NOT HAVE A SERIAL NUMBER THAT IS SPECIFIED IN APPENDIX A. MOS 03-APR-2014 58 [SSN REDACTED] TABLE 1.3.1 DO FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN PART 1: FUEL VALVE ADAPTER SHAFT ASSEMBLY - OPEN ACCESS (IF CONDITION 2: EACH FUEL VALVE ADAPTER SHAFT ASSEMBLY THAT HAS A SERIAL NUMBER THAT IS SPECIFIED IN APPENDIX A) MOS - Is) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 62 Of 748 @ Camp Systems EFTA00618353 C O MP Atiant.fran Meowed lip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-28-1318 TABLE 1.3.2 SB 737-28-1318 TABLE 1.3.3 SB 737-28-1318 TABLE 1.4.1 SB 737-28-1318 TABLE 1.4.2 DO FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN PART 3: FUEL VALVE ADAPTER SHAFT ASSEMBLY - REPLACEMENT (IF CONDITION 2: EACH FUEL VALVE ADAPTER SHAFT ASSEMBLY THAT HAS A SERIAL NUMBER THAT IS SPECIFIED IN APPENDIX A) MOS - (s) DO FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN PART 4: FUEL VALVE ADAPTER SHAFT ASSEMBLY - CLOSE ACCESS (IF CONDITION 2: EACH FUEL VALVE ADAPTER SHAFT ASSEMBLY THAT HAS A SERIAL NUMBER THAT IS SPECIFIED IN APPENDIX A) MOS - (s) DO FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN PART 1: FUEL VALVE ADAPTER SHAFT ASSEMBLY - OPEN ACCESS (IF CONDITION 3: EACH FUEL VALVE ADAPTER SHAFT ASSEMBLY WHERE THE SERIAL NUMBER CANNOT BE IDENTIFIED IN THE MAINTENANCE RECORDS) MOS - (s) DO FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN PART 2: FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION - TO SEE IF THE SERIAL NUMBER IS SPECIFIED IN APPENDIX A (IF CONDITION 3: EACH FUEL VALVE ADAPTER SHAFT ASSEMBLY WHERE THE SERIAL NUMBER CANNOT BE IDENTIFIED IN THE MAINTENANCE RECORDS) MOS - (s) SB 737-28-1318 TABLE 1.5 DO FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN PART 4: FUEL VALVE ADAPTER SHAFT ASSEMBLY - CLOSE ACCESS (IF CONDITION 4: EACH FUEL VALVE ADAPTER SHAFT ASSEMBLY THAT DOES NOT HAVE A SERIAL NUMBER THAT IS SPECIFIED IN APPENDIX A) 03-APR-2014 SB 737-28-1318 TABLE 1.6.1 SB 737-28-1318 TABLE 1.6.2 MOS DO FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN PART 3: FUEL VALVE ADAPTER SHAFT ASSEMBLY - REPLACEMENT (IF CONDITION 5: EACH FUEL VALVE ADAPTER SHAFT ASSEMBLY THAT HAS A SERIAL NUMBER THAT IS SPECIFIED IN APPENDIX A. OR THAT CANNOT BE DETERMINED) MOS - (s) DO FUEL - ENGINE FUEL FEED SYSTEM - FUEL VALVE ADAPTER SHAFT ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN PART 4: FUEL VALVE ADAPTER SHAFT ASSEMBLY - CLOSE ACCESS (IF CONDITION 5: EACH FUEL VALVE ADAPTER SHAFT ASSEMBLY THAT HAS A SERIAL NUMBER THAT IS SPECIFIED IN APPENDIX A OR THAT CANNOT BE DETERMINED) MOS - (s) RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 63 Of 748 @ Camp Systems EFTA00618354 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 SB 737-28-1323 10-JUL-2014 737-28M142 07-FEB-2002 FUEL - DISTRIBUTION - LEFT WING TANK WATER SCAVENGE SYSTEM - PERFORMANCE IMPROVEMENT EVALUATION. SERVICE BULLETIN MOS IMPROVED FUEUNG FLOAT SWITCH AND WIRING PROVISION INSTALLATION, SERVICE BULLETIN MOS 24 (s) RECOMMENDED RECOMMENDED SB 737-28A1142 RI IMPROVED FUEUNG FLOAT SWITCH AND WIRING PROVISION INSTALLATION, SERVICE BULLETIN MOS 24 (s) 1 7-JUN-2002 SB 737-28A1142 R2 IMPROVED FUEUNG FLOAT SWITCH AND WIRING PROVISION INSTALLATION. SERVICE BULLETIN MOS 24 (s) 21-AUG-2002 07-FEB-2002 1057:48 AFL 271 SB 737-28A1142 R3 IMPROVED FUEUNG FLOAT SWITCH AND WIRING PROVISION INSTALLATION, SERVICE BULLETIN MOS 24 (s) 21-AUG-2002 21-AUG-2003 1057:48 AFL 271 SB 737-28A1142 R4 IMPROVED FUEUNG FLOAT SWITCH AND WIRING PROVISION INSTALLATION, SERVICE BULLETIN MOS 24 (s) 21-AUG-2002 15-JUL-200d 1057:48 AFL 271 SB 737-28A1148 TANK FUEL BOOST PUMP. SERVICE BULLETIN COMPUED WITH - PREVIOUSLY REV 2 DOESN7 AFFECT A/C MOS 6 (s) 09-JAN-200d Id-SEP-2000 1547:30 AFL 391 SB 737-28A1148 RI AFT BOOST PUMP WIRING SUPPORT BRACKET INSTALLATION. SERVICE BULLETIN MOS 6 (s) 22-AUG-2002 SB 737-28A1148 R2 AFT BOOST PUMP WIRING SUPPORT BRACKET INSTALLATION (SUPERSEDED BY SB 737-28A1148 R3). SERVICE SUPERSEDED COMPUED WITH - PREVIOUSLY DONE WITH SB BULLETIN 737-28A1148 IN AUG 14.8.01 MOS 16-DEC-2004 - Is) 1951:36 AFL 476 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 64 Of 748 @ Camp Systems EFTA00618355 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-28A1148 R3 13-JUL-2004 ENGINE FUEL FEED SYSTEM - TANK FUEL BOOST PUMP - AFT BOOST PUMP WIRING SUPPORT BRACKET INSTALLATION. SERVICE BULLETIN MOS 6 (s) RECOMMENDED SB 737-28A1184 FUEL BOOST AND OVERRIDE PUMP MOTOR-IMPELLAR REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 14-SEP-2000 SB 737-28A1188 AFT FUEL BOOST PUMP GROUND SHIELD WIRE CHANGE, SERVICE BULLETIN COMPLIED WITH MOS 18 (s) 13-AUG-2004 06-MAR-2003 1785:06 AFL 446 SB 737-28A1188 IN 01 FUEL BOOST PUMP-AFT FUEL BOOST PUMP GROUND SHIELD WIRE CHANGE. SERVICE BULLETIN MOS 12-JUN-2096 SB 737-28A1188 R1 AFT FUEL BOOST PUMP GROUND SHIELD WIRE CHANGE.. SERVICE BULLETIN COMPLIED WITH - PREVIOUSLY MOS 30-NOV-2005 18-MAR-2004 2338:24 AFL 573 SB 737-28A1197 FUEL PUMP MOTOR-IMPELLER INSPECTION (SUPERSEDED BY 737-28A1197 R1), SERVICE BULLETIN SUPERSEDED MOS 23-SEP-2002 - (s) SB 737-28A1197 RI FUEL PUMP MOTOR-IMPELLER INSPECTION (SUPERSEDED BY 737-28A1197 R2), SERVICE BULLETIN SUPERSEDED MOS 01-MAY-2003 SB 737-28A1197 R2 FUEL - DISTRIBUTION - FUEL PUMP MOTOR-IMPELLER INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS 25-AUG-2005 SB 737-28Al201 FUEL - ENGINE FUEL FEED SYSTEM - FUEL PUMP CONTROL GROUND FAULT INTERRUPTER (GFI) RELAY SUPERSEDED INSTALLATION (SUPERSEDED BY 737-28Al201 R1). SERVICE BULLETIN MOS SB 737-28Al201 RI FUEL - ENGINE FUEL FEED SYSTEM - FUEL PUMP CONTROL GROUND FAULT INTERRUPTER (GFI) RELAY RECOMMENDED COMPLIED WITH INSTALLATION. SERVICE BULLETIN MOS 29-AUG-201I 28-MAY-2009 3533:32 AFL 863 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 65 Of 748 @ Camp Systems EFTA00618356 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-28A1206 II -JAN-2006 FUEL - DISTRIBUTION - CENTER FUEL TANK BOOST PUMP AUTO SHUTOFF AND MASTER CAUTION LOGIC CHANGE. SERVICE BULLETIN MOS SB 737-28A1206 RI FUEL - DISTRIBUTION - CENTER FUEL TANK BOOST PUMP AUTO SHUTOFF AND MASTER CAUTION LOGIC CHANGE, SERVICE BULLETIN MOS I I -JAN-2006 SB 737-28A1206 R2 CENTER FUEL TANK BOOST PUMP AUTO SHUTOFF AND MASTER CAUTION LOGIC CHANGE (SUPERSEDED BY SB SUPERSEDED COMPLIED WITH 737-28A1206 R3), SERVICE BULLETIN MOS 29-AUG-2011 3533:32 AFL 863 SB 737-28A1206 R3 FUEL - DISTRIBUTION - CENTER FUEL TANK BOOST PUMP AUTO SHUTOFF AND MASTER CAUTION LOGIC CHANGE. RECOMMENDED SERVICE BULLETIN MOS 36 (EFF) 30-SEP-2014 30-SEP-2014 30-SEP-2011 SB 737-28A1207 FUEL - ENGINE FUEL FEED SYSTEM - MOTOR OPERATED VALVE - ACTUATOR REPLACEMENT (SUPERSEDED BY SUPERSEDED 737-28A1207 RI). SERVICE BULLETIN MOS I5-FEB-2007 SB 737-28A1207 RI FUEL - ENGINE FUEL FEED SYSTEM -MOTOR OPERATED VALVE - ACTUATOR REPLACEMENT. SERVICE BULLETIN RECOMMENDED COMPLIED WITH MOS 29-AUG-201 I I9-APR-2010 - (s) 3533:32 AFL 863 SB 737-28A1221 I4-JAN-2007 SB 737-28A1221 RI 09-NOV-2007 FUEL - INDICATING - HOT SHORT PROTECTOR INSTALLATION FOR MIS FUEL DENSITOMETER. SERVICE BULLETIN MOS 60 (s) FUEL - INDICATING - HOT SHORT PROTECTOR INSTALLATION FOR FOIS FUEL DENSITOMETER (SUPERSEDED BY SB 737-28A1221 R2), SERVICE BULLETIN MOS 29-AUG-201 I -(s) 3533:32 NOT APPLICABLE - N/A BY EFFECTIVITY AFL 863 SB 737-28A1221 R2 FUEL - INDICATING - HOT SHORT PROTECTOR INSTALLATION FOR FOIS FUEL DENSITOMETER. SERVICE BULLETIN RECOMMENDED NOT APPLICABLE - N/A BY EFFECTIVITY MOS 29-AUG-2011 I4-JAN-2007 - (s) 3533:32 AFL 863 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 66 Of 7,18 @ Camp Systems EFTA00618357 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-28A1248 FUEL - ENGINE FUEL FEED SYSTEM - CENTER FUEL TANK. FUEL PUMPS - POWER FAILED ON PROTECTION SYSTEM (UN-COMMANDED PUMP ON)- RELAYS INSTALLATION (SUPERSEDED BY 737-28A1248 R1). SERVICE BULLETIN MOS SUPERSEDED SB 737-28A1248 RI FUEL - ENGINE FUEL FEED SYSTEM - CENTER FUEL TANK. FUEL PUMPS - POWER FAILED ON PROTECTION SYSTEM SUPERSEDED (UN-COMMANDED PUMP ON)- RELAYS INSTALLATION (SUPERSEDED BY 737-28A1248 R2). SERVICE BULLETIN MOS SB 737-28A1248 R2 ENGINE FUEL FEED SYSTEM - CENTER FUEL TANK. FUEL PUMPS - POWER FAILED ON PROTECTION SYSTEM SUPERSEDED COMPLIED WITH- WO BVBBJ006 (UN-COMMANDED PUMP ON)- RELAYS INSTALLATION (SUPERSEDED BY SB 737-28A1248 R3). SERVICE BULLETIN MOS 29-AUG-2011 3533:32 AFL 863 SB 737-28A1248 R3 FUEL - ENGINE FUEL FEED SYSTEM - CENTER FUEL TANK. FUEL PUMPS -POWER FAILED ON PROTECTION SYSTEM RECOMMENDED (UN-COMMANDED PUMP ON)- RELAYS INSTALLATION. SERVICE BULLETIN MOS 60 (s) 30-SEP-2011 SB 737-29-1077 . SERVICE BULLETIN COMPLIED WITH - CM MOS 23-SEP-1999 - (s) SB 737-29-1083 HYDRAULIC POWER - PARKING BRAKE SHUTOFF VALVE (NON-SENSITIVE LOCATIONS) REPLACEMENT. SERVICE RECOMMENDED BULLETIN MOS 25-JAN-2001 - (s) SB 737-29-1084 HYDRAULIC POWER TRANSFER UNIT SYSTEM. SERVICE BULLETIN RECOMMENDED MOS 01-JUN-2000 - (s) SB 737-29-1090 HYDRAULIC POWER - DC MOTOR OPERATED SHUTOFF VALVE (ALL LOCATIONS) REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 25-JAN-2001 - SB 737-29-1094 MODIFICATION OF THE RESERVOIR PRESSURIZATION MODULE. SERVICE BULLETIN RECOMMENDED MOS I5-MAR-2001 - (s) SB 737-29-1094 RI MODIFICATION OF THE HYDRAULIC RESERVOIR PRESSURIZATION MODULE. SERVICE BULLETIN RECOMMENDED MOS 29-MAR-2001 - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 67 Of 748 @ Camp Systems EFTA00618358 CAMAsiont.P inn• Ad-tilting:KY AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-29-1106 23-DEC-2002 HYDRAULIC POWER-HYDRAULIC RESERVOIR PRESSURIZATION SYSTEM-REMOVAL OF THE RESERVOIR PRESSURIZATION MODULE AND DEPRESSURIZATION VALVES. SERVICE BULLETIN MOS (s) SB 737-29-1106 RI HYDRAULIC POWER-HYDRAULIC RESERVOIR PRESSURIZATION SYSTEM-REMOVAL OF THE RESERVOIR PRESSURIZATION MODULE AND DEPRESSURIZATION VALVES. SERVICE BULLETIN MOS 15-MAY-2603 -(s) - REF:REV.4 - REF:REV.4 SB 737-29-1106 R2 05-FEB-2004 REMOVAL OF THE RESERVOIR PRESSURIZATION MODULE AND DEPRESSURIZATION VALVES. SERVICE BULLETIN MOS - REF: REV.4 SB 737-29-1106 R3 REMOVAL OF THE RESERVOIR PRESSURIZATION MODULE AND DEPRESSURIZATION VALVES. SERVICE BULLETIN RECOMMENDED - REF:REV.4 MOS 28-JUL-200.5 SB 737-29-1106 R4 REMOVAL OF THE RESERVOIR PRESSURIZATION MODULE AND DEPRESSURIZATION VALVES. SERVICE BULLETIN COMPLIED WITH MOS 24-AUG-2C07 23-JUN-2066 (s) 29618:28 AFL 699 SB 737-29-1106 RS HYDRAULIC POWER - HYDRAULIC RESERVOIR PRESSURIZATION SYSTEM - REMOVAL OF THE - INFORMATION REFER TO. REv.6 RESERVOIR PRESSURIZATION MODULE AND DEPRESSURIZATION VALVES. SERVICE BULLETIN MOS 16-JAN-2008 Is) SB 737-29-1106 R6 HYDRAULIC RESERVOIR PRESSURIZATION SYSTEM - REMOVAL OF THE RESERVOIR PRESSURIZATION MODULE AND SUPERSEDED COMPLIED WITH DEPRESSURIZATION VALVES (SUPERSEDED BY SB 737-29-1106 R7). SERVICE BULLETIN MOS 28-SEP-2009 - 3378.04 AFL 812 SB 737-29-1106 R7 HYDRAULIC POWER - HYDRAULIC RESERVOIR PRESSURIZATION SYSTEM - REMOVAL OF THE RESERVOIR SUPERSEDED PRESSURIZATION MODULE AND DEPRESSURIZATION VALVES (SUPERSEDED BY SB 737-29-1166 R8). SERVICE BULLETIN MOS SB 737-29-1106 R8 HYDRAULIC POWER - HYDRAULIC RESERVOIR PRESSURIZATION SYSTEM - REMOVAL OF THE RESERVOIR PRESSURIZATION MODULE AND DEPRESSURIZATION VALVES. SERVICE BULLETIN MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time 68 Of 748 LI Camp Systems EFTA00618359 COMP Astant.frn• thernand up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-29-1110 HYDRAULIC POWER - HYDRAULIC RESERVOIR - OVERFILL WARNING MARKER INSTALLATION. SERVICE BULLETIN 28-NOV-2007 SB 737-29-1110 RI 30-OCT-2008 SB 737-29-1111 30-JUL-2009 SB 737-29-1113 MOS - (s) 22-AUG-2008 3260:48 AFL 782 HYDRAULIC RESERVOIR - OVERFILL WARNING MARKER INSTALLATION. SERVICE BULLETIN MOS 60 (s) HYDRAULIC SYSTEMS A AND B ENGINE DRIVEN PUMP - SUPPORT BRACKET CHANGE FOR THE HYDRAULIC PRESSURE HOSE. SERVICE BULLETIN MOS HYDRAULIC POWER - RIGHT MAIN LANDING GEAR WHEEL WELL - WIRE BUNDLE AND HYDRAULIC TUBING - INSPECTION. REPAIR AND NEW CLAMPS INSTALLATION (SUPERSEDED BY SB 737-29-1113 R1). SERVICE BULLETIN RECOMMENDED RECOMMENDED COMPLIED WITH SB 23-MAR-2011 [SSN REDACTED] RI MOS 24 (s) HYDRAULIC POWER - RIGHT MAIN LANDING GEAR WHEEL WELL - WIRE BUNDLE AND HYDRAULIC TUBING - INSPECTION. REPAIR AND NEW CLAMPS INSTALLATION. SERVICE BULLETIN MOS SB 737-29-1114 HYDRAULIC POWER - MAIN - HYDRAULIC SYSTEMS A AND B PRESSURE MODULE CHECK VALVE INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS - (s) SB 737-29-1114 RI HYDRAULIC POWER - MAIN - HYDRAULIC SYSTEMS A AND B PRESSURE MODULE CHECK VALVE INSPECTION AND RECOMMENDED REPLACEMENT. SERVICE BULLETIN MOS 24 (s) (EFF) 10-SEP-2012 SB 737-29A1073 HYD POWER - DC MOTOR OPERATED 5/0 INSP.. SERVICE BULLETIN RECOMMENDED MOS 01-MAY-1997 -(s) SB 737-29A1073 R2 DC MOTOR OPERATED SHUTOFF VALVE. SERVICE BULLETIN RECOMMENDED MOS 6 (s) 08-OCT-1999 OI -JUL-1999 SB 737-29A1073 R3 HYDRAULIC POWER - DC MOTOR OPERATED SHUTOFF VALVE INSPECTION. SERVICE BULLETIN MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 69 Of 748 @ Camp Systems EFTA00618360 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-29A1077 SB 737-29A1077 RI SB 737-29A1077 R2 HYDRAULIC SYSTEM B ELECTRIC MOTOR-DRIVEN PUMP CASE DRAIN HOSE AND WIRE BUNDLE CLAMP INSTALLATION (SUPERSEDED BY SB 737-29A1077 R1). SERVICE BULLETIN MOS - (s) SUPERSEDED MAIN - HYDRAULIC SYSTEM B ELECTRIC MOTOR-DRIVEN PUMP (SUPERSEDED BY SB 737-29A1077 R2). SERVICE SUPERSEDED COMPLIED WITH BULLETIN MOS 09-SEP-1999 - (s) HYDRAULIC POWER -MAIN - HYDRAUUC SYSTEM B ELECTRIC MOTOR-DRIVEN PUMP CASE DRAIN HOSE. PRESSURE SUPERSEDED HOSE AND WIRE BUNDLE INSPECTION AND CLAMP INSTALLATION (SUPERSEDED BY SB 737-29A1077 R3). SERVICE BULLETIN MOS SB 737-29A1077 R3 HYDRAULIC POWER - MAIN - HYDRAUUC SYSTEM 8 ELECTRIC MOTOR-DRIVEN PUMP CASE DRAIN HOSE. PRESSURE RECOMMENDED HOSE AND WIRE BUNDLE INSPECTION AND CLAMP INSTALLATION. SERVICE BULLETIN MOS 07-APR-2010 SB 737-29A1078 DC MOTOR OPERATED SHUTOFF VALVE (SENSITIVE LOCATIONS) REPLACEMENT. SERVICE BULLETIN MOS - (s) SB 737-29A1081 DC MOTOR OPERATED SHUTOFF VALVE. SERVICE BULLETIN MOS 6 (s) 02-DEC-1999 SB 737-29A1081 RI 01-NOV-2001 822:06 AFL 220 HYDRAULIC POWER - DC MOTOR OPERATED SHUTOFF VALVE INSPECTION. SERVICE BULLETIN MOS 6(s) 01-NOV-2001 11-OCT-2001 822:06 AFL 220 SB 737-29A1082 HYDRAULIC POWER - DC MOTOR OPERATED SHUTOFF VALVE (SENSITIVE LOCATIONS) REPLACEMENT. SERVICE BULLETIN MOS 01-NOV-2001 07-DEC-2000 - (s) 822:06 AFL 220 SB 737-30-1050 WINDSHIELD WIPER MOTOR REPLACEMENT. SERVICE BULLETIN MOS 18-AUG-2006 09-MAY-2002 - (s) 2633:50 AFL 633 RECOMMENDED COMPLIED WITH RECOMMENDED COMPLIED WITH RECOMMENDED COMPLIED WITH RECOMMENDED COMPLIED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 70 Of 748 @ Camp Systems EFTA00618361 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-30-1054 RI C6-MAR-2003 SB 737-30-1056 28-FEB-2007 WINDSHIELD WIPER MOTOR REPLACEMENT. SERVICE BULLETIN MOS 18-AUG-2006 2633:50 AFL 633 ICE AND RAIN PROTECTION - WATER AND DRAIN LINE HEATERS - CHANGE - GRAY WATER COMPOSITE DRAIN MAST BONDING JUMPER INSTALLATION. SERVICE BULLETIN MOS CO (5) SB 737-30-1056 RI ICE AND RAIN PROTECTION - WATER AND DRAIN LINE HEATERS - CHANGE - GRAY WATER COMPOSITE DRAIN MAST BONDING JUMPER INSTALLATION. SERVICE BULLETIN 25-OCT-2007 MOS 22-AUG-2C08 (s) 3260:48 RECOMMENDED COMPLIED WITH AFL 782 SB 737-30-1056 R2 ICE AND RAIN PROTECTION - WATER AND DRAIN LINE HEATERS - CHANGE - GRAY WATER COMPOSITE DRAIN MAST RECOMMENDED BONDING JUMPER INSTALLATION. SERVICE BULLETIN MOS CO (s) 27-MAY-2008 SB 737-30-1056 R3 WATER AND DRAIN LINE HEATERS - CHANGE - GRAY WATER COMPOSITE DRAIN MAST BONDING JUMPER INSTALLATION. SERVICE BULLETIN MOS CO (5) 27-MAY-2008 SB 737-30-1058 ICE AND RAIN PROTECTION - CONTROL CABIN WINDOW ANTI-ICING SYSTEM - COIL CORD ASSEMBLY REPLACEMENT ON THE NUMBER 2 WINDOWS IN THE FLIGHT COMPARTMENT. SERVICE BULLETIN MOS 27-JUL-2000 SB 737-30-1058 RI ICE AND RAIN PROTECTION - CONTROL CABIN WINDOW ANTI-ICING SYSTEM - COIL CORD ASSEMBLY REPLACEMENT ON THE NUMBER 2 WINDOWS IN THE FLIGHT COMPARTMENT. SERVICE BULLETIN MOS 18-JUN-2007 SB 737-30-1058 R2 13-FEB-2009 CONTROL CABIN WINDOW ANTI-ICING SYSTEM - COIL CORD ASSEMBLY REPLACEMENT ON THE NUMBER 2 WINDOWS IN THE FLIGHT COMPARTMENT 9SUPERSEDED BY 737-30-1058 R3). SERVICE BULLETIN MOS RECOMMENDED SUPERSEDED SB 737-30-1058 R3 ICE AND RAIN PROTECTION - CONTROL CABIN' INDOW ANTI-ICING SYSTEM - COIL CORD ASSEMBLY REPLACEMENT SUPERSEDED ON THE NUMBER 2 WINDOWS IN THE FLIGHT COMPARTMENT (SUPERSEDED BY SB 737-30-1058 R4). SERVICE BULLETIN MOS COMPLIED WITH ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time 71 Of 748 Camp Systems EFTA00618362 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-30-1058 R4 ICE AND RAIN PROTECTION - CONTROL CABIN WINDOW ANTI-ICING SYSTEM - COIL CORD ASSEMBLY REPLACEMENT ON THE NUMBER 2 WINDOWS IN THE FLIGHT COMPARTMENT (SUPERSEDED BY SB 737-30-1058 R5). SERVICE BULLETIN MOS SUPERSEDED - Is) SB 737-30-1058 RS ICE AND RAIN PROTECTION- CONTROL CABIN WINDOW ANTI-ICING SYSTEM - COIL CORD ASSEMBLY REPLACEMENT RECOMMENDED ON THE NUMBER 2 WINDOWS IN THE FLIGHT COMPARTMENT. SERVICE BULLETIN MOS 24-APR-20I3 - Is) SB 737-30-1070 ICE AND RAIN PROTECTION - PITOT AND STATIC - POLARITY STANDARDIZATION TO ADDRESS UN-ANNUNCIATED SUPERSEDED FAILURE OF PITOT PROBE HEATERS (SUPERSEDED BY SB 737-30-1070 R1). SERVICE BULLETIN MOS 58 [SSN REDACTED] RI ICE AND RAIN PROTECTION - PITOT AND STATIC - POLARITY STANDARDIZATION TO ADDRESS UN-ANNUNCIATED RECOMMENDED FAILURE OF PITOT PROBE HEATERS. SERVICE BULLETIN MOS 04-JUN-2014 - (6) SB 737-30A1049 WINDOWS. WINDSHIELDS AND DOORS. WINDSHIELD WIPER SYSTEM. WIRING CHANGE. SERVICE BULLETIN RECOMMENDED COMPLIED WITH-CM MOS 10-AUG-2000 01 -JUN-2000 - (s) SB 737-30A1049 RI WINDOWS. WINDSHIELDS AND DOORS. WINDSHIELD WIPER SYSTEM. SERVICE BULLETIN RECOMMENDED MOS 12-OCT-2000 - (s) SB 737-30A1049 RI LEFT CHANGE WINDOWS. WINDSHIELDS AND DOORS. WINDSHIELD WIPER SYSTEM. SERVICE BULLETIN WIRING RECOMMENDED SIDE DAYS 90 (s) 12-OCT-2000 SB 737-30A1049 RI CHANGE WINDOWS. WINDSHIELDS AND DOORS. WINDSHIELD WIPER SYSTEM. SERVICE BULLETIN WIRING RECOMMENDED RIGHT SIDE MOS 12-OCT-2000 5000 (s) SB 737-30A1057 ICE AND RAIN PROTECTION - WINDSHIELD WIPER SYSTEM - CHANGE THE WINSHIELD WIPER MOTOR (SUPERSEDED SUPERSEDED - INFORMATION REFER TO REV.1 IA.W. AD BY 737-30A1057 RI. SERVICE BULLETIN 2008-24-05 MOS 06-OCT-2006 - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 72 Of 748 @ Camp Systems EFTA00618363 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: O5-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-30A1057 RI SB 737-30A1057 R2 SB 737-30A1057 R3 31-OCT-2011 SB 737-30A1057 R3 TABLE 1 (001.1) 30-DEC-2008 SB 737-30A1057 R3 TABLE 1 (001.2) ICE AND RAIN PROTECTION - WINDSHIELD WIPER SYSTEM - CHANGE THE WINDSHIELD WIPER MOTOR (SUPERSEDED BY 88 737-30A1057 R2). SERVICE BULLETIN MOS - (s) ICE AND RAIN PROTECTION- WINDSHIELD WIPER SYSTEM - CHANGE THE WINDSHIELD WIPER MOTOR (SUPERSEDED BY 737-30A1057 R3), SERVICE BULLETIN MOS - (0 SUPERSEDED SUPERSEDED ICE AND RAIN PROTECTION- WINDSHIELD WIPER SYSTEM - CHANGE THE WINDSHIELD WIPER MOTOR. SERVICE COMPLIED WITH- IAW. AD 2008-24-05 BULLETIN MOS I I -SEP-2013 VERIFY ICE AND RAIN PROTECTION - WINDSHIELD WIPER SYSTEM - CHANGE THE WINDSHIELD WIPER MOTOR. SERVICE BULLETIN THE LH WINDSHIELD WIPER MOTOR PART NUMBER AND SERIAL NUMBER (REFERRED TO AS'MODEL NUMBER' IN THE GOODRICH SERVICE BULLETIN 2313M-347/2313M-348-30-01) OF THE WINDSHIELD WIPER MOTORS AS GIVEN IN WORK PACKAGE 1 OF THE ACCOMPLISHMENT INSTRUCTIONS FOR ALL AIRPLANES! REPLACE OR CHANGE GOODRICH PART NUMBER AS NEEDED. MOS If -SEP-2013 VERIFY ICE AND RAIN PROTECTION - WINDSHIELD WIPER SYSTEM - CHANGE THE WINDSHIELD WIPER MOTOR. SERVICE BULLETIN THE RH WINDSHIELD WIPER MOTOR PART NUMBER AND SERIAL NUMBER (REFERRED TO AS'MODEL NUMBER' IN THE GOODRICH SERVICE BULLETIN 2313M-347/2313M-348-30-01) OF THE WINDSHIELD WIPER MOTORS AS GIVEN IN WORK PACKAGE 1 OF THE ACCOMPLISHMENT INSTRUCTIONS FOR ALL AIRPLANES! REPLACE OR CHANGE GOODRICH PART NUMBER AS NEEDED. MOS f f -SEP-2013 RECOMMENDED COMPUED WITH -CHANGE LH: PN 10-61329-39 TO P/N 10-1329-41 RECOMMENDED COMPLIED WITH - CHANGE PN TO 231351348-4 / SN 00338 30-DEC-2008 SB 737-30A1063 ICE AND RAIN PROTECTION - PITOT AND STATIC - AIR DATA PROBE ANTI-ICING SYSTEM - AIR DATA PROBE HEAT SUPERSEDED AUTOMATION INSTALLATION (SUPERSEDED BY SB 737-30A1063 R1). SERVICE BULLETIN MOS (EFF) SB 737-30A1063 RI ICE AND RAIN PROTECTION - PITOT AND STATIC - AIR DATA PROBE ANTI-ICING SYSTEM - AIR DATA PROBE HEAT SUPERSEDED AUTOMATION INSTALLATION (SUPERSEDED BY SB 737-30A1063 R2). SERVICE BULLETIN MOS (EFF) SB 737-30A1063 R2 ICE AND RAIN PROTECTION - PITOT AND STATIC - AIR DATA PROBE ANTI-ICING SYSTEM - AIR DATA PROBE HEAT MANDATORY 14-JAN-2013 AUTOMATION INSTALLATION. SERVICE BULLETIN MOS 24 (EFF) 14-JAN-2015 SB 737-31-1124 ADDITION OF THE RUDDER PEDAL FORCE TRANSDUCER. SERVICE BULLETIN RECOMMENDED MOS 20-MAY-1999 - (s) 7-Insufficient Information +-Task exists in Inspection Manual (0-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time @ Camp Systems 73 Of 748 EFTA00618364 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: O5-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-31-1124 RI 22-JUN-2000 SB 737-31-1150 06-APR-2000 SB 737-31-1153 I3-JAN-2000 SB 737-31-1153 RI OI -JUN-2000 SB 737-31-1153 R2 I0-AUG-2000 SB 737-31-1169 08-JUN-2000 SB 737-31-1169 R3 02-MAY-2002 ADDITION OF THE RUDDER PEDAL FORCE TRANSDUCER. SERVICE BULLETIN MOS - Is) INDICATING/RECORDING SYSTEMS - CENTRAL DISPLAY SYSTEM. SERVICE BULLETIN MOS - Is) RECOMMENDED RECOMMENDED OPERATIONAL PROGRAM CONFIGURATION (OPC) SOFTWARE UPGRADE REPLACEMENT. SERVICE BULLETIN RECOMMENDED - (s) RECOMMENDED . SERVICE BULLETIN MOS MOS - (s) INDICATING AND RECORDING SYSTEM - COMMON DISPLAY SYSTEMS. SERVICE BULLETIN RECOMMENDED MOS - (s) SOFTWARE CHANGE TO DISPLAY THE FLIGHT DIRECTOR COMMAND AS SPLIT AXIS COMMAND BARS. SERVICE RECOMMENDED BULLETIN MOS SOFTWARE CHANGE TO DISPLAY THE FLIGHT DIRECTOR COMMAND AS SPLIT AXIS COMMAND BARS. SERVICE RECOMMENDED BULLETIN MOS SB 737-31-1170 INDICATING/RECORDING - RIGHT DATA RECORDER SYSTEM - PARAMETER ADDITION TO RECORD STANDBY RUDDER SYSTEM ENGAGED (ON-OFF) STATUS. SERVICE BULLETIN MOS 21-MAR-2002 - (s) SB 737-31-1170 RI INDICATING/RECORDING - RIGHT DATA RECORDER SYSTEM - PARAMETER ADDITION TO RECORD STANDBY RUDDER SYSTEM ENGAGED (ON-OFF) STATUS. SERVICE BULLETIN MOS I8-SEP-2007 SB 737-31-1205 OPERATIONAL PROGRAM SOFTWARE (OPS) UPGRADE. SERVICE BULLETIN RECOMMENDED MOS 20-FEB-2003 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 74 Of 748 @ Camp Systems EFTA00618365 C O MP A.m." vgnie• Megnund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-31-1246 05-MAY-2005 INDICATING AND RECORDING SYSTEMS - COMMON DISPLAY SYSTEM - DISPLAY ELECTRONIC UNIT OPERATIONAL PROGRAM SOFTWARE CHANGE. SERVICE BULLETIN MOS SB 737-31-1284 INDICATING/RECORDING SYSTEMS - MASTER CAUTION - ADDITION OF QUICK DISCONNECTS TO THE MASTER CAUTION AND FIRE WARNING SWITCHLIGHT WIRES. SERVICE BULLETIN MOS 23-FEB-2006 SB 737-31-1284 RI INDICATING/RECORDING SYSTEMS - MASTER CAUTION - ADDITION OF QUICK DISCONNECTS TO THE MASTER CAUTION AND FIRE WARNING SWITCHLIGHT WIRES. SERVICE BULLETIN MOS 01-MAR-2007 SB 737-31-1293 06-AUG-2009 SB 737-31-1295 27-OCT-2005 COMMON DISPLAY SYSTEM - UPDATED PHASE 3 DISPLAY UNIT DATABASE INSTALLATION. SERVICE BULLETIN MOS INDICATING AND RECORDING SYSTEMS - COMMON DISPLAY SYSTEM - DISPLAY ELECTRONIC UNIT OPERATIONAL PROGRAM SOFTWARE CHANGE. SERVICE BULLETIN MOS SB 737-31-1327 INDICATING/RECORDING SYSTEMS - COMMON DISPLAY SYSTEM (CDS)- CHANGE THE OPERATIONAL PROGRAM SOFTWARE (OPS) FOR THE CDS DISPLAY ELECTRONIC UNIT (DEU). SERVICE BULLETIN 14-DEC-2006 SB 737-31-1327 RI I0-OCT-2007 SB 737-31-1449 SB 737-31-1449 RI MOS INDICATING/RECORDING SYSTEMS - COMMON DISPLAY SYSTEM (CDS) - CHANGE THE OPERATIONAL PROGRAM SOFTWARE (OPS) FOR THE CDS DISPLAY ELECTRONIC UNIT (DEU). SERVICE BULLETIN MOS 22-AUG-2008 3260:48 RECOMMENDED AFL 782 INDICATING/RECORDING SYSTEMS- FLIGHT DATA RECORDER SYSTEM- GROUND WIRE CHANGE (SUPERSEDED BY SUPERSEDED SB 737-31-1449 RI), SERVICE BULLETIN MOS INDICATING/RECORDING SYSTEMS - FLIGHT DATA RECORDER SYSTEM- GROUND WIRE CHANGE (SUPERSEDED BY SUPERSEDED SB 737-31-1449 R3). SERVICE BULLETIN MOS COMPLIED WITH - IAW THE 58 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 75 Of 748 @ Camp Systems EFTA00618366 C O MP A.m." vgnie• Megnsind AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-31-1449 R2 INDICATING/RECORDING SYSTEMS - FLIGHT DATA RECORDER SYSTEM - GROUND WIRE CHANGE (SUPERSEDED BY SUPERSEDED SB 737-31-1449 R3). SERVICE BULLETIN MOS SB 737-31-1449 R3 INDICATING/RECORDING SYSTEMS- FLIGHT DATA RECORDER SYSTEM- GROUND WIRE CHANGE. SERVICE RECOMMENDED BULLETIN MOS 23-JUL-2013 SB 737-31-1471 INDICATING/RECORDING SYSTEMS - COMMON DISPLAY SYSTEM - INSTALLATION OF PHASE 3A DISPLAY UNIT AND SUPERSEDED DATABASE SOFTWARE (SUPERSEDED BY SB 737-31-1471 R1). SERVICE BULLETIN MOS - SB 737-31-1471 RI INDICATING/RECORDING SYSTEMS - COMMON DISPLAY SYSTEM - INSTALLATION OF PHASE 3A DISPLAY UNIT AND RECOMMENDED DATABASE SOFTWARE. SERVICE BULLETIN MOS 60 (s) 29-NOV-2012 SB 737-31-1472 INDICATING/RECORDING SYSTEMS - COMMON DISPLAY SYSTEM - INSTALLATION OF FLIGHT DIRECTOR COMMAND RECOMMENDED DISPLAY AS A SPLIT AXIS COMMAND BAR. SERVICE BULLETIN MOS 12-JAN-2011 SB 737-31-1475 INDICATING / RECORDING SYSTEMS - COMMON DISPLAY SYSTEM - REMOVAL OF OPTIONS. SERVICE BULLETIN RECOMMENDED MOS 21-JAN-2011 SB 737-31-1506 INDICATING/RECORDING SYSTEMS - FLIGHT DATA RECORDER SYSTEM- DIGITAL FLIGHT DATA ACQUISITION UNIT RECOMMENDED LOADABLE SOFTWARE CHANGE. SERVICE BULLETIN MOS 04-OCT-2011 SB 737-31-1552 INDICATING/RECORDING SYSTEMS - COMMON DISPLAY SYSTEM - SOFTWARE CHANGE. SERVICE BULLETIN RECOMMENDED MOS 08-MAR-2013 SB 737-31A1332 INDICATING / RECORDING SYSTEMS - AURAL WARNING SYSTEM - INSTALLATION OF THE CABIN ALTITUDE WARNING SUPERSEDED SYSTEM AND TAKEOFF CONFIGURATION WARNING SYSTEM LIGHTS (SUPERSEDED BY SB 737-31A1332 R1). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 76 Of 748 @ Camp Systems EFTA00618367 C O MP A.m." vgnie• Megnundop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: O5-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-31A1332 R1 INDICATING / RECORDING SYSTEMS - AURAL WARNING SYSTEM - INSTALLATION OF THE CABIN ALTITUDE WARNING SUPERSEDED SYSTEM AND TAKEOFF CONFIGURATION WARNING SYSTEM LIGHTS (SUPERSEDED BY SB 737-31A1332 R2). SERVICE BULLETIN MOS (EFF) SB 737-31A1332 R2 INDICATING / RECORDING SYSTEMS - AURAL WARNING SYSTEM - INSTALLATION OF THE CABIN ALTITUDE WARNING SUPERSEDED SYSTEM AND TAKEOFF CONFIGURATION WARNING SYSTEM LIGHTS (SUPERSEDED BY SB 737-31A1332 R3). SERVICE BULLETIN MOS (EFF) SB 737-31A1332 R3 INDICATING / RECORDING SYSTEMS - AURAL WARNING SYSTEM - INSTALLATION OF THE CABIN ALTITUDE WARNING SUPERSEDED SYSTEM AND TAKEOFF CONFIGURATION WARNING SYSTEM LIGHTS (SUPERSEDED BY SB 737-31A1332 R4). SERVICE BULLETIN MOS (EFF) SB 737-31A1332 R4 INDICATING / RECORDING SYSTEMS -AURAL WARNING SYSTEM - INSTALLATION OF THE CABIN ALTITUDE WARNING RECOMMENDED 06-MAR-2013 SYSTEM AND TAKEOFF CONFIGURATION WARNING SYSTEM LIGHTS. SERVICE BULLETIN MOS 36 (EFF) 06-MAR-2016 06-MAR-2016 SB 737-32-1305 NOSE LANDING GEAR AFT LOCK LINK REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS - (s) SB 737-32-1305 RI NOSE LANDING GEAR AFT LOCK LINK REPLACEMENT. SERVICE BULLETIN RECOMMENDED I3-MAR-2003 MOS SB 737-32-1311 LANDING GEAR- WHEELS AND BRAKES - HYDRAULIC BRAKE SYSTEM. SERVICE BULLETIN RECOMMENDED MOS I9-AUG-1999 - (s) SB 737-32-1312 SHIMMY DAMPER ADDITION. SERVICE BULLETIN MOS 24-FEB-1999 - Is/ SB 737-32-1312 RI SHIMMY DAMPER ADDITION. SERVICE BULLETIN MOS 0I-APR-1999 - Is/ SB 737-32-1312 R2 MLG SHIMMY DAMPER ADDITION. SERVICE BULLETIN MOS IS-JUL-1999 - (s) RECOMMENDED RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 77 Of 748 @ Camp Systems EFTA00618368 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: O5-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32-1312 R3 27 -SEP-2000 SHIMMY DAMPER ADDITION. SERVICE BULLETIN MOS - (s) SB 737-32-1317 LANDING GEAR - POSITION AND WARNING. SERVICE BULLETIN MOS 09-SEP-I999 - (s) SB 737-32-1317 RI LANDING GEAR- POSITION AND WARNING. SERVICE BULLETIN MOS I8-JAN-2001 - (s) SB 737-32-1330 MAIN LANDING GEAR (STRUCTURE). SERVICE BULLETIN MOS 08-JUN-2000 - (s) SB 737-32-1332 NOSE GEAR EXTENSION AND RETRACTION. SERVICE BULLETIN RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED COMPUED WITH - PREVIOUSLY NO WORK NECCESSARY REF: GVBBJ039-0220 -2 KIT USED FOR ORIGINAL COMPLIANCE 07-FEB-2000 MOS 24-AUG-2007 - (s) 2968:28 AFL 699 SB 737-32-1332 RI LANDING GEAR. NOSE GEAR EXTENSION 8 RETRACTION. RELOCATION OF THE NOSE GEAR EXTEND FUSE. SERVICE RECOMMENDED - REF: RO BULLETIN MOS 08-JUN-2000 - (s) SB 737-32-1332 R2 RELOCATION OF THE NOSE GEAR EXTEND FUSE, SERVICE BULLETIN - REF: RO MOS 28-FEB-2002 - (s) SB 737-32-1342 LANDING GEAR-STEERING-INSPECTION AND MODIFICATION TO THE NOSE LANDING GEAR STEERING COLLAR AND RECOMMENDED STEERING PLATE. SERVICE BULLETIN MOS I I -MAY-2000 SB 737-32-1342 RI 01-MAY-2001 SB 737-32-1362 07-FEB-2000 - Is) LANDING GEAR - STEERING - INSPECTION AND MODIFICATION TO THE NOSE LANDING GEAR STEERING COLLAR AND RECOMMENDED STEERING PLATE. SERVICE BULLETIN MOS CHANGE THE LOWER BEARING SEAL RETAINER, SERVICE BULLETIN RECOMMENDED MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 78 Of 748 @ Camp Systems EFTA00618369 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32-1362 RI 26-JAN-2006 SB 737-32-1368 09-SEP-2004 LANDING GEAR - NOSE LANDING GEAR - CHANGE THE LOWER BEARING SEAL RETAINER.. SERVICE BULLETIN MOS LEFT AND RIGHT MAIN LANDING GEAR SHIMMY DAMPER ASSEMBLY REPAIRS AND SEALS REPLACEMENT. SERVICE RECOMMENDED BULLETIN MOS SB 737-32-1368 RI LEFT AND RIGHT MAIN LANDING GEAR SHIMMY DAMPER ASSEMBLY REPAIRS AND SEALS REPLACEMENT. SERVICE RECOMMENDED BULLETIN 25-JUN-2009 SB 737-32-1369 SB 01-APR-2004 [SSN REDACTED] RI MOS AFL 3000(s) LANDING GEAR - MAIN LANDING GEAR EXTENSION AND RETRACTION - RETRACT ACTUATOR CYLINDER ASSEMBLY MODIFICATION OR REPLACEMENT. SERVICE BULLETIN MOS 09-AUG-20C6 AFL 3000 (s) SB 737-32-1369 R2 LANDING GEAR - MAIN LANDING GEAR EXTENSION AND RETRACTION - RETRACT ACTUATOR CYLINDER ASSEMBLY MODIFICATION OR REPLACEMENT. SERVICE BULLETIN MOS I6-AUG-2007 AFL 3000 (s) SB 737-32-1369 R3 LANDING GEAR - MAIN LANDING GEAR EXTENSION AND RETRACTION - RETRACT ACTUATOR CYLINDER ASSEMBLY SUPERSEDED MODIFICATION OR REPLACEMENT (SUPERSEDED BY SB 737-32-1369 R4). SERVICE BULLETIN MOS - (s) SB 737-32-1369 R4 LANDING GEAR - MAIN LANDING GEAR EXTENSION AND RETRACTION- RETRACT ACTUATOR CYLINDER ASSEMBLY RECOMMENDED MODIFICATION OR REPLACEMENT. SERVICE BULLETIN MOS AFL 1000 (s) SB 737-32-1376 INSPECT. LUBRICATE. REPAIR OR REPLACE MAIN LANDING GEAR-FORWARD TRUNION PIN INSPECTION AND NOT APPLICABLE - BY EFFECTIVITY REPLACEMENT. SERVICE BULLETIN MOS I2-MAY-2005 - (s) MOS RETRACT ACTUATOR CYLINDER ASSEMBLY MODIFICATION OR REPLACEMENT. SERVICE BULLETIN 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 79 Of 748 @ Camp Systems EFTA00618370 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32-1376 RI INSPECT. LUBRICATE. REPAIR OR REPLACE MAIN LANDING GEAR- FORWARD TRUNION PIN INSPECTION AND NOT APPLICABLE - BY EFFECTIVITY REPLACEMENT.. SERVICE BULLETIN MOS - (s) SB 737-32-1376 R2 MAIN LANDING GEAR - FORWARD TRUNNION PIN INSPECTION AND NOT APPLICABLE - BY EFFECTIVITY REPLACEMENT. SERVICE BULLETIN MOS I6-FEB-2010 06-AUG-2008 3417:51 AFL 829 58 [SSN REDACTED] LANDING GEAR - MAIN GEAR AND DOORS - OUTER CYLINDER WALKING BEAM CLEVIS BUSHING AND RETRACT ACTUATOR CLEVIS BUSHING REPLACEMENT. SERVICE BULLETIN MOS 02-JUL-2007 58 [SSN REDACTED] RI MAIN GEAR AND DOORS - OUTER CYLINDER WALKING BEAM CLEVIS BUSHING RECOMMENDED AND RETRACT ACTUATOR CLEVIS BUSHING REPLACEMENT. SERVICE BULLETIN MOS 05-JAN-2010 SB 737-32-1394 LANDING GEAR - NOSE LANDING GEAR EXTENSION AND RETRACTION - GEAR LOCK ACTUATOR TRUNNION SEALS REPLACEMENT. SERVICE BULLETIN MOS I6-NOV-2006 SB 737-32-1402 MAIN LANDING GEAR - FORWARD TRUNNION PIN INSPECTION AND REPLACEMENT (SUPERSEDED BY SB 737-32-1402 R1). SERVICE BULLETIN MOS 02-FEB-2010 06-AUG-2008 3411:56 AFL 827 SB 737-32-1402 RI LANDING GEAR - MAIN LANDING GEAR- FORWARD TRUNNION PIN INSPECTION AND REPLACEMENT. SERVICE RECOMMENDED BULLETIN MOS 07-FEB-20I3 - (s) SB 737-32-1402 RI TABLE LUBRICATE LANDING GEAR - MAIN LANDING GEAR- FORWARD TRUNNION PIN INSPECTION AND REPLACEMENT. RECOMMENDED 1.1 & 1.2 SERVICE BULLETIN THE MLG FORWARD TRUNNION PIN DAYS 30 (s) 07-FEB-20I3 SB 737-32-1402 RI TABLE DETAILED INSPECTION LANDING GEAR - MAIN LANDING GEAR - FORWARD TRUNNION PIN INSPECTION AND RECOMMENDED 1.3 81.4 REPLACEMENT. SERVICE BULLETIN OF THE TRANSITION RADIUS LOCATION (IN-SITU) MOS 6 (s) 07-FEB-20I3 NOT APPLICABLE - BY EFFECTIVITY 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 80 Of 748 @ Camp Systems EFTA00618371 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32-1402 RI TABLE REPAIR LANDING GEAR - MAIN LANDING GEAR - FORWARD TRUNNION PIN INSPECTION AND REPLACEMENT. 1.5 SERVICE BULLETIN THE FINISH FOR AIRPLANES WITH FINISH DAMAGE (SCRAPES OR SCRATCHES THROUGH THE FULL THICKNESS OF THE PRIMER OR AREAS OF MISSING PRIMER) FOUND IN THE TRANSITION RADIUS LOCATION. AND NO CORROSION. NO PITTING. AND NO B SF METAL SCRATCHES 8 DO A DETAILED INSPECTION OF THE TRANSITION RADIUS LOCATION (IN-SITU) MOS BFIF (s) SB 737-32-1402 RI TABLE LUBRICATE LANDING GEAR - MAIN LANDING GEAR - FORWARD TRUNNION PIN INSPECTION AND REPLACEMENT. 2.1 & 2.2 SERVICE BULLETIN LUBRICATE THE MLG FOR WARD TRUNNION PIN DAYS 30 (s) 07-FEB-2013 SB 737-32-1402 RI TABLE DETAILED INSPECTION LANDING GEAR - MAIN LANDING GEAR - FORWARD TRUNNION PIN INSPECTION AND 2.3 & 2.4 REPLACEMENT. SERVICE BULLETIN OF THE TRANSITION RADIUS LOCATION (IN-SITU) MOS 6 (s) 07-FEB-2013 SB 737-32-1402 RI TABLE REPAIR LANDING GEAR - MAIN LANDING GEAR- FORWARD TRUNNION PIN INSPECTION AND REPLACEMENT. 2.5 SERVICE BULLETIN THE FINISH FOR AIRPLANES WITH FINISH DAMAGE (SCRAPES OR SCRATCHES THROUGH THE FULL THICKNESS OF THE PRIMER OR AREAS OF MISSING PRIMER) FOUND IN THE TRANSITION RADIUS LOCATION AND NO CORROSION. NO PITTING. AND NO BASE METAL SCRATCHES 8 DO DETAILED INSPECTION OF THE TRANSITION RADIUS LOCATION (IN-SITU) SB 737-32-1408 09-SEP-2009 SB 737-32-1408 RI SB 737-32-1408 R2 24-JUN-2011 SB 737-32-1410 20-FEB-2008 MOS BFIF (s) RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED WHEELS AND BRAKES - REPLACE STEEL BRAKES AND WHEELS WITH MESSIER-BUGATTI CARBON BRAKES AND SUPERSEDED WHEELS (SUPERSEDED BY 737-32-1408 RI). SERVICE BULLETIN MOS LANDING GEAR- WHEELS AND BRAKES - REPLACE STEEL BRAKES AND WHEELS WITH MESSIER-BUGATTI CARBON SUPERSEDED BRAKES AND WHEELS FOR 737-700 AIRPLANES (SUPERSEDED BY SB 737-32-1408 R2). SERVICE BULLETIN MOS LANDING GEAR- WHEELS AND BRAKES - REPLACE STEEL BRAKES AND WHEELS WITH MESSIER-BUGATTI CARBON RECOMMENDED BRAKES AND WHEELS FOR 737-700 AIRPLANES. SERVICE BULLETIN MOS LANDING GEAR - MAIN LANDING GEAR - WIRE BUNDLE AND HANGER LINK ASSEMBLY COMPLIED WITH INSPECTION. REPAIR AND MODIFICATION. SERVICE BULLETIN MOS 22-AUG-2008 3260:48 AFL 782 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 81 Of 748 @ Camp Systems EFTA00618372 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32-1410 RI 20-NOV-2008 MAIN LANDING GEAR - WIRE BUNDLE AND HANGER LINK ASSEMBLY INSPECTION. REPAIR AND MODIFICATION. SERVICE BULLETIN MOS SB 737-32-1410 R2 MAIN LANDING GEAR - WIRE BUNDLE AND HANGER LINK ASSEMBLY RECOMMENDED INSPECTION. REPAIR AND MODIFICATION. SERVICE BULLETIN 29-SEP-2009 MOS SB 737-32-1418 LANDING GEAR - EXTENSION AND RETRACTION- MAIN LANDING GEAR RETRACT ACTUATOR CHANGE OR RECOMMENDED REPLACEMENT (SUPERSEDED BY SB 737-32-1418 RI). SERVICE BULLETIN MOS I3-JUL-2010 SB 737-32-1418 RI LANDING GEAR - EXTENSION AND RETRACTION- MAIN LANDING GEAR RETRACT ACTUATOR CHANGE OR RECOMMENDED REPLACEMENT. SERVICE BULLETIN MOS 05-APR-20I3 SB 737-32-1422 LANDING GEAR- EXTENSION AND RETRACTION- CONTROL SYSTEM AFT CONTROL QUADRANT CLEARANCE RECOMMENDED MEASUREMENT AND REPLACEMENT. SERVICE BULLETIN MOS 29-JAN-2010 SB 737-32-1429 REPLACE STEEL BRAKES AND WHEELS WITH MESSIER-BUGATTI CARBON BRAKES AND WHEELS FOR 737-800 SUPERSEDED AIRPLANES (SUPERSEDED BY SB 737-32-1429 RI). SERVICE BULLETIN MOS SB 737-32-1429 RI LANDING GEAR- WHEELS AND BRAKES- REPLACE STEEL BRAKES AND WHEELS WITH MESSIER-BUGATTI CARBON SUPERSEDED BRAKES AND WHEELS FOR 737-800 AIRPLANES (SUPERSEDED BY SB 737-32-1429 R2). SERVICE BULLETIN MOS SB 737-32-1429 R2 LANDING GEAR- WHEELS AND BRAKES- REPLACE STEEL BRAKES AND WHEELS WITH MESSIER-BUGATTI-DOWTY SUPERSEDED CARBON BRAKES AND WHEELS FOR 737-800 AIRPLANES (SUPERSEDED BY SB 737-32-1429 R3). SERVICE BULLETIN MOS SB 737-32-1429 R3 LANDING GEAR- WHEELS AND BRAKES- REPLACE STEEL BRAKES AND WHEELS WITH MESSIER-BUGATTI-DOWTY RECOMMENDED CARBON BRAKES AND WHEELS FOR 737-803 AIRPLANES. SERVICE BULLETIN MOS 09-AUG-20I2 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 82 Of 748 @ Camp Systems EFTA00618373 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32-1430 LANDING GEAR - WHEELS AND BRAKES - MAIN LANDING GEAR STEEL BRAKES AND RELATED WHEELS TO SUPERSEDED MESSIER-SUGATTI CARBON BRAKES AND RELATED WHEELS REPLACEMENT FOR 737-900ER AIRPLANES (SUPERSEDED BY SS 737-32-1430 R1). SERVICE BULLETIN MOS 58 [SSN REDACTED] RI LANDING GEAR - WHEELS AND BRAKES - MAIN LANDING GEAR STEEL BRAKES AND RELATED WHEELS TO SUPERSEDED MESSIER-BUGATTI CARBON BRAKES AND RELATED WHEELS REPLACEMENT FOR 737-900ER AIRPLANES (SUPERSEDED BY S8 [SSN REDACTED] R2). SERVICE BULLETIN MOS SB 737-32-1430 R2 LANDING GEAR - WHEELS AND BRAKES - MAIN LANDING GEAR STEEL BRAKES AND RELATED WHEELS TO RECOMMENDED MESSIER-BUGATTI-DOWTY CARBON BRAKES AND RELATED WHEELS REPLACEMENT FOR 737-900ER AIRPLANES. SERVICE BULLETIN MOS 09-JAN-2012 SB 737-32-1433 LANDING GEAR - WHEELS AND BRAKES- REPLACE STEEL BRAKES AND WHEELS WITH GOODRICH CARBON BRAKES SUPERSEDED AND WHEELS FOR 737-700 AIRPLANES (SUPERSEDED BY SB 737-32-1433 R1). SERVICE BULLETIN MOS SB 737-32-1433 RI LANDING GEAR- WHEELS AND BRAKES - REPLACE STEEL BRAKES AND WHEELS WITH GOODRICH CARBON BRAKES SUPERSEDED AND WHEELS FOR 737-700 AIRPLANES (SUPERSEDED BY SB 737-32-1433 R2). SERVICE BULLETIN MOS SB 737-32-1433 R2 LANDING GEAR- WHEELS AND BRAKES -REPLACE STEEL BRAKES AND WHEELS WITH GOODRICH CARBON BRAKES RECOMMENDED AND WHEELS FOR 737-700 AIRPLANES. SERVICE BULLETIN MOS I9-APR-2012 58 [SSN REDACTED] LANDING GEAR- EXTENSION AND RETRACTION- NOSE LANDING GEAR RETRACT ACTUATOR CHANGE OR RECOMMENDED REPLACEMENT. SERVICE BULLETIN MOS 14-JUL-2011 SB 737-32-1441 LANDING GEAR- WHEELS AND BRAKES- REPLACE STEEL BRAKES AND WHEELS WITH GOODRICH CARBON BRAKES SUPERSEDED AND WHEELS FOR 737-800 AIRPLANES (SUPERSEDED BY SB 737-32-1441 R1). SERVICE BULLETIN MOS SB 737-32-1441 RI LANDING GEAR - WHEELS AND BRAKES- REPLACE STEEL BRAKES AND WHEELS WITH GOODRICH CARBON BRAKES SUPERSEDED AND WHEELS FOR 737-800 AIRPLANES (SUPERSEDED BY S8 [SSN REDACTED] R2). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 83 Of 748 @ Camp Systems EFTA00618374 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32-1441 R2 06-AUG-2012 LANDING GEAR - WHEELS AND BRAKES - REPLACE STEEL BRAKES AND WHEELS WITH GOODRICH CARBON BRAKES AND WHEELS FOR 737400 AIRPLANES. SERVICE BULLETIN MOS RECOMMENDED SB 737-32-1442 LANDING GEAR - STEERING - NOSE WHEEL STEERING SYSTEM MECHANISM COMPONENT CHANGE (SUPERSEDED SUPERSEDED BY SB SB 737-32-1442 RI), SERVICE BULLETIN MOS SB 737-32-1442 RI LANDING GEAR - STEERING - NOSE WHEEL STEERING SYSTEM MECHANISM COMPONENT CHANGE (SUPERSEDED SUPERSEDED BY SB 737-32-1442 R2). SERVICE BULLETIN MOS SB 737-32-1442 R2 LANDING GEAR - STEERING - NOSE WHEEL STEERING SYSTEM MECHANISM COMPONENT CHANGE (SUPERSEDED RECOMMENDED 15-AUG-2011 BY SB 737-32-1442 R3). SERVICE BULLETIN MOS SB 737-32-1442 R3 LANDING GEAR - STEERING - NOSE WHEEL STEERING SYSTEM MECHANISM COMPONENT CHANGE. SERVICE RECOMMENDED 11-MAR-2013 BULLETIN MOS 58 [SSN REDACTED] R4 LANDING GEAR - STEERING - NOSE WHEEL STEERING SYSTEM MECHANISM COMPONENT CHANGE. SERVICE RECOMMENDED 29-JUL-2013 BULLETIN MOS 58 [SSN REDACTED] LANDING GEAR- EXTENSION AND RETRACTION - MANUAL EXTENSION CONTROL MECHANISM ACCESS DOOR RECOMMENDED 18-N0V-2011 SWITCH REPLACEMENT. SERVICE BULLETIN MOS SB 737-32-1443 RI LANDING GEAR- EXTENSION AND RETRACTION - MANUAL EXTENSION CONTROL MECHANISM ACCESS DOOR RECOMMENDED 16-AUG-2013 SWITCH REPLACEMENT. SERVICE BULLETIN MOS SB 737-32-1444 LANDING GEAR- TIRES AND WHEELS - MAIN LANDING GEAR INBOARD WHEEL HALF INSPECTION. SERVICE BULLETIN RECOMMENDED MOS 08-APR-2010 SB 737-32-1445 LANDING GEAR - MAIN LANDING GEAR GLAND NUT INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks %Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 84 Of 748 @ Camp Systems EFTA00618375 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32-1448 LANDING GEAR - MAIN LANDING GEAR - FORWARD AND AFT TRUNNION PIN ASSEMBLIES INSPECTION AND CHANGE. SERVICE BULLETIN MOS SB 737-32-1448 TABLE 1.1 LUBRICATE LANDING GEAR - MAIN LANDING GEAR - FORWARD AND AFT TRUNNION PIN ASSEMBLIES INSPECTION RECOMMENDED COMPUED WITH AND CHANGE. SERVICE BULLETIN THE MLG FORWARD AND AFT TRUNNION PIN ASSEMBLIES FOR ALL AIRPLANES DAYS 30 (s) 13-JUN-2014 19-MAY-2011 3749:42 AFL 920 SB 737-32-1448 TABLE INSTALL LANDING GEAR- MAIN LANDING GEAR - FORWARD AND AFT TRUNNION PIN ASSEMBLIES INSPECTION AND RECOMMENDED 1.10 CHANGE. SERVICE BULLETIN IMPROVED MLG OUTER CYLINDER TRUNNION BUSHINGS. IMPROVED AFT TRUNNION BEARING ASSEMBLY. NEW FORWARD TRUNNION PIN CROSS BOLT BUSHINGS (GROUP 1 ONLY) AND AFT TRUNNION PIN CROSS BOLT BUSHINGS FOR ALL AIRPLANES SB MOS 120(s) 19-MAY-2011 [SSN REDACTED] TABLE 1.2 PERFORM LANDING GEAR - MAIN LANDING GEAR - FORWARD AND AFT TRUNNION PIN ASSEMBLIES INSPECTION AND CHANGE. SERVICE BULLETIN A GENERAL VISUAL INSPECTION OF THE MLG FORWARD AND AFT TRUNNION PIN ASSEMBLIES WITH THE MLG NOT REMOVED FOR SIGNS OF CORROSION AND/OR CHROME PLATING DAMAGE FOR ALL AIRPLANES RECOMMENDED COMPUED WITH MOS 18 09-AUG-2011 09-FEB-2013 RECURRING 19-MAY-2011 3533:32 AFL 863 SB 737-32-1449 LANDING GEAR- WHEELS AND BRAKES - REPLACE STEEL BRAKES AND WHEELS WITH GOODRICH CARBON BRAKES SUPERSEDED AND WHEELS FOR 737-900ER AIRPLANES (SUPERSEDED BY SB 737-32-1449 RI). SERVICE BULLETIN MOS SB 737-32-1449 RI LANDING GEAR- WHEELS AND BRAKES - REPLACE STEEL BRAKES AND WHEELS WITH GOODRICH CARBON BRAKES RECOMMENDED AND WHEELS FOR 737-900ER AIRPLANES. SERVICE BULLETIN MOS 15-SEP-2011 SB 737-32-1449 R2 LANDING GEAR- WHEELS AND BRAKES- REPLACE STEEL BRAKES AND WHEELS WITH GOODRICH CARBON BRAKES RECOMMENDED AND WHEELS FOR 737-900ER AIRPLANES. SERVICE BULLETIN MOS 08-AUG-2012 SB 737-32-1456 LANDING GEAR- WHEELS AND BRAKES- MAIN LANDING GEAR STEEL BRAKES AND RELATED WHEELS TO RECOMMENDED MESSIER-BUGATTI CARBON BRAKES AND RELATED WHEELS REPLACEMENT FOR 737-900 AIRPLANES. SERVICE BULLETIN MOS 13-JUN-2011 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 85 Of 748 @ Camp Systems EFTA00618376 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32-1457 LANDING GEAR - WHEELS AND BRAKES - MAIN LANDING GEAR STEEL BRAKES AND RELATED WHEELS TO GOODRICH RECOMMENDED CARBON BRAKES AND RELATED WHEELS REPLACEMENT FOR 737-900 AIRPLANES (SUPERSEDED BY SB 737-32-1457 R1). SERVICE BULLETIN SB 03-OCT-2011 [SSN REDACTED] RI 01-FEB-2013 MOS LANDING GEAR- WHEELS AND BRAKES - MAIN LANDING GEAR STEEL BRAKES AND RELATED WHEELS TO GOODRICH RECOMMENDED CARBON BRAKES AND RELATED WHEELS REPLACEMENT FOR 737-900 AIRPLANES. SERVICE BULLETIN MOS SB 737-32-1458 LANDING GEAR- TIRES AND WHEELS - REPLACEMENT OF WHEEL WELL BLADE SEALS. LOWER FAIRING SUPERSEDED ASSEMBLIES. AND 43.5 INCH DIAMETER TIRES WITH 44.5 INCH DIAMETER TIRES (SUPERSEDED BY SB 737-32-1458 R1). SERVICE BULLETIN MOS SB 737-32-1470 LANDING GEAR - TIRES AND WHEELS - MAIN LANDING GEAR RADIAL PLY TIRES IN SERVICE EVALUATION FOR SUPERSEDED AIRPLANES WITH GOODRICH CARBON BRAKES (SUPERSEDED BY SB 737-32-1470 R1), SERVICE BULLETIN MOS SB 737-32-1470 RI LANDING GEAR- TIRES AND WHEELS - MAIN LANDING GEAR RADIAL PLY TIRES IN SERVICE EVALUATION FOR RECOMMENDED 13-AUG-2013 AIRPLANES WITH GOODRICH CARBON BRAKES. SERVICE BULLETIN MOS SB 737-32-1471 LANDING GEAR- TIRES AND WHEELS - MAIN LANDING GEAR RADIAL PLY TIRES IN SERVICE EVALUATION FOR SUPERSEDED AIRPLANES WITH MESSIER-BUGATTI-DOWTY CARBON BRAKES (SUPERSEDED BY SB 737-32-1471 R1). SERVICE BULLETIN MOS SB 737-32-1471 RI LANDING GEAR- TIRES AND WHEELS - MAIN LANDING GEAR RADIAL PLY TIRES IN SERVICE EVALUATION FOR SUPERSEDED AIRPLANES WITH MESSIER-BUGATTI-DOWTY CARBON BRAKES (SUPERSEDED BY SB 737-32-1471 R2). SERVICE BULLETIN MOS SB 737-32-1471 R2 LANDING GEAR- TIRES AND WHEELS - MAIN LANDING GEAR RADIAL PLY TIRES IN SERVICE EVALUATION FOR RECOMMENDED 15-JUL-2013 AIRPLANES WITH MESSIER-BUGATTI-DOWTY CARBON BRAKES. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 86 Of 748 @ Camp Systems EFTA00618377 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-32A1343 26-JUL-2001 SB 737-33-1116 I6-DEC-1999 REPLACEMENT OF THE PROXIMITY SWITCH ELECTRONICS. SERVICE BULLETIN MOS 09-NOV-2005 2281 AFL 563 PASSENGER SERVICE UNIT NO-SMOKING FASTEN SEAT BELT SIGN-WIRING CHANGE. SERVICE BULLETIN MOS RECOMMENDED COMPUED WITH - PREVIOUSLY UNK - PART INSTALLED: P/N 285A1600-4 SN 001197 REF: COMPONENT CODE 311051 RECOMMENDED SB 737-33-1121 R2 LIGHTS - FLIGHT COMPARTMENTS- AUDIO CONTROL PANEL LAMP TEST WIRING INSTALLATION. SERVICE BULLETIN RECOMMENDED MOS 30-MAR-2011 SB 737-33-1128 LIGHTS - EXTERIOR - REPLACE POSITION LIGHT TRANSFORMERS. SERVICE BULLETIN RECOMMENDED MOS I8-JAN-2001 - SB 737-33-1130 PASSENGER COMPARTMENT LIGHTS - REPLACE THE 115VAC ATM CONNECTORS. SERVICE BULLETIN RECOMMENDED MOS 24-JAN-2002 - SB 737-33-1130 RI LIGHTS - PASSENGER COMPARTMENT LIGHTS - REPLACE THE 115VAC ATM CONNECTORS. SERVICE BULLETIN MOS 02-MAR-2006 SB 737-33-1133 MASTER DIMMER AND TEST- SUPPLY TEST GROUND SIGNAL WIRING SEPERATION. SERVICE BULLETIN MOS 12 (s) I9-DEC-2002 SB 737-33-1133 RI MASTER DIMMER AND TEST- SUPPLY TEST GROUND SIGNAL WIRING SEPERATION. SERVICE BULLETIN MOS 12 (s) 17-APR-2003 SB 737-33-1133 R2 MASTER DIMMER AND TEST- SUPPLY TEST GROUND SIGNAL WIRING SEPERATION. SERVICE BULLETIN MOS 30 (s) 04-DEC-2003 SB 737-33-1133 R3 LIGHTS - MASTER DIM AND TEST - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION. SERVICE BULLETIN COMPUED WITH - IAW THE AD AD 2006-15-18 MOS 09-AUG-2010 08-SEP-2005 - (s) 3448:31 AFL 841 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 87 Of 748 @ Camp Systems EFTA00618378 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-33-1133 R0 MASTER DIM AND TEST - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION (SUPERSEDED BY SB 737-33-1133 R5). SUPERSEDED - INFORMATION NO MORE WORK IS SERVICE BULLETIN NECESSARY ON AIRPLANES CHANGED AS SHOWN IN THE REVISION 3 OF THIS SERVICE BULLETIN MOS - Is) SB 737-33-1133 RS UGHTS - MASTER DIM AND TEST- SUPPLY TEST GROUND SIGNAL WIRING SEPARATION. SERVICE BULLETIN RECOMMENDED MOS 48 (s) 05-SEP-2006 SB 737-33-1146 UGHTS - STROBE POSITION UGHTS - LIGHTNING PROTECTION OF THE TAIL STROBE UGHT SYSTEM WIRING SUPERSEDED (SUPERSEDED BY SB 737-33-1146 RI). SERVICE BULLETIN MOS - (s) SB 737-33-1146 RI UGHTS - STROBE POSITION UGHTS - LIGHTNING PROTECTION OF THE TAIL STROBE UGHT AND SYSTEM WIRING. RECOMMENDED SERVICE BULLETIN MOS 72 (s) 02-NOV-2011 S8 [SSN REDACTED] LIGHTS - EMERGENCY LIGHTING - MID-CABIN CENTER-AISLE EXIT SIGN INSTALLATION. SERVICE BULLETIN RECOMMENDED MOS 27-JAN-2011 SB 737-33-1152 UGHTS - RETRACTABLE LANDING LIGHT - REPLACEMENT OF RETRACTABLE LANDING LIGHTS AND WIRE RECOMMENDED CONNECTORS. SERVICE BULLETIN MOS 29-AUG-201 I SB 737-33-1153 UGHTS - FLIGHT CREW LIGHTS - CAPTAINS AND FIRST OFFICERS UTILITY LIGHT LOCATION CHANGES. SERVICE RECOMMENDED BULLETIN MOS 13-OCT-2011 SB 737-34-1496 NAVIGATION-HEAD UP DISPLAY SYSTEM. SERVICE BULLETIN RECOMMENDED MOS 01 -JUL-1999 - (s) SB 737-34-1496 RI NAVIGATION-HEAD UP DISPLAY SYSTEM. SERVICE BULLETIN RECOMMENDED MOS 30-SEP-1999 - Is) SB 737-34-1503 FLIGHT MANAGEMENT COMPUTER SYSTEM SOFTWARE VERSION U10.3 UPDATE. SERVICE BULLETIN RECOMMENDED COMPLIED WITH-CM MOS 08-NOV-2000 27-JUL-2000 - (s) 74nsufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 88 Of 748 @ Camp Systems EFTA00618379 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-34-1503 RI I8-JAN-2001 SB 737-34-1522 03-JUN-1999 SB 737-34-1538 II -NOV-1999 SB 737-34-1539 27-JUL-2000 FLIGHT MANAGEMENT COMPUTER SYSTEM. SERVICE BULLETIN MOS - (s) FLIGHT MANAGEMENT COMPUTING - UPDATE SOFTWARE. SERVICE BULLETIN MOS I3-SEP-1999 - (s) FLIGHT MANAGEMENT COMPUTING-DUST COVER. SERVICE BULLETIN RECOMMENDED RECOMMENDED COMPUED WITH - CM RECOMMENDED MOS - COLLISION AVOIDANCE-TCAS WIRING CHANGE. SERVICE BULLETIN RECOMMENDED MOS - (s) SB 737-34-1540 27-JUL-I 999 ALTERNATE NAVIGATION SYSTEM. SERVICE BULLETIN MOS - (s) RECOMMENDED SB 737-34-1540 RI ALTERNATE NAVIGATION SYSTEM. SERVICE BULLETIN RECOMMENDED 23-SEP-I999 MOS - (s) SB 737-34-1540 R2 ALTERNATE NAVIGATION SYSTEM. SERVICE BULLETIN RECOMMENDED 07-DEC-2000 MOS - (s) SB 737-34-1545 R7 REPLACEMENT OF THE ROCKWELUCOLLINS TCAS COMPUTER, SERVICE BULLETIN RECOMMENDED 08-NOV-2001 MOS - (s) SB 737-34-1545 R8 REPLACEMENT OF THE ROCKWELUCOLLINS TCAS COMPUTER, SERVICE BULLETIN RECOMMENDED I4-FEB-2002 MOS SB 737-34-1545 R9 REPLACEMENT OF ROCKWELL/COLLINS TCAS COMPUTER, SERVICE BULLETIN RECOMMENDED 06-MAY-2004 MOS SB 737-34-1551 UPGRADE DATA LINK-NAVIGATION SYSTEM. SERVICE BULLETIN RECOMMENDED MOS 10-AUG-200O - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 89 Of 748 @ Camp Systems EFTA00618380 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-34-1551 RI 05-OCT-2000 UPGRADE DATA LINK-NAVIGATION SYSTEM. SERVICE BULLETIN MOS - Is) SB 737-34-1551 R2 UPGRADE DATA LINK-NAVIGATION SYSTEM. SERVICE BULLETIN MOS 07-DEC-2000 - (s) SB 737-34-1562 FLIGHT MANAGEMENT COMPUTING - UPGRADE SOFTWARE. SERVICE BULLETIN MOS 21-OCT-1999 - (s) SB 737-34-1566 FLIGHT MANAGEMENT COMPUTER-SOFTWARE CHANGE. SERVICE BULLETIN MOS 08-NOV-2000 03-AUG-2000 - (s) SB 737-34-1567 GROUND PROXIMITY WARNING SYSTEM. SERVICE BULLETIN MOS 20-APR-2000 - (s) SB 737-34-1572 FLIGHT MANAGEMENT COMPUTER SYSTEM. SERVICE BULLETIN MOS 09-NOV-2000 - (s) SB 737-34-1572 RI FLIGHT MANAGEMENT COMPUTER SYSTEM INSTALLATION OF HEADING REFERENCE SWITCH FOR POLAR NAVIGATION. SERVICE BULLETIN 25-JAN-2001 SB 737-34-1607 20-SEP-2001 SB 737-34-1616 MOS - Is) UPDATE FLIGHT MANAGEMENT COMPUTER SYSTEM. SERVICE BULLETIN MOS - Is) NAVIGATION - INDEPENDENT POSITION DETERMINING - ENHANCED GROUND PROXIMITY WARNING COMPUTER REPLACEMENT. SERVICE BULLETIN MOS I8-JAN-2001 - (s) SB 737-34-1634 RI INSTALLATION OF AN ALTERNATE NAVIGATION SYSTEM AND DATA LINK SERVICE BULLETIN MOS 15-NOV-2001 - (s) RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED COMPUED WITH -Cm RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 90 Of 748 @ Camp Systems EFTA00618381 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: O5-Aug-2O14 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-34-1650 06-FEB-2003 SB 737-34-1650 RI 27-FEB-2003 SB 737-34-1652 18-OCT-2001 SB 737-34-1656 23-MAY-2002 SB 737-34-1666 I I -APR-2002 SB 737-34-1672 I9-DEC-2002 SB 737-34-1720 I 7-APR-2003 SB 737-34-1721 03-APR-2003 SB 737-34-1762 R3 27-JAN-2005 NAVIGATION-FLIGHT MANAGEMENT COMPUTER (FMC) SYSTEM- UPDATE THE FMC SOFTWARE TO VERSION 10.5. RECOMMENDED SERVICE BULLETIN RECOMMENDED MOS UPDATE THE FMC SOFTWARE TO VERSION 10.5. SERVICE BULLETIN MOS SOFTWARE CHANGE TO ACTWATE FMCS AND DEU FEATURES.. SERVICE BULLETIN RECOMMENDED MOS - (s) FLIGHT MANAGEMENT COMPUTER SYSTEM. SERVICE BULLETIN RECOMMENDED MOS - (s) NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM - UPDATE THE FMC SOFTWARE TO VERSION 10.4A. RECOMMENDED SERVICE BULLETIN RECOMMENDED MOS - (s) INSTALL FMC OPC SOFTWARE FOR THE 'MISSED APPROACH ON MAP IN CYAN' OPTION. SERVICE BULLETIN MOS INTEGRATED STANDBY FLIGHT DISPLAY (ISFD) REPLACEMENT. SERVICE BULLETIN MOS RECOMMENDED AIR DATA INERTIAL REFERENCE SYSTEM (ADIRS)-WIRING CHANGE TO ACTIVATE 2005 MAGVAR TABLE. SERVICE RECOMMENDED BULLETIN MOS REPLACEMENT OF ATC TRANSPONDERS. AND ACTWATION OF ELEMENTARY SURVEILLANCE (ELS). ENHANCED RECOMMENDED SURVEILLANCE (EHS) AND EXTENDED SOUITTER (ES) PARAMETERS. SERVICE BULLETIN MOS SB 737-34-1768 NAVIGATION - FLIGHT MANAGEMENT COMPUTER (FMC) SYSTEM - UPDATE THE FMC SOFTWARE TO VERSION 10.6. SERVICE BULLETIN MOS I I -MAY-2006 I I -AUG-2005 2619:10 AFL 629 COMPLIED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 91 Of 748 @ Camp Systems EFTA00618382 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-34-1811 SB 737-34-1811 RI 05-OCT-2006 SB 737-34-1811 RI El 05-OC-1-2006 SB 737-34-1811 RI E3 OS-OCT-200G NAVIGATION - FLIGHT ENVIRONMENT DATA - PITOT STATIC PROBE BOND INSPECTION AND GROUNDING PLATE INSTALLATION. SERVICE BULLETIN MOS 24 (5) NAVIGATION - FLIGHT ENVIRONMENT DATA - PITOT STATIC PROBE BOND INSPECTION AND GROUNDING PLATE INSTALLATION. SERVICE BULLETIN MOS INSTALL NAVIGATION - FLIGHT ENVIRONMENT DATA - PITOT STATIC PROBE BOND INSPECTION AND GROUNDING PLATE INSTALLATION. SERVICE BULLETIN GROUND PLATE. STUD. AND JUMPER AS SHOWN IN WORK PACKAGE 1 OF THIS SERVICE BULLETIN. MOS 30 (5) REPLACE NAVIGATION - FLIGHT ENVIRONMENT DATA - PITOT STATIC PROBE BOND INSPECTION AND GROUNDING PLATE INSTALLATION. SERVICE BULLETIN THE NUTPLATES WITH CRES NUTPLATES AND SOLID ALUMINUM RIVETS AS SHOWN IN WORK PACKAGE 2 OF THIS SERVICE BULLETIN. MOS 60 (5) SB 737-34-1811EI 25-AUG-2005 MEASURE NAVIGATION - FLIGHT ENVIRONMENT DATA - PITOT STATIC PROBE BOND INSPECTION AND GROUNDING PLATE INSTALLATION. SERVICE BULLETIN PITOT PROBE RESISTANCE AS SHOWN IN WORK PACKAGE 1 MOS 18 (s) SB 737-34-1811E2 GENERAL VISUAL INSPECTION NAVIGATION - FLIGHT ENVIRONMENT DATA- PITOT STATIC PROBE BOND 25-AUG-2005 INSPECTION AND GROUNDING PLATE INSTALLATION. SERVICE BULLETIN OF THE PITOT PROBE MOUNTING PLATE NUTPLATES FOR PULL-TYPEA-IOLLOW RIVETS AND CORROSION ON THE FASTNER THREADS MD IN THE NUTPLATES. MOS 30 (5) SB 737-34-1811E3 INSTALL NAVIGATION - FLIGHT ENVIRONMENT DATA - PITOT STATIC PROBE BOND INSPECTION AND GROUNDING 25-AUG-2005 PLATE INSTALLATION. SERVICE BULLETIN GROUND PLATE. STUD AND JUMPER AS SHOWN IN WORK PACKAGE 3 MOS 30 (s) SB 737-34-1811E4 REPLACE NAVIGATION - FLIGHT ENVIRONMENT DATA - PITOT STATIC PROBE BOND INSPECTION AND GROUNDING 25-AUG-2005 PLATE INSTALLATION. SERVICE BULLETIN THE NUTPLATES WITH CRES NUTPLATES AND SOLID ALUMINUM RIVETS AS SHOWN IN WORK PACKAGE 4 MOS 72 (5) SB 737-34-1844 WIRING PROVISIONS FOR FUTURE ACTIVATION OF ELEMENTARY SURVEILLANCE. ENHANCED SURVEILLANCE AND RECOMMENDED 29-NOv-200.1 EXTENDED SOUITTER PARAMETERS. SERVICE BULLETIN MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CAV (EBT)-Estimated Base Time 92 Of 748 Camp Systems EFTA00618383 C O MP Mien winin Mernund up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-34-1875 22-SEP-2005 SB 737-34-1885 09-JUN-2005 NAVIGATION - INDEPENDENT POSITION DETERMINING - ENHANCED GROUND PROXIMITY WARNING SYSTEM COMPUTER CHANGE. SERVICE BULLETIN MOS ANTENNA WATER WICKING. SERVICE BULLETIN MOS RECOMMENDED SB SB 737-34-1918 27-MAR-2007 [SSN REDACTED] RI 14-MAR-2008 FLIGHT MANAGEMENT COMPUTER (FMC) SYSTEM - UPDATE THE FMC SOFTWARE TO VERSION 10.7. SERVICE BULLETIN MOS NAVIGATION- FLIGHT MANAGEMENT COMPUTER (FMC) SYSTEM - UPDATE THE FMC SOFTWARE TO VERSION 10.7. SERVICE BULLETIN MOS SB 737-34-2138 AIR DATA INERTIAL REFERENCE UNIT - STATIC SOURCE ERROR CORRECTION TABLE WIRING CHANGE SUPERSEDED (SUPERSEDED BY SB 737-34-2138 RI), SERVICE BULLETIN MOS SB 737-34-2138 RI NAVIGATION -AIR DATA INERTIAL REFERENCE UNIT - STATIC SOURCE ERROR CORRECTION TABLE WIRING CHANGE. RECOMMENDED 06-FEB-2014 SERVICE BULLETIN MOS SB 737-34-2155 NAVIGATION - HEAD-UP DISPLAY (HUD) SYSTEM - COMBINER MOUNTING BRACKET CHANGE (SUPERSEDED BY SB SUPERSEDED 737-34-2155 R1). SERVICE BULLETIN MOS SB 737-34-2155 RI NAVIGATION - HEAD-UP DISPLAY (HUD) SYSTEM - COMBINER MOUNTING BRACKET CHANGE. SERVICE BULLETIN RECOMMENDED 08-AUG-2011 MOS SB 737-34-2284 NAVIGATION- GROUND PROXIMITY WARNING SYSTEM - ENHANCED GROUND PROXIMITY WARNING SYSTEM SUPERSEDED ALTITUDE CALLOUTS MENU ID 23. SMART 500 CALLOUT. LOW VOLUME FOR ALTITUDE CALLOUTS. AND PEAKS AND OBSTACLES SELECTION CHANGE (SUPERSEDED BY SB 737-34-2284 R1). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 93 Of 748 @ Camp Systems EFTA00618384 C O MP Mien winin Mernund up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SS 737-34-2284 RI SB 737-34-2286 21 -JAN-2011 58 [SSN REDACTED] RI 27-JAN-2011 SB 737-34-2290 7-DEC-2010 SB 737-34-2293 10-DEC-2010 SB 737-34-2294 SB 737-34-2296 28-JAN-2011 NAVIGATION - GROUND PROXIMITY WARNING SYSTEM - ENHANCED GROUND PROXIMITY WARNING SYSTEM ALTITUDE CALLOUTS MENU ID 23. SMART 500 CALLOUT. LOW VOLUME FOR ALTITUDE CALLOUTS. AND PEAKS AND OBSTACLES SELECTION CHANGE (SUPERSEDED BY SB 737-34-2284 R2). SERVICE BULLETIN MOS SUPERSEDED NAVIGATION - GLOBAL POSITIONING SYSTEM - CHANGE AND DEACTIVATION OF CATEGORY I APPROACH CAPABILITY RECOMMENDED OF THE GLOBAL NAVIGATION SATELLITE SYSTEM LANDING SYSTEM. SERVICE BULLETIN MOS NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM- AUTOFLIGHT. RIGHT MANAGEMENT COMPUTER RECOMMENDED SYSTEM. COMMON DISPLAY SYSTEM. FUEL QUANTITY INDICATION SYSTEM - CHANGE OPTIONS. SERVICE BULLETIN MOS NAVIGATION - AUTOMATIC DIRECTION FINDER SYSTEM - INSTALLATION OF SECOND AUTOMATIC DIRECTION FINDER RECOMMENDED INTO EXISTING PROVISIONS. SERVICE BULLETIN MOS NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM - CHANGE OPERATION FROM FAA TO JAPJEASA FLIGHT RECOMMENDED RULES. SERVICE BULLETIN MOS NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM - CHANGE OPERATION FROM FAA TO JAA/EASA FLIGHT SUPERSEDED RULES (SUPERSEDED BY SB 737-34-2294 R1). SERVICE BULLETIN MOS NAVIGATION - AUTOMATIC DIRECTION FINDER SYSTEM - INSTALLATION OF SECOND AUTOMATIC DIRECTION FINDER RECOMMENDED INTO EXISTING PROVISIONS. SERVICE BULLETIN MOS SB 737-34-2297 NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM - CHANGE OPERATION FROM FEDERAL AVIATION RECOMMENDED ADMINISTRATION TO JOINT AVIATION AUTHORITIES/EUROPEAN AVIATION SAFETY AGENCY FLIGHT RULES. SERVICE BULLETIN 20-JAN-2011 SB 737-34-2298 04-JAN-2011 MOS NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM - CHANGE FROM JOINT AVIATION AUTHORITIES TO RECOMMENDED FEDERAL AVIATION ADMINISTRATION FLIGHT RULES AND DUAL AIRPLANE FLIGHT MANUAL FORMAT SERVICE BULLETIN. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 94 Of 748 @ Camp Systems EFTA00618385 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SS 737-34-2300 27-JAN-2011 NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM - CHANGE OPERATION FROM JOINT AVIATION AUTHORITIES/EUROPEAN AVIATION SAFETY AGENCY TO FEDERAL AVIATION ADMINISTRATION FLIGHT RULES (SUPERSEDED BY SB 737-34-2300 RI). SERVICE BULLETIN MOS RECOMMENDED SS 737-34-2327 NAVIGATION - FLIGHT MANAGEMENT COMPUTING - DIP SWITCH POSITION CHANGE. SERVICE BULLETIN RECOMMENDED MOS 05-DEC-2011 SS 737-34-2384 NAVIGATION - WEATHER RADAR SYSTEM - INSPECTION AND REPLACEMENT OF WEATHER RADAR ANTENNA WIRE RECOMMENDED BUNDLE W8489. SERVICE BULLETIN MOS 27-NOV-2012 SS 737-34-2395 NAVIGATION- LOW RANGE RADIO ALTIMETER - INSTALLATION OF THE ANTENNA GASKETS (SUPERSEDED BY SB SUPERSEDED 737-34-2395 RI). SERVICE BULLETIN MOS SS 737-34-2395 RI NAVIGATION- LOW RANGE RADIO ALTIMETER - INSTALLATION OF THE ANTENNA GASKETS. SERVICE BULLETIN RECOMMENDED MOS 17-OCT-2013 SS 737-34-2413 NAVIGATION- STANDBY ATTITUDE REFERENCE SYSTEM - INTEGRATED STANDBY FLIGHT DISPLAY BACK COURSE RECOMMENDED PROGRAM PIN CHANGE. SERVICE BULLETIN MOS I0-OCT-2012 SS 737-34-2432 NAVIGATION- GROUND PROXIMITY WARNING SYSTEM - INTEGRATED AREA NAVIGATION TURNED OFF BY WIRING RECOMMENDED CHANGE. SERVICE BULLETIN MOS 28-NOV-20I2 SB 737-34-2454 NAVIGATION- AIR DATA SYSTEM - ALTIMETRY SYSTEM TEST. SERVICE BULLETIN MOS SS 737-34-2461 NAVIGATION- ATC SYSTEM- ROCKWELL COLLINS AIR TRAFFIC CONTROL TRANSPONDER REPLACEMENT. SERVICE RECOMMENDED BULLETIN MOS 17-MAY-2013 SS 737-34A1502 FLIGHT MANAGEMENT COMPUTER SYSTEM (SUPERSEDED BY SB 737-34A1502 RI). SERVICE BULLETIN SUPERSEDED MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 95 Of 748 @ Camp Systems EFTA00618386 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB SB 737-34A1502 RI 20-MAY-1999 737-34A1801 FLIGHT MANAGEMENT COMPUTER SYSTEM. SERVICE BULLETIN MOS - (s) CHANGE THE OPERATIONAL PROGRAM SOFTWARE TO VERSION 10.5A. SERVICE BULLETIN RECOMMENDED COMPUED WITH DAYS 1 1 -MAY-2006 15-JUL-2004 2619:10 AFL 629 SB 737-34A2104 FLIGHT MANAGEMENT COMPUTER SYSTEM - RIGHT MANAGEMENT COMPUTER OPERATIONAL PROGRAM SUPERSEDED - INFO: THIS SOFTWARE WAS SUPERSEDED BY SOFTWARE U10.8 INSTALLATION (SUSPENDED BY 737-34A2104 N1). SERVICE BULLETIN U10.8A SOFTWARE WHICH WAS RECENTLY INSTALLED. MOS SB 737-34A2216 NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM - FLIGHT MANAGEMENT COMPUTER OPERATIONAL SUPERSEDED PROGRAM SOFTWARE U10.8A SOFTWARE INSTALLATION (SUPERSEDED BY SB 737-34A2216 R1). SERVICE BULLETIN MOS SB 737-34A2216 RI NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM - FLIGHT MANAGEMENT COMPUTER OPERATIONAL RECOMMENDED COMPUED WITH PROGRAM SOFTWARE U10.8A SOFTWARE INSTALLATION . SERVICE BULLETIN MOS 16-MAY-2012 09-JUN-2010 3634:25 AFL 882 SB 737-34A2292 NAVIGATION - ENHANCED GROUND PROXIMITY WARNING SYSTEM - AIR SPEED LOW ALERT CHANGES. SERVICE RECOMMENDED BULLETIN MOS 12 (s) 27-APR-20I2 SB 737-35-1049 PURITAN-BENETT OXYGEN MASKS. SERVICE BULLETIN NOT APPLICABLE - BY EFFECTIVITY MOS 06-JAN-2007 - (s) SB 737-35-1077 OXYGEN GENERATOR FIRING PIN LOCATION. SERVICE BULLETIN RECOMMENDED DAYS 90 (s) 01-MAR-2001 SB 737-35-1080 OXYGEN - FLIGHT CREW OXYGEN SYSTEM - INSTALLATION OF HOSE SEPARATION SUPPORT FOR REMOTE FILL RECOMMENDED NOT APPLICABLE TUBING. SERVICE BULLETIN MOS 07-JUL-2005 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 96 Of 748 @ Camp Systems EFTA00618387 C O MP Atiant.fran Ad-own/lop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB SB 737-35-1107 04-JAN-2008 737-35A1058 OXYGEN - PASSENGER OXYGEN SYSTEM - CHANGE 22 MINUTE OXYGEN GENERATOR RETENTION IN THE PASSENGER SERVICE UNITS. SERVICE BULLETIN MOS 60 (s) CREW OXYGEN - HOSE REPLACEMENT (SUPERSEDED BY SB 737-35A1058 RI ). SERVICE BULLETIN MOS - (s) SUPERSEDED SB 737-35A1058 RI CREW OXYGEN - HOSE REPLACEMENT (SUPERSEDED BY SB 737-35A1058 R2). SERVICE BULLETIN SUPERSEDED COMPUED WITH - AND REPLACED PARTS I.A.W. AD 2010-16-06 MOS 27-AUG-2010 - (s) 3448:31 AFL 841 SB 737-35A1058 R2 OXYGEN - CREW OXYGEN - CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE REPLACEMENT. SERVICE BULLETIN RECOMMENDED COMPUED WITH - DURING COMPLIED WITH 737-35A1058 RI REPLACED PILOT a CO PILOT FLEX HOSES BY PM 60850059-618. REPLACED FIRST OBSERVER FLEX HOSE BY P/N 60850056-614 NO MORE ACTION REQUIRED MOS 21-FEB-2013 09-SEP-2010 3702:13 AFL 897 SB 737-35A1121 CREW OXYGEN MASK STOWAGE BOX UNIT -INSPECT/REPLACE (SUPERSEDED BY SB 737-35A1121 R1). SERVICE SUPERSEDED BULLETIN MOS (EFF) SB 737-35A1121 Ft1 OXYGEN - CREW OXYGEN SYSTEM - CREW OXYGEN MASK STOWAGE BOX UNIT - INSPECT/REPLACE. SERVICE RECOMMENDED NOT APPLICABLE - DUE TO VARIABLE NUMBER BULLETIN OF THE A/C YG006 MOS 19-JAN-2012 I4-DEC-2009 3609:52 AFL 879 SB 737-35A1126 CREW AND PASSENGER GASEOUS OXYGEN SYSTEMS - OXYGEN CYLINDER RECOMMENDED NOT APPLICABLE - BY SERIAL NUMBER INSPECTION/REPLACEMENT. SERVICE BULLETIN INSTALLED DAYS I6-FEB-2010 29-OCT-2009 3417:51 AFL 829 SB 737-36-1019 ENGINE BLEED AIR DISTRIBUTION SYSTEM - CLAMP INSTALLATION ON ENGINE RECOMMENDED SENSE TUBES FOR THE PNEUMATIC SYSTEM FLEX LINES. SERVICE BULLETIN MOS 14-SEP-2009 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 97 Of 748 @ Camp Systems EFTA00618388 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-36-1019 RI 16-FEB-2010 SB 737-36-1020 CLAMP INSTALLATION ON ENGINE SENSE TUBES FOR THE PNEUMATIC SYSTEM FLEX LINES. SERVICE BULLETIN RECOMMENDED MOS DISTRIBUTION- PNEUMATIC MANIFOLD SYSTEM - REPLACEMENT OF AUXILIARY POWER UNIT PNEUMATIC DUCTS. RECOMMENDED SERVICE BULLETIN 27-JAN-2011 MOS SB 737-36-1021 PNEUMATIC - BLEED AIR PRECOOLER SYSTEM- CHANGE TO THE AIRCRAFT CONDITION MONITORING SYSTEM TO SUPERSEDED GIVE MORE INPUTS TO THE DIGITAL FLIGHT DATA ACQUISITION UNIT FOR EASIER ENVIRONMENTAL CONTROL SYSTEM TROUBLESHOOTING (SUPERSEDED BY S8 [SSN REDACTED] R1). SERVICE BULLETIN MOS SB 737-36-1021 RI PNEUMATIC - BLEED AIR PRECOOLER SYSTEM- CHANGE TO THE AIRCRAFT CONDITION MONITORING SYSTEM TO SUPERSEDED GIVE MORE INPUTS TO THE DIGITAL FLIGHT DATA ACQUISITION UNIT FOR EASIER ENVIRONMENTAL CONTROL SYSTEM TROUBLESHOOTING (SUPERSEDED BY SB 737-36-1021 R2). SERVICE BULLETIN MOS SB 737-36-1021 R2 PNEUMATIC - BLEED AIR PRECOOLER SYSTEM - CHANGE TO THE AIRCRAFT CONDITION MONITORING SYSTEM TO SUPERSEDED GIVE MORE INPUTS TO THE DIGITAL FLIGHT DATA ACQUISITION UNIT FOR EASIER ENVIRONMENTAL CONTROL SYSTEM TROUBLESHOOTING (SUPERSEDED BY SEI 737-36-1021 R3). SERVICE BULLETIN MOS SB 737-36-1021 R3 PNEUMATIC - BLEED AIR PRECOOLER SYSTEM - CHANGE TO THE AIRCRAFT CONDITION MONITORING SYSTEM TO RECOMMENDED GIVE MORE INPUTS TO THE DIGITAL FLIGHT DATA ACQUISITION UNIT FOR EASIER ENVIRONMENTAL CONTROL SYSTEM TROUBLESHOOTING. SERVICE BULLETIN MOS 03-OCT-2013 SB 737-38-1046 POTABLE WATER - ADDITION OF INSULATION TO THE WATER SUPPLY LINES. SERVICE BULLETIN MOS 07-MAR-2002 - (s) SB 737-38-1048 WATERAMASTE-WASTE DISPOSAL-DRAIN MAST-INSPECTION FOR FATIGUE CRACKS/REPLACEMENT OF A CRACKED RECOMMENDED - SUPERSEDED BY S/B [SSN REDACTED] FORWARD DRAIN MAST ASSEMBLY (REPLACED BY 737-38-1053). SERVICE BULLETIN MOS I6-JAN-2003 SOO (s) SB 737-38-1048 RI WATER/WASTE - WASTE DISPOSAL - DRAIN MAST - INSPECTION FOR FATIGUE CRACKS/REPLACEMENT OF A SUPERSEDED CRACKED FORWARD DRAIN MAST ASSEMBLY (SUPERSEDED BY 737-38-1053). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 98 Of 748 @ Camp Systems EFTA00618389 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-38-1053 15-SEP-2005 WATERIWASTE - WASTE DISPOSAL - DRAIN MAST - INSPECTION FOR FATIGUE CRACKS/REPLACEMENT OF A CRACKED FORWARD DRAIN MAST ASSEMBLY. SERVICE BULLETIN MOS 560 (s) SB 737-38-1053 RI WASTE DISPOSAL - DRAIN MAST - INSPECTION FOR FATIGUE 14-SEP-2009 RECOMMENDED CRACKS/REPLACEMENT OF A CRACKED FORWARD DRAIN MAST ASSEMBLY. SERVICE BULLETIN MOS SB 737-38-1053 R1.1 GENERAL VISUAL INSPECTION WASTE DISPOSAL- DRAIN MAST - INSPECTION FOR FATIGUE RECOMMENDED CRACKS/REPLACEMENT OF A CRACKED FORWARD DRAIN MAST ASSEMBLY. SERVICE BULLETIN OF THE FORWARD DRAIN MAST ASSEMBLY MOS 14-SEP-2009 500 (s) SB 737-38-1053 RI .2 REPLACE WASTE DISPOSAL - DRAIN MAST - INSPECTION FOR FATIGUE RECOMMENDED CRACKS/REPLACEMENT OF A CRACKED FORWARD DRAIN MAST ASSEMBLY. SERVICE BULLETIN WITH ALUMINUM DRAIN MAST ASSEMBLY 14-SEP-2009 SB 737-38-1057 19-FEB-2010 MOS 60 (s) POTABLE WATER - PASSENGER WATER SYSTEM - HOSE AND FITTING REPLACEMENT. FITTING HEATER AND RECOMMENDED SHROUD INSTALLATION. SERVICE BULLETIN MOS SB 737-44-1001 CABIN SYSTEMS - INFLIGHT ENTERTAINMENT SYSTEM - INSTALLATION OF LATCH PLATES ON THE AFT AUDIO DISTRIBUTION BOX. SERVICE BULLETIN MOS 07-JUN-2010 SB 737-44-1006 03-JUL-2013 SB 737-04-1007 03-DEC-2013 SB 737-06-1009 08-JAN-2009 CABIN SYSTEMS - PASSENGER AUDIONIDEO ENTERTAINMENT SYSTEM - IN-FLIGHT ENTERTAINMENT SYSTEM AUDIO RECOMMENDED HUM NOISE CORRECTIVE WIRING CHANGES. SERVICE BULLETIN MOS CABIN SYSTEMS- CREW PANELS - GROMMET INSTALLATION FOR IN-FLIGHT ENTERTAINMENT SYSTEM CONTROL RECOMMENDED PANEL STOWAGE BOX. SERVICE BULLETIN MOS CREW INFORMATION SYSTEM - ELECTRONIC FLIGHT BAG HARDWARE AND SOFTWARE REPLACEMENT. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 99 Of 748 @ Camp Systems EFTA00618390 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YO006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 73746-1011 20-OCT-2010 SB 737-46-1013 INFORMATION SYSTEMS - CREW INFORMATION SYSTEM - ELECTRONIC FLIGHT BAG HARDWARE AND SOFTWARE RECOMMENDED REPLACEMENT. SERVICE BULLETIN MOS INFORMATION SYSTEMS - CREW INFORMATION SYSTEM - ELECTRONIC FLIGHT BAG SOFTWARE REPLACEMENT. RECOMMENDED SERVICE BULLETIN 29-NOv-2012 MOS SB 73747-1002 INERT GAS SYSTEM - INSTALLATION OF THE PROVISIONS FOR NITROGEN GENERATION SYSTEM (SUPERSEDED BY SUPERSEDED SB 73747-1002 RI). SERVICE BULLETIN MOS SB 73747-1002 RI INERT GAS SYSTEM - INSTALLATION OF THE PROVISIONS FOR NITROGEN GENERATION SYSTEM (SUPERSEDED BY SUPERSEDED SB 73747-1002 R2). SERVICE BULLETIN MOS SB 73747-1002 R2 INERT GAS SYSTEM - INSTALLATION OF THE PROVISIONS FOR NITROGEN GENERATION SYSTEM. SERVICE BULLETIN RECOMMENDED 14-NOv-2013 MOS SB 73747-1003 INERT GAS SYSTEM - INSTALLATION OF THE NITROGEN GENERATION SYSTEM (SUPERSEDED BY SB 73747-1003 RN. SUPERSEDED SERVICE BULLETIN MOS SB 73747-1003 RI INERT GAS SYSTEM - INSTALLATION OF THE NITROGEN GENERATION SYSTEM (SUPERSEDED BY SB 73747-1003 R2). SUPERSEDED SERVICE BULLETIN MOS SB 73747-1003 R2 INERT GAS SYSTEM - INSTALLATION OF THE NITROGEN GENERATION SYSTEM. SERVICE BULLETIN RECOMMENDED 27-SEP-2013 MOS SB 73747-10as NITROGEN GENERATION SYSTEM - INSTALLATION OF OXYGEN SENSOR. REPLACEMENT OF EQUIPMENT AND WIRE RECOMMENDED BUNDLES. SERVICE BULLETIN MOS 02-FEB-2010 SB 73747-1011 INERT GAS SYSTEM - AIR SEPARATION UNIT - AIR SEPARATION MODULE HIGH FLOW VALVE CONNECTOR RECOMMENDED REPLACEMENT. SERVICE BULLETIN MOS 14-OCT.20 1 u ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 100 Of 748 Camp Systems EFTA00618391 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-07-1012 INERT GAS SYSTEM - AIR SEPARATION UNIT - INSPECTION OF TUBES AND CLAMP INSTALLATION. SERVICE BULLETIN RECOMMENDED MOS 12-APR-2012 SB 737-09-1119 APU - ELECTRONIC CONTROL UNIT. SERVICE BULLETIN 10-JUN-1999 MOS - (s) SB 737-09-1133 AIRBORNE AUXILIARY POWER- AUXILARY POWER UNIT AIR INLET - AUXILARY POWER UNIT FLAP AND VORTEX GENERATOR ASSEMBLY MOSIFICATION. SERVICE BULLETIN MOS 22-SEP-2005 SB 737-09-1133 RI 21-SEP-2007 SB 737-09-1133 R2 26-JAN-2009 SB 737-09-1130 16-OCT-2007 MOS SB 737-09-1139 AIRBORNE AUXILIARY POWER - COWL DOOR INSULATION PANEL AND AFT BULKHEAD SEAL REPLACEMENT SUPERSEDED (SUPERSEDED BY S8 [SSN REDACTED] RI). SERVICE BULLETIN MOS SB 737-09-1139 RI AIRBORNE AUXILIARY POWER -COWL DOOR INSULATION PANEL AND AFT BULKHEAD SEAL REPLACEMENT. SERVICE RECOMMENDED 04-OCT-2012 BULLETIN MOS SB 737-51-1017 RI EVES MOISTURE SHROUD SEAL INSTALLATION, SERVICE BULLETIN RECOMMENDED 28-MAR-2002 MOS SB 737-51-1018 CARGO DOORWAY STOP PAD REPLACEMENT. SERVICE BULLETIN RECOMMENDED AIRBORNE AUXILIARY POWER - AUXILIARY POWER UNIT AIR INLET - AUXILIARY POWER UNIT FLAP AND VORTEX GENERATOR ASSEMBLY MODIFICATION. SERVICE BULLETIN MOS AUXILIARY POWER UNIT FLAP AND VORTEX GENERATOR ASSEMBLY MODIFICATION. SERVICE BULLETIN MOS AIRBORNE AUXILIARY POWER - APU AIR INLET - INLET PLENUM REPLACEMENT. SERVICE BULLETIN RECOMMENDED I I -APR-2002 MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 101 Of 748 @ Camp Systems EFTA00618392 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-51-1019 25-APR-2002 STRUCTURES - WIRE SHIELD ASSEMBLY INSTALLATION UNDER THE E5-2 SHELF. SERVICE BULLETIN MOS SB 737-51-1019 RI STRUCTURES - WIRE SHIELD ASSEMBLY INSTALLATION UNDER THE E5-2 SHELF. SERVICE BULLETIN MOS 18-DEC-2003 SB 737-52-1136 EMERGENCY EXIT. SERVICE BULLETIN MOS 22-JUN-2000 - (s) SB 737-52-1137 DOORS - CONTROL CABIN EMERGENCY EXIT PANEL. SERVICE BULLETIN MOS - (s) SB 737-52-1138 ELECTRONIC EQUIPMENT ACCESS DOOR, SERVICE BULLETIN MOS 29-JUL-1999 - (s) SB 737-52-1140 FORWARD ENTRY - UPPER AFT CORNER DOOR STOP REPLACEMENT. SERVICE BULLETIN MOS 20-AUG-2001 RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED AFL 18000 (s) SB 737-52-1142 AFT GALLEY SERVICE DOOR, SERVICE BULLETIN RECOMMENDED MOS 4 (s) 22-FEB-2001 SB 737-52-1148 HORIZONTAL AIRSTAIRS MOISTURE SHROUD INSTALATION SUPPORT RAIL REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 12-DEC-2002 SB 737-52-1148 RI FUSELAGE - HORIZONTAL AIRSTAIRS MOISTURE SHROUD INSTALLATION - SUPPORT RAIL REPLACEMENT. SERVICE BULLETIN MOS 11-MAY-2006 SB 737-52-1152 DOORS - FORWARD AIRSTAIR DOOR RELIABILITY IMPROVEMENT - REPLACE DOOR LOCKPIN ACTUATORS. OPEN UMITAMARNING SWITCH BRACKETS. AND RACEWAY COVER ASSEMBLY. SERVICE BULLETIN MOS 08-SEP-2005 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 102 Of 748 @ Camp Systems EFTA00618393 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YO006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-52-1156 01-DEC-2005 DOORS - FORWARD AIRSTAIR AND DOOR - FORWARD AIRSTAIR SPEEDUP AND SLOWDOWN SYSTEM DELETION. SERVICE BULLETIN MOS SB 737-52-1157 ENTRANCE STAIRS - FORWARD AIRSTAIR - AIRSTAIR HANDRAIL SAFETY IMPROVEMENTS (SUPERSEDED BY SB SUPERSEDED 737-52-1157 RI). SERVICE BULLETIN MOS SB 737-52-1157 RI DOORS - ENTRANCE STAIRS - FORWARD AIRSTAIR AIRSTAIR HANDRAIL SAFETY IMPROVEMENTS. SERVICE BULLETIN SB 737-52-1159 26-NOV-2C07 SB 737-52-1159 RI 21-SEP-2009 SB 737-52-1164 20-JAN-2009 SB 737-52-1165 29-JUL-2008 SB 737-52-1165 RI 15-JAN-2009 SB 737-52-1169 13-DEC-201 I MOS DOORS - DOOR WARNING SYSTEM - FORWARD ENTRY DOOR LATCH SWITCH AND WIRING INSTALLATION AND MODIFICATION. SERVICE BULLETIN MOS DOOR WARNING SYSTEM - FORWARD ENTRY DOOR LATCH SWITCH AND WIRING INSTALLATION AND MODIFICATION. SERVICE BULLETIN MOS FORWARD AND AFT CARGO DOORS - LANYARD ASSEMBLY REPLACEMENT. SERVICE BULLETIN MOS AFT ENTRY AND AFT GALLEY SERVICE DOOR - DOOR SNUBBER STOP LINK ASSEMBLY CHANGE. SERVICE BULLETIN MOS AFT ENTRY AND AFT GALLEY SERVICE DOOR - DOOR SNUBBER STOP LINK ASSEMBLY CHANGE. SERVICE BULLETIN MOS DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. SERVICE BULLETIN MOS RECOMMENDED SB 737-52-1169 TABLE 1 PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED SERVICE BULLETIN A GENERAL VISUAL INSPECTION OF THE INBOARD MLG DOOR FOR IDENTIFICATION MOS 13-DEC-2011 AFL 51)03(s1 ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 103 Of 748 Camp Systems EFTA00618394 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YO006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-52-1169 TABLE 2.1L 13-DEC-2011 PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED SERVICE BULLETIN A DETAILED INSPECTION OF THE LEFT INBOARD MLG DOOR FOR ANY CRACKS MOS AFL 5500(s) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.1R SERVICE BULLETIN A DETAILED INSPECTION OF THE RIGHT INBOARD MLG DOOR FOR ANY CRACKS MOS 13-DEC-2011 AFL 5500 (5) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.2L SERVICE BULLETIN APPLICABLE SRM REPAIR WITHIN THE ALLOWABLE DAMAGE 1 LIMITS ( ANY PART-THROUGH CRACK IS FOUND.) LEFT MLG INBOARD DOOR MOS BF,'F (5) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.2R SERVICE BULLETIN APPLICABLE SRM REPAIR WITHIN THE ALLOWABLE DAMAGE I LIMITS ( ANY PART-THROUGH CRACK IS FOUND.) RIGHT MLG INBOARD DOOR MOS BF,F (so SB 737-52-1169 TABLE REPLACE DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.3L SERVICE BULLETIN THE LEFT INBOARD MLG DOOR AND PREFORM A DETAILED INSPECTION OF THE INBOARD MLG DOOR FOR ANY CRACKS MOS BF,F (so SB 737-52-1169 TABLE REPLACE DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.3R SERVICE BULLETIN THE RIGHT INBOARD MLG DOOR AND PREFORM A DETAILED INSPECTION OF THE INBOARD MLG DOOR FOR ANY CRACKS MOS BF,F (so SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.1L SERVICE BULLETIN A DETAILED INSPECTION OF THE LEFT INBOARD MLG DOOR FOR ANY CRACKS MOS 13-DEC-2011 AFL 5503 (5) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.1R SERVICE BULLETIN A DETAILED INSPECTION OF THE RIGHT INBOARD MLG DOOR FOR ANY CRACKS MOS 31-DEC-2011 AFL 5503 (5) ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 104 Of 748 Camp Systems EFTA00618395 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.2L SERVICE BULLETIN APPLICABLE SRM REPAIR WITHIN THE ALLOWABLE DAMAGE 1 LIMITS AND DETAILED INSPECTION OF THE LEFT INBOARD MLG DOOR MOS BFIF (s) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.2R SERVICE BULLETIN APPLICABLE SRM REPAIR WITHIN THE ALLOWABLE DAMAGE 1 LIMITS AND DETAILED INSPECTION OF THE RIGHT INBOARD MLG DOOR MOS BF/F (s) SB 737-52-1169 TABLE REPLACE DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.3L SERVICE BULLETIN THE LEFT INBOARD MLG DOOR DOOR WITH INBOARD MLG DOOR MADE FROM MACHINED ALUMINUM. 113A8335-( ). OR INBOARD MLG DOOR MADE FROM CAST ALUMINUM. 113A8331-( ). AND DETAILED INSPECTION MOS BFIF (s) SB 737-52-1169 TABLE REPLACE DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.3R SERVICE BULLETIN THE RIGHT INBOARD MLG DOOR DOOR WITH INBOARD MLG DOOR MADE FROM MACHINED ALUMINUM. 113A8335-( ). OR INBOARD MLG DOOR MADE FROM CAST ALUMINUM. 113A8331- ). AND DETAILED INSPECTION SB 737-52-1170 29-JUL-2014 MOS BFIF (s) DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN MOS SB 737-52-1170 T84. 1.1 DETAILED INSPECTION DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR RECOMMENDED AND MODIFICATION. SERVICE BULLETIN OF MLG CENTER DOOR ASSEMBLY ATTACHMENTS (PART 2) FOR ANY LOOSE. MISSING. DAMAGED OR BOTTOMED OUT BOLTS. OR ANY WEAR TO THE RETENTION CLIP ASSEMBLIES. OR IF RETENTION CLIP ASSEMBLIES ARE NOT INSTALLED. FOR ANY LOOSE. MISSING OR DAMAGED BOLTS (ALL AIRPLANES) MOS AFL 12000 (s) SB 737-52-1170 TB1 1.2 DO DOORS -LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN PART 4: MLG CENTER DOOR ASSEMBLY ATTACHMENTS - REMOVAL! PART 5: MLG CENTER DOOR ASSEMBLY RETENTION CLIP ASSEMBLIES - MODIFICATION f REPEAT PART -2 (IF CONDITION 1: NO LOOSE. MISSING. DAMAGED OR BOTTOMED OUT BOLTS AND NO WEAR TO THE RETENTION CLIP ASSEMBLIES) MOS 29-JUL-2014 BFIF 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 105 Of 748 @ Camp Systems EFTA00618396 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2O14 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-52-1170 TBL 1.3 DO DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN PART 3 MLG CENTER DOOR ASSEMBLY ATTACHMENTS - REMOVAL AND BUSHING DETAILED INSPECTION MEASUREMENT FOR EXCESSIVE WEAR. GALLING AND CRACKS (IF CONDITION 2: ANY LOOSE. MISSING. DAMAGED OR BOTTOMED OUT BOLTS. OR ANY WEAR TO THE RETENTION CLIP ASSEMBLIES) MOS 29-JUL-2014 BPIF SB 737-52-1170 TBL 1.4 DO DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN PART 7: BUSHING REMOVAL/ REPAIR. LUG MAGNETIC PARTICLE INSPECTION' REPAIR PART 5: MLG CENTER DOOR ASSEMBLY RETENTION CLIP ASSEMBLIES - MODIFICATION PART 7: BUSHING REMOVAL] REPAIR. LUG MAGNETIC PARTICLE INSPECTION' REPAIR PART 6: MLG CENTER DOOR ASSEMBLY BOLTS AND RETENTION CLIP ASSEMBLIES - REPLACEMENT REPEAT PART 2 (IF CONDITION 3: ANY EXCESSIVE WEAR FOUND IN THE INTERNAL DIAMETER OF THE BUSHING OR ANY GALLING FOUND OR ANY CRACK FOUND) MOS 29-JUL-2014 BPIF SB 737-52-1170 TBL 1.5 DO DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN PART 5 MLG CENTER DOOR RETENTION CLIP ASSEMBLIES - MODIFICATION / PART 6: MLG CENTER DOOR ASSEMBLY BOLTS AND RETENTION CLIP ASSEMBLIES - REPLACEMENT I REPEAT PART 2 (IF CONDITION 4: NO EXCESSIVE WEAR FOUND IN THE INTERNAL DIAMETER OF THE BUSHING AND NO GALLING AND NO CRACKS FOUND) MOS 29-JUL-2014 BF.'F SB 737-52-1173 FORWARD AIRSTAIR - STAIR TREAD - ANTI-SLIP MATERIAL EDGE SEAL MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 24-JUN-201•I • (s) SB 737-52A1167 DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOOR HINGE FITTINGS - INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS (EFF) 01-DEC-201I SB 737-52A1167 TABLE 1 PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOOR HINGE FITTINGS - INSPECTION RECOMMENDED LMLG AND REPLACEMENT. SERVICE BULLETIN DETAILED INSPECTION OR HFEC INSPECTION OF THE LEFT INBOARD MLG DOOR HINGE FITTINGS FOR CRACKS FOR AIRPLANES MOS AFL 1C000 10000 SB 737-52A1167 TABLE 1 PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOOR HINGE FITTINGS INSPECTION RECOMMENDED RMLG AND REPLACEMENT. SERVICE BULLETIN DETAILED INSPECTION OR SURFACE HFEC INSPECTION OF THE RIGHT INBOARD MLG DOOR HINGE FITTINGS FOR CRACKS MOS AFL 1C000 10000 ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 106 Of 748 Camp Systems EFTA00618397 CAMP MionistAlmthermumlitli AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1217 SECTION 43 AND SECTION 47 - STIR 17 SKIN CRACKS AT STA 364-371 AND STA 890-900. SERVICE BULLETIN MOS 09-AUG-2001 RECOMMENDED AFL 36000 (s) SS 737-53-1219 FUSELAGE SECTION 44- S18A WEB FITTING FLANGE CRACKS. INSPECTION AND REPAIR, SERVICE BULLETIN RECOMMENDED MOS I6-AUG-2001 AFL 30000 30000 SS 737-53-1222 FUSELAGE - SECTION 41 CAB - POINT D SPLICE FITTING REPLACEMENT (SUPERSEDED BY 737-53A1222 R1). SERVICE SUPERSEDED BULLETIN MOS 06-JUN-2002 SS 737-53-1223 29-NOV-2001 SS 737-53-1227 03-OCT-2002 SS 737-53-1227 RI 26-AUG-2006 SS 737-53-1227 R2 MAIN LANDING GEAR FAIRING REPLACEMENT. SERVICE BULLETIN MOS - Is) NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS - (s) NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS FUSELAGE - WHEEL WELLS - NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS 22-AUG-2008 Id-NOV-2007 3260:48 RECOMMENDED RECERTIFY - INFORMATION REF TO R2 - INFORMATION REF TO R2 COMPUED WITH - TERMINATED AFL 782 SB 737-53-1227 R2 PARA REPLACE FUSELAGE - WHEEL WELLS - NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACE COMPUED WITH - REPLACEMENT 0 REPLACEMENT. SERVICE BULLETIN BUSHINGS MOS 22-AUG-2008 Id-NOV-2007 3260:48 AFL 782 SS 737-53-1227 R2 PARA INSPECT FUSELAGE - WHEEL WELLS - NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING COMPUED WITH - MIGRATION FOUND / E REPLACEMENT. SERVICE BULLETIN REPLACEMENT PERFORMED TERMINATING ACTION MOS 22-AUG-2008 3260:48 AFL 782 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 107 Of 748 @ Camp Systems EFTA00618398 CAMP Mianistfrn• thermiewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1227 R3 18-NOV-2009 SB 737-53-1227 R3 PARA DETAILED INSPECTION NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN E (DT INS) FOR CORROSION OF THE FITTINGS MOS 3 (s) NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS RECOMMENDED SB 737-53-1227 R3 PARA INITIAL INSPECTION NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN RECOMMENDED E (I INSP) MOS 18-NOV-2009 AFL 2000(s) SB 737-53-1227 R3 PARA REPLACE NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN BUSHING REPLACE E (RPL) 18-NOV-2009 SB 737-53-1232 SB 737-53-1232 RI SB 737-53-1232 RI TABLE SB 737-53-1232 R2 26-JUL-2013 SB 737-53-1232 R2 TABLE MOS 12 (s) FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTATIVE MODIFICATION (SUPERSEDED BY 737-53-1232 R1). SERVICE BULLETIN MOS SUPERSEDED FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTATIVE MODIFICATION SUPERSEDED (SUPERSEDED BY SB 737-53-1232 R2). SERVICE BULLETIN MOS DETAILED INSPECTION FUSELAGE - SKIN - CHEMICALLY MILLED STEPS- INSPECTION. REPAIR AND PREVENTATIVE RECOMMENDED MODIFICATION (SUPERSEDED BY SB 737-53-1232 R2). SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKS IN THE FUSELAGE SKIN AT THE CHEM-MILLED STEPS AT SPECIFIED LOCATIONS MOS AFL 35000 35000 FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE RECOMMENDED BULLETIN MOS EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND 1.01 PREVENTIVE MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NDI (EXT.MFECMCWC-SCAN/EXT.UTPA) FOR CRACKS IN THE FUSELAGE SKIN AT THE CHEM-MILLED STEPS AT SPECIFIED LOCATIONS (FOR AIRPLANES WITHOUT THE PREVENTATIVE MODIFICATION. TIME-LIMITED REPAIR OR PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 108 Of 748 @ Camp Systems EFTA00618399 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 [SSN REDACTED] R2 TABLE REPAIR FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 1.02 SERVICE BULLETIN ANY CRACK THAT IS FOUND IN THE SKIN MOS SB 737-53-1232 R2 TABLE INSPECT FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 1A.01 SERVICE BULLETIN FOR CRACKS IN THE FUSELAGE SKIN AT THE CHEM-MILLED STEPS AT THE SPECIFIED LOCATIONS (FOR AIRPLANES WITH PREVENTATIVE MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SB AT OR BEFORE 30.000 TOTAL FC) MOS AFL SB 737-53-1232 R2 TABLE INSPECT FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 1A.02 SERVICE BULLETIN FOR CRACKS IN THE FUSELAGE SKIN AT THE CHEM-MILLED STEPS AT THE SPECIFIED LOCATIONS (FOR AIRPLANES WITH PREVENTATIVE MODIFICATION THAT WERE INSTALLED IN ACCORDANCE WITH THIS SB AFTER 30.000 TOTAL FC) MOS AFL 58 [SSN REDACTED] R2 TABLE CONTACT FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 1A.03 SERVICE BULLETIN BOEING AND ACCOMPLISH THE WORK INSTRUCTED (IF ANY CRACK IS FOUND IN THE SKIN) MOS 58 [SSN REDACTED] R2 TABLE HFEC FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 18.01.1 SERVICE BULLETIN INSPECTION FOR CRACKS (IF PREVENTATIVE MODIFICATION INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL 58 [SSN REDACTED] R2 TABLE DEATILED INSPECTION FUSELAGE - SKIN - CHEMICALLY MILLED STEPS- INSPECTION. REPAIR AND PREVENTIVE 18.01.2 MODIFICATION. SERVICE BULLETIN FOR CRACKS AND ANY LOOSE OR MISSING FASTENERS (IF PREVENTATIVE MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS 58) MOS AFL SB 737-53-1232 R2 TABLE CONTACT FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 18.02 SERVICE BULLETIN BOEING AND ACCOMPLISH THE WORK INSTRUCTED (IF ANY CRACK FOUND IN THE SKIN) MOS SB 737-53-1232 R2 TABLE REPLACE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 18.03 SERVICE BULLETIN THE LOOSE OR MISSING FASTENER MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 109 Of 748 @ Camp Systems EFTA00618400 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE 2.01.1.1 BULLETIN SKIN INSPECTION OPTION 1 - EXTERNAL LFEC FOR CRACKS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE 2.01.1.2 BULLETIN SKIN INSPECTION OPTION 1 - DOUBLER INSPECTION: EXTERNAL LFEC FOR CRACKS AND AN EXTERNAL DETAILED INSPECTION FOR CRACKS AND LOOSE/MISSING FASTENERS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION, SERVICE 2.01.2.1 BULLETIN SKIN INSPECTION OPTION 2 - EXTERNAL LFEC FOR CRACKS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE 2.01.2.2 BULLETIN SKIN INSPECTION OPTION 2 - INTERNAL MFEC FOR CRACKS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE 2.01.2.3 BULLETIN SKIN INSPECTION OPTION 2 - DOUBLER INSPECTION: EXTERNAL LFEC FOR CRACKS AND AN EXTERNAL DETAILED INSPECTION FOR CRACKS AND LOOSE/MISSING FASTENERS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE REPAIR FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 2.02 SERVICE BULLETIN ANY CRACK FOUND (IF ANY CRACK IS FOUND IN THE SKIN) MOS SB 737-53-1232 R2 TABLE REPLACE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 2.03 SERVICE BULLETIN LOOSE AND MISSING FASTENERS (IF ANY LOOSE OR MISSING FASTENER) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 110 Of 748 @ Camp Systems EFTA00618401 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SS 737-53-1232 R2 TABLE INTERNAL FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 3.01.1 SERVICE BULLETIN / EXTERNAL DETAILED INSPECTION OF A TIME-LIMITED REPAIR FOR CRACKS AND LOOSE OR MISSING FASTENERS (FOR AIRPLANES WITH THE TIME-LIMITED REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE REPLACE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 3.01.2 SERVICE BULLETIN THE TIME-LIMITED REPAIR WITH THE PERMANENT REPAIR (FOR AIRPLANES WITH THE TIME-LIMITED REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE REPAIR FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 3.02 SERVICE BULLETIN ANY CRACK FOUND IN THE SKIN MOS SB 737-53-1232 R2 TABLE REPLACE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 3.03 SERVICE BULLETIN LOOSE AND MISSING FASTENERS MOS SB 737-53-1232 TABLE 1 AIRPLANES WITHMJTHOUT THE PREVENTATIVE MODIFICATION INSTALLED. (SUPERSEDED BY 737-53-1232 RI). SUPERSEDED SERVICE BULLETIN MOS - (s) SB 737-53-1232 TABLE 2 AIRPLANES WITH THE PERMANENT REPAIR INSTALLED. (SUPERSEDED BY 737-53-1232 RI). SERVICE BULLETIN SUPERSEDED NOT APPLICABLE MOS - (s) SB 737-53-1232 TABLE 3 AIRPLANES WITH THE TIME-LIMITED REPAIR INSTALLED. INTERNAUEXTEFtNAL DETAILED INSPECTION OF A NOT APPLICABLE TIME-LIMITED REPAIR FOR CRACKS AND LOOSE OR MISSING FASTENERS AS GIVEN IN -PART IV - TIME-LIMITED REPAIR'.. SERVICE BULLETIN MOS 02-APR-2007 AFL 2500 (s) SB 737-53-1233 INSPECTION AND REPLACEMENT OF KEEL BEAM LOWER CHORD FORWARD SPLICE AT STATION 535. SERVICE BULLETIN DAYS 30 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 111 Of 748 @ Camp Systems EFTA00618402 C O MP Mien winin Mernund up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: O5-Aug-2O14 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1233 RI 28-FEB-2002 SB 737-53-1236 I I -JUL-2002 INSPECTION AND REPLACEMENT OF KEEL BEAM LOWER CHORD FORWARD SPLICE AT STATION 535. SERVICE BULLETIN MOS 18 (s) 25-JUL-2002 1057:48 AFL 271 AIRSTAIR DOORSTOP INTERCOSTAL - INSPECTION AND FASTENER REPLACEMENT. SERVICE BULLETIN MOS AFL 24000 (0 SB 737-53-1236 RI FUSELAGE - AIRSTAIR DOORSTOP INTERCOSTAL - INSPECTION AND FASTENER REPLACEMENT. SERVICE BULLETIN 10-NOV-2005 SB 737-53-1237 04-DEC-2003 SB 737-53-1237 RI 07-DEC-2006 SB 737-53-1239 22-AUG-2002 SB 737-53-1239 RI I4-AUG-2003 SB 737-53-1239 R2 28-APR-2005 SB 737-53-1239(A) 22-AUG-2002 SB 737-53-1239(E) 22-AUG-2002 MOS 29-AUG-2011 -(s) 3533:32 AFL FASTENER REPLACEMENT. SERVICE BULLETIN MOS 863 FUSELAGE - WING TO BODY FAIRING - WHEEL WELL - BONDED PANEL (BOW-TIE PANEL) - FASTENER REPLACEMENT. SERVICE BULLETIN MOS KEEL CHORD SPLICE WASHERS. BOLTS AND NUTS REPLACEMENT. SERVICE BULLETIN MOS KEEL CHORD SPLICE WASHERS. BOLTS. AND NUTS REPLACEMENT. SERVICE BULLETIN MOS 6 (s) FUSELAGE - KEEL BEAM LOWER CHORDS - FORWARD AND AFT SPLICES AT STATIONS 540 AND 727 - KEEL CHORD SPLICE WASHERS. BOLTS. AND NUTS REPLACEMENT. SERVICE BULLETIN MOS 6 (s) INSPECT KEEL CHORD SPLICE WASHERS. BOLTS AND NUTS REPLACEMENT. SERVICE BULLETIN MOS 6 (s) REPLACE KEEL CHORD SPLICE WASHERS. BOLTS AND NUTS REPLACEMENT. SERVICE BULLETIN MOS 6 (s) RECOMMENDED RECOMMENDED COMPUED WITH - REPLACEMENT COMPUED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 112 Of 748 @ Camp Systems EFTA00618403 COMP up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1243 AUTOMATIC OVERWING EXIT DOUBLERS (BEARSTRAPS) INSPECTION INTERVAL CHANGE. SERVICE BULLETIN MOS SB 26-SEP-2002 [SSN REDACTED] AFL 75000 (s) PIVOT LINK ASSEMBLY REPAIR/REPLACE, SERVICE BULLETIN MOS SB 737-53-1244 RI PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN MOS SB 737-53-1244 RI (8)2 REPLACE PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN BLIND FASTENERS MOS AFL 10000 (s) SB 737-53-1244 R2 PIVOT LINK ASSEMBLY REPAIRIREPLACE. SERVICE BULLETIN MOS 12 (s) 15-MAR-2007 SB 737-53-1244 R2 (8)1 INSPECT PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN BLIND FASTNERS MOS 15-MAR-2007 AFL WOO (s) SB 737-53-1244 R2 (8)2 REPLACE PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN BLIND FASTNERS MOS 15-MAR-2007 AFL 10000 (s) SB 737-53-1244 R4 FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - PIVOT LINK ASSEMBLY REPAIR/REPLACE SUPERSEDED (SUPERSEDED BY S8 [SSN REDACTED] R5), SERVICE BULLETIN MOS SB 737-53-1244 RS FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN MOS 27-JUL-2011 SB 737-53-1244 R5 TABLE INSTALL FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540- PIVOT LINK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.1 SERVICE BULLETIN NEW PIVOT LINK - NO CHANGES TO PIVOT LINK STRUCTURE AND PASSENGER SEATS HAVE NOT BEEN MOVED AFTER AIRPLANE DELIVERY MOS 12(s) I 7-APR-2003 RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time @ Camp Systems 113 Of 748 EFTA00618404 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1244 R5 TABLE ACCOMPLISH FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540- PIVOT LINK ASSEMBLY RECOMMENDED 1.2 REPAIR/REPLACE. SERVICE BULLETIN MOVE THE SEATS - NO CHANGES TO PIVOT LINK STRUCTURE AND I 7-APR-2003 PASSENGER SEATS HAVE NOT BEEN MOVED AFTER AIRPLANE DELIVERY MOS 12 (s) 58 [SSN REDACTED] RS TABLE INSTALL FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540- PIVOT LINK ASSEMBLY FtEPAIRJREPLACE. RECOMMENDED 1.3 SERVICE BULLETIN BLIND CENTERLINE FASTNERS IN THE SEAT TRACK 17-APR-2003 MOS 12 (s) SB 737-53-1244 R5 TABLE INSPECT FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540 - PIVOT UNK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.3.1 SERVICE BULLETIN BLIND FASTENERS MOS AFL 3800 (s) SB 737-53-1244 RS TABLE REPLACE FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540- PIVOT LINK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.3.2 SERVICE BULLETIN BLIND FASTENERS WITH SOLID FASTENERS MOS AFL 10000 (s) 58 [SSN REDACTED] R5 TABLE INSTALL FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540- PIVOT LINK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.4 SERVICE BULLETIN SOLID CENTERLINE FASTNERS IN THE SEAT TRACK 17-APR-2003 MOS 12 (s) 58 [SSN REDACTED] R5 TABLE INSTALL FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540- PIVOT LINK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.5 SERVICE BULLETIN NEW PIVOT LINK 27-JUL-2011 MOS 60 (s) SB 737-53-1245 HIGH PRESSURE DOOR AND DOUBLER-REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 05-AUG-2004 SB 737-53-1249 FUSELAGE - FRAMES AND BULKHEADS - BODY STATION 1016 AFT PRESSURE BULKHEAD - VERTICAL FIN ATTACHMENT FITTINGS -BOLT HOLE INSPECTION AND REPAIR. SERVICE BULLETIN MOS 16-NOV-2006 AFL 36000 (s) SB 737-53-1251 AFT PRESSURE BULKHEAD APEX INSPECTION. SERVICE BULLETIN MOS 22-AUG-2008 03-JUN-2004 3260:48 AFL 4000 (s) 782 COMPUED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 114 Of 748 @ Camp Systems EFTA00618405 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1252 13-OCT-2005 FUSELAGE - STABILIZER CENTER SECTION FRONT SPAR - SLIDING SEAL AND TRACK MODIFICATION. SERVICE BULLETIN MOS SB 737-53-1252 RI FUSELAGE - STABILIZER CENTER SECTION FRONT SPAR - SLIDING SEAL AND TRACK MODIFICATION.. SERVICE BULLETIN MOS 15-FEB-2007 SB 737-53-1256 CHEMICAL MILL PITTING AT S-4 LAP SPLICE. SERVICE BULLETIN MOS 18-SEP-2003 RECOMMENDED SB SB 737-53-1264 04-MAY-2006 [SSN REDACTED] RI 24-JAN-2008 FUSELAGE - FILLET FAIRINGS - AFT WING-TO-BODY FAIRING - INBOARD FLAP PRIMARY TORQUE TUBE INSPECTION/REPAIR AND AFT WING-TO-BODY FAIRING MODIFICATION. SERVICE BULLETIN MOS FUSELAGE - FILLET FAIRINGS - AFT WING-TO-BODY FAIRING - INBOARD FLAP PRIMARY TORQUE TUBE INSPECTION/REPAIR AND AFT WING-TO-BODY FAIRING MODIFICATION, SERVICE BULLETIN MOS SB 737-53-1276 FUSELAGE - FORWARD AND AFT CARGO COMPARTMENT- CORROSION PREVENTION MODIFICATION (SUPERSEDED SUPERSEDED BY SB 737-53-1276 RI), SERVICE BULLETIN MOS SB 737-53-1276 RI FUSELAGE - FORWARD AND AFT CARGO COMPARTMENT - CORROSION PREVENTION MODIFICATION. SERVICE RECOMMENDED 01-AUG-2014 BULLETIN MOS - SB 737-53-1277 FUSELAGE - STRUCTURE ATTACHMENT FITTINGS - NOSE WHEEL WELL RETRACT ACTUATOR SUPPORT FITTING SUPERSEDED INSPECTION AND MODIFICATION (SUPERSEDED BY 737-53-1277 R1). SERVICE BULLETIN MOS 14-NOV-2007 SB 737-53-1277 RI FUSELAGE - STRUCTURE ATTACHMENT FITTINGS - NOSE WHEEL WELL RETRACT ACTUATOR SUPPORT FITTING INSPECTION AND MODIFICATION. SERVICE BULLETIN MOS 14-MAY-2010 SB 737-53-1280 22-MAY-2008 FUSELAGE - FILLET FAIRINGS - AFT OUTBOARD WING TO BODY FAIRING MODIFICATION. SERVICE BULLETIN MOS 74nsufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 115 Of 748 @ Camp Systems EFTA00618406 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1280 OPTION 1 INSTALL FUSELAGE - FILLET FAIRINGS - AFT OUTBOARD WING TO BODY FAIRING MODIFICATION. SERVICE BULLETIN MODIFICATION AS GIVEN IN PARAGRAPH 3.8.. WORK INSTRUCTIONS MOS 24 (s) 22-MAY-2008 SB 737-53-1280 OPTION 2 INSPECT FUSELAGE- FILLET FAIRINGS - AFT OUTBOARD WING TO BODY FAIRING MODIFICATION. SERVICE (A) BULLETIN AS GWEN IN PARAGRAPH 3.8.. WORK INSTRUCTIONS MOS 24 (5) 22-MAY-2008 SB 737-53-1280 OPTION 2 INSTALL FUSELAGE - FILLET FAIRINGS - AFT OUTBOARD WING TO BODY FAIRING MODIFICATION. SERVICE BULLETIN (3) MODIFICATION AS GIVEN IN PARAGRAPH 3.8., WORK INSTRUCTIONS MOS 72 (s) 22-MAY-2008 SB 737-53-1282 FUSELAGE - WHEEL WELL - NOSE WHEEL UPPER DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS 14-NOV-2007 SB 737-53-1282 RI 14-MAR-2008 SB 737-53-1285 58 [SSN REDACTED] RI 23-JUL-2014 FUSELAGE - WHEEL WELL - NOSE WHEEL UPPER DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN 61OS 22-AUG-2008 3260:48 AFL 782 FUSELAGE - PASSENGER CABIN FLOORS - SECTIONS 41 AND 47 - ADDITION OF GEL TAPE TO PREVENT CORROSION SUPERSEDED OF PASSENGER CABIN FLOOR PANEL SUPPORT STRUCTURE (SUPERSEDED BY SB 737-53-1285 RI ). SERVICE BULLETIN MOS FUSELAGE - PASSENGER CABIN FLOORS - SECTIONS 41 AND 47 - ADDITION OF GEL TAPE TO PREVENT CORROSION RECOMMENDED OF PASSENGER CABIN FLOOR PANEL SUPPORT STRUCTURE. SERVICE BULLETIN MOS 58 [SSN REDACTED] FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SI3 [SSN REDACTED] RI ). SERVICE BULLETIN MOS 58 [SSN REDACTED] RI 12-JUN-2013 FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN MOS (EFF) SUPERSEDED RECOMMENDED COMPLIED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 116 Of 748 @ Camp Systems EFTA00618407 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1294 RI TABLE DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. 1.1 CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN AND A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE SKIN FOR CRACKS IN THE AREA AROUND THE EIGHT FASTENERS SECURING THE STA 540 BULKHEAD CHORDS BETWEEN STRINGER S-22 AND S-23 (AIRPLANES WITH LESS THAN 27.500 TOTAL FLIGHT CYCLES AS OF THE ORIGINAL ISSUE DATE OF THIS SERVICE BULLETIN) MOS SB 737-53-1294 RI TABLE DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. 1.2 CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN AND A HFEC INSPECTION OF THE SKIN FOR CRACKS IN THE AREA AROUND THE EIGHT FASTENERS SECURING THE STA 540 BULKHEAD CHORDS BETWEEN STRINGER S-22 AND S-23 (AIRPLANES WITH 27.500 OR MORE TOTAL FLIGHT CYCLES AS OF THE ORIGINAL ISSUE DATE OF THIS SERVICE BULLETIN) MOS 58 [SSN REDACTED] RI TABLE REPAIR FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE 1.3 INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN THE CRACKING ON LEFT SIDE (AND) DO THE PREVENTIVE MODIFICATION ON THE RIGHT SIDE (IF ANY CRACK IS FOUND IN THE SKIN ON THE LEFT SIDE OF THE AIRPLANE AND NO CRACK IS FOUND ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE REPAIR FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE 1.4 INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN THE CRACKING ON RIGHT SIDE (AND) DO THE PREVENTIVE MODIFICATION ON THE LEFT SIDE (IF ANY CRACK IS FOUND IN THE SKIN ON THE RIGHT SIDE OF THE AIRPLANE AND NO CRACK IS FOUND ON THE LEFT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE REPAIR FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE 1.5 INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN THE CRACKS (IF ANY CRACK IS FOUND IN THE SKIN ON BOTH SIDES OF THE AIRPLANE) MOS 58 [SSN REDACTED] RI TABLE DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. 2.1.1 CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN OF THE SKIN SURROUNDING THE FILLER UNDER THE DRAG LINK ASSEMBLY FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD 2.1.2 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN EXTERNAL LOW FREQUENCY EDDY CURRENT (LFEC) INSPECTION OF THE SKIN AND DOUBLER AND AN EXTERNAL HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE TRIPLER FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 117 Of 748 @ Camp Systems EFTA00618408 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD 2.1.3 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN INTERNAL HFEC INSPECTION OF THE SKIN FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD 2.1.4 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN INTERNAL HFEC INSPECTION OF THE SPLICE PLATE AND STA 540 BULKHEAD OUTER CHORD FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. 2.2.1 CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN OF THE SKIN SURROUNDING THE FILLER UNDER THE DRAG LINK ASSEMBLY FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD 2.2.2 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN EXTERNAL LFEC INSPECTION OF THE SKIN AND DOUBLER AND AN EXTERNAL HFEC INSPECTION OF THE TRIPLER FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD 2.2.3 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN INTERNAL HFEC INSPECTION OF THE SKIN FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD 2.2.4 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN INTERNAL HFEC INSPECTION OF THE SPLICE PLATE AND STA 540 BULKHEAD OUTER CHORD FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE CONTACT FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPUCE 2.3 INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN BOEING FOR INSTRUCTIONS AND DO THE WORK (ANY CRACK IS FOUND) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 118 Of 748 @ Camp Systems EFTA00618409 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1294 TABLE 1.1 DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. RECOMMENDED CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN AND A HFEC INSPECTION OF THE SKIN FOR CRACKS IN THE AREA AROUND THE EIGHT FASTENERS SECURING THE STA 540 BULKHEAD CHORDS BETWEEN STRINGER S-22 AND S-23 FOR AIRPLANES WITH LESS THAN 27.500 TOTAL FLIGHT CYCLES AS OF THE ORIGINAL ISSUE DATE OF THIS SERVICE BULLETIN MOS 31-MAR-2011 AFL 2000 (s) SB 737-53-1294 TABLE 1.2 DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. RECOMMENDED CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN AND A HFEC INSPECTION OF THE SKIN FOR CRACKS IN THE AREA AROUND THE EIGHT FASTENERS SECURING THE STA 540 BULKHEAD CHORDS BETWEEN STRINGER S-22 AND S-23 FOR AIRPLANES WITH 27.500 OR MORE TOTAL FLIGHT CYCLES AS OF THE ORIGINAL ISSUE DATE OF THIS SERVICE BULLETIN. MOS 31-MAR-2011 SB 737-53-1294 TABLE 2.1.1 SB 737-53-1294 TABLE 2.1.2 SB 737-53-1294 TABLE 2.1.3 SB 737-53-1294 TABLE 2.1.4 AFL 750(s) DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. RECOMMENDED CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN OF THE SKIN SURROUNDING THE FILLER UNDER THE DRAG LINK ASSEMBLY FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE MOS AFL 2500 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 RI). SERVICE BULLETIN EXTERNAL INSPECTION OF THE SKIN AND DOUBLER AND AN EXTERNAL HFEC INSPECTION OF THE TRIFLER FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE MOS AFL SCO0 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN INTERNAL INSPECTION OF THE SKIN FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE MOS AFL 5000 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 RI). SERVICE BULLETIN INTERNAL INSPECTION OF THE SPLICE PLATE AND STA 540 BULKHEAD OUTER CHORD FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE MOS AFL 5000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 119 Of 748 @ Camp Systems EFTA00618410 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1294 TABLE 2.2.1 DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN OF THE SKIN SURROUNDING THE FILLER UNDER THE DRAG LINK ASSEMBLY FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE MOS RECOMMENDED AFL 2500 (5) SB 737-53-1294 TABLE LFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE RECOMMENDED 2.2.2 INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 RI). SERVICE BULLETIN EXTERNAL INSPECTION OF THE SKIN AND DOUBLER AND AN EXTERNAL HFEC INSPECTION OF THE TRIPLER FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE SB 737-53-1294 TABLE 2.2.3 SB 737-53-1294 TABLE 2.2.4 SB 737-53-1295 RI SB 737-53-1295 R2 18-JUN-20I3 SB 737-53-1295 R2 TABLE MOS AFL 5000 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN INTERNAL INSPECTION OF THE SKIN FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE MOS AFL 5000 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 RI). SERVICE BULLETIN INTERNAL INSPECTION OF THE SPLICE PLATE AND STA 540 BULKHEAD OUTER CHORD FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE MOS AFL 5000(s) FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY REPLACEMENT SUPERSEDED (SUPERSEDED BY 93 [SSN REDACTED] R2). SERVICE BULLETIN MOS FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY REPLACEMENT. RECOMMENDED SERVICE BULLETIN MOS EXTERNAL - DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER I WINDOW FRAME AND 1.1.1 WINDSHIELD ASSEMBLY REPLACEMENT. SERVICE BULLETIN OF THE CROWN SKIN FOR CORROSION (GROUP 1. CONFIGURATION 6: GROUP 2. CONFIGURATION 4) (ALL AIRPLANES) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 120 Of 748 @ Camp Systems EFTA00618411 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1295 R2 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD 1.1.2 ASSEMBLY REPLACEMENT. SERVICE BULLETIN FOR CORROSION AND INSTALL NEW FASTENERS (GROUP 1. CONFIGURATION 6: GROUP 2. CONFIGURATION 4) (ALL AIRPLANES) MOS - (s) SB 737-53-1295 R2 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY 1.2 REPLACEMENT. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED (IF CORROSION IS FOUND) MOS SB 737-53-1295 R2 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD 2.1 ASSEMBLY REPLACEMENT. SERVICE BULLETIN FOR CORROSION AND INSTALL NEW FASTENERS (ALL AIRPLANES) MOS - Is) SB 737-53-1295 R2 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY 2.2 REPLACEMENT. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED (IF CORROSION IS FOUND) SB 737-53-1296 11-JAN-2011 MOS FUSELAGE - PASSENGER CABIN FLOORS - STATION 7278 SPLICE STRAP INSTALLATION. SERVICE BULLETIN MOS SB 737-53-1296 TABLE 1.1 REPLACE FUSELAGE - PASSENGER CABIN FLOORS - STATION 727B SPLICE STRAP INSTALLATION. SERVICE RECOMMENDED BULLETIN SEAT TRACK BOLTS FOR ALL AIRPLANES MOS 24 (s) 11-JAN-2011 SB 737-53-1296 TABLE 1.2 DETAILED INSPECTION FUSELAGE - PASSENGER CABIN FLOORS - STATION 7278 SPLICE STRAP INSTALLATION. RECOMMENDED SERVICE BULLETIN AND HFEC INSPECTION OF SPLICE STRAP AND FORWARD SEAT TRACK FOR ALL AIRPLANES MOS 24 (s) 11-JAN-2011 SB 737-53-1297 FUSELAGE - EQUIPMENT ATTACHMENT FITTINGS- AFT CARGO WASTE TANK ENCLOSURE - STANCHION RECOMMENDED MODIFICATION. SERVICE BULLETIN MOS 03-SEP-2010 SB 737-53-1298 FUSELAGE - SKIN - DORSAL FIN SEAL RETAINER AND FUSELAGE SKIN STATION 847 TO 1007- INSPECTION. SERVICE BULLETIN MOS 27-AUG-2010 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 121 Of 748 @ Camp Systems EFTA00618412 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1298 TABLE 1.1/2 27-AUG-2010 INSPECTION FUSELAGE - SKIN - DORSAL FIN SEAL RETAINER AND FUSELAGE SKIN STATION 847 TO 1007- RECOMMENDED INSPECTION. SERVICE BULLETIN OF THE DORSAL FIN LOWER SEAL RETAINERS FOR CONTACT WITH THE FUSELAGE SKIN BETWEEN STA 847 AND STA 1007 IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 1 FOR ALL AIRPLANES MOS 24 (s) AFL 4000 SB 737-53-1298 TABLE 1.6 MODIFY FUSELAGE - SKIN - DORSAL FIN SEAL RETAINER AND FUSELAGE SKIN STATION 847 TO 1007 - INSPECTION. RECOMMENDED SERVICE BULLETIN THE LOWER AND VERTICAL SEALS IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5 FOR AIRPLANES THAT HAVE NOT MODIFIED THE LOWER AND VERTICAL SEALS OR. REPLACED THE LOWER SEAL IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 4. MOS 24 (s) 27-AUG-20I0 SB 737-53-1303 513 [SSN REDACTED] RI 06-MAY-2014 513 [SSN REDACTED] RI TBL 1.1 513 [SSN REDACTED] RI TBL 1.2 06-MAY-2014 SB 737-53-1303 RI TBL AFL 4000 FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG SUPERSEDED INSTALLATION (SUPERSEDED BY SB 737-53-1303 RI). SERVICE BULLETIN MOS FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG RECOMMENDED INSTALLATION. SERVICE BULLETIN MOS HIGH FREQUENCY EDDY CURRENT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG INSTALLATION. SERVICE BULLETIN (HFEC) INSPECTION OF THE AFFECTED NUMBER 3 WINDOW FRAME FASTENER HOLES FOR CRACKS. COLD WORK AND INSTALL FREEZE PLUGS IN AFFECTED NUMBER 3 WINDOW FRAME HOLES MOS AFL INSTALL FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE RECOMMENDED PLUG INSTALLATION. SERVICE BULLETIN TEMPORARY REPAIR STRAP OR INSTALL THE NUMBER 3 WINDOW FRAME PERMANENT REPAIR (ANY CRACK INDICATION FOUND) MOS BFIF REPLACE FUSELAGE- STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME- INSPECTION AND FREEZE RECOMMENDED 1.3 PLUG INSTALLATION. SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME OR INSTALL THE NUMBER 3 WINDOW FRAME PERMANENT REPAIR (IF ANY CRACK FOUND BEYOND THE TEMPORARY REPAIR STRAP INSTALLATION UMITS) MOS 06-MAY-2014 BF/F 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 122 Of 748 @ Camp Systems EFTA00618413 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1303 RI TBL EXTERNAL - DETAILED INSPECTION FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG INSTALLATION. SERVICE BULLETIN OF THE TEMPORARY REPAIR STRAP FOR CORROSION AND ANY OTHER NICKS. GAPS. LOOSE FASTENERS OR MISSING SEALANT (IF TEMPORARY REPAIR STRAP INSTALLED) MOS - (s) SB 737-53-1303 RI TBL REPLACE FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE 1.4.2 PLUG INSTALLATION. SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME (IF TEMPORARY REPAIR STRAP INSTALLED) MOS - Is) SB 737-53-1303 RI TBL EXTERNAL - DETAILED INSPECTION FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - 1.5.1 INSPECTION AND FREEZE PLUG INSTALLATION. SERVICE BULLETIN OF THE TEMPORARY REPAIR STRAP FOR CORROSION AND ANY OTHER NICKS. GAPS. LOOSE FASTENERS OR MISSING SEALANT (IF TEMPORARY REPAIR STRAP OPTION 2 WITH STRAIGHT LINE FASTENER PATTERN INSTALLED) MOS - (s) SB 737-53-1303 RI TBL INSTALL FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE 1.5.2 PLUG INSTALLATION. SERVICE BULLETIN THE NUMBER 3 WINOW FRAME PERMANENT REPAIR OR REPLACE THE NUMBER 3 WINDOW FRAME (IF TEMPORARY REPAIR STRAP OPTION 2 WITH STRAIGHT LINE FASTENER PATTERN INSTALLED) MOS - (s) SB 737-53-1303 RI TBL REPLACE FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE RECOMMENDED 1.6 PLUG INSTALLATION. SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME OR INSTALL THE NUMBER 3 WINDOW FRAME PERMANENT REPAIR (IF ANY CRACK FOUND AROUND THE NUMBER 3 WINDOW FRAME REPAIR FASTENERS COMMON TO THE TEMPORARY REPAIR STRAP) MOS OS-MAY-20M BF/F SB 737-53-1303 TABLE 1.1 HFEC FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG SUPERSEDED INSTALLATION (SUPERSEDED BY SB 737-53-1303 R1). SERVICE BULLETIN INSPECTION OF THE AFFECTED NUMBER 3 WINDOW FRAME FASTENER HOLES FOR CRACKS. COLD WORK AND INSTALL FREEZE PLUGS IN AFFECTED NUMBER 3 WINDOW FRAME HOLES FOR ALL AIRPLANES SB 737-53-1303 TABLE 1.4.1 MOS - Is) HFEC FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG SUPERSEDED INSTALLATION (SUPERSEDED BY SB 737-53-1303 R1). SERVICE BULLETIN - INTERNAL INSPECTION OF THE NUMBER 3 WINDOW FRAME MOUND THE REPAIR FASTENERS COMMON TO THE TEMPORARY REPAIR STRAP FOR CRACKS AND DO A GENERAL VISUAL INSPECTION OF THE TEMPORARY REPAIR STRAP FOR TEMPORARY REPAIR STRAP INSTALLED AIRPLANES MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 123 Of 748 @ Camp Systems EFTA00618414 COMP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1303 TABLE REPLACE FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE SUPERSEDED 1.4.2 PLUG INSTALLATION (SUPERSEDED BY SB 737-53-1303 RI). SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME MOS - S8 [SSN REDACTED] FUSELAGE - FILLET FAIRINGS - AFT WING TO BODY FAIRING - PANEL 194E AND AFT CENTER WHEEL WELL PANEL RECOMMENDED 193D - INSPECTION AND REWORK. SERVICE BULLETIN 12-JAN-2012 MOS SB 737-53-1307 TABLE 1.1 PERFORM FUSELAGE - FILLET FAIRINGS - AFT WING TO BODY FAIRING - PANEL 194E AND AFT CENTER WHEEL WELL RECOMMENDED PANEL 193D - INSPECTION AND REWORK. SERVICE BULLETIN A GENERAL VISUAL INSPECTION OF THE LOWER AFT WING TO BODY FAIRING PANEL AND SUPPORT STRUCTURE MOS 24 (s) 12-JAN-2012 SB 737-53-1307 TABLE 1.4 PERFORM FUSELAGE - FILLET FAIRINGS -AFT WING TO BODY FAIRING -PANEL 194E AND AFT CENTER WHEEL WELL RECOMMENDED PANEL 193D - INSPECTION AND REWORK. SERVICE BULLETIN THE PANEL AND SUPPORT STRUCTURE REWORK MOS 72 (s) 12-JAN-2012 SB 737-53-1310 FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND MODIFICATION RECOMMENDED . SERVICE BULLETIN MOS 20-OCT-2011 SB 737-53-1310 TABLE 1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL DETAILED INSPECTION AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEPS AT SPECIFIED LOCATIONS OPTION 1 OR OPTION 2 FOR ALL AIRPLANES MOS 20-OCT-2011 AFL 1500(s) SB 737-53-1310 TABLE 2.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION DOUBLER OPTION 1 OR OPTION 2 FOR AU. EXTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS AFL 50000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 124 Of 748 @ Camp Systems EFTA00618415 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1310 TABLE 2.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER OPTION 1 OR OPTION 2 FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS AFL 50000 (s) SB 737-53-1310 TABLE 3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER OPTION 1 OR OPTION 2 FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS AFL 50000 (s) SB 737-53-1310 TABLE 4 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER OPTION 1 OR OPTION 2 FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS AFL 50000 (s) 58 [SSN REDACTED] TABLE 5.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS AFL 50000 (s) SB 737-53-1310 TABLE 5.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43.000 TOTAL FLIGHT CYCLES MOS AFL 43000 (s) SB 737-53-1310 TABLE 5.3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI - FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS AFL 5500 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 125 Of 748 @ Camp Systems EFTA00618416 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1310 TABLE 6.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS AFL 50000 (s) 513 [SSN REDACTED] TABLE 6.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43.000 TOTAL FLIGHT CYCLES MOS AFL 5500 (s) SB 737-53-1310 TABLE 6.3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN DO AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS AFL 5500(s) 513 [SSN REDACTED] TABLE 7.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS AFL 50000 (s) SB 737-53-1310 TABLE 7.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43.000 TOTAL FLIGHT CYCLES MOS AFL 5500(s) SB 737-53-1310 TABLE 7.3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS AFL 5500 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 126 Of 748 @ Camp Systems EFTA00618417 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1311 21-OCT-201 I FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN MOS AFL 28-MAY-20I3 3714:04 900 NOT APPLICABLE - N/A BY AIRCRAFT MODEL SB 737-53-1311 TABLE 1 EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEK1-MILL STEPS IN CROWN SKINS AT SPECIFIED RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEPS AT SPECIFIED LOCATIONS FOR ALL AIRPLANES MOS 21-OCT-2011 - (s) 28-MAY-20I3 3714:04 AFL 900 SB 737-53-1311 TABLE 2 EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) OF THE FUSELAGE SKIN FOR CRACKING AT THE CHEM-MILL STEPS COMMON TO SHEAR WRINKLE AREAS FOR ALL AIRPLANES. GROUP 2.5-6 MOS 28-MAY-2013 21-OCT-2011 -(s) 3714:04 AFL 900 SB 737-53-1311 TABLE 3.1 NON DESTRUCTIVE FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL AND MODIFICATION. SERVICE BULLETIN INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION DOUBLER FOR ALL EXTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS - (s) 28-MAY-2013 3714:04 AFL 900 SB 737-53-1311 TABLE 3.2 EXTERNAL INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL INSPECTION AND MODIFICATION. SERVICE BULLETIN OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS 28-MAY-2013 - (s) 3714:04 AFL 900 SB 737-53-1311 TABLE 4.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 127 Of 748 @ Camp Systems EFTA00618418 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1311 TABLE 4.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43,000 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 SB 737-53-1311 TABLE 4.3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 SB 737-53-1312 FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN MOS 28-MAY-2013 21-OCT-2011 3714:04 NOT APPLICABLE - N/A BY AIRCRAFT MODEL AFL 900 SB 737-53-1312 RI FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS- INSPECTION AND MODIFICATION. RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL SERVICE BULLETIN MOS 28-MAY-2013 I4-MAR-2012 3714:04 AFL 900 SB 737-53-1312 TABLE 1 EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEPS AT SPECIFIED LOCATIONS AND OPTION 1 (OR) OPTION 2 FOR ALL AIRPLANES MOS 28-MAY-2013 21-OCT-2011 -(s) 3714:04 AFL 900 SB 737-53-1312 TABLE 2 EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) OF THE FUSELAGE SKIN FOR CRACKING AT THE CHEM-MILL STEPS AT SPECIFIED LOCATIONS AND OPTION 1 (OR) OPTION 2 FOR ALL AIRPLANES MOS 28-MAY-2013 21-OCT-2011 -(s) 3714:04 AFL 900 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 128 Of 748 @ Camp Systems EFTA00618419 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1312 TABLE 3 EXTERNAL INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS- INSPECTION AND MODIFICATION. SERVICE BULLETIN OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER AND OPTION 1 (OR) OPTION 2 FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS - (s) 28-MAY-2013 3714:04 RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL AFL 900 SB 737-53-1312 TABLE 4.1 ACCOMPLISH FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 SB 737-53-1312 TABLE 4.2 ACCOMPLISH FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43.000 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 SB 737-53-1312 TABLE 4.3 ACCOMPLISH FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 SB 737-53-1316 SB 737-53-1316 RI 03-JUL-2013 SB 737-53-1316 RI TABLE AFL 5500 (s) 900 FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY REPLACEMENT SUPERSEDED AND HEAD UP DISPLAY REALIGNMENT (SUPERSEDED BY SB 737-53-1316 R1). SERVICE BULLETIN MOS FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY REPLACEMENT RECOMMENDED AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN MOS EXTERNAL - DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND 1.1.1 WINDSHIELD ASSEMBLY REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN OF THE CROWN SKIN FOR CORROSION FOR ALL AIRPLANES (GROUP 1. CONFIGURATION 6) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 129 Of 748 @ Camp Systems EFTA00618420 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1316 R1 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD 1.1.2 ASSEMBLY REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN FOR CORROSION AND INSTALL NEW FASTENERS FOR ALL AIRPLANES (GROUP 1. CONFIGURATION 6) MOS SB 737-53-1316 RI TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY 1.2 REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF CORROSION IS FOUND (GROUP 1. CONFIGURATION 6) MOS SB 737-53-1316 RI TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD 2.1 ASSEMBLY REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN FOR CORROSION AND INSTALL NEW FASTENERS FOR ALL AIRPLANES (GROUP 1. CONFIGURATION 5) MOS SB 737-53-1316 RI TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY 2.2 REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF CORROSION IS FOUND (GROUP 1. CONFIGURATION 5) MOS SB 737-53-1326 FUSELAGE - CARGO COMPARTMENT SIDEWALL LININGS - INSPECTION AND REPAIR. SERVICE BULLETIN MOS 26-OCT-2012 RECOMMENDED SB 737-53-1326 TABLE 1.1 INSPECTION FUSELAGE - CARGO COMPARTMENT SIDEWALL LININGS - INSPECTION AND REPAIR. SERVICE BULLETIN RECOMMENDED OF THE FORWARD AND AFT CARGO COMPARTMENTS SIDEWALL PANELS FOR ALL AIRPLANES MOS 24 (5) 26-OCT-2012 SB 737-53-1326 TABLE 1.2 REMOVE FUSELAGE - CARGO COMPARTMENT SIDEWALL LININGS - INSPECTION AND REPAIR. SERVICE BULLETIN RECOMMENDED AND REPLACE ALUMINUM SIDEWALL LININGS MOS 60 (s) 26-OCT-2012 SB 737-53-1330 FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED SERVICE BULLETIN MOS 26-FEB-2013 SB 737-53-1330 RI FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED SERVICE BULLETIN MOS 10-JUN-2013 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 130 Of 748 @ Camp Systems EFTA00618421 C O MP Atiant.fran Meowed lip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1330 TABLE 1 (1.1.1) DO FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. SERVICE BULLETIN A HFEC INSPECTION OF THE CRACK IN THE NUMBER 1 WINDOW FRAME TO DETERMINE IF THE CRACK HAS GROWN BEYOND THE ALLOWABLE STOP DRILL REGION AND STOP DRILL THE CRACK IF WITHIN THE ALLOWABLE STOP DRILL REGION MOS BF/F RECOMMENDED SB 737-53-1330 TABLE 1 OO FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED (1.1.2) SERVICE BULLETIN A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION ABOVE AND BELOW THE CRACKED NUMBER 1 WINDOW FRAME AROUND THE FASTENERS THAT HOLD THE NUMBER 1 AND NUMBER 2 WINDOW FRAMES TOGETHER MOS BF/F SB 737-53-1330 TABLE 1 OO FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED (1.1.3) SERVICE BULLETIN A DETAILED INSPECTION OF THE AREA TWO INCHES ABOVE AND BELOW THE CRACK MOS BF/F SB 737-53-1330 TABLE 1 INSTALL FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY RECOMMENDED (1.1.4) REPAIR. SERVICE BULLETIN THE TEMPORARY REPAIR DOUBLER ON THE NUMBER 1 WINDOW FRAME MOS BF/F SB 737-53-1330 TABLE 1 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY RECOMMENDED (1.2) REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING. FOR CRACK FOUND OUTSIDE OF THE UPPER AFT CORNER AREA OF THE NUMBER 1 WINDOW FRAME MOS BF1F SB 737-53-1330 TABLE 1 OO FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED (1.3.1) SERVICE BULLETIN AN EXTERNAL DETAILED INSPECTION FOR CORROSION AND ANY OTHER NICKS. GAPS. LOOSE FASTENERS OR MISSING SF41 ANT FOR TEMPORARY REPAIR DOUBLER INSTALLED MOS 6 (s) SB 737-53-1330 TABLE 1 REPLACE FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER I WINDOW FRAME CRACKING - TEMPORARY RECOMMENDED (1.3.2) REPAIR. SERVICE BULLETIN THE NUMBER 1 WINDOW FRAME FOR TEMPORARY REPAIR DOUBLER INSTALLED MOS 24 (s) AFL 6000 SB 737-53-1330 TABLE 1 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY RECOMMENDED (1.4) REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING FOR ANY CRACK FOUND AROUND THE NUMBER 1 WINDOW FRAME FASTENERS COMMON TO THE TEMPORARY REPAIR DOUBLER MOS BF/F 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 131 Of 748 @ Camp Systems EFTA00618422 CAMP Mianistfrn• thermiewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1334 04-AUG-2014 SB 737-53-1334 TBL 1.1.1 SB 737-53-1334 TBL 1.1.2 SB 737-53-1334 TBL 1.3 04-AUG-2014 SB 737-53-1334 TBL 1.5 04-AUG-2014 SB 737-53-1334 TBL 2.1.1 SB 737-53-1334 T/31. 2.12 FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN MOS - (s) RECOMMENDED OO FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN PART 2: CROWN RECOMMENDED SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - HIGHER STRESS LOCATIONS (ALL AIRPLANES) (GROUP 1-5) MOS AFL 7500 (s) OO FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN PART 3: CROWN RECOMMENDED SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - LOWER STRESS LOCATIONS (ALL AIRPLANES) (GROUP 1-5) MOS AFL 10000 (s) CONTACT FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN THE BOEING RECOMMENDED COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR! REPEAT PART 2: CROWN SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - HIGHER STRESS LOCATIONS (IF CONDITION 2: ANY CRACK FOUND (DURING PART 2 MFEC INSPECTION OF HIGHER STRESS LOCATIONS)) (GROUP 1-5) MOS BFIF (s) CONTACT FUSELAGE -CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN THE BOEING RECOMMENDED COMPANY FOR REPAIR INSTRUCTIONS AND OO THE REPAIR! REPEAT PART 3: CROWN SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - LOWER STRESS LOCATIONS (IF CONDITION 2 ANY CRACK FOUND (DURING PART 3 MFEC INSPECTION OF LOWER STRESS LOCATIONS)) (GROUP 1-5) MOS BFIF (s) OO FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN PART 2: CROWN RECOMMENDED SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - HIGHER STRESS LOCATIONS (ALL AIRPLANES) (GROUP 6) MOS AFL 7500 (s) OO FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN PART 3: CROWN RECOMMENDED SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - LOWER STRESS LOCATIONS (ALL AIRPLANES) (GROUP 6) MOS AFL 20O00 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 132 Of 748 @ Camp Systems EFTA00618423 CAMP Aiont.inn• AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YO006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2O14 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1334 TBL 2.3 CONTACT FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN THE BOEING RECOMMENDED COMPANY REPAIR INSTRUCTIONS AND DO THE REPAIR/REPEAT PART 2: CROWN SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC)INSPECTION - HIGHER STRESS LOCATIONS (B) MOS 04-AUG-2014 BF/F (s) SB 737-53-1334 TBL 2.5 CONTACT FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN THE BOEING RECOMMENDED COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR/ REPEAT PART 3: CROWN SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - LOWER STRESS LOCATIONS (IF CONDITION 3: ANY CRACK FOUND (DURING PART 3 MFEC INSPECTION OF LOWER STRESS LOCATIONS)) (GROUP 6) MOS 04-AUG-2014 SB 737-53-1335 31-JUL-2013 BF/F (s) FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS SB 737-53-1335 TABLE 11 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN NUMBER 1 WINDOW FRAME DETAILED AND HFEC INSPECTION FOR ANY CRACK INDICATION (FOR ALL AIRPLANES) (GROUP 1. CONFIGURATION 1-3) MOS AFL SB 737-53-1335 TABLE 1.2 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN NUMBER 1 WINDOW FRAME PREVENTIVE MODIFICATION DOUBLER INSTALLATION (IF NO CRACK INDICATION FOUND) (GROUP 1. CONFIGURATION 1-3) MOS AFL SB 737-53-1335 TABLE 1.3 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN NUMBER 1 WINDOW FRAME TEMPORARY REPAIR INSTALLATION OR REPLACEMENT (IF ANY CRACK INDICATION FOUND) (GROUP 1. CONFIGURATION 1-3) MOS SB 737-53-1335 TABLE 2.1 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN POST PREVENTIVE MODIFICATION DOUBLER INSTALLATION SEALANT INSPECTION (FOR AIRPLANES WITH THE PREVENTIVE MODIFICATION DOUBLER INSTALLED) (GROUP 1. CONFIGURATION 1-3) MOS AFL SB 737-53-1335 TABLE 2.3 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN SEALANT APPLICATION (IF SEALANT CRACKS. EROSION. SPLITS. LOOSE BEADS OR MISSING SECTIONS FOUND) (GROUP I. CONFIGURATION 1-3) MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time 133 Of 748 '2 Camp Systems EFTA00618424 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1335 TABLE 3.1 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER I WINDOW FRAME - MODIFICATION. SERVICE BULLETIN POST PREVENTIVE MODIFICATION DOUBLER INSTALLATION WINDOW FRAME DETAILED AND HFEC INSPECTION (FOR AIRPLANES WITH THE PREVENTIVE MODIFICATION DOUBLER INSTALLED) (GROUP 1. CONFIGURATION 1-3) MOS AFL SB 737-53-1335 TABLE 3.3 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN BOEING (IF ANY CRACK INDICATION FOUND) (GROUP 1. CONFIGURATION 1-3) SB 737-53-1336 23-OCT-2013 MOS FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 11MNDOW FRAME - PERMANENT REPAIR. SERVICE RECOMMENDED BULLETIN MOS SB 737-53-1336 TABLE 1.1 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN PART 12: POST PERMANENT REPAIR INSTALLATION NUMBER 1 WINDOW FRAME AND PERMANENT REPAIR TRIPLER HFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL SB 737-53-1336 TABLE 1.2 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN PART 12: POST PERMANENT REPAIR INSTALLATION NUMBER 1 WINDOW FRAME AND PERMANENT REPAIR TRIPLER HFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS AFL SB 737-53-1336 TABLE 1.3 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (CONDITION 2: ANY CRACK INDICATION FOUND) MOS SB 737-53-1336 TABLE 2.1 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN PART 13: POST PERMANENT REPAIR INSTALLATION FUSELAGE SKIN LFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 134 Of 748 @ Camp Systems EFTA00618425 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1336 TABLE 2.2 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN PART 13: POST PERMANENT REPAIR INSTALLATION FUSELAGE SKIN LFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS AFL SB 737-53-1336 TABLE 2.3 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (CONDITION 2: ANY CRACK INDICATION FOUND) MOS SB 737-53-1341 FUSELAGE - MISCELLANEOUS EXTERIOR SERVICE DOORS - EXTERNAL POWER RECEPTACLE DOOR - BONDING SUPERSEDED JUMPER INSPECTION AND REPLACEMENT (SUPERSEDED BY SB 737-53-1341 R1). SERVICE BULLETIN MOS SB 737-53-1341 RI FUSELAGE - MISCELLANEOUS EXTERIOR SERVICE DOORS - EXTERNAL POWER RECEPTACLE DOOR - BONDING RECOMMENDED JUMPER INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS 11-APR-2014 SB 737-53-1345 FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR RECOMMENDED . SERVICE BULLETIN MOS 05-NOV-2013 SB 737-53-1345 TABLE 1.1 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 1 NUMBER 3 WINDOW FRAME INSPECTION. COLD WORKING AND FREEZE PLUG INSTALLATION (AIRPLANES THAT COULD NOT BE REPAIRED WITH THE MAXIMUM FREEZE PLUG DIAMETER ALLOWED IN ACCORDANCE WITH BOEING SERVICE BULLETIN 737-53.1303) MOS SB 737-53-1345 TABLE 1.2.1 SB 737-53-1345 TABLE 1.2 .2 AFL ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 2: NUMBER 3 WINDOW FRAME SEPARATION (CONDITION 1: CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CANNOT BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 3: NUMBER 3 WINDOW FRAME CUTTING (CONDITION 1 CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CANNOT BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 135 Of 748 Camp Systems EFTA00618426 C O MP Mien winin Mernund up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1345 TABLE 1.2.3 SB 737-53-1345 TABLE 1.2.4 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 4: NUMBER 3 WINDOW FRAME PERMANENT REPAIR INSTALLATION (CONDITION 1: CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CANNOT BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS REPLACE FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME (CONDITION 1: CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CANNOT BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS SB 737-53-1345 TABLE 1.3 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 4: NUMBER 3 WINDOW FRAME PERMANENT REPAIR INSTALLATION (CONDITION 2: CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CAN BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS SB 737-53-1345 TABLE 2.1.1 SB 737-53-1345 TABLE 2.1.2 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 5: POST PERMANENT REPAIR INSTALLATION PERMANENT REPAIR TRIPLER HFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 6: POST PERMANENT REPAIR INSTALLATION NUMBER 3 WINDOW FRAME HFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL SB 737-53-1345 TABLE ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR 2.2.1 . SERVICE BULLETIN PART 5: POST PERMANENT REPAIR INSTALLATION PERMANENT REPAIR TRIPLER HFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS SB 737-53-1345 TABLE 2.2.2 AFL ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 6: POST PERMANENT REPAIR INSTALLATION NUMBER 3 WINDOW FRAME HFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 136 Of 748 @ Camp Systems EFTA00618427 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1345 TABLE 2.3 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (CONDITION 2: ANY CRACK INDICATION FOUND) MOS SB 737-53-1345 TABLE 3.1 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 7: POST PERMANENT REPAIR INSTALLATION REPAIR DOUBLER LFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL SB 737-53-1345 TABLE 3.2 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 7: POST PERMANENT REPAIR INSTALLATION REPAIR DOUBLER LFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS AFL SB 737-53-1345 TABLE 3.3 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (CONDITION 2: ANY CRACK INDICATION FOUND) MOS SB 737-53A1222 R1 POINT D SPLICE FITTING REPLACEMENT (SUPERSEDED BY 737-53A1222 R2). SERVICE BULLETIN SUPERSEDED MOS SB 737-53A1222 R2 FUSELAGE - SECTION 41 CAB - POINT D SPLICE FITTING REPLACEMENT (SUPERSEDED BY 737-53A1222 R3). SERVICE SUPERSEDED BULLETIN MOS SB 737-53A1222 R3 FUSELAGE - SECTION 41 CAB - POINT D SPLICE FITTING REPLACEMENT (SUPERSEDED BY 737-53A1222 R4). SERVICE SUPERSEDED BULLETIN MOS SB 737-53A1222 R4 FUSELAGE - SECTION 41 CAB - POINT D SPLICE FITTING REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 20-OCT-2005 AFL 13500 (s) SB 737-53A1238 FUSELAGE - SECTION 08 - STRUCTURE - INSPECTION (SUPERSEDED BY SS 737-53A1238 R1). SERVICE BULLETIN SUPERSEDED MOS - (s) 74nsufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 137 Of 748 @ Camp Systems EFTA00618428 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1238 RI FUSELAGE - SECTION 48 - STRUCTURE - INSPECTION. SERVICE BULLETIN RECOMMENDED DAYS 30 (s) 10-OCT-2002 SB 737-53A1242 SEALING AROUND VERTICAL FIN LUGS. SERVICE BULLETIN MOS 18 (s) I 7-OCT-2002 AFL 2500 SB 737-53A1242 RI FUSELAGE - STRUCTURE ATTACHMENT FITTINGS - INADEQUATE SEALING AROUND VERTICAL FIN LUGS. SERVICE COMPUED WITH - PREVIOUSLY BULLETIN MOS )8 (s) 13-OCT-2006 28-APR-2005 2686:29 AFL 2500 644 SB 737-53A1242 R2 FUSELAGE - STRUCTURE ATTACHMENT FITTINGS-INADEQUATE SEALING AROUND VERTICAL FIN LUGS. SERVICE COMPUED WITH - IAW THE AD BULLETIN MOS 22-AUG-2008 23-APR-2007 -(s) 3260:48 AFL 782 SB 737-53A1248 NDT INSPECTION OF WEB AT "r CHORD-ABOVE STR 15L AND ISR (STR SL TO 7L AND STR SR TO 9R). SERVICE RECOMMENDED BULLETIN MOS 09-SEP-2004 S8 737-53A1248 E(A)1 INSPECT (NON-DESTRUCTIVE TEST) NDT INSPECTION OF WEB AT 'r CHORD-ABOVE STR ISL AND 15R (STR 5L TO 7L RECOMMENDED AND STR 5R TO 9R). SERVICE BULLETIN (STR SL TO 7L AND STR SR TO 9R) MOS 09-SEP-2004 AFL 25000 (s) SB 737-53A1248 E(A)2 INSPECT (NON-DESTRUCTIVE TEST) NDT INSPECTION OF WEB AT 'r CHORD-ABOVE STR 15L AND 15R (STR 5L TO 7L RECOMMENDED AND STR 5R TO 9R). SERVICE BULLETIN (ABOVE STR 15L AND 15R EXCEPT 5L TO 7L AND 5R TO BR) MOS 09-SEP-2004 AFL 25000 (s) SB 737-53A1248 E(B) INSPECT (NON-DESTRUCTIVE TEST) NDT INSPECTION OF WEB AT -NT CHORD-ABOVE STR 15L AND 15R (STR 5L TO 7L RECOMMENDED AND STR 5R TO 9R). SERVICE BULLETIN 'Y-CHORD BELOW S-15UR MOS 09-SEP-2004 AFL 66000 (s) SB 737-53A1248 RI FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB - INSPECTION FOR WEB CRACKS AT THE Y-CHORD. SERVICE BULLETIN MOS 10-SEP-2007 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 138 Of 748 @ Camp Systems EFTA00618429 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1248 R1 E (A) INSPECTION FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB - INSPECTION FOR WEB 1 CRACKS AT THE Y-CHORD. SERVICE BULLETIN - NDT - OF WEB AT 1Y" CHORD STR 15L AND 15R (STR 5L TO 7L AND STR 5R TO 9R) MOS 10-SEP-2007 AFL 25000 (s) SB 737-53A1248 RI E (A) INSPECTION FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB- INSPECTION FOR WEB 2 CRACKS AT THE Y-CHORD. SERVICE BULLETIN - NDT - OF WEB AT'Y" CHORD (ABOVE STR 15L AND 15R EXCEPT 5L TO 7L AND 5R TO 9R) 10-SEP-2007 SB 737-53A1248 RI E (B) 10-SEP-2007 SB 737-53A1253 SB 737-53A1253 RI 13-MAY-2011 MOS AFL 25000 (s) INSPECTION FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB - INSPECTION FOR WEB CRACKS AT THE Y-CHORD. SERVICE BULLETIN - NDT - OF WEB ATI"' CHORD -BELOW S-15UR MOS AFL 66000 (s) FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING (SUPERSEDED BY SB 737-53A1253 R1). SERVICE BULLETIN MOS 22-AUG-2008 3260:48 AFL 782 FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING. SERVICE BULLETIN MOS (EFF) SUPERSEDED COMPUED WITH - TABLE 1 I.A.W. AD 2007-25-03 / TABLE 2 8 3 ARE N/A TO At SB 737-53A1253 RI GENERAL VISUAL INSPECTION FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR MANDATORY TABLE 1.1 WEB OIL CANNING. SERVICE BULLETIN FOR OIL CAN CONDITIONS OR BULGES FOR ALL AIRPLANES MOS RECURRING SB 737-53A1253 RI TABLE 1.2 SB 737-53A1253 RI TABLE 2.1 AFL 15000 15000 PERFORM FUSELAGE - GENERAL - STATION 1016 Af T PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING. MANDATORY SERVICE BULLETIN OPTION A: STEP 1 OF 2 OR STEP 2 OF 2 OR OPTION B MOS BF/F (s) GENERAL VISUAL INSPECTION FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR MANDATORY WEB OIL CANNING. SERVICE BULLETIN TO IDENTIFY REPAIRS TO THE GORE WEB 8 VERIFY THAT THEY HAVE FOLLOW-ON INSPECTIONS (SRM SECTION 53-80-08-2R) FOR ALL AIRPLANES MOS AFL 15000 15000 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 139 Of 748 @ Camp Systems EFTA00618430 COMP Astant.fran 'Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1253 RI TABLE 2.2 DETERMINE FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING. SERVICE BULLETIN FAA APPROVED FOLLOW-ON INSPECTION PROCEDURES. THRESHOLDS. AND REPEAT INTERVALS AND INCORPORATE INTO MAINTENANCE PROGRAM IF A REPAIR IS FOUND THAT DOES NOT HAVE FOLLOW-ON SUPPLEMENTAL INSPECTIONS MOS 12(s) MANDATORY SB 737-53A1253 RI FM FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING. MANDATORY TABLE 3 SERVICE BULLETIN APPROVED REPAIR INSPECTION PROCEDURES MOS AFL 36000 (s) SB 737-53A1253 TABLE 1 PERFORM A GENERAL VISUAL INSPECTION FOR OIL CAN CONDITIONS OR BULGES AS GIVEN IN ACCOMPLISHMENT INSTRUCTIONS. 3.8.2 OR 3.8.3. SERVICE BULLETIN MOS 22-AUG-2008 I8-MAY-2007 3260:48 AFL 10000 (s) 782 SB 737-53A1253 TABLE 2 GENERAL VISUAL INSPECTION TO IDENTIFY REPAIRS TO THE GORE WEB 8 VERIFY THAT THEY HAVE FOLLOW-ON INSPECTIONS (SRM SECTION 53-80-08-2R). SERVICE BULLETIN MOS 22-AUG-2008 I8-MAY-2007 - (s) 3260:48 AFL 782 SB 737-53A1253 TABLE 3 FM APPROVED REPAIR INSPECTION PROCEDURES. SERVICE BULLETIN MOS 22-AUG-2008 I8-MAY-2007 3260:48 SB 737-53A1289 SB 737-53A1289 R1 I8-NOV-2009 SB 737-53A1289R1 TABLE (1.1) I8-NOV-2009 AFL 24000 (s) 782 INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN MOS AFL INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN MOS SUPERSEDED RECOMMENDED EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE FOR ANY SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.1. PART 1 -SKIN LAP JOINT - ZONE 1 INSPECTION (GROUP 1-5) MOS AFL 4000 (s) COMPLIED WITH NOT APPLICABLE NOT APPLICABLE 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 140 Of 748 @ Camp Systems EFTA00618431 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (1.10) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN . HFEC INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10.A. PART 10 - LRTS PROGRAM INSPECTION.IN ZONE 17 (GROUP 1-5) MOS RECOMMENDED AFL 40O00 (s) SS 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (1.11) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.10.8. PART 10 -LRTS PROGRAM INSPECTION. IN ZONE 18 (GROUP 1-5) MOS AFL 50000 (s) S8 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (1.12) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.10.C. PART 10 -LRTS PROGRAM INSPECTION. IN ZONE 19 (GROUP 1-5) SB 737-53A1289 RI TABLE (1.14) S8 737-53A1289 RI TABLE (1.2) I8-NOV-2009 MOS AFL 50000 (s) CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR ADDITIONAL INSPECTIONS OR REPAIR (GROUP 1-5) MOS RECOMMENDED AFL 75000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.2. PART 2 -SKIN LAP JOINT - ZONE 2 INSPECTION (GROUP 1-5) MOS AFL 40O0 (s) SS 737-53A1289 RI PERFORM INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN INSPECTIONS AS NEEDED IF ANY RECOMMENDED TABLE (1.4) SCRIBE LINE IS FOUND (GROUP 1-5) S8 737-53AI289 RI TABLE (1.7) MOS BF/F (s) HFEC INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AND UT INSPECTION OF THE SCRIBE LINE RECOMMENDED FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.9. PART 9 - SCRIBE UNE INSPECTION. IN ZONE 1 (GROUP 1-5) MOS AFL 40000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 141 Of 748 @ Camp Systems EFTA00618432 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 737-53A1289 RI TABLE (1.8) SS 737-53A1289 Ft1 TABLE (10.1) HFEC INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN INSPECTION AND UT INSPECTION OF THE RECOMMENDED SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.9. PART 9 - SCRIBE LINE IN ZONE 2 (GROUP 1-5) INSPECTION. MOS AFL 50000 (s) DETERMINE INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN THE THICKNESS OF THE PARENT RECOMMENDED SKIN IN THE AREA OF THE EXTERNAL APPROVED REPAIR BETWEEN STA 360 AND STA 1016 AND BELOW S-10L AND 5-10R WHICH IS 20 INCHES OR LONGER IN THE FORE AND AFT DIRECTION WITH NO CIRCUMFERENTIAL LIMITATIONS MOS AFL 40O0 (s) SS 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (10.11) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM EXTERNAL APPROVED REPAIR REPEAT INSPECTION.(G) SCRIBE LINE IS FOUND COMMON TO EXTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.040 - 0.044 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION MOS AFL 1500 (s) SS 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (10.12) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM EXTERNAL APPROVED REPAIR REPEAT INSPECTION.(G) SCRIBE LINE IS FOUND COMMON TO EXTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.045 - 0.049 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION 61OS AFL 2000 (s) SS 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (10.13) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM EXTERNAL APPROVED REPAIR REPEAT INSPECTION.(G) SCRIBE LINE IS FOUND COMMON TO EXTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.050 - 0.055 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION. S8 737-53A1289 RI TABLE (10.15) MOS AFL 3000(s) CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR ADDITIONAL INSPECTIONS OR REPAIR ALL AIRPLANES WITH SCRIBE LINE USING A LRTS PROGRAM INSPECTION MOS AFL 75000 (s) RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 142 Of 748 @ Camp Systems EFTA00618433 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (10.2) SB 737-53AI289 RI TABLE (10.3) SB 737-53A1289 R1 TABLE (10.4) I8-NOV-2009 SB 737-53AI289 RI TABLE (10.5) I8-NOV-2009 SB 737-53A1289 RI TABLE (11.1) 18-N0V-2809 DETERMINE INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN THE THICKNESS OF THE PARENT RECOMMENDED SKIN IN THE AREA OF THE EXTERNAL APPROVED REPAIR EXISTING EXTERNAL APPROVED REPAIR LOCATED BETWEEN STA 360 AND STA 1016 AND ABOVE S-10L AND S-10R WHICH IS 20 INCHES OR LONGER IN THE FORE AND AFT DIRECTION OR WIDER THAN 12 INCHES CIRCUMFERENTIALLY. (B) MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.5. PART 5 - EXTERNAL APPROVED REPAIR - INSPECTION PARENT SKIN THICKNESS 0.040 - 0.044 INCH IN THE AREA OF THE EXTERNAL APPROVED REPAIR MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.5. PART 5 - EXTERNAL APPROVED REPAIR - INSPECTION PARENT SKIN THICKNESS 0.045 - 0.049 INCH IN THE AREA OF THE EXTERNAL APPROVED REPAIR. MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 32.5. PART 5 - EXTERNAL APPROVED REPAIR - INSPECTION (AXB) PARENT SKIN THICKNESS 0.050 - 0.055 INCH IN THE AREA OF THE EXTERNAL APPROVED REPAIR MOS AFL 4000 (s) DETERMINE INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN THE THICKNESS OF THE PARENT RECOMMENDED SKIN IN THE AREA OF THE INTERNAL APPROVED REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.6. PART 6- INTERNAL APPROVED REPAIR - INSPECTION.EXISTING INTERNAL APPROVED REPAIR LOCATED BETWEEN STA 360 AND STA 1016 AND BELOW 5-10L AND 5-10R AND THE SKIN CUTOUT IS GREATER THAN 20 INCHES LONG IN THE FORE AND AFT DIRECTION WITH NO CIRCUMFERENTIAL LIMITATIONS. MOS AFL 4000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 143 Of 748 @ Camp Systems EFTA00618434 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 737-53A1289 R1 TABLE (11.10) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM INTERNAL APPROVED REPAIR REPEAT INSPECTION SCRIBE LINE IS FOUND COMMON TO INTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.040 - 0.044 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION MOS RECOMMENDED AFL 2600 (s) SB 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (11.11) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM INTERNAL APPROVED REPAIR REPEAT INSPECTION SCRIBE LINE IS FOUND COMMON TO INTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.045 - 0.049 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION SB 737-53A1289 RI TABLE (11.12) SB 737-53A1289 RI TABLE (11.2) I8-NOV-2009 S8 737-53A1289 RI TABLE (11.3) I8-NOV-2009 MOS AFL 2500 (s) CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR ADDITIONAL INSPECTIONS OR REPAIR. ALL AIRPLANES WITH SCRIBE LINE USING A LRTS PROGRAM INSPECTION MOS RECOMMENDED AFL 75000 (s) DETERMINE INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN THE THICKNESS OF THE PARENT RECOMMENDED SKIN IN THE AREA OF THE INTERNAL APPROVED REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.6. PART 6- INTERNAL APPROVED REPAIR - INSPECTION EXISTING INTERNAL APPROVED REPAIR LOCATED BETWEEN STA 360 AND STA 1016 AND ABOVE S-10L AND S-10R AND THE SKIN CUTOUT IS GREATER THAN 20 INCHES LONG IN THE FORE AND AFT DIRECTION OR WIDER THAN 12 INCHES CIRCUMFERENTIALLY MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN ANY SCRIBE RECOMMENDED UNE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.6. PART 6 - INTERNAL APPROVED REPAIR - INSPECTION PARENT SKIN THICKNESS 0.040 - 0.044 INCH INCHES IN THE AREA OF THE INTERNAL APPROVED REPAIR. MOS AFL 4000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 144 Of 748 @ Camp Systems EFTA00618435 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (11.4) I8-NOV-20D9 SB 737-53AI289 RI TABLE (3.1) SB 737-53A1289 RI TABLE (3.11) SB 737-53A1289 RI TABLE (3.2) SB 737-53A1289 RI TABLE (3.4) SB 737-53A1289 RI TABLE (3.8) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.6. PART 6 - INTERNAL APPROVED REPAIR - INSPECTION PARENT SKIN THICKNESS 0.045 - 0.049 INCH IN THE AREA OF THE INTERNAL APPROVED REPAIR MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN OF CIRCUMFERENTIAL BUTT JOINT STA 887 BETWEEN S-10L AND 5-10R FOR ANY SCRIBE LINE IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.3. PART 3-CIRCUMFERENTIAL BUTT JOINT -INSPECTION. (GROUP 1-3.5-8.10) MOS AFL 40000 (s) CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR ADDITIONAL INSPECTIONS OR REPAIR FOR ALL AIRPLANES WITH SCRIBE LINE USING A LRTS PROGRAM INSPECTION. (GROUP 1-3.5-8. 10) MOS AFL 75000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN OF CIRCUMFERENTIAL BUTT JOINT STA 360 BETWEEN S-10L AND S-1 0R FOR ANY SCRIBE LINE IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.3. PART 3 -CIRCUMFERENTIAL BUTT JOINT -INSPECTION. (GROUP 1-3.5-8.10) MOS RECOMMENDED RECOMMENDED RECOMMENDED AFL 45000 (s) ACCOMPLISH INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN INSPECTIONS AS NEED FOR ANY RECOMMENDED SCRIBE LINE FOUND MOS BF/F (s) LFEC INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN - EXTERNAL - SLIDING PROBE INSPECTION RECOMMENDED OR AN INTERNAL MFEC INSPECTION OR AN EXTERNAL HFEC PENCIL PROBE INSPECTION OR AN INTERNAL HFEC INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS (GROUP 1-3.5-8. 10) PARAGRAPH 3.6.10.D. PART 10 - LRTS PROGRAM CIRCUMFERENTIAL BUTT JOINT - REPEAT INSPECTION STATION 360 (GROUP 1-3.5-8.10) MOS AFL 45000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 145 Of 748 @ Camp Systems EFTA00618436 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (3.9) SB 737-53A1289 RI TABLE (6.1) 18-NOV-2009 SB 737-53A1289 RI TABLE (6.12) SB 737-53A1289 RI TABLE (6.13) SB 737-53A1289 RI TABLE (6.14) LFEC INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN - EXTERNAL - SLIDING PROBE INSPECTION RECOMMENDED OR AN INTERNAL MFEC INSPECTION OR AN EXTERNAL HFEC PENCIL PROBE INSPECTION OR AN INTERNAL HFEC INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10.D. PART 10 - LRTS PROGRAM CIRCUMFERENTIAL BUTT JOINT -REPEAT INSPECTION. STATION 887 (GROUP 1-3.5-8. 10) MOS AFL 40000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 32.4. PART 4 -DECAL - INSPECTION. IN ZONE 6 (GROUP 2.7) MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AND HFEC RECOMMENDED INSPECTION OF THE SCRIBE LINES FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.10. PART 10 - LRTS PROGRAM REPEAT INSPECTION. (A)IN ZONE 6 (GROUP 2. 7) MOS AFL 10000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AND HFEC RECOMMENDED INSPECTION OF THE SCRIBE LINES FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10 - LRTS PROGRAM REPEAT INSPECTION. IN ZONE 7 (GROUP 2.7) MOS AFL WOO (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AND HFEC RECOMMENDED INSPECTION OF THE SCRIBE LINES FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.10. PART 10 - LRTS PROGRAM REPEAT INSPECTION IN ZONE 8 (GROUP 2.7) MOS AFL 2500 (s) SB 737-53A1289 RI CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR FOR ADDITIONAL RECOMMENDED TABLE (6.16) INSPECTIONS OR REPAIRALL AIRPLANES WITH SCRIBE LINE USING A LRTS PROGRAM INSPECTION (GROUP 2. 7) MOS AFL 75000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 146 Of 748 @ Camp Systems EFTA00618437 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (6.2) I8-NOV-2009 SB 737-53A1289 RI TABLE (6.3) I8-NOV-2009 ACCOMPLISH INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN EXTERNAL GENERAL VISUAL INSPECTIONFOR ANY SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.4. PART 4 - DECAL - INSPECTIONIN ZONE 6 (GROUP 2. 7) MOS RECOMMENDED AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.4. PART 4 - DECAL - INSPECTION. IN ZONE 7 (GROUP 2. 7) MOS AFL 4000 (s) SB 737-53A1289 RI PERFORM INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AN EXTERNAL GENERAL VISUAL RECOMMENDED TABLE (6.4) INSPECTION FOR ANY SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 32.4. PART 4 - DECAL -INSPECTION. IN ZONE 7 (GROUP 2.7) I8-NOV-2009 SB 737-53A1289 RI TABLE (6.5) I8-NOV-2009 MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.4. PART 4 -DECAL - INSPECTION. IN ZONE 8 (GROUP 2.7) MOS AFL 4000 (s) SB 737-53A1289 Ft1 ACCOMPLISH INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN EXTERNAL GENERAL VISUAL RECOMMENDED TABLE (6.6) INSPECTION FOR ANY SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.4. PART 4 - DECAL -INSPECTION IN ZONE 8 (GROUP 2.7) I8-NOV-2009 SB 737-53A1325 03-DEC-2013 MOS AFL 4000 (s) FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER MANDATORY CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN MOS SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 1.01 LH WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE LEFT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE LEFT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1 (FOR ALL AIRPLANES) (GROUP 1) MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 147 Of 748 @ Camp Systems EFTA00618438 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 1.01 RH DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1 (FOR ALL AIRPLANES) (GROUP 1) MOS AFL SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 1.02 LH WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE LEFT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE LEFT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.J. (IF NO CRACK FOUND ON BOTH THE LEFT AND RIGHT SIDES) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 1.02 RH WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.J. (IF NO CRACK FOUND ON BOTH THE LEFT AND RIGHT SIDES) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.03 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 1 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP IA. (IF ANY CRACK FOUND. ON THE LEFT SIDE. LESS THAN OR EQUAL TO 0.18 INCHES) (GROUP 1) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.04 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 1 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.8. (ANY CRACK FOUND. ON THE RIGHT SIDE. LESS THAN OR EQUAL TO 0.18 INCHES) (GROUP 1) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.05 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 2 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.0 (IF ANY CRACK FOUND. ON THE LEFT SIDE. GREATER THAN 0.18 INCHES AND LESS THAN OR EQUAL TO 1.50 INCHES IN LENGTH. THAT DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 148 Of 748 @ Camp Systems EFTA00618439 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.06 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 2 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.0. (IF ANY CRACK FOUND. ON THE RIGHT SIDE. GREATER THAN 0.18 INCHES AND LESS THAN OR EQUAL TO 1.50 INCHES IN LENGTH. THAT DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.07 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 3 IN ACCOR DANCE WITH PARAGRAPH 3.B..WORK INSTRUCTIONS. PART 2. STEP 1.E. (IF ANY CRACK FOUND. ON THE LEFT SIDE. GREATER THAN 0.18 INCHES. THAT EXTENDS INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.08 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 3 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP IF. (IF ANY CRACK FOUND. ON THE RIGHT SIDE. GREATER THAN 0.18 INCHES. THAT EXTENDS INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.09 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING. (IF ANY CRACK FOUND GREATER THAN 1.50 INCHES IN LENGTH AND DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS SB 737-53A1325 TABLE ACCOMPLISH FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB 1.10 AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN PREVENTIVE MODIFICATION ON THE LEFT SIDE IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.H. (IF NO CRACK FOUND ON THE LEFT SIDE AND A REPAIR WAS ACCOMPLISHED ON THE RIGHT SIDE) (GROUP 1) MOS SB 737-53A1325 TABLE ACCOMPLISH FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB 1.11 AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN PREVENTIVE MODIFICATION ON THE RIGHT SIDE IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.1. (IF NO CRACK FOUND ON THE RIGHT SIDE AND A REPAIR WAS ACCOMPLISHED ON THE LEFT SIDE) (GROUP 1) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 149 Of 748 @ Camp Systems EFTA00618440 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 2.01 DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2 (ALL AIRPLANES) (GROUP 2) MOS AFL SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 2.02 WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.E. (NO CRACK FOUND ON THE RIGHT SIDE) (GROUP 2) MOS - Is) SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.03 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 1 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.A. (ANY CRACK FOUND LESS THAN OR EQUAL TO 0.18 INCHES) (GROUP 2) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.04 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 2 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.8. (ANY CRACK FOUND GREATER THAN 0.18 INCHES AND LESS THAN OR EQUAL TO 1.50 INCHES IN LENGTH. THAT DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 2) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.05 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 3 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.C. (ANY CRACK FOUND GREATER THAN 0.18 INCHES. THAT EXTENDS INTO THE FLANGE OF THE INNER CHORD) (GROUP 2) MOS SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.06 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND GREATER THAN 1.50 INCHES IN LENGTH AND DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 2) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 150 Of 748 @ Camp Systems EFTA00618441 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.07 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR LEFT SIDE INSPECTION AND MODIFICATION INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ALL AIRPLANES) (GROUP 2) MOS AFL SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 3.01 WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2 (ALL AIRPLANES) (GROUP 3) MOS AFL SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 3.02 WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2. (NO CRACK FOUND) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 3.03 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 1 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.A. (ANY CRACK FOUND LESS THAN OR EQUAL TO 0.18 INCHES) (GROUP 3) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 3.04 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 2 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.8. (ANY CRACK FOUND GREATER THAN 0.18 INCHES AND LESS THAN OR EQUAL TO 1.50 INCHES IN LENGTH. THAT DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 3) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 3.05 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 3 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.C. (ANY CRACK FOUND GREATER THAN 0.18 INCHES. THAT EXTENDS INTO THE FLANGE OF INNER CHORD) (GROUP 3) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 151 Of 748 @ Camp Systems EFTA00618442 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 3.06 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND GREATER THAN 1.50 INCHES IN LENGTH AND DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 3) MOS SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.01.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 2.A. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.01.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 2.8. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.02.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 5.A. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.02.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 5.8. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.03.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.A. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.03.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.8. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 152 Of 748 @ Camp Systems EFTA00618443 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 4.04.1 HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.A. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.04.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.8. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPUSHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.05 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 4. STEP 3. (AIRPLANES WITH REPAIR 2 ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.06 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 3. (AIRPLANES WITH REPAIR 2 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.07 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 4. STEP 4. (AIRPLANES WITH REPAIR 3 ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.08 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 4. (AIRPLANES WITH REPAIR 3 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 4.09 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND) (GROUP 1) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 153 Of 748 @ Camp Systems EFTA00618444 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 5.01.1 HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.A. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.01.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.8. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.02.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.A. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.02.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.8. (AIRPLANES WITH THE PREVENTNE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 2) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.03 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 3. (AIRPLANES WITH REPAIR 2 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.04 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 4. (AIRPLANES WITH REPAIR 3 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 5.05 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND) (GROUP 2) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 154 Of 748 @ Camp Systems EFTA00618445 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 6.01.1 HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE LEFT SIDE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 6.A. (ALL AIRPLANES) (GROUP 3) MOS AFL SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 6.01.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE LEFT SIDE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 4. STEP 6.8. (ALL AIRPLANES) (GROUP 3) MOS AFL SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 802.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.A. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 3) MOS - SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 802.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.8. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 803.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.A. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 803.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.8. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 6.04 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 3. (AIRPLANES WITH REPAIR 2 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 3) MOS - Is) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 155 Of 748 @ Camp Systems EFTA00618446 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 6.05 HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 4. (AIRPLANES WITH REPAIR 3 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 6.06 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND) (GROUP 3) MOS SB 737-54-1039 STRUT -APPLICATION OF °saki ANT AT BULKHEAD/DIAGONAL BRACE INTERFACE. SERVICE BULLETIN 13-JUN-2002 MOS 18 (5) 800 SB 737-54-1039 RI APPLICATION OF SEALANT AT BULKHEAD/DIAGONAL BRACE INTERFACE, SERVICE BULLETIN COMPLIED WITH MOS 18(s) 11-MAY-2006 IO-OCT-2002 2619:10 AFL 3500 629 SB 737-54-1040 14-NOV-2002 GENERAL VISUAL INSPECTION OF SEALANT ON ENGINE STRUT STRUCTURE. SERVICE BULLETIN MOS 18 (s) AFL 3500 SB 737-54-1040 RI APPLICATION OF SEALANT ON ENGINE STRUT STRUCTURE. SERVICE BULLETIN COMPLIED WITH MOS 18 (s) 18-AUG-2006 14-NOV-2002 2633:50 AFL 3500 633 SB 737-54-1040 R2 APPLICATION OF SEALANT ON ENGINE STRUT STRUCTURE. SERVICE BULLETIN MOS 18 (5) 07-NOV-2006 AFL 3500 SB 737-54-1040 R3 APPLICATION OF SEALANT ON ENGINE STRUT STRUCTURE. SERVICE BULLETIN MOS 18 (5) 14-NOV-2002 AFL 3500 SB 737-54-1041 ENGINE STRUT AFT FAIRING. SERVICE BULLETIN COMPLIED WITH 22,JAN-2004 MOS AR 24-AUG-2007 2968:28 AFL 699 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 156 Of 748 @ Camp Systems EFTA00618447 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-54-1041 PART 1811 INSPECT ENGINE STRUT AFT FAIRING. SERVICE BULLETIN FOR FLUID ACCUMULATION MOS 30 (s) 22-JAN-2004 24-AUG-2007 2968:28 AFL 4000 699 SB 737-54-1041 PART MODIFY ENGINE STRUT AFT FAIRING. SERVICE BULLETIN SEALS IIIBN 22-JAN-2004 MOS 24-AUG-2007 2968:28 AFL 9000 (s) 699 SB 737-54-1041 RI ENGINE STRUT AFT FAIRING. SERVICE BULLETIN MOS 24-AUG-2007 OI -DEC-2005 2968:28 COMPUED WITH COMPUED WITH RECOMMENDED COMPUED WITH - IAW THE AD AD 2006-07-04 /MARTS 1.11 AND III MOD SB 737-54-1041R1 REF (R2) - IN 02) AFL 699 SB 737-54-1041 RI PART INSPECT ENGINE STRUT AFT FAIRING. SERVICE BULLETIN FOR FLUID ACCUMULATION COMPUED WITH 18.11 MOS 30 (s) 24-AUG-2007 OI -DEC-2005 2968:28 AFL 4000 699 SB 737-54-1041 RI PART MODIFY ENGINE STRUT AFT FAIRING. SERVICE BULLETIN SEALS RECOMMENDED COMPUED WITH IIIBN MOS 24-AUG-2007 12-JAN-2005 - (s) 2968:28 AFL 699 SB 737-54-1041 R2 NACELLES / PYLONS - AFT FAIRING - FLUID ACCUMULATION IN ENGINE STRUT AFT FAIRING -INSTALLATION OF NEW ENGINE STRUT AFT FAIRING SEALS. SERVICE BULLETIN MOS 03-OCT-2007 SB 737-54-1041 R2 PART INSPECT NACELLES / PYLONS - AFT FAIRING - FLUID ACCUMULATION IN ENGINE STRUT AFT FAIRING -INSTALLATION 1811 OF NEW ENGINE STRUT AFT FAIRING SEALS. SERVICE BULLETIN FOR FLUID ACCUMULATION MOS 30 (s) 03-OCT-2007 AFL 4000 SB 737-54-1041 R2 PART MODIFY NACELLES / PYLONS - AFT FAIRING - FLUID ACCUMULATION IN ENGINE STRUT AFT FAIRING -INSTALLATION III & IV OF NEW ENGINE STRUT AFT FAIRING SEALS. SERVICE BULLETIN SEALS 03-OCT-2007 MOS AFL 9000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 157 Of 748 @ Camp Systems EFTA00618448 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-54-1042 I2-FEB-2004 SB 737-54-1042 RI ENGINE STRUT UPPER LINK - INSPECTION / MODIFICATION. SERVICE BULLETIN 30-JUL-2009 SB 737-54-1043 NACELLES/PYLONS - STRUT DRAINS AND SEALS - AFT FAIRING DRAIN TUBE ASSEMBLY REPLACEMENT.. SERVICE BULLETIN 02-MAY-2007 ENGINE STRUT UPPER LINK-INSPECTION MODIFICATION. SERVICE BULLETIN MOS 30 (s) MOS 30 (s) MOS 60 (s) RECOMMENDED SB 737-54-1043 RI STRUT DRAINS AND SEALS - AFT FAIRING DRAIN TUBE ASSEMBLY SUPERSEDED REPLACEMENT.(SUPPERSEDED BY 737-54-1043 R2). SERVICE BULLETIN MOS - Is) SB 737-54-1043 R2 NACELLES/PYLONS- STRUT DRAINS AND SEALS- AFT FAIRING DRAIN TUBE ASSEMBLY REPLACEMENT SUPERSEDED (SUPERSEDED BY SB 737-54-1043 R3). SERVICE BULLETIN MOS - Is) SB 737-54-1043 R3 NACELLES/PYLONS - STRUT DRAINS AND SEALS - AFT FAIRING DRAIN TUBE ASSEMBLY REPLACEMENT. SERVICE RECOMMENDED BULLETIN MOS 60 (s) 31-DEC-2012 SB 737-54-1045 NACELLES/PYLONS - HEAT INSULATION BLANKETS - REPLACEMENT. SERVICE BULLETIN MOS 29-AUG-2011 25-JUL-2007 - (s) 3533:32 SB 737-54-1046 SB 737-54-1046 RI AFL 863 NACELLES/PYLONS -STRUT TO WING FAIRINGS - THUMBNAIL FAIRING EDGE SEAL REPLACEMENT (SUPERSEDED BY SUPERSEDED SB 737-54-1046 RI), SERVICE BULLETIN MOS - (s) NACELLES/PYLONS - STRUT TO WING FAIRINGS - THUMBNAIL FAIRING EDGE SEAL REPLACEMENT. SERVICE BULLETIN MOS SB 737-54-1047 NACELLES/PYLONS - STRUT AFT FAIRING HEAT SHIELD ASSEMBLY AND INSULATION BLANKET INSTALLATION. RECOMMENDED SERVICE BULLETIN MOS 14-SEP-2012 COMPLIED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 158 Of 748 @ Camp Systems EFTA00618449 C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SS 737-54-1049 13-SEP-2012 NACELLES/PYLONS- STRUT DRAINS AND SEALS - STRUT SEAL PLANE ACCESS PANELS LEAK INSPECTION. SERVICE RECOMMENDED BULLETIN MOS SB 737-54-1049 TABLE 1.1 DETAILED INSPECTION NACELLES/PYLONS- STRUT DRAINS AND SEALS - STRUT SEAL PLANE ACCESS PANELS LEAK RECOMMENDED INSPECTION. SERVICE BULLETIN OF THE STRUT SEAL PLANE ACCESS PANELS FOR ANY LEAK (GROUP 1 AIRPLANES) MOS 30 (s) AFL 9000 SB 737-54-1049 TABLE 1.2 DETAILED INSPECTION NACELLES/PYLONS- STRUT DRAINS AND SEALS - STRUT SEAL PLANE ACCESS PANELS LEAK INSPECTION. SERVICE BULLETIN OF THE STRUT SEAL PLANE ACCESS PANELS FOR ANY LEAK (GROUP 2 AIRPLANES) MOS 36 (s) RECOMMENDED SB 737-55-1062 LEADING EDGE RIB. SERVICE BULLETIN RECOMMENDED MOS 10-AUG-2000 - (s) SB 737-55-1063 TAB MAST FITTING. SERVICE BULLETIN RECOMMENDED COMPLIED WITH - CM MOS 13-SEP-1999 01 -JUL-1999 - SB 737-55-1063 RI TAB MAST FITTING. SERVICE BULLETIN RECOMMENDED MOS 18 (s) 14-SEP-2000 AFL 4000 SB 737-55-1067 ELEVATOR HINGE PLATES. SERVICE BULLETIN NOT APPLICABLE - NO ACTION REQUIRED MOS 22-AUG-2003 1342 AFL 351 SB 737-55-1069 LOWER CLOSURE RIB & RUDDER HINGE PLATE NUT. SERVICE BULLETIN RECOMMENDED MOS 31-AUG-2000 - (s) SB 737-55-1074 INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS. SERVICE BULLETIN RECOMMENDED COMPLIED WITH - PERMANENT REPAIR. PART 3 OF SB. MOS 09-AUG-2010 15-AUG-2000 3448:31 AFL 841 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 159 Of 748 @ Camp Systems EFTA00618450 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1074 PART 1 ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS. SERVICE BULLETIN INSPECTION MOS 18 (s) IS-AUG-2002 09-AUG-20I0 3448:31 AFL 841 SB 737-55-1074 PART 2 ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS. SERVICE BULLETIN INTERIM REPAIR MOS 18 (s) 22-AUG-2008 3260:48 COMPLIED WITH - PERMANENT REPAIR. PART 3 OF SB. COMPLIED WITH AFL 782 SB 737-55-1074 PART 3 ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS. SERVICE BULLETIN PERMANENT REPAIR COMPLIED WITH - PERMANENT REPAIR. PART 3 OF SB. MOS 09-AUG-2010 - (s) 3448:31 AFL 841 SB 737-55-1074 RI INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS BETWEEN THE HORIZONTAL STABILIZERS AND THE RECOMMENDED COMPLIED WITH - PERMANENT REPAIR HORIZONTAL STABILIZER CENTER SECTION. SERVICE BULLETIN MOS 29-AUG-2011 18-DEC-2003 3533:32 AFL 863 SB 737-55-1074 RI PART ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS BETWEEN THE HORIZONTAL STABILIZERS COMPLIED WITH 1 AND THE HORIZONTAL STABILIZER CENTER SECTION. SERVICE BULLETIN INSPECTION MOS 18 (5) 29-AUG-20I I 18-DEC-2003 3533:32 AFL 863 SB 737-55-1074 RI PART ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS BETWEEN THE HORIZONTAL STABILIZERS RECOMMENDED 2 AND THE HORIZONTAL STABILIZER CENTER SECTION, SERVICE BULLETIN INTERIM REPAIR MOS 18 (5) 12-DEC-2003 SB 737-55-1074 RI PART ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS BETWEEN THE HORIZONTAL STABILIZERS RECOMMENDED COMPLIED WITH 3 AND THE HORIZONTAL STABILIZER CENTER SECTION. SERVICE BULLETIN PERMANENT REPAIR MOS 29-AUG-2011 09-SEP-2004 - (s) 3533:32 AFL 863 SB 737-55-1086 INSPECTION OF THE PINS AND BOLTS THAT ATTACH THE HORIZONTAL STABILIZER TO THE HORIZONTAL STABLIZER - IAW THE SB CENTER SECTION (SUPERSEDED BY SB 737-55-1086 RI). SERVICE BULLETIN MOS 22-AUG-2008 II -DEC-2003 3260:48 AFL 782 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 160 Of 748 © Camp Systems EFTA00618451 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB SB 737-55-1086 RI 16-DEC-2004 [SSN REDACTED] R2 INSPECTION OF THE PINS AND BOLTS THAT ATTACH THE HORIZONTAL STABILIZER TO THE HORIZONTAL STABLIZER CENTER SECTION (SUPERSEDED BY SB 737-55-1086 R2). SERVICE BULLETIN MOS STABILIZERS - HORIZONTAL STABILIER - INSPECTION OF THE PINS AND BOLTS THAT ATTACH THE HORIZONTAL STABILIZER TO THE HORIZONTAL STABILIZER CENTER SECTION (SUPERSEDED BY SB 737-55-1086 R3). SERVICE BULLETIN - INFORMATION REF TO IR AND REV.2 (REPLACEMENT) SUPERSEDED COMPLIED WITH MOS 29-AUG-20m 3533:32 AFL 863 SB 737-55-1086 R3 STABILIZERS - HORIZONTAL STABILIZER - INSPECTION OF THE PINS AND BOLTS THAT ATTACH THE HORIZONTAL RECOMMENDED STABILIZER TO THE HORIZONTAL STABILIZER CENTER SECTION. SERVICE BULLETIN DAYS 90 (5) 13-JUN-2012 SB 737-55-1089 HORIZONTAL STABILIZER - TRAILING EDGE PANEL. CONDUCTIVE STRIP AND TIP CAP ASSEMBLY - CHANGE SUPERSEDED (SUPERSEDED BY SB 737-55-1089 R1). SERVICE BULLETIN MOS SB 737-55-1089 RI STABILIZERS - HORIZONTAL STABILIZER - TRAILING EDGE PANEL. CONDUCTIVE STRIP AND TIP CAP ASSEMBLY - RECOMMENDED CHANGE. SERVICE BULLETIN MOS 09-SEP-201 SB 737-55-1090 STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR TERMINATION FITTING- INSPECTION. SERVICE BULLETIN MANDATORY MOS 30-MAR-201 I SB 737-55-1090 TABLE 1 INSPECTION STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR TERMINATION FITTING - INSPECTION. SERVICE MANDATORY BULLETIN OF THE LEFT AND RIGHT SIDE HORIZONTAL STABILIZER IDENTIFICATION PLATE FOR A SERIAL NUMBER THAT START WITH SAX FOR ALL AIRPLANES MOS 12 (5) 30-MAR-201 I SB 737-55-1090 TABLE 1.2 DETAILED INSPECTION STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR TERMINATION FITTING - INSPECTION. MANDATORY SERVICE BULLETIN OF THE HORIZONTAL STABILIZER TERMINATION FITTING FASTENERS FOR INCORRECT BOLT PROTRUSION AND CHAMFER FOR HORIZONTAL STABILIZERS IDENTIFICATION PLATES WHICH HAVE A SERIAL NUMBER STARTING WITH SAIC. MOS 12 (5) 30-MAR-201 I SB 737-55-1090 TABLE 1.6 HFEC STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR TERMINATION FITTING - INSPECTION. SERVICE BULLETIN AND UT INSPECTIONS OF THE TERMINATION FITTING FOR CRACKS FOR NEW BACB30US14K( ) BOLT IS INSTALLED MOS 12 (5) 3C-MAR-201I MANDATORY ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time Camp Systems 161 Of 748 EFTA00618452 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1093 09-APR-2012 SB 737-55-1096 22-MAR-2013 STABILIZERS - HORIZONTAL STABILIZER - REPLACEMENT OF REAR SPAR ATTACH PINS WITH UNAPPROVED SURFACE COATING. SERVICE BULLETIN MOS AFL 3000(s) STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN MOS SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN DO A 1(01.1) DETAILED INSPECTION OF THE SKIN. MODIFICATION SKIN AND SPAR DOUBLERS FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN AN 1(01.2) EDDY CURRENT INSPECTION OF THE SKIN. MODIFICATION SKIN. SPLICE DOUBLERS AND SPAR LOWER CHORDS FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL 58 [SSN REDACTED] TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(01.3) LOW FREQUENCY EDDY CURRENT (LFEC) INSPECTION OF THE FRONT SPAR UPPER CHORD AFT FLANGE. FROM STAB STA 66.50 TO STAB TIP. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(01.4) HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE FRONT SPAR UPPER CHORD FORWARD FLANGE. FROM STAB STA 66.50 TO STAB TIP. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(01.5) LFEC INSPECTION OF THE FRONT SPAR UPPER CHORD WEB FLANGE. FROM STAB STA 66.50 TO STAB STA 175.5 AND FROM STAB STA 258.28 TO STAB TIP. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 162 Of 748 @ Camp Systems EFTA00618453 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1096 TABLE 1(01.6) DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD WEB FLANGE. FROM STAB STA 66.50 TO STAB STA 175.5 AND FROM STAB STA 258.28 TO STAB TIP. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(01.7) HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD FORWARD FLANGE. FROM STAB STA 175.5 TO STAB STA 258.28. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL RIGHT CYCLES MOS AFL SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE 1(02.1) BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IN ANY CRACK FOUND IN THE SKIN. MODIFICATION SKIN. SPAR DOUBLERS. SPLICE DOUBLERS OR SPAR LOWER CHORDS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS SB 737-55-1096 TABLE REMOVE STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN 1(03.1) THE CRACK DAMAGE IF ANY CRACK FOUND IN THE FRONT SPAR UPPER CHORD FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS 58 [SSN REDACTED] TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(00.1) DETAILED INSPECTION OF THE SKIN. MODIFICATION SKIN AND SPAR DOUBLERS FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN AN 1(00.2) EDDY CURRENT INSPECTION OF THE SKIN. MODIFICATION SKIN. SPLICE DOUBLERS AND SPAR LOWER CHORDS FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 163 Of 748 @ Camp Systems EFTA00618454 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1096 TABLE 1(04.3) DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A LFEC INSPECTION OF THE FRONT SPAR UPPER CHORD AFT FLANGE. FROM STAB STA 66.50 TO STAB TIP. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(04.4) HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD FORWARD FLANGE. FROM STAB STA 66.50 TO STAB TIP. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(04.5) LFEC INSPECTION OF THE FRONT SPAR UPPER CHORD WEB FLANGE. FROM STAB STA 66.50 TO STAB STA 175.5 AND FROM STAB STA 258.28 TO STAB TIP. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL 58 [SSN REDACTED] TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(04.6) HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD WEB FLANGE. FROM STAB STA 66.50 TO STAB STA 175.5 AND FROM STAB STA 258.28 TO STAB TIP. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL 58 [SSN REDACTED] TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(04.7) HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD FORWARD FLANGE. FROM STAB STA 175.5 TO STAB STA 258.28. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE 1(05.1) BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF ANY CRACK FOUND IN THE SKIN. MODIFICATION SKIN. SPAR DOUBLERS. SPLICE DOUBLERS OR SPAR LOWER CHORDS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 164 Of 748 @ Camp Systems EFTA00618455 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1096 TABLE REMOVE STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN THE CRACK DAMAGE IF ANY CRACK FOUND IN THE FRONT SPAR UPPER CHORD FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES 1(06.1) MOS SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(07.1) DETAILED INSPECTION OF THE SKIN. MODIFICATION SKIN AND SPAR DOUBLERS FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS AFL 58 [SSN REDACTED] TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN AN 1(07.2) EDDY CURRENT INSPECTION OF THE SKIN. MODIFICATION SKIN. SPLICE DOUBLERS AND SPAR LOWER CHORDS FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE RECOMMENDED 1(07.3) BULLETIN BOEING FOR ADDITIONAL POST MODIFICATION INSPECTIONS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE 1(08.1) BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF ANY CRACK FOUND IN THE SKIN. MODIFICATION SKIN. SPAR DOUBLERS. SPLICE DOUBLERS OR SPAR LOWER CHORDS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS 58 [SSN REDACTED] TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(09.1) DETAILED INSPECTION OF THE SKIN. MODIFICATION SKIN AND SPAR DOUBLERS FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 165 Of 748 @ Camp Systems EFTA00618456 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN AN 1(09.2) EDDY CURRENT INSPECTION OF THE SKIN. MODIFICATION SKIN. SPLICE DOUBLERS AND SPAR LOWER CHORDS FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE RECOMMENDED 1(09.3) BULLETIN BOEING FOR ADDITIONAL POST MODIFICATION INSPECTIONS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS 58 [SSN REDACTED] TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE 1(10.1) BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF ANY CRACK FOUND IN THE SKIN. MODIFICATION SKIN. SPAR DOUBLERS. SPLICE DOUBLERS OR SPAR LOWER CHORDS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES SB 737-55A1064 I5-OCT-1998 MOS ELEVATOR BALANCE PANEL ASSEMBLIES. SERVICE BULLETIN MOS 250(s) 44 RECOMMENDED SB 737-55A1064 R1 ELEVATOR BALANCE PANEL ASSEMBLIES. SERVICE BULLETIN RECOMMENDED NOT APPLICABLE - BY SERIAL NUMBER MOS 20-APR-2001 07-DEC-2000 - (s) 697:54 AFL 188 SB 737-55A1066 FRONT SPAR HINGE FITTING REPLACEMENT-HINGE 3-8. SERVICE BULLETIN NOT APPLICABLE - NO ACTION REQUIRED MOS 24 (s) 22-AUG-2003 19-SEP-2002 1342 AFL 18000 351 SB 737-55A1066 RI FRONT SPAR HINGE FITTING REPLACEMENT-HINGES 3-8. SERVICE BULLETIN - 737-55A1080R1 MOS 24 (s) 19-SEP-2002 AFL 18000 SB 737-55A1068 ELEVATOR TAB ASSEMBLY. SERVICE BULLETIN RECOMMENDED COMPLIED WITH -OW MOS I3-SEP-1999 09-JUN-1999 - Is) SB 737-55A1068 R1 ELEVATOR TAB ASSEMBLY. SERVICE BULLETIN RECOMMENDED MOS 11-JUN-1999 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 166 Of 748 @ Camp Systems EFTA00618457 COMP Astant.frn• thernand up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55A1068 R2 ELEVATOR TAB ASSEMBLY. SERVICE BULLETIN DAYS 15 (s) 24-FEB-2000 AFL 100 SB 737-55A1072 PKG 1 STABILIZERS - ELEVATOR - TAB ASSEMBLY - INSPECTION OF ELEVATOR TAB HINGE AND ELEVATOR TAB CONTROL MECHANISM. SERVICE BULLETIN MOS 28-DEC-2000 - Is) RECOMMENDED SB 737-55A1072 PKG 2 STABILIZERS - ELEVATOR - TAB ASSEMBLY- INSPECTION OF ELEVATOR TAB HINGE AND ELEVATOR TAB CONTROL RECOMMENDED MECHANISM. SERVICE BULLETIN MOS 28-DEC-2000 AFL 750(s) SB 737-55A1072 PKG 3 STABILIZERS - ELEVATOR - TAB ASSEMBLY- INSPECTION OF ELEVATOR TAB HINGE AND ELEVATOR TAB CONTROL RECOMMENDED MECHANISM. SERVICE BULLETIN MOS 28-DEC-2000 1500 (s) AFL 750 SB 737-55A1072 RI ELEVATOR HINGE AND TAB ASSEMBLY. SERVICE BULLETIN RECOMMENDED MOS 11 -JAN-2001 - (s) SB 737-55A1072 RI PKG 1 INSPECT ELEVATOR HINGE AND TAB ASSEMBLY. SERVICE BULLETIN MOS 20-APR-2001 11 -JAN-2001 702:24 AFL 250(s) 188 SB 737-55A1072 RI PKG 2 INSPECT ELEVATOR HINGE AND TAB ASSEMBLY. SERVICE BULLETIN MOS IWAN-2001 AFL 750(s) SB 737-55A1072 RI PKG 3 INSPECT ELEVATOR HINGE AND TAB ASSEMBLY. SERVICE BULLETIN MOS I I -JAN-2001 1500 (s) SB 737-55A1076 AFL 750 ELEVATOR TAB HINGE FASTNER REPLACEMENT. SERVICE BULLETIN MOS 24 (s) AFL 4500 RECOMMENDED RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 167 Of 748 @ Camp Systems EFTA00618458 MP Aseant.ftne tAernand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BB.1): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55A1079 19-JUL-2001 ELEVATOR TAB. SPEEDBRAKE RESTRICTION. PLACARD INSTALLATION. SERVICE BULLETIN MOS 1 (s) SB 737-55A1079 RI ELEVATOR TAB. SPEEDBREAK RESTRICTION, PLACARD INSTALLATION. SERVICE BULLETIN RECOMMENDED MOS I (s) 16-MAY-2002 SB 737-55A1080 ELEVATOR AND ELEVATOR TAB REPLACEMENT. SERVICE BULLETIN COMPUED WITH - PREVIOUSLY REF. AD 2003-03-22 / 737-55A1080R1 MOS 24 (s) 18-AUG-2006 19-SEP-2002 2633:50 AFL 18000 633 SB 737-55A1080 RI ELEVATOR AND ELEVATOR TAB REPLACEMENT, SERVICE BULLETIN COMPUED WITH MOS 22-AUG-2003 19-SEP-2002 1342 AFL 351 SB 737-55A1082 ELEVATOR MODIFICATION. SERVICE BULLETIN COMPLIED WITH - PREVIOUSLY MOS 24 (s) 22-AUG-2003 19-SEP-2002 1342 AFL 18000 351 SB 737-55A1082 RI MODIFICATION TO IMPROVE THE STRUCTURAL DAMPING CHARACTERISTICS AND ENHANCE THE WEAR - 737-55A1080RI CHARACTERISTICS OF THE ELEVATOR TAB. SERVICE BULLETIN MOS 24 (s) 19-SEP-2002 AFL 18000 SB 737-55A1084 HORIZONTAL STABILIZER - TRAILING EDGE - ELEVATOR BALANCE BAY PANEL SEAL TRIM. SERVICE BULLETIN RECOMMENDED MOS 07-MAR-2002 - (s) SB 737-55A1084 RI HORIZONTAL STABILIZER - ELEVATOR BALANCE BAY PANEL SEAL TRIM. SERVICE BULLETIN RECOMMENDED MOS 20-JUN-2002 - (s) SB 737-56-1011 DRAIN OPENABLE WINDOWS INSTALLATIONS. SERVICE BULLETIN RECOMMENDED MOS 19-NOV-1998 - (s) SB 737-56-1011 RI DRAIN OPENABLE WINDOWS INSTALLATIONS. SERVICE BULLETIN RECOMMENDED MOS 29-JUN-2000 - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks *-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 168 Of 748 @Camp Systems EFTA00618459 COMP Jm. tMrrnM•O AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-56-1014 INSPECTION AND REPLACEMENT OF NO. 3 FLIGHT COMPARTMENT WINDOWS. SERVICE BULLETIN MOS 26-APR-2001 SB 737-56-1016 -AUG-2005 SB 737-56-1017 I7-MAY-2006 SB 737-56-1017 RI AFL 2000 (s) WINDOWS - CONTROL CABIN SLIDING WINDOWS - NUMBER 2 OPENABLE WINDOW - HOLD OPEN LATCH ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS WINDOWS - FLIGHT COMPARTMENT - CONTROL CABIN FIXED WINDOWS - DELEATION OF NUMBER 4 AND NUMBER 5 WINDOWS (SUPERSEDED BY 737-56-1017 R1). SERVICE BULLETIN MOS WINDOWS - FLIGHT COMPARTMENT - CONTROL CABIN FIXED WINDOWS - DELETION OF NUMBER 4 AND NUMBER 5 SUPERSEDED WINDOWS. (SUPERSEDED BY SB 737-56-1017 R2). SERVICE BULLETIN MOS SB 737-56-1017 R2 WINDOWS - FLIGHT COMPARTMENT - CONTROL CABIN FIXED WINDOWS - DELETION OF NUMBER 4 AND NUMBER 5 RECOMMENDED WINDOWS.. SERVICE BULLETIN MOS 28-JAN-2011 SB 737-56-1024 WINDOWS - CONTROL CABIN SLIDING WINDOWS - LEFT SIDE AND RIGHT SIDE NUMBER 2 WINDOW FRAME REPAIR AND MODIFICATION. SERVICE BULLETIN MOS 21 -SEP-2007 SB 737-56-1025 20-JAN-2010 SB 737-56-1025 (LH) SB 737-56-1025 (RH) FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2 WINDOW PANE - REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS REPLACE FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2 WINDOW PANE- REPLACEMENT. SERVICE BULLETIN RECOMMENDED LEFT FLIGHT DECK NUMBER 2 (SLIDING) WINDOW MOS REPLACE FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2 WINDOW PANE - REPLACEMENT. SERVICE BULLETIN RECOMMENDED RIGHT FLIGHT DECK NUMBER 2 (SLIDING) WINDOW MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 169 Of 748 @ Camp Systems EFTA00618460 C O MP &Wiwi's. Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-56A1022 WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION SUPERSEDED COMPUED WITH - INSPECTIONS TABLES 2 & 3 (SUPERSEDED BY 737-56A1022 RI). SERVICE BULLETIN FOR THE 114 AND #5 WINDOWS ONLY LA.W. AD 2008-11-08 FOUND SATSFACTORY MOS 16-FEB-20I0 18-JUL-2007 3417:51 AFL 829 SB 737-56A1022 RI WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION. RECOMMENDED COMPUED WITH - DETAIL INSPECTION I.A.W. AD SERVICE BULLETIN 2008-11-08 (F) FLIGHT DECK NO2. NO.4 AND NO.5 WINDOWS MOS 12-FEB-2014 12-MAR-2010 3743:34 AFL 917 SB 737-56A1022 RI DETAILED INSPECTION WINDOWS - RIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 RECOMMENDED COMPUED WITH - DETAIL INSPECTION TABLE 1.01 12-MAR-2010 SB 737-56A1022 RI TABLE 1.02 12-MAR-2010 SB 737-56A1022 RI TABLE 2.01 12-MAR-2010 SB 737-56A1022 RI TABLE 2.02 12-MAR-2010 SB 737-56A1022 RI TABLE 3.01 12-MAR-2010 SB 737-56A1022 RI TABLE 3.02 WINDOWS - INSPECTION. SERVICE BULLETIN OF THE LEFT AND RIGHT FLIGHT DECK NUMBER 2 WINDOW (GROUP 1-2) MOS 36 (s) 12-FEB-2014 7500 3743:34 AFL 917 REPLACE WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - RECOMMENDED INSPECTION. SERVICE BULLETIN THE LEFT AND RIGHT FLIGHT DECK NUMBER 2 WINDOW AND PERFORM A DETAILED INSPECTION (GROUP 1-2) MOS DETAILED INSPECTION WINDOWS - RIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 RECOMMENDED COMPUED WITH - DETAIL INSPECTION WINDOWS - INSPECTION. SERVICE BULLETIN OF FLIGHT DECK NUMBER 4 WINDOW (GROUP 1. CONFIGURATION 1) MOS 24 (s) I2-FEB-2014 6000 3743:34 AFL 917 REPLACE WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - RECOMMENDED INSPECTION. SERVICE BULLETIN THE FLIGHT DECK NUMBER 4 WINDOW AND PERFORM DETAILED INSPECTION (GROUP 1. CONFIGURATION 1) MOS BFIF (s) DETAILED INSPECTION WINDOWS - RIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 RECOMMENDED COMPUED WITH - DETAIL INSPECTION WINDOWS - INSPECTION. SERVICE BULLETIN OF THE FLIGHT DECK NUMBER 5 WINDOW (GROUP 1. CONFIGURATION 1) MOS 24 (s) 6000 I2-FEB-2014 3743:34 AFL 917 REPLACE WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - RECOMMENDED INSPECTION. SERVICE BULLETIN THE FLIGHT DECK NUMBER 5 WINDOW (GROUP 1. CONFIGURATION 1) MOS I2-MAR-2010 BFIF (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 170 Of 748 @ Camp Systems EFTA00618461 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-56A1022 TABLE 1 18-JUL-2007 SB 737-56A1022 TABLE 2 18-JUL-2007 SB 737-56A1022 TABLE 3 18-JUL-2007 SB 737-57-1250 07-FEB-2002 DETAIL INSPECTION WINDOWS - FLIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION (SUPERSEDED BY 737-56A1022 RI). SERVICE BULLETIN OF FLIGHT DECK NUMBER 2 WINDOW FOR GROUP 1 AND 2 MOS 36 (5) 7500 14-FEB-2008 3151:22 AFL 746 DETAIL INSPECTION WINDOWS- FLIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION (SUPERSEDED BY 737-56A1022 R1). SERVICE BULLETIN OF FLIGHT DECK NUMBER 4 WINDOW FOR GROUP 1 CONFIGURATION 1 MOS 24 (s) I6-FEB-2010 6000 3417:51 AFL 829 DETAIL INSPECTION WINDOWS - FLIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION (SUPERSEDED BY 737-56A1022 RI). SERVICE BULLETIN OF FLIGHT DECK NUMBER 5 WINDOW FOR GROUP 1 CONFIGURATION 1 MOS 24 (5) I6-FEB-2010 6000 3417:51 AFL 829 INSPECTION OF SECONDARY FUEL VAPOR-BARRIER APPLICATION ON THE WING CENTER SECTION. SERVICE BULLETIN MOS 48 (5) - INSPECTION SB 737-57-1250 RI INSPECTION OF THE SECONDARY FUEL VAPOR-BARRIER APPLICATION ON THE WING CENTER SECTION TOP PANEL COMPUED WITH AND FRONT SPAR. SERVICE BULLETIN MOS 48 (5) 28-SEP-2009 04-SEP-2003 3378:04 AFL 812 SB 737-57-1250 R2 INSPECTION OF THE SECONDARY FUEL VAPOR-BARRIER APPLICATION ON THE WING CENTER SECTION TOP PANEL COMPUED WITH AND FRONT SPAR. SERVICE BULLETIN MOS 28-SEP-2009 28-NOV-2006 - (s) 3378:04 AFL 812 SB 737-57-1253 CENTER WING REAR SPAR - STIFFENER MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 16-DEC-1999 AFL 4500 (s) SB 737-57-1253 RI CENTER WING REAR SPAR - STIFFENER MODIFICATION. SERVICE BULLETIN MOS II -JAN-2001 AFL 4500 (s) RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 171 Of 748 @ Camp Systems EFTA00618462 COMP Astant.frn• thernand up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57-1255 WING - LEFT SIDE MIDSPAR LOWER PANEL REPLACEMENT. SERVICE BULLETIN MOS 21 -JUN-2001 - Is) SB 737-57-1255 RI LEFT SIDE MIDSPAR LOWER PANEL REPLACEMENT. SERVICE BULLETIN MOS II -MAR-2004 SB 737-57-1264 FLAP CARRIAGE BUSHING REPLACEMENT. SERVICE BULLETIN MOS 24-MAY-2001 SB 737-57-1268 WINGS-LOWER WING SKIN PANELS-INSTALLATION OF THE RUB STRIPS. SERVICE BULLETIN - (s) MOS 06-JUN-2002 - (s) SB 737-57-1268 RI WING LOWER SKIN PANELS INSTALLATION OF THE RUB STRIPS. SERVICE BULLETIN MOS I7-OCT-2002 - SB 737-57-1272 OUTBOARD KRUEGER FLAP INSPECTION. REPAIR. AND PREVENTIVE MODIFICATION. SERVICE BULLETIN MOS 24-JUN-2004 - (s) SB 737-57-1272 PART 1 INSPECT OUTBOARD KRUEGER FLAP INSPECTION. REPAIR. AND PREVENTIVE MODIFICATION. SERVICE BULLETIN MOS 24-JUN-2004 3000 (s) SB 737-57-1272 PART 2 MODIFICATION OUTBOARD KRUEGER FLAP INSPECTION. REPAIR. AND PREVENTIVE MODIFICATION. SERVICE BULLETIN !REPLACEMENT MOS 24-JUN-2004 RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED SB 737-57-1275 LOWER WING SKIN PANEL - NACELLE SUPPORT FITTINGS ATTACHMENT FASTENERS INSPECTION AND RECOMMENDED REPLACEMENT. SERVICE BULLETIN MOS 04-SEP-2003 30000 Is) AFL 30000 SB 737-57-1275 RI LOWER WING SKIN PANEL - NACELLE SUPPORT FITTINGS ATTACHMENT FASTENERS INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS I8-AUG-2005 30000 Is) AFL 30000 - REF: REV.3 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 172 Of 748 @ Camp Systems EFTA00618463 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57-1275 R2 LOWER WING SKIN PANEL - NACELLE SUPPORT FITTINGS ATTACHMENT FASTENERS INSPECTION AND - REF: REV.3 REPLACEMENT. SERVICE BULLETIN MOS 12-JUL-2006 - (s) SB 737-57-1275 R3 LOWER WING SKIN PANEL - NACELLE SUPPORT FITTINGS ATTACHMENT FASTENERS INSPECTION AND COMPLIED WITH - IAW THE AD 2005-24-03R1 REPLACEMENT. SERVICE BULLETIN MOS 24-AUG-2007 I7-OCT-2006 - (5) 2968:28 AFL 699 SB 737-57-1278 OUTBOARD FLAP BELLCRANK ASSEMBLY INSPECTION AND MODIFICATION. SERVICE BULLETIN RECOMMENDED 02-DEC-2004 MOS SB 737-57-1278 RI WINGS - TRAILING EDGE AND TRAIUNG EDGE DEVICES - OUTBOARD FLAP BELLCRANK ASSEMBLY INSPECTION AND MODIFICATION.. SERVICE BULLETIN MOS 27 -SEP-2006 58 [SSN REDACTED] R2 WINGS - TRAILING EDGE AND TRAIUNG EDGE DEVICES - OUTBOARD FLAP BELLCRANK ASSEMBLY INSPECTION AND MODIFICATION.. SERVICE BULLETIN MOS 04-JUN-2007 SB 737-57-1281 REPAIR OF INBOARD MAIN FLAP UPPER SKIN AND MODIFICATION OF NUTPLATE STRIP ASSEMBLY. SERVICE RECOMMENDED BULLETIN MOS I 5-JUL-2004 SB 737-57-1284 WINGS - TRAILING EDGE AND TRAIUNG EDGE DEVICES - INSPECTION. REPAIR 7 MODIFICATION - WING BUTTOCK LINE 147 TO WING BUTTOCK LINE 201. SERVICE BULLETIN MOS 09-APR-2007 SB 737-57-1285 WINGS - WING STRINGERS - INSTALL STRINGERS 7 AND 9 REINFORCEMENT. SERVICE BULLETIN MOS SB 737-57-1285 RI WINGS - WING STRINGERS - INSTALL STRINGERS 7 AND 9 REINFORCEMENT. SERVICE BULLETIN MOS SB 737-57-1286 WINGS - CENTER - REAR SPAR VAPOR BARRIER - INSPECTION. REPAIR AND MODIFICATION.. SERVICE BULLETIN MOS 03-APR-2006 - INFORMATION REFER TO REV.1 AFL 5500 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 173 Of 748 @ Camp Systems EFTA00618464 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57-1286 RI 26-JUL-2007 SB 737-57-1288 30-MAR-2007 SB 737-57-1288 RI 03-JUN-2008 SB 737-57-1293 13-NOV-2008 MOS 24 (5) SB 737-57-1293 RI LEADING EDGE AND LEADING EDGE DEVICES - FUEL DRAIN PATH MODIFICATION (SUPERSEDED BY SB 737-57-1293 SUPERSEDED R2). SERVICE BULLETIN MOS SB 737-57-1293 R2 WINGS - LEADING EDGE AND LEADING EDGE DEVICES - FUEL DRAIN PATH MODIFICATION (SUPERSEDED BY SB SUPERSEDED 737-57-1293 R3). SERVICE BULLETIN MOS - Is) SB 737-57-1293 R3 WINGS - LEADING EDGE AND LEADING EDGE DEVICES - FUEL DRAIN PATH MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 24 (s) 28-SEP-2011 SB 737-57-1295 WINGS - TRAILING EDGE AND TRAIUNG EDGE DEVICES - WING INBOARD FIXED TRAILING EDGE UPPER PANEL BULB SEAL CHAFING ON WING-TO-BODY FAIRING PANEL - INSPECTION. REPAIR AND MODIFICATION.. SERVICE BULLETIN WINGS - CENTER WING - REAR SPAR VAPOR BARRIER - INSPECTION. REPAIR AND MODIFICATION. SERVICE BULLETIN MOS 28-SEP-2009 3378:04 AFL 5500 812 6312 TRAILING EDGE FLAP - NUMBER 3 AND NUMBER 6 TAILCONE ASSEMBLIES - INSPECTION AND REPAIR. SERVICE BULLETIN MOS AFL 5600 (s) WINGS - TRAILING EDGE FLAP - NUMBER 3 AND NUMBER 6 TAILCONE ASSEMBLES - INSPECTION AND REPAIR. SERVICE BULLETIN MOS AFL 5000(s) LEADING EDGE AND LEADING EDGE DEVICES - FUEL DRAIN PATH MODIFICATION. SERVICE BULLETIN RECURRING COMPUED WITH - PARTIALLY GENERAL MOS 12 (s) 04-JUN-2007 4500 SB 737-57-1300 04-JUN-2007 WINGS - TRAILING EDGE FLAPS - INBOARD FLAPS- INBOARD MAIN FLAP TRACKS. K4 AND #5- INSPECTION AND RECOMMENDED EXCHANGE PROGRAM. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 174 Of 748 @ Camp Systems EFTA00618465 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57-1300 NO 4 DETAILED INSPECTION WINGS - TRAILING EDGE FLAPS - INBOARD FLAPS - INBOARD MAIN FLAP TRACKS. 84 AND 85 - RECOMMENDED FLAP INSPECTION AND EXCHANGE PROGRAM. SERVICE BULLETIN MOS 24 (5) 03-FEB-2010 AFL 5500 SB 737-57-1300 NO 5 DETAILED INSPECTION WINGS - TRAILING EDGE FLAPS - INBOARD FLAPS - INBOARD MAIN FLAP TRACKS. #4 AND 85 - RECOMMENDED FLAP INSPECTION AND EXCHANGE PROGRAM. SERVICE BULLETIN MOS 24 (s) 03-FEB-2010 SB 737-57-1306 26-SEP-2008 AFL 5500 INBOARD FLAPS - INBOARD MAIN FLAP TRACKS. #4 AND 85 - SUPER 0-GUN COATING. DETAILED INSPECTION AND EXCHANGE PROGRAM. SERVICE BULLETIN MOS 24 (s) AFL 5500 SB 737-57-1309 28-JAN-2011 WINGS - CENTER WING BOX- FRONT SPAR SHEAR FITTING - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE BULLETIN MOS RECOMMENDED SB 737-57-1310 WINGS - CENTER WING - WING SPARS- FORWARD TRUNNION SUPPORT FITTING- FUSE PIN BORES - INSPECTION SUPERSEDED FOR CORROSION (SUPERSEDED BY SB 737-57-1310 RN. SERVICE BULLETIN MOS - Is) SB 737-57-1310 RI WINGS - CENTER WING - WING SPARS- FORWARD TRUNNION SUPPORT FITTING- FUSE PIN BORES - INSPECTION SUPERSEDED FOR CORROSION (SUPERSEDED BY SB 737-57-1310 R2). SERVICE BULLETIN MOS - Is) SB 737-57-1310 R2 WINGS - CENTER WING - WING SPARS- FORWARD TRUNNION SUPPORT FITTING- FUSE PIN BORES - INSPECTION RECOMMENDED FOR CORROSION. SERVICE BULLETIN MOS 120(s) SB 737-57-1312 WINGS - OUTER WING - WIRE BUNDLE SUPPORT GENERAL VISUAL INSPECTION. REPLACE TFE-4X WITH TFE-2X RECOMMENDED SLEEVE. SERVICE BULLETIN MOS 60 (s) 07-SEP-2010 SB 737-57-1316 WINGS - SPOILERS - INSTALLATION OF POLYURETHANE PROTECTIVE TAPE ON LOWER SKIN SURFACE OF INBOARD RECOMMENDED GROUND SPOILER NUMBER 6 AND 7. SERVICE BULLETIN MOS 05-SEP-2012 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 175 Of 748 @ Camp Systems EFTA00618466 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1279 24-JAN-2007 WINGS - CENTER AND OUTER WING - FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL INSPECTION (SUPERSEDED BY 737-57A1279 R1). SERVICE BULLETIN MOS SUPERSEDED S8 737-57A1279 RI CENTER AND OUTER WING - FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL INSPECTION SUPERSEDED (SUPERSEDED BY 737-57A1279 R2), SERVICE BULLETIN MOS (EFF) S8 737-57A1279 R2 WINGS - CENTER AND OUTER WING- FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL SUPERSEDED INSPECTION (SUPERSEDED BY SB 737-57A1279 R3). SERVICE BULLETIN MOS - (s) S8 737-57A1279 R3 WINGS - CENTER AND OUTER WING - FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL INSPECTION. SERVICE BULLETIN I5-FEB-20 I 1 SB 737-57A1279 R3 TABLE 1 24-JAN-2007 MOS (EFF) PERFORM WINGS - CENTER AND OUTER WING - FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL RECOMMENDED INSPECTION. SERVICE BULLETIN ACTIONS REQUIRED FOR FASTENER SEALEANT IN THE FUEL TANK AND WIRE CLAMP FOR GROUP 1.4 AIRPLANES MOS 60 (s) SB 737-57A1294 WINGS - WING CENTER SECTION - UPPER AND LOWER SWINGERS - DRILL START INSPECTION AND REPAIR. NOT APPLICABLE - BY EFFECTIVITY SB FOUND SERVICE BULLETIN TO BE NA BY VARIABLE NUMBER (YG006) MOS 16-FEB-2010 23-APR-2007 3417:51 AFL 829 SB 737-57A1294 TABLE 1 DETAILED INSPECTION WINGS - WING CENTER SECTION - UPPER AND LOWER STRINGERS - DRILL START INSPECTION AND REPAIR. SERVICE BULLETIN OF THE WING CENTER SECTION LOWER AND UPPER STRINGERS TO MINIMIZE CRACK SIZE. MOS 23-APR-2007 AFL 9000 9000 SB 737-57A1294 TABLE2 DETAILED INSPECTION WINGS - WING CENTER SECTION - UPPER AND LOWER STRINGERS - DRILL START INSPECTION AND REPAIR. SERVICE BULLETIN OF THE WING CENTER SECTION LOWER STRINGERS FOR SAFETY MOS 23-APR-2007 AFL 18000 18000 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 176 Of 748 @ Camp Systems EFTA00618467 C O MP Atiant.fran Ad-own/lop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1302 SB 737-57A1302 RI 78-OCT-2010 SB 737-57A1302 RI TABLE 1 A 15-DEC-2008 SB 737-57A1302 RI TABLE 1 LEADING EDGE SLATS- MAIN TRACK DOWN STOP MODIFICATION AND DETAILED INSPECTION (SUPERSEDED BY SB SUPERSEDED 737-57A1302 R1). SERVICE BULLETIN MOS WINGS - LEADING EDGE SLATS- MAIN TRACK DOWN STOP MODIFICATION AND DETAILED INSPECTION, SERVICE BULLETIN MOS 12-FEB-2014 3743:34 AFL 917 REPLACE WINGS - LEADING EDGE SLATS- MAIN TRACK DOWN STOP MODIFICATION AND DETAILED INSPECTION. SERVICE BULLETIN DOWN STOP ASSEMBLY HARDWARE WITH NEW DOWN STOP ASSEMBLY HARDWARE AND DOA DETAILED INSPECTION OF THE SLAT CANS AND SLAT MAIN TRACKS FOR DEBRIS IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. STEP 2. AT ALL 16 SLAT MAIN TRACK LOCATIONS.(A) FOR ALL AIRPLANES MOS 12-FEB-2014 - (s) 3743:34 AFL 917 REPLACE WINGS - LEADING EDGE SLATS- MAIN TRACK DOWN STOP MODIFICATION AND DETAILED INSPECTION. SERVICE BULLETIN AFT SIDE GUIDE BOLTS WITH NEW AFT SIDE GUIDE BOLTS IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. STEP 2. AT ALL 16 SLAT MAIN TRACK LOCATIONS.(A) FOR ALL AIRPLANES MOS 12-FEB-2014 15-DEC-2008 -(s) 3743:34 AFL 917 SB 737-57A1308 RI OUTER WING - SKINS - LOWER WING SKIN AT FUEL TANK ACCESS DOOR CUTOUT KEYWAY - INSPECTION AND CHANGE. SERVICE BULLETIN MOS 01-OCT-2009 SB 737-57A1308 RI TABLE 1.1 01-OCT-2009 SB 737-57A1308 RI TABLE 1.2 01-OCT-2009 PERFORM OUTER WING - SKINS - LOWER WING SKIN AT FUEL TANK ACCESS DOOR CUTOUT KEYWAY - INSPECTION AND CHANGE. SERVICE BULLETIN A ONE TIME INSPECTION FOR A KEYWAY IN THE FUEL TANK ACCESS DOOR 53188 AND 631BB CUTOUTS MOS AFL 7500 (s) PERFORM OUTER WING - SKINS - LOWER WING SKIN AT FUEL TANK ACCESS DOOR CUTOUT KEYWAY - INSPECTION AND CHANGE. SERVICE BULLETIN A ONE TIME HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE FUEL TANK ACCESS DOOR 531 BB CUTOUT KEYWAY AND FUEL TANK ACCESS DOOR 631BB CUTOUT KEYWAY ON THE LEFT AND RIGHT WING MOS AFL 7500 (s) COMPUED WITH - IAW. AD 2011-06-05 PARA (I) DETAILED INSPECTION AND MODIFICATION REPLACED ALL DOWN STOP ASSEMBLY HARDWARE- RECOMMENDED COMPUED WITH - DETAILED INSPECTION AND MODIFICATION REPLACED ALL DOWN STOP ASSEMBLY HARDWARE RECOMMENDED COMPUED WITH - DETAILED INSPECTION AND MODIFICATION REPLACED ALL DOWN STOP ASSEMBLY HARDWARE RECOMMENDED RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 177 Of 748 @ Camp Systems EFTA00618468 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - SUPERSEDED INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 RD. SERVICE BULLETIN MOS - (s) SB 737-57A1314 RI WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - RECOMMENDED INSPECTION AND MODIFICATION. SERVICE BULLETIN MOS I5-JUL-2014 - (s) SB 737-57A1314 Ftt TBL TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED 1.1 LH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN FOR LOOSE FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (ALL AIRPLANES) MOS AFL 32000 (s) SB 737-57A1314 Rt TBL TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY- INBOARD CARRIAGE TO TORQUE RECOMMENDED 1.1 RH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN FOR LOOSE FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (ALL AIRPLANES) MOS AFL 32000 (s) SB 737-57A1314 RI TBL RETOROUE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 1.2 LH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT 7 ACCOMPLISH THE MODIFICATION (IF ANY LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS 15-JUL-2014 BFIF (s) SB 737-57A1314 RI TBL RETOROUE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 1.3 RH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT / ACCOMPLISH THE MODIFICATION (IF ANY LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS IS-JUL-2014 BFIF (s) SB 737-57A1314 RI TBL DO WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE 1.4 LH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN ONE OF THE OPTIONS THAT FOLLOW: OPTION 1: ACCOMPLISH THE MODIFICATION! OPTION 2: RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (IF NO LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS I5-JUL-2014 BFIF (s) RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 178 Of 748 @ Camp Systems EFTA00618469 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 R1 TBL 1.5 RH 15-JUL-2014 DO WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN ONE OF THE OPTIONS THAT FOLLOW: OPTION 1: ACCOMPLISH THE MODIFICATION! OPTION 2: RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (IF NO LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS BFIF (s) RECOMMENDED SB 737-57A1314 RI TBL REPLACE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 1.6 ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN EACH PART THAT HAS A CRACK OR WEAR OR CONTACT BOEING FOR A REPAIR AND DO THE REPAIR (IF ANY CRACK OR WEAR FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 6 - LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION THAT CANNOT BE REMOVED BY OVERSIZING THE TORQUE TUBE ATTACHMENT HOLE TO SECOND OVERSIZE) 5-JUL-2014 MOS BF/F (s) SB 737-57A1314 RI TBL REPLACE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 1.8 ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE INBOARD CARRIAGE OR CONTACT BOEING FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (IF ANY CHAFING OR FRETTING FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 38.. WORK INSTRUCTIONS. PART 6- LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION THAT IS DEEPER THAN 0.020 INCH) MOS 15-JUL-2014 BF/F (s) SB 737-57AI314 RI TBL WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - RECOMMENDED 1.9 INSPECTION AND MODIFICATION. SERVICE BULLETIN BLEND THE INBOARD CARRIAGE TO REMOVE THE CHAFING AND FRETTING (IF ANY CHAFING OR FRETTING FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 6 - LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION UP TO A MAXIMUM DEPTH OF 0.020 INCH) MOS 15-JUL-2014 BF/F (s) SB 737-57AI314 RI TBL TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED 2.01 LH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN FOR LOOSE FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (ALL AIRPLANES) MOS AFL 11000(s) SB 737-57A1314 RI TBL TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED 2.01 RH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN FOR LOOSE FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (ALL AIRPLANES) MOS AFL 11000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 179 Of 748 @ Camp Systems EFTA00618470 CAMP AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 RI TBL 2.02 LH I5-JUL-2014 DETAIL INSPECTION WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN OF THE INBOARD CARRIAGE FOR CHAFING AND FRETTING / RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT /ACCOMPLISH THE MODIFICATION (IF ANY LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS BFIF (s) SB 737-57A1314 RI TBL ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY- INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 2.03 LH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE MODIFICATION (IF ANY CHAFING OR FRETTING FOUND BY DETAILED INSPECTION OF INBOARD CARRIAGE OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS 15-JUL-2014 BFIF (s) SB 737-57A1314 RI TBL DETAIL INSPECTION WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED 2.05 RH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN OF THE INBOARD CARRIAGE FOR CHAFING AND FRETTING / RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT 1 ACCOMPLISH THE MODIFICATION (IF ANY LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS I5-JUL-2014 BFIF (s) SB 737-57A1314 RI TBL ACCOMPLISH WINGS - TRAILING EDGE FLAPS- INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 2.06 RH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE MODIFICATION (IF ANY CHAFING OR FRETTING FOUND BY DETAILED INSPECTION OF INBOARD CARRIAGE OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS 15-JUL-2014 BF/F (s) SB 737-57A1314 RI TBL DO WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE 2.08 LH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN ONE OF THE OPTIONS THAT FOLLOW: OPTION 1: ACCOMPLISH THE MODIFICATION! OPTION 2: RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (IF NO LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS 5-JUL-2014 BF/F (s) SB 737-57A1314 RI TBL DO WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE 2.09 RH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN ONE OF THE OPTIONS THAT FOLLOW: OPTION 1: ACCOMPLISH THE MODIFICATION! OPTION 2: RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (IF NO LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS 5-JUL-2014 BF/F (s) RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 180 Of 748 @ Camp Systems EFTA00618471 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 R1 TBL REPLACE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 2.10 ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN EACH PART THAT HAS A CRACK OR WEAR OR CONTACT BOEING FOR A REPAIR AND DO THE REPAIR (IF ANY CRACK OR WEAR FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 6 - LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION THAT CANNOT BE REMOVED BY OVERSIZING THE TORQUE TUBE ATTACHMENT HOLE TO SECOND OVERSIZE) 5-JUL-2014 MOS BF/F (s) SB 737-57AI314 RI TBL REPLACE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 2.12 ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE INBOARD CARRIAGE OR CONTACT BOEING FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (IF ANY CHAFING OR FRETTING FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 6- LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION THAT IS DEEPER THAN 0.020 INCH) MOS 5-JUL-2014 BF/F (s) SB 737-57AI314 RI TBL WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - RECOMMENDED 2.13 INSPECTION AND MODIFICATION. SERVICE BULLETIN BLEND THE INBOARD CARRIAGE TO REMOVE THE CHAFING AND FRETTING (IF ANY CHAFING OR FRETTING FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 6 - LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION UP TO A MAXIMUM DEPTH OF 0.020 INCH) MOS I5-JUL-2014 BF/F (s) SB 737-57A1314 TABLE TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE SUPERSEDED 1.1 TUBE ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 R1). SERVICE BULLETIN (REQUIRED MINIMUM FOR SAFETY) MOS - (s) SB 737-57A1314 TABLE ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE SUPERSEDED 1.2 ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 RH. SERVICE BULLETIN THE MODIFICATION FOR LEFT WING (REQUIRED MINIMUM FOR SAFETY) MOS - (s) SB 737-57A1314 TABLE ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE SUPERSEDED 1.3 ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 RH. SERVICE BULLETIN THE MODIFICATION FOR RIGHT WING (REQUIRED MINIMUM FOR SAFETY) MOS - (s) SB 737-57A1314 TABLE TORQUE CHECK WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE SUPERSEDED 2.1 TUBE ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 RI). SERVICE BULLETIN (RECOMMENDED ECONOMIC INSPECTION) MOS - Is) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks %Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 181 Of 748 @ Camp Systems EFTA00618472 C O MP Atiant.fran Meowed lip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 TABLE ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE SUPERSEDED 2.2 ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 R1). SERVICE BULLETIN THE MODIFICATION FOR LEFT WING (RECOMMENDED ECONOMIC INSPECTION) MOS - Is) SB 737-57A1314 TABLE ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE SUPERSEDED 2.4 ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 R1). SERVICE BULLETIN THE MODIFICATION FOR RIGHT WING (RECOMMENDED ECONOMIC INSPECTION) MOS - (s) SB 737-71-1422 21 -JUN-I999 CONVERSION OF CFM56-76 TO 7827433. SERVICE BULLETIN MOS 7-OCT-2000 - (s) RECOMMENDED COMPUED WITH - CM SB 737-71-1422 RI CONVERSION OF CFM56-76 TO 7827433. SERVICE BULLETIN RECOMMENDED MOS 02-NOV-2000 - (s) SB 737-71-1422 R2 CONVERSION OF CFM56-76 TO 7827433. SERVICE BULLETIN RECOMMENDED MOS IS-FEB-2001 - (s) SB 737-71-1422 R3 CONVERSION OF CFM56-76 TO 7827/83. SERVICE BULLETIN MOS 12-FEB-2002 - (s) SB 737-71-1464 DRAIN TUBE REPLACEMENT. ENGINE FUEL PUMP PAD. SERVICE BULLETIN RECOMMENDED MOS 02-OCT-2003 SB 737-71-1551 RI POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-76 SINGLE ANNULAR SUPERSEDED COMBUSTOR (SACy3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES (SUPERSEDED BY SB 737-71-1551 R2). SERVICE BULLETIN MOS SB 737-71-1582 POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-7B SINGLE ANNULAR SUPERSEDED COMBUSTOR (SAC) ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-7B SAC/3 TECHNOLOGY INSERTION PROGRAM BASE ENGINES (SUPERSEDED BY SB 737-71-1582 R1). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 182 Of 748 @ Camp Systems EFTA00618473 C O MP A.m." vgnie• Megnsind AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1582 RI 58 [SSN REDACTED] R2 13-JAN-2012 58 [SSN REDACTED] 02-AUG-2007 POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-78 SINGLE ANNULAR SUPERSEDED COMBUSTOR (SAC) ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-7B SAC/3 TECHNOLOGY INSERTION PROGRAM BASE ENGINES (SUPERSEDED BY SB 737-71-1582 R2). SERVICE BULLETIN MOS POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-7B SINGLE ANNULAR RECOMMENDED COMBUSTOR (SAC) ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-7B SACf3 TECHNOLOGY INSERTION PROGRAM BASE ENGINES. SERVICE BULLETIN MOS POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-7B SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56- 78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN MOS SB 737-71-1588 RI POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56- 78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN I5-AUG-2007 SB 737-71-1588 R2 I 7-DEC-2007 SB 737-71-1588 R3 24-DEC-2007 58 [SSN REDACTED] R4 18-JUL-2008 MOS POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-76 SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN MOS POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-76 SINGLE ANNULAR COMBUSTOR (SACO TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN MOS INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 183 Of 748 @ Camp Systems EFTA00618474 C O MP A.m." vgnie• Megnundop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1588 RS 58 [SSN REDACTED] R6 07-DEC-2011 58 [SSN REDACTED] S8 [SSN REDACTED] RI SB 737-71-1603 R2 S8 [SSN REDACTED] R3 S8 [SSN REDACTED] R4 58 [SSN REDACTED] 02-OCT-2009 INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFMS6-78 SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES (SUPERSEDED BY S8 [SSN REDACTED] R6). SERVICE BULLETIN MOS SUPERSEDED POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-7B SINGLE ANNULAR RECOMMENDED COMBUSTOR (SACy3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFMS6-78 SAC BASE ENGINES. SERVICE BULLETIN MOS POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFMS6-78 SAC/3 (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 782773 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY SB 737-71-1603 RI). SERVICE BULLETIN MOS POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFM56-78 SAC/3 (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 7827/3 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY SB 737-71-1603 R2). SERVICE BULLETIN MOS POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFMS6-78 SAM (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 782773 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY SB 737-71-1603 R3). SERVICE BULLETIN MOS POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFM56-78 SAC/3 (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 7827/3 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY S8 [SSN REDACTED] R4). SERVICE BULLETIN MOS POWER PLANT -POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFM56-78 SAC/3 (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 782773 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY S8 [SSN REDACTED] RS). SERVICE BULLETIN MOS INSPECTION AND REPAIR OF THE ENGINE BUILD UP BRACKETS TO PREVENT DAMAGE TO THE ENGINE FAN CASE. SERVICE BULLETIN MOS RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 184 Of 748 @ Camp Systems EFTA00618475 C O MP A.m." vgnie• Megnund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1625 POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF CFM56-78 ENGINES FROM CFM56-7824 TO CFM56-7826/B2 THRUST RATING OR FROM CFM56-7824/3 TO CFM56-7826/382 OR CFM56-7826/382F THRUST RATING. SERVICE BULLETIN MOS RECOMMENDED 28-JUL-2010 SB 737-71-1634 POWER PLANT - GENERAL - CHANGE THE OPERATIONAL THRUST RATING OF CFM56-78 SACJ3 (TECH INSERTION) SUPERSEDED ENGINES FROM 7827/3 TO 7B24/3 OR 7826/3. OR FROM 7826/3 TO 7824/3 (SUPERSEDED BY SB 737-71-1634 RI). SERVICE BULLETIN MOS S8 [SSN REDACTED] RI POWER PLANT - GENERAL - CHANGE THE OPERATIONAL THRUST RATING OF CFM56-78 SACJ3 (TECH INSERTION) SUPERSEDED ENGINES FROM 7827/3 TO 7824/3 OR 7826/3. OR FROM 7826/3 TO 7824/3 (SUPERSEDED BY S8 [SSN REDACTED] R2). SERVICE BULLETIN MOS SB 737-71-1634 R2 POWER PLANT - GENERAL - CHANGE THE OPERATIONAL THRUST RATING OF CFM56-78 SAC/3 (TECH INSERTION) RECOMMENDED ENGINES FROM 7827/3 TO 7824/3 OR 7826/3. OR FROM 7626/3 TO 7824/3, SERVICE BULLETIN MOS 15-DEC-2010 SB 737-71-1658 POWER PLANT - CHANGE ONE OR TWO CFM56-78E ENGINES FOR ONE OR ANY COMBINATION OF TWO CFM56-78 SUPERSEDED SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56-78/3 SAC ENGINES (SUPERSEDED BY S8 [SSN REDACTED] RI). SERVICE BULLETIN MOS SB 737-71-1658 RI POWER PLANT - CHANGE ONE OR TWO CFM56-78E ENGINES FOR ONE OR ANY COMBINATION OF TWO CFM56-78 SUPERSEDED SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56-78/3 SAC ENGINES (SUPERSEDED BY S8 [SSN REDACTED] R2). SERVICE BULLETIN MOS SB 737-71-1658 R2 POWER PLANT - CHANGE ONE OR TWO CFM56-78E ENGINES FOR ONE OR ANY COMBINATION OF TWO CFM56-78 RECOMMENDED SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56-78/3 SAC ENGINES. SERVICE BULLETIN MOS 08-DEC-2011 SB 737-71-1673 POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC) SUPERSEDED ENGINES OR CFM56-78/3 SAC ENGINES FOR ONE OR TWO CFM56-78E ENGINES (SUPERSEDED BY SB 737-71-1673 R1). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 185 Of 748 @ Camp Systems EFTA00618476 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1673 RI 08-DEC-2011 SB 737-71-1674 SB 737-71-1674 RI SB 737-71-1674 R2 08-DEC-2011 POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56.78:3 SAC ENGINES FOR ONE OR TWO CFM56-7BE ENGINES. SERVICE BULLETIN MOS POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFP.I56-78 SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56.78:3 SAC ENGINES FOR ONE OR TWO CFM56-7BE ENGINES (SUPERSEDED BY SB 737-71-1674 RI). SERVICE BULLETIN MOS POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56.78:3 SAC ENGINES FOR ONE OR TWO CFM56-7BE ENGINES (SUPERSEDED BY SB 737-71-1674 R2). SERVICE BULLETIN MOS POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56.78:3 SAC ENGINES FOR ONE OR TWO CFM56-7BE ENGINES. SERVICE BULLETIN MOS RECOMMENDED SUPERSEDED SUPERSEDED RECOMMENDED SB 737-71-1675 POWER PLANT - CHANGE TWO CFM56-78x2 DUAL ANNULAR COMBUSTOR (DAC) ENGINES FOR TWO CFM56-7BE SUPERSEDED ENGINES (SUPERSEDED BY S8 [SSN REDACTED] RI). SERVICE BULLETIN MOS SB 737-71-1675 RI POWER PLANT - CHANGE TWO CFM56-78x2 DUAL ANNULAR COMBUSTOR (DAC) ENGINES FOR TWO CFM56-7BE RECOMMENDED 16-DEC-201I ENGINES. SERVICE BULLETIN MOS SB 737-71-1682 POWER PLANT - POWER PLANT - B1 FLANGE INSPECTION (SUPERSEDED BY S8 [SSN REDACTED] R1). SERVICE BULLETIN SUPERSEDED MOS SB 737-71-1682 RI POWER PLANT - POWER PLANT - B1 FLANGE INSPECTION (SUPERSEDED BY S8 [SSN REDACTED] R2). SERVICE BULLETIN SUPERSEDED MOS SB 737-71-1682 R2 POWER PLANT - POWER PLANT - B1 FLANGE INSPECTION (SUPERSEDED BY S8 [SSN REDACTED] R3). SERVICE BULLETIN SUPERSEDED MOS SB 737-71-1682 R3 POWER PLANT - POWER PLANT - B1 FLANGE INSPECTION. SERVICE BULLETIN RECOMMENDED 07-MAR-2014 MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 186 Of 748 Camp Systems EFTA00618477 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1705 21-DEC-2010 POWER PLANT - POWER PLANT - CHANGE OPERATIONAL THRUST RATING OF CFM5G-7B ENGINES FROM 7822 TO RECOMMENDED 7824 AND RETURN TO 7822. SERVICE BULLETIN MOS SB 737-71-1709 POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF TWO CFM56-78 ENGINES FROM RECOMMENDED 7826 TO 7827 AND RETURN TO 7826. SERVICE BULLETIN MOS 12-JAN-2011 • SB 737-71-1717 POWER PLANT - ENGINE COWLING - HEAT RESISTANT ALUMINIZED PRIMER INSTALLATION TO THE LIPSKIN OF THE RECOMMENDED ENGINE INLET COWL. SERVICE BULLETIN MOS 12-SEP-2013 SB 737-71-1725 POWER PLANT - POWER PLANT - INSTALLATION OF ENGINE OWNERSHIP PLACARD. SERVICE BULLETIN RECOMMENDED MOS 23-NOV-2011 • SB 737-71A1462 AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION. SERVICE BULLETIN 29-AUG-2C02 SB 737-71A1462 Fti POWER PLANT-ENGINE MOUNTS-AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION. SERVICE BULLETIN DAYS CO (5) DAYS 90 (5) 29-AUG-2C02 SB 737-71A1462 R2 AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. SERVICE RECOMMENDED BULLETIN MOS 29-MAY-2C03 SB 737-71A1462 R2 PART INSPECT AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. RECOMMENDED SERVICE BULLETIN FOR CORRECT INSTALLATION MOS 29-MAY-2C03 SB 737-71A1462 R2 PART APPLY AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. RECOMMENDED 2 SERVICE BULLETIN PERMANENT MARKINGS MOS 29-MAY-2C03 (51 ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 187 Of 748 1, Camp Systems EFTA00618478 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71A1462 R3 AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. SERVICE BULLETIN 20-MAY-2004 MOS 26-OCT-2011 3573:06 AFL 872 SB 737-71A1462 R3 PART INSPECT AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. 1 SERVICE BULLETIN FOR CORRECT INSTALLATION 20-MAY-2004 MOS 26-OCT-2011 3573:06 AFL 872 SB 737-71A1462 R3 PART INSTALL AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. 2 SERVICE BULLETIN PERMANENTLY MARKED MOUNT 20-MAY-2004 MOS 26-OCT-2011 3573:06 AFL 872 COMPUED WITH - PERFORMED UNDER WO GVBBJ206 COMPUED WITH - PERFORMED UNDER WO GVBBJ206 COMPUED WITH - PERFORMED UNDER WO GVBBJ206 SB 737-73-1014 Of -JUL-7999 ELECTRONIC ENGINE CONTROL. SERVICE BULLETIN MOS I3-SEP-1999 - (s) RECOMMENDED COMPUED WITH-CM SB 737-73-1014 RI ELECTRONIC ENGINE CONTROL. SERVICE BULLETIN RECOMMENDED MOS 27-JUL-2000 - (s) SB 737-73A-026 . SERVICE BULLETIN MOS I3-SEP-1999 - (s) SB 737-73A1011 ENGINE FUEL SUPPLY HOSE (SUPERSEDED BY SB 737-73A1011 R1). SERVICE BULLETIN SUPERSEDED MOS - (s) SB 737-73A1011 RI ENGINE FUEL SUPPLY HOSE (SUPERSEDED BY SB 737-73A1011 R2). SERVICE BULLETIN SUPERSEDED MOS - (s) SB 737-73A1011 R2 ENGINE FUEL SUPPLY HOSE. SERVICE BULLETIN RECOMMENDED MOS I9-APR-2002 73-JUL-2000 988:36 AFL 250 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 188 Of 748 @ Camp Systems EFTA00618479 COMP Moan Aim thernand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-73A1016 ELECTRONIC ENGINE CONTROL SOFTWARE CHANGE. SERVICE BULLETIN 20-FEB-2003 SB 737-73A1016 RI 08-MAY-2003 SB 737-77-1056 I6-AUG-2001 SB 737-77-1069 R2 10-DEC-2008 MOS 6 (s) 22-AUG-2003 1342 AFL 351 ELECTRONIC ENGINE CONTROL-SOFTWARE CHANGE. SERVICE BULLETIN MOS 22-AUG-2003 1342 AFL 351 AIRBORNE VIBRATION MONITORING SYSTEM UNIVERSAL SIGNAL CONDITIONER INSTALLATION, SERVICE BULLETIN RECOMMENDED MOS - (s) AIRBORNE VIBRATION MONITORING (AVM) SYSTEM - REPLACE CONDITIONER UNIT FOR CFM56-7B ENGINES. SERVICE BULLETIN MOS SB 737-78-1063 R2 EXHAUST- THRUST REVERSER - INNER WALL BLANKET INSULATION CHANGE. SERVICE BULLETIN MOS 28-MAR-2014 07-OCT-1999 SB 737-78-1067 THRUST REVERSER, SERVICE BULLETIN MOS 10-AUG-2000 3000 (s) 44 AFL 2100 38 RECOMMENDED COMPUED WITH COMPUED WITH NOT APPLICABLE - BY EFFECTIVITY SB 737-78-1069 28-FEB-2002 EXHAUST- THRUST REVERSER- INSULATION BLANKET MODIFICATION. SERVICE BULLETIN MOS - (s) SB 737-78-1069 RI EXHAUST - THRUST REVERSER - INSULATION BLANKET MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS I3-JUN-2002 SB 737-78-1069 R2 INSULATION BLANKET MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 06-FEB-2003 SB 737-78-1069 R3 INSULATION BLANKET MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 05-AUG-2004 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 189 Of 748 @ Camp Systems EFTA00618480 COMP Moan Aim thernand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1069 R4 16-JUN-2005 SB 737-78-1071 06-DEC-2001 SB 737-78-1071 RI 09-MAY-2002 SB 737-78-1072 28-MAR-2002 SB 737-78-1073 EXHAUST - THRUST REVERSER - INSULATION BLANKET MODIFICATION. SERVICE BULLETIN MOS REPLACE THRUST REVERSER EXHAUST FASTNERS FOR TRACKING SEALS. SERVICE BULLETIN MOS - RECOMMENDED THRUST REVERSER - REPLACE FASTNERS FOR TRACK FAIRING SEALS. SERVICE BULLETIN RECOMMENDED MOS - (s) EXHAUST - THRUST REVERSER - INSPECT/CHANGE CASCADE SUPPORT RING TO CORRECTLY INSTALL BARREL RECOMMENDED NUTS. SERVICE BULLETIN MOS - (s) INSPECTION AND MODIFICATION OR REPLACEMNT OF BUSHINGS IN THE ATTACH FITTING ASSEMBLIES FOR THE RECOMMENDED COMPLIED WITH DRAG LINKS. SERVICE BULLETIN 09-DEC-2004 MOS 07-SEP-2005 2202:21 AFL 541 SB 737-78-1073 RI EXHAUST - THRUST REVERSER - BLOCKED DOORS - INSPECTION AND MODIFICATION OR REPLACEMENT OF RECOMMENDED BUSHINGS IN THE ATTACH FITTING ASSEMBUES FOR THE DRAG LINKS. SERVICE BULLETIN MOS 21-APR-2005 SB 737-78-1073 R2 EXHAUST - THRUST REVERSER - BLOCKERS DOORS - INSPECTION AND MODIFICATION OR REPLACEMENT OF BUSHINGS IN THE ATTACH FITTING ASSEMBUES FOR THE DRAG LINKS. SERVICE BULLETIN MOS 12-JAN-2006 SB 737-78-1073 R3 EXHAUST - THRUST REVERSER - BLOCKER DOORS - INSPECTION AND MODIFICATION OR REPLACEMENT OF BUSHINGS IN THE ATTACH FITTING ASSEMBUES FOR THE DRAG LINKS. SERVICE BULLETIN MOS 20-JUL-2006 SB 737-78-1073 R4 EXHAUST - THRUST REVERSER - BLOCKER DOORS - INSPECTION AND MODIFICATION OR REPLACEMENT OF BUSHINGS IN THE ATTACH FITTING ASSEMBUES FOR THE DRAG LINKS. SERVICE BULLETIN MOS 16-NOV-2006 SB 737-78-1074 EXHAUST - THRUST REVERSER - BLOCKER DOOR AERO/FIRE SEAL REPLACEMENT. SERVICE BULLETIN MOS 24 (s) 07-APR-2005 AFL 4000 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 190 Of 748 @ Camp Systems EFTA00618481 COMP Moan. Aim thernand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1074 RI EXHAUST - THRUST REVERSER - BLOCKER DOOR AEROIFI RE SEAL REPLACEMENT. SERVICE BULLETIN MOS 60 (s) 15-SEP-2005 AFL 8200 SB 737-78-1075 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND REPLACEMENT OF THE FIRE SEAL ON EACH THRUST SUPERSEDED REVERSER HALF (SUPERSEDED BY SB 737-78-1075 RI). SERVICE BULLETIN MOS SB 737-78-1075 RI EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND REPLACEMENT OF THE FIRE SEAL ON EACH THRUST SUPERSEDED REVERSER HALF (REPLACED BY 737-78-1086 R2). SERVICE BULLETIN MOS SB 737-78-1076 RI EXHAUST - THRUST REVERSER SYSTEM - REPLACEMENT OF CASCADE ASSEMBLIES. SERVICE BULLETIN RECOMMENDED MOS 12-MAR-2010 SB 737-78-1078 EXHAUST - THRUST REVERSER INDICATING SYSTEM - ADDITION OF A RESISTOR TO THE THRUST REVERSER SYNC LOCK TIME DELAY CIRCUIT. SERVICE BULLETIN SB 17-AUG-2006 [SSN REDACTED] RI 30-MAY-2007 MOS EXHAUST - THRUST REVERSER INDICATING SYSTEM - ADDITION OF A RESISTOR TO THE THRUST REVERSER SYNC LOCK TIME DELAY CIRCUIT. SERVICE BULLETIN MOS SB 737-78-1078 R2 EXHAUST - THRUST REVERSER INDICATING SYSTEM - ADDITION OF A RESISTOR TO THE THRUST REVERSER SYNC LOCK TIME DELAY CIRCUIT. SERVICE BULLETIN MOS 19-FEB-2008 SB 737-78-1078 R3 THRUST REVERSER INDICATING SYSTEM - ADDITION OF A RESISTOR TO THE THRUST RECOMMENDED REVERSER SYNC LOCK TIME DELAY CIRCUIT. SERVICE BULLETIN MOS 16-OCT-2009 SB 737-78-1079 EXHAUST - THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION. REPAIR. AND COOLING HOLE MODIFICATION. SERVICE BULLETIN MOS 06-AUG-2007 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 191 Of 748 @ Camp Systems EFTA00618482 C O MP Atiant.fran Ad-own/lop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1079 RI 17-DEC-2007 SB 737-78-1079 R2 SB 737-78-1079 R3 SB 737-78-1082 SB 737-78-1082 RI 10-MAY-2012 SB 737-78-1083 SB 737-78-1083 RI SB 737-78-1083 RI TABLE 1 01-JAN-2000 EXHAUST - THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION. REPAIR. AND COOLING HOLE MODIFICATION 9SUPERSEDED BY 737-78-1079 R2). SERVICE BULLETIN MOS SUPERSEDED EXHAUST - THRUST REVERSER- THRUST REVERSER INNER WALL INSPECTION. REPAIR. AND COOLING HOLE SUPERSEDED MODIFICATION (SUPERSEDED BY SB 737-78-1079 R3). SERVICE BULLETIN MOS EXHAUST - THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION. REPAIR. AND COOLING HOLE MODIFICATION. SERVICE BULLETIN MOS EXHAUST - THRUST REVERSER - INSTALLATION OF A COOLING HOLE AND BUSHING. APPLY SEALANT AND INSTALL SUPERSEDED COMPLIED WITH - LAW. AD 2012-05-02 PARA (G) FLANGE INSULATION ASSEMBLIES ON THE THRUST REVERSERS (SUPERSEDED BY SB 737-78-1082 R1). SERVICE - FOUND SATISFACTORY - TOP KIT RETROFIT BULLETIN THR / 002A0004-16 MOS 12-FEB-2014 - (s) 3743:34 AFL 917 EXHAUST - THRUST REVERSER - INSTALLATION OF A COOLING HOLE AND BUSHING. APPLY SEALANT AND INSTALL FLANGE INSULATION ASSEMBLIES ON THE THRUST REVERSERS. SERVICE BULLETIN MOS 12-FEB-2014 - (s) 3743:34 RECOMMENDED DECLINED - NO MORE WORK IS NECESSARY ON THE AIRPLANE(S) CHANGED IN ACCORDANCE WITH THE ORIGINAL ISSUE OF THIS SERVICE BULLETIN. AFL 917 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST SUPERSEDED REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS (SUPERSEDED BY SB 737-78-1083 R1). SERVICE BULLETIN MOS - (s) EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST SUPERSEDED REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS (SUPERSEDED BY SB 737-78-1083 R2). SERVICE BULLETIN MOS DEATILED INSPECTION EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT SUPERSEDED OF THE THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS (SUPERSEDED BY SB 737-78-1083 R2). SERVICE BULLETIN OF THE THRUST REVERSER HYDRAULIC ACTUATOR ROD ENDS AND ACTUATOR ATTACH FITTINGS MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 192 Of 748 @ Camp Systems EFTA00618483 C O MP Atiant.fran Ad-own/lop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1083 R2 13-JUN-2014 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN MOS RECOMMENDED SB 737-78-1083 R2 TBL DETAILED INSPECTION EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT RECOMMENDED 1.01 OF THE THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN FOR DAMAGE ON THE HYDRAULIC ACTUATOR ROD END ASSEMBLIES AND A DETAILED INSPECTION FOR DAMAGE ON THE ACTUATOR ATTACH FITTINGS (FOR ALL AIRPLANES) (GROUP 1 - 2. CNF 2) MOS 30-JUN-2010 7500 (s) SB 737-78-1083 R2 TBL DO EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.03 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN DETAILED INSPECTIONS FOR DAMAGE ON THE HYDRAULIC ACTUATOR ROD END ASSEMBLIES (IF ANY DAMAGE FOUND ON THE HYDRAULIC ACTUATOR ROD END ASSEMBLIES) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BFIF SB 737-78-1083 R2 TBL REPAIR EXHAUST - THRUST REVERSER SYSTEM- INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.04 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN OR REPLACE THE HYDRAULIC ACTUATOR ROD END BODY (IF ANY DAMAGE FOUND ON HYDRAULIC ACTUATOR ROD END BODY AND THE DAMAGE IS LESS THAN OR EQUAL TO THE REPAIR LIMITS) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BF/F SB 737-78-1083 R2 TBL REPLACE EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE RECOMMENDED 1.05 THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN HYDRAULIC ACTUATOR ROD END ASSEMBLY (IF ANY DAMAGE FOUND ON HYDRAULIC ACTUATOR ROD END BODY AND THE DAMAGE IS GREATER THAN THE REPAIR LIMITS) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BFIF SB 737-78-1083 R2 TBL EXHAUST- THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.06 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN RETURN SPHERICAL BEARING TO SERVICE (IF WEAR LESS THAN OR EQUAL TO SERVICEABLE LIMITS FOUND ON SPHERICAL BEARING ON THE HYDRAULIC ACTUATOR ROD END) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BFIF SB 737-78-1083 R2 TBL REPLACE EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE RECOMMENDED 1.07 THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN THE SPHERICAL BEARING (IF WEAR GREATER THAN SERVICEABLE LIMITS FOUND ON SPHERICAL BEARING ON THE HYDRAULIC ACTUATOR ROD END) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BF/F 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 193 Of 748 @ Camp Systems EFTA00618484 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1083 R2 TBL 1.08 13-JUN-20I1 INSTALL EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN SPACER (IF NO DAMAGE FOUND ON AN ACTUATOR ATTACH FITTING) (GROUP 1 - 2. CNF 2) MOS BFIF RECOMMENDED 58 [SSN REDACTED] R2 TBL REPAIR EXHAUST - THRUST REVERSER SYSTEM- INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.09 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN FITTING AND INSTALL SPACER (IF ANY DAMAGE FOUND ON ACTUATOR ATTACH FITTING AND THE DAMAGE IS LESS THAN OR EQUAL TO 0.020 INCH IN DEPTH) (GROUP 1- 2. CNF 2) MOS 13-JUN-2014 BFIF 58 [SSN REDACTED] R2 TBL REPLACE EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE RECOMMENDED 1.10 THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN FITTING (IF ANY DAMAGE FOUND ON ACTUATOR ATTACH FITTING AND THE DAMAGE IS GREATER THAN 0.020 INCH IN DEPTH) (GROUP 1 - 2. CNF 2) MOS I3-JUN-2014 BFIF 58 [SSN REDACTED] R2 TBL EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.11 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN CHANGE THE SCHEDULED MAINTENANCE PROGRAM (FOR AIRPLANES WITH WEAR SPACERS INSTALLED ON THE ACTUATOR ATTACH FITTINGS) (GROUP 1 - 2. CNF 2) MOS 20000 (s) 58 [SSN REDACTED] R2 TBL EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 2.1 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN CHANGE THE SCHEDULED MAINTENANCE PROGRAM (FOR ALL AIRPLANES WITH WEAR SPACERS INSTALLED ON THE ACTUATOR ATTACH FITTINGS) (GROUP 1 - 2. CNF 1) MOS 12 (s) 13-JUN-2014 SS 737-78-1085 EXHAUST - THRUST REVERSER SYSTEM - CHANGE TO THE INSULATION BLANKETS ON THE THRUST REVERSERS SUPERSEDED (SUPERSEDED BY SS 737-78-1085 RI). SERVICE BULLETIN MOS SS 737-78-1085 RI EXHAUST - THRUST REVERSER SYSTEM - CHANGE TO THE INSULATION BLANKETS ON THE THRUST REVERSERS. RECOMMENDED SERVICE BULLETIN MOS 16-DEC-2011 SS 737-78-1086 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION OF THE FIRE SEAL AND INSTALLATION OF A NEW FIRE SEAL SUPERSEDED BRACKET ON THE THRUST REVERSER (SUPERSEDED BY SB 737-78-1086 R1). SERVICE BULLETIN 1/10S - Is) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 194 Of 748 @ Camp Systems EFTA00618485 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1086 RI EXHAUST - THRUST REVERSER SYSTEM - INSPECTION OF THE FIRE SEAL AND INSTALLATION OF A NEW FIRE SEAL SUPERSEDED BRACKET ON THE THRUST REVERSER (SUPERSEDED BY SB 737-78-1086 R2). SERVICE BULLETIN MOS - (s) SB 737-78-1086 R2 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION OF THE FIRE SEAL AND INSTALLATION OF A NEW FIRE SEAL BRACKET ON THE THRUST REVERSER . SERVICE BULLETIN MOS SB 737-78-1087 REPLACEMENT OF THE LOCKOUT HANDLE ASSEMBLY ON THE THRUST REVERSER ACTUATORS (SUPERSEDED BY SUPERSEDED SB 737-78-1087 R1). SERVICE BULLETIN MOS SB 737-78-1087 RI EXHAUST - THRUST REVERSER SYSTEM - REPLACEMENT OF THE LOCKOUT HANDLE ASSEMBLY ON THE THRUST RECOMMENDED REVERSER ACTUATORS. SERVICE BULLETIN MOS 29-MAY-20 1 3 SB 737-78-1088 EXHAUST - THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION AND REPAIR (SUPERSEDED BY SB SUPERSEDED 737-78-1088 R1). SERVICE BULLETIN MOS - (s) SB 737-78-1088 RI EXHAUST- THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION AND REPAIR. SERVICE BULLETIN MOS SB 737-78-1089 EXHAUST - ENGINE PRIMARY EXHAUST NOZZLE AND PLUG ASSEMBLY INSTALLATION (SUPERSEDED BY SB SUPERSEDED 737-78-1089 R1). SERVICE BULLETIN MOS SB 737-78-1089 RI EXHAUST- ENGINE PRIMARY EXHAUST NOZZLE AND PLUG ASSEMBLY INSTALLATION. SERVICE BULLETIN RECOMMENDED MOS 25-OCT-2013 SB 737-78-1090 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION FOR AND REMOVAL OF THE THRUST REVERSER INNER WALL COOLING HOLE BLOCKAGE. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 195 Of 748 @ Camp Systems EFTA00618486 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 [SSN REDACTED] EXHAUST - TURBINE EXHAUST SYSTEM - REWORK OF INTERFERENCE CONDITION AT EXHAUST NOZZLE FORWARD RECOMMENDED LABYRINTH. SERVICE BULLETIN MOS 22-JAN-2013 SB 737-SL-21-056 RAM AIR INLET DUCT CLIP ASSEMBLY REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 25-OCT-2002 -(5) SB 737-SL-28-044 AIRCRAFT USE OF DYED FUELS (SUPERSEDED BY SL 737-SL-28-044 REV. A). SERVICE BULLETIN SUPERSEDED SB 737-SL-30-020 OI -MAR-2006 SB 737-SL-31-034 MOS WINDOW HEAT CONTROL UNIT MODIFICATION TO CORRECT A4 CIRCUIT BOARD CORROSION. SERVICE BULLETIN MOS TAKEOFF CONFIGURATION WARNING- ALTERNATE METHOD OF COMPLIANCE A.D., SERVICE BULLETIN MOS SB 737-SL-32-129 REV. A NOSE GEAR LOCK VALVE MANIFOLD DUPLICATE SERIAL NUMBERS. SERVICE BULLETIN MOS I0-JUL-2006 SB 737-SL-32-134 REV. A NLG SHOCK STRUT ALTERNATE DYNAMIC SEAL. SERVICE BULLETIN MOS 10-JUL-2006 OPTIONAL SB 737-SL-32-154 MAIN LANDING GEAR ACTUATOR BARREL CRACKS RECOMMENDED FOLLOWING REPAIR PER SERVICE BULLETIN. SERVICE BULLETIN MOS 09-FEB-2009 AFL 500(s) SB 737-SL-34-187 LOSS OF RELIABLE AIR DATA DUE TO ICING OF STATIC PORTS - SRP 34-0111. SERVICE BULLETIN MOS 04-JUN-2007 SB 737-SL-52-046 AUXILIARY POWER UNIT (APU) ACCESS DOOR SKIN LATCH RECOMMENDED CUTOUTS. SERVICE BULLETIN MOS I4-APR-2009 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 196 Of 748 @ Camp Systems EFTA00618487 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 920-34-25 ROCKWELL COLLINS - SB 25 - GLU-920 GLOBAL LANDING UNIT (CPN 822-1152-0011002/003) GNSS RECEIVER CIRCUIT CARD A8 (CPN 828-2940-302) REDUCE OCCURRENCE OF INCORRECT GPS DATE. SERVICE BULLETIN COMPLIED WITH 03-OCT-2008 MOS 23-FEB-2009 3353:18 AFL 804 SB 964-0452-23-39 COMMUNICATION - XK516D HF RADIO SYSTEM - UNIT MODIFICATION (MOD) 48 TO XK516D1 HF TRANSCEIVER (HF RECOMMENDED TRANSCEIVER). PN 964-0452-012. -042. OR -052: INSPECTION AND REPLACEMENT OF HIGH FREOUENCY (HF) MODEM NON-CONFORMING INTEGRATED CIRCUIT (VOICE BAND ANALOG INTERFACE). SERVICE BULLETIN MOS 05-N0V-2013 SB 965-0976-0XXX-34-38 . SERVICE BULLETIN R1 MOS - (s) SB A001-25-96 . SERVICE BULLETIN - IPECO SEATS MOS 13-SEP-1999 - (s) SB Bill 28-136 INSTALLATION OF COMPONENT IDENTIFICATIONS PLACARDS. SERVICE BULLETIN MOS - (s) SB BBJ-25-34 REMOVAL OF CARGO COMPARTMENT LOWER BILGE INSULATION BLANKETS. SERVICE BULLETIN MOS - (s) SB BB.J-28-001-K ST00936NY-D-28-SB-001- K SFAR 88 AFS INTERNAL FUEL CELL MODIFICATION AND VALVE PLATE ASSEMBLY. COMPLIED WITH SERVICE BULLETIN MOS 28-SEP-2009 3378:04 AFL 812 SB BBJ-28-02 MODIFICATION OF THE FORWARD HALF TANK, INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS 17-AUG-1999 - (s) SB BBJ-28-021-K ST00936NY-D-28-SB-021-_K SFAR88 {AND FAR 25.981 (A) (8) (C1) (AMENDMENT 102)} AUXILIARY FUEL SYSTEM UPGRADE FOR PATS MODIFIED AIRCRAFT SERVICE BULLETIN, SERVICE BULLETIN MOS 28-SEP-2009 3378:04 AFL 812 RECOMMENDED COMPLIED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 197 Of 748 @ Camp Systems EFTA00618488 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ-28-02A 17-AUG-1999 SB Bill-28-02B 15-OCT-1999 SB BBJ-28-02C 28-NOV-1999 SB BBJ-28-03 10-JUN-1999 SB BBJ-28-04 SB BBJ-28-04A 12-AUG-1999 SB BBJ-28-048 14-APR-2000 SB BEJ-28-05 10-JUN-1999 SB BBJ-28-06 MODIFICATION OF THE FORWARD HALF TANK. INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS - Is) MODIFICATION OF THE FORWARD HALF TANK. INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS - Is) MODIFICATION OF THE FORWARD HALF TANK. INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS - (s) MODIFICATION OF THE AUXILIARY FUEL ELECTRICAL SYSTEM. SERVICE BULLETIN MOS - (s) MODIFICATION OF THE AUXILIARY FUEL SYSTEM PRESSURE SWITCH, SERVICE BULLETIN MOS - Is) MODIFICATION OF THE AUXILIARY FUEL SYSTEM PRESSURE SWITCH, SERVICE BULLETIN MOS - (s) MODIFICATION OF THE AUXILIARY FUEL SYSTEM PRESSURE SWITCH, SERVICE BULLETIN MOS - (s) INSTALLATIONOF AUXILIARY FUEL SHROUD DRAIN SYSTEM FLOW RESTRICTOR. SERVICE BULLETIN MOS - Is) MODIFICATION TO ADDED ELECTRONICS RACK FOR INCREASED LOAD CAPACITY. SERVICE BULLETIN MOS - (s) SB BBJ-28-09 CONVERSION FROM AN EXISTING NINE (4FWD. 5 AFT) AFS CONFIGURATION 2-G TO AN EIGHT CELL (3 FWD. 5 AFT) AFS. CONFIGURATION 2-F. SERVICE BULLETIN SB BBJ-28-098 MOS RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED CONVERSION FROM AN EXISTING NINE (4FWD. 5 AFT) AFS CONFIGURATION 2-G TO AN EIGHT CELL (3 FWD. 5 AFT) RECOMMENDED AFS. CONFIGURATION 2-F. SERVICE BULLETIN MOS 23-AUG-1999 -(s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 198 Of 748 @ Camp Systems EFTA00618489 CAMP fin. thermiewlqi AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ-28-09F 29-OCT-2001 CONVERSION FROM AN EXISTING NINE (4FWD. S AFT) AFS CONFIGURATION 2-G TO AN EIGHT CELL (3 FWD. S AFT) RECOMMENDED AFS. CONFIGURATION 2-F. SERVICE BULLETIN MOS - (s) SB BB.J-28-10 RELOCATION OF HOSE SHROUD CHECK VALVES. SERVICE BULLETIN RECOMMENDED MOS 10-JUN-1999 - (s) SB BBJ-28-108-A AUXILIARY FUEL SYSTEM (AFS) CONVERSION FROM AN EXISTING (2M) 1 FWD 5 AFT CELL CONFIGURATION TO A (3A) RECOMMENDED 0 FWD 3 AFT CELL CONFIGURATION, SERVICE BULLETIN MOS 08-MAR-2004 SB BBJ-28-11 INSTALLATION OF CARGO NET ATTACH PROVISIONS (FORWARD). SERVICE BULLETIN MOS - (s) SB BBJ-28-13 INSTALLATION: COMPONENT IDENTIFICATION PLACARDS. SERVICE BULLETIN MOS SB BBJ-28-13 . SERVICE BULLETIN - (s) MOS I3-SEP-1999 - (s) SB BBJ-28-13A INSTALLATION: COMPONENT IDENTIFICATION PLACARDS. SERVICE BULLETIN RECOMMENDED MOS 09-AUG-1999 - (s) SB BBJ-28-138 INSTALLATION OF COMPONENT IDENTIFICATIONS PLACARDS. SERVICE BULLETIN MOS - (s) SB BBJ-28-16 MODIFICATION OF THE AUX FUEL HALF TAW INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS SB BBJ-28-16A 31-AUG-1999 - (s) MOUNTING OF THE AFT HALF FUEL CELL INBOARD SUPPORT RAIL AND THE ADDITION OF THE FASTENERS IN THE RECOMMENDED FLOOR BEAM REINFORCEMENT STRAPS. SERVICE BULLETIN MOS - PATS SB 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 199 Of 748 @ Camp Systems EFTA00618490 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ-28-18 31-AUG-1999 SB BBJ-28-19 INSPECTION/MODIFICATION OF FASTENERS ON RAIL AND FLOOR. SERVICE BULLETIN MOS - Is) MODIFICATION OF THE WIRING OF THE AUX FUEL PROCESSING UNIT. SERVICE BULLETIN MOS - SB BBJ-28-19A MODIFICATION OF THE WIRING OF THE AUX FUEL PROCESSING UNIT. SERVICE BULLETIN 06-JUL-2001 MOS - (s) SB BBJ-28-21 FUEL MIGRATION PREVENTION. SERVICE BULLETIN MOS - (s) SB BBJ-28-21A SB Bill-28-21B SB Bill-28-21C FUEL MIGRATION PREVENTION.. SERVICE BULLETIN MOS - FUEL MIGRATION PREVENTION.. SERVICE BULLETIN MOS - FUEL MIGRATION PREVENTION.. SERVICE BULLETIN MOS - Is) SB BBJ-28-210 FUEL MIGRATION PREVENTION. SERVICE BULLETIN MOS 28-AUG-2009 07-SEP-2000 - (s) 3378:04 AFL 812 SB BBJ-28-23 MODIFICATION TO PREVENT BATTERY DRAINING. SERVICE BULLETIN MOS 01-JAN-2000 - (s) RECOMMENDED RECOMMENDED RECOMMENDED COMPLIED WITH SB BBJ-28-23A MODIFICATION TO PREVENT BATTERY DRAIN. SERVICE BULLETIN RECOMMENDED MOS 21-DEC-1999 - (s) SB BBJ-28-24 THE INSTALLATION OF A CLIP ASSEMBLY IN THE FORWARD CARGO COMPARTMENT TO ALLOW FOR THE PROPER RECOMMENDED REINSTALLATION OF THE FORWARD MOST CARGO NET AT THE CARGO BAY DOOR.. SERVICE BULLETIN MOS 14-JAN-2000 - 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 200 Of 748 @ Camp Systems EFTA00618491 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ-28-25 I9-JAN-2000 INSTALLATION OF A PLATE & CHANNEL IN THE FORWARD CARGO COMPARTMENT TO ALLOW FOR THE PROPER RECOMMENDED REINSTALLATION OF THE AFT MOST CARGO NET AT THE CARGO BAY DOOR. SERVICE BULLETIN MOS - (s) SB BBJ-28-26A CONVERSION: FROM (2 WD 5 Fl) TO el FWD 5 AFT) 6 TANK.. SERVICE BULLETIN MOS - (s) SB BBJ-28-268 CONVERSION: FROM (2 WD 5 Fl) TO el FWD 5 AFT) 6 TANK.. SERVICE BULLETIN MOS - (s) SB BBJ-28-26C CONVERSION: FROM A 7 TANK (2 WD 5 FT) TO A 6 TANK. ( FWD 5 AFT). SERVICE BULLETIN RECOMMENDED MOS 30-JUN-2060 - (s) SB BBJ-28-30 CONVERSION OF A SEVEN TANK FUEL SYSTEM TO A SIXTANK FUEL SYSTEM. SERVICE BULLETIN MOS - (s) SB BBJ-28-39E EIGHT CELL TO SEVEN CELL CONVERSION. SERVICE BULLETIN RECOMMENDED MOS 77-JUL-2001 - (s) SB BBJ-28-39F CONVERSION FROM AN EXISTING 8 TANK (3 FWD. 5 AFT) TO A 7 TANK (2 FWD. 5 AFT) AFS. CONFIGURATION. RECOMMENDED SERVICE BULLETIN 04-OCT-2001 SB BBJ-28-00A MOS - (s) SB BB-I-28-00B MODIFICATION TO FORWARD BLEED AIR. SERVICE BULLETIN RECOMMENDED MOS 29-SEP-2000 - (s) SB Bal-28-038 FUEL LINE BRACKET MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 29-SEP-2000 - (s) SB BBJ-28-45A RELOCATION OF CHECK VALVE IN MIX BAY. SERVICE BULLETIN RECOMMENDED MOS I8-SEP-2000 - (s) MOS MODIFICATION TO FWD BLEED AIR.. SERVICE BULLETIN 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 201 Of 748 @ Camp Systems EFTA00618492 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ-28-458 I2-JUL-2001 SB BBJ-28-47F CONVERSION FROM 5 TANK(1 FWD 4 AFT) TO A4 TANK (0 FWD 4AFT) CONFIGURATION. SERVICE BULLETIN RECOMMENDED I6-AUG-2001 SB BBJ-28-56 REPLACEMENT OF THE BBJ FUELING PLACARDS. SERVICE BULLETIN SB BBJ-28-58 05-JUL-2001 SB BBJ-28-61 RELOCATION OF CHECK VALVE IN MIX BAY. SERVICE BULLETIN MOS MOS MOS - Is) - (s) - Is) REPLACEMENT OF THE BBJ CARGO LOADING PLACARDS. SERVICE BULLETIN MOS - (s) RECOMMENDED RECOMMENDED CONVERSION FROM AN EXISTING EIGHT CELL (3 FWD 5AFT) AFS. CONFIGURATION 2-F TO A SIX CELL (1 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 24.1. SERVICE BULLETIN MOS I7-APR-2001 -Is) SB BBJ-28-63C 09-NOV-2001 CONVERSION FROM AN EXISTING SIX CELL (2 FWD. 4 AFT) AFS. CONFIGURATION 2-D TO A EIGHT CELL (3 FWD. 5 AFT) RECOMMENDED AFS. CONFIGURATION 2-F WITH AFT STRUCTURAL PROVISIONS PREVIOUSLY INSTALLED. SERVICE BULLETIN MOS SB BBJ-28-67 CONVERSION FROM AN EXISTING SIX CELL (1 FWD 5 AFT) AFS. CONFIGURATION 2-M TO A SEVEN CELL (2 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 2-E.. SERVICE BULLETIN 05-DEC-2001 SB BBJ-28-6A 02-SEP-1999 SB BBJ-28-70 16-JAN-2002 SB BBJ-28-73A MOS - Is) MODIFICATION TO ADDED ELECTRONICS RACK FOR INCREASED LOAD CAPACITY. SERVICE BULLETIN MOS - (s) MODIFICATION OF THE EQUIPMENT EQUIPMENT RACK INSTALLED IN THE FORWARD CARGO COMPARTMENT. SERVICE BULLETIN MOS RELOCATION OF THE ATOP INSTALLED ON THE ELECTRICAL EQUIPMENT RACK IN THE FORWARD CARGO COMPARTMENT. SERVICE BULLETIN MOS 28-MAY-2002 - (s) RECOMMENDED RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 202 Of 748 @ Camp Systems EFTA00618493 COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ-28-78-D SB BBJ-28-78A 05-JUN-2002 SB BBJ-28-788 13-NOV-2002 SB BBJ-28-84A CONVERSION UPDATE TO SOFTWARE 2.1. SERVICE BULLETIN MOS 28-SEP-2009 3378:04 AFL 812 AIRCRAFT CONVERSION TO UPDATE TO SOFTWARE 2.1 (STC: ST00936NY). SERVICE BULLETIN MOS - (s) AIRCRAFT CONVERSION TO UPDATE TO SOFTWARE 2.1 (AFCU/AFDU). SERVICE BULLETIN MOS - (s) INSTALLATION OF PRESSURE EQUALIZATION PANELS INTO EXISTING AUXILIARY FUEL SYSTEM (AFS) CONFIGURATIONS WITH ONE TANK FORWARD AND/OR TWO. THREE AND FOUR TANKS AFT.. SERVICE BULLETIN MOS 08-OCT-2002 - (s) SB BBJ-28-84B INSTALLATION OF PRESSURE EQUALIZATION PANELS. SERVICE BULLETIN MOS 31-DEC-2003 - (s) RECOMMENDED RECOMMENDED RECOMMENDED SB BBJ-28-84C INSTALLATION OF PRESSURE EQUALIZATION PANELS INTO EXISTING AUXILIARY FUEL SYSTEM (AFS) RECOMMENDED CONFIGURATION WITH ONE TANK FORWARD AN/OR TWO. THREE. AND FOUR TANKS AFT. SERVICE BULLETIN MOS 27-FEB-2003 SB BBJ-28-86 CONVERSION FROM AN EXISTING SIX CELL (1FWD 5 AFT). CONFIGURATION 244 TO A NINE CELL (4 FWD 5 AFT) AFS. RECOMMENDED CONFIGURATION 2-G WITH STRUCTURAL PROVISIONS PREVIOUSLY INSTALLED. (STC: ST00936NY AMENDED JUNE 17. 2002). SERVICE BULLETIN MOS 28-AUG-2002 - (s) SB BBJ-28-86A CONVERSION FROM AN EXISTING SIX CELL (1 FWD 5 AFT), CONFIGURATION 3-M TO A NINE CELL (4 FWD 5 AFT) AFS. RECOMMENDED CONFIGURATION 3-G WITH STRUCTURAL PROVISIONS PREVIOUSLY INSTALLED.. SERVICE BULLETIN MOS 30-SEP-2002 - (s) SB BRJ-28-890 ADDING ADDITIONAL PROVISIONS ONLY TO AN EXISITING THREE CELL (0 FWD 3 AFT) AFS. CONFIGURATION 3-A. FOR RECOMMENDED FUTURE INSTALLATION OF 2 FWD TANKS FOR A FIVE CELL (2 FWD 3 AFT) AFS. CPNFIGURATION 3-C. SERVICE BULLETIN MOS 15-JAN-2003 COMPLIED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 203 Of 748 @ Camp Systems EFTA00618494 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 88J-28-89E 14-FEB-2003 SB 88J-28-89F I7-APR-2003 SB 88J-28-90 07-NOV-2002 SB 88J-28-90A 05-DEC-2002 SB 88J-28-92 22-NOV-2002 ADDING ADDITIONAL PROVISIONS ONLY TO AN EXISITING THREE CELL (0 FWD 3 AFT) AFS. CONFIGURATION 3-A. FOR RECOMMENDED FUTURE INSTALLATION OF 2 FWD TANKS FOR A FIVE CELL (2 FWD 3 AFT) AFS. CPNFIGURATION 3-C. SERVICE BULLETIN MOS CONVERSION OF EXISTING CONFIGURATION 3-A A THREE CELL (0 FWD 3 AFT) AFS PER STC ST00936NY TO A RECOMMENDED CONFIGURATION 3-C A FIVE CELL (2 FWD 3 AFT) AFS ALSO PER STC ST00936NY.. SERVICE BULLETIN MOS CONVERSION TO CONFIGURATION TO A FIVE CELL. SERVICE BULLETIN MOS RECOMMENDED CONVERSION FROM AN EXISTING SEVEN CELL (2 FWD. 5 AFT) AFS. CONFIGURATION 2-E TO A FIVE CELL (1 FWD. 4 RECOMMENDED AFT) AFS. CONFIGURATION 3-K. SERVICE BULLETIN MOS CONVERSION FROM AN EXISTING SIX CELL (1 FWD. 5 AFT) AFS. CONFIGURATION 2-M TO A SEVEN CELL (2 FWD. 5 RECOMMENDED AFT) AFS. CONFIGURATION 3-E. SERVICE BULLETIN MOS SB 88J-28-928 CONVERSION FROM AN EXISTING SIX CELL (1 FWD 5 AFT) AFS. CONFIGURATION 3-M TO A SEVEN CELL (2 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 3-E.. SERVICE BULLETIN MOS 20-NOV-2003 SB 88J-28-92C CONVERSION FROM AN EXISTING SIX CELL (1 FWD 5 AFT) AFS. CONFIGURATION 3-M TO A SEVEN CELL (2 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 3-E.. SERVICE BULLETIN MOS 02-DEC-2003 SB 88J-28-93 1S-JAN-2003 IN AUX FUEL MODIFIED AIRPLANES. TO RELOCATE EXPOSED TEST PLUG IN THE AFT CARGO COMPARTMENT 8. RECOMMENDED STOW THE FUEL CONNECTOR PLUG IN THE FWD CARGO TO A PROTECTED AREA. SERVICE BULLETIN MOS SB 88J-28-94A CONVERSION OF PREVIOUS CONFIGURATION: FROM AN EXISTING SIX CELL (1 FWD 5 AFT) AFS. CONFIGURATION RECOMMENDED 2-M TO A EIGHT CELL (3 FWD 5 AFT) AFS. CONFIGURATION 3-F. SERVICE BULLETIN MOS 17-APR-2003 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 204 Of 748 @ Camp Systems EFTA00618495 COMP Jm. thernanditfi AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 88J-28-95 CHANGE THE FUEL QUANTITY INDICATING SYSTEM FROM KILOGRAMS TO POUNDS STC: ST00936NY AMENDED JUNE RECOMMENDED 17. 2002. SERVICE BULLETIN MOS I0-MAR-2003 SB 88J-33-37A DE-ACTIVATIONIREACTIVATION OF CARGO LIGHTING ABOVE AUX FUEL TANKS. SERVICE BULLETIN MOS - (s) SB 88J-33-37B DE-ACTIVATION! REACTIVATION OF CARGO LIGHTING ABOVE AUX FUEL TANKS.. SERVICE BULLETIN RECOMMENDED MOS I3-NOV-2000 - (s) SB 88J-34-79 REMOVAL OF EXISTING ARINC 740 MILTOPE COCKPIT PRINTER AND AND REPLACE WITH ALLIED SIGNAL PRIMER. RECOMMENDED SERVICE BULLETIN MOS I4-MAR-2003 SB 88J-53-38A IMPROVED MIX BAY ACCESS.. SERVICE BULLETIN RECOMMENDED MOS 06-JUL-2001 - (s) SB BB-Q-28-08A AIRCRAFT CONVERSION TO UPDATE TO SOFTWARE 2.1 (STC SA01384NY). SERVICE BULLETIN RECOMMENDED MOS 05-JUN-2002 - (s) SB 88J2-28-11A CONVERSION FROM AN EXISTING SEVEN CELL (2 FWD 5 AFT) AFS. CONFIGURATION 1-G TOA SIX CELL (1 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 1-0. SERVICE BULLETIN MOS 08-JAN-2003 SB 88J2-28-118 15-APR-2003 CONVERSION FROM AN EXISTING SEVEN CELL (2 FWD 5 AFT) AFS. CONFIGURATION 1-G TOA SIX CELL (1 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 1 -D. SERVICE BULLETIN MOS SB 88J2-28-15 CONVERSION FROM AN EXISITNG SIX CELL (2 FWD 4 AFT) AFS. CONFIGURATION 1-F TO A FIVE CELL (1 FWD 4 AFT) RECOMMENDED AFS. CONFIGURATION 1-C. SERVICE BULLETIN MOS 12-FEB-2003 SB 88J2-28-17A CHANGE FUEL OUANITY INDICATING SYSTEM. SERVICE BULLETIN RECOMMENDED MOS 21-FEB-2003 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 205 Of 748 @ Camp Systems EFTA00618496 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ2-28-9 IA CHANGE FUEL OUANITY INDICATING SYSTEM. SERVICE BULLETIN MOS SB CFM56-78S880-005 . SERVICE BULLETIN COMPUED WITH-CM SB CFMI-S872-168 . SERVICE BULLETIN MOS - (s) 10-AUG-2000 SB S-0380-34-02 . SERVICE BULLETIN MOS - (s) 17-OCT-2000 SB S-0380-34-03 . SERVICE BULLETIN MOS - (s) SB S8-17 . SERVICE BULLETIN MOS - (s) MOS - (s) SB TPR-901-34-10R2 ROCKWELL COLLINS- ELIMINATE OCCURANCE OF ERRANT MODE A CODE (0607) AND IMPROVE DESENDE RECOVERY TIMING. SERVICE BULLETIN MOS 20-DEC-2006 2785:43 AFL 661 SIL 920-08-1 ROCKWELL COLLINS - GLU-920 GLOBAL LANDING UNIT COMPUED WITH (CPN 822-1152-001/002=31220) GPS DATE CODE - 08-1. SERVICE INFORMATION LETTER MOS 23-FEB-2009 26-AUG-2008 3353:18 AFL 804 SIL D200808000008 R5 HONEYWELL HAS ISSUED A SPECIAL PRICE FOR THE PARTS NECESSARY FOR THE ATA 36 UPGRADES FOR 737. SERVICE INFORMATION LETTER MOS 07-AUG-20I3 SIL D201103000023 R1 INTRODUCTION OF WHEEL HUB ULTRASONIC INSPECTION KIT. PN 7416886. SERVICE INFORMATION LETTER RECOMMENDED MOS 27-NOV-20I3 COMPUED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 206 Of 748 @ Camp Systems EFTA00618497 C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SIL D201104000050 R2 RE-INTRODUCTION OF VACUUM BLOWER. PN 606802-2. IN PLACE OF VACUUM BLOWER. PN 645172-1. -2. SERVICE OPERATORS 28-JUN-2013 INFORMATION LETTER MOS DISCRETION SIL D201311000043 POSSIBLE INCORRECT PACK DISCHARGE OVERHEAT SWITCH INSTALLED ON CERTAIN BOEING MODEL SUPERSEDED 737-800/-900/-900ER AIRCRAFT (SUPERSEDED BY SIL D201311000043 R1), SERVICE INFORMATION LETTER MOS SIL D201311000043 RI POSSIBLE INCORRECT PACK DISCHARGE OVERHEAT SWITCH INSTALLED ON CERTAIN BOEING MODEL RECOMMENDED 15-JAN-2011 737-800/-900/-900ER AIRCRAFT. SERVICE INFORMATION LETTER MOS SIL D201312000067 MK V ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS). PN 965-0976-003-XXX-XXX. PN RECOMMENDED 965-0976-020-XXX-XXX. PN 965-0976-040-XXX-XXX. PN 965-0976-060-XXX-XXX. PN 965-1676-00X. AND PN 965-1690-05X: 20-DEC-2013 END OF PRODUCTION ANNOUNCEMENT DUE TO PARTS OBSOLESCENCE. SERVICE INFORMATION LETTER MOS SIL D201401000052 BOEING 737 UGHT EMITTING DIODE (LED) WINGLET AND COLLISION LIGHT SYSTEM - WINGLET STROBE NOT RECOMMENDED 13-MAR-2011 FLASHING. SERVICE INFORMATION LETTER MOS SIL D201402000030 INSPECTION OF THE LEVER. PN 3177656-1 OR PN 63000974-1. AND ADAPTER ASSEMBLY. PN 3177635-2 OR -3. ON THE RECOMMENDED 26-FEB-2014 PRECOOLER CONTROL VALVE (PCCV). PN 3289562-6.-7. SERVICE INFORMATION LETTER MOS SL 737-SL-00-014 REV. A LOADABLE SOFTWARE MEDIA BINDERS. SERVICE LETTER INFORMATIONAL 19-SEP-2001 MOS - (s) SL 737-SL-00-015 FLIGHT DECK FAULT INDICATIONS AND NUISANCES MESSAGES. SERVICE LETTER INFORMATIONAL 29-JUN-1999 MOS - (s) SL 737-SL-00-016 SOFTWARE STORAGE ON DISKETTE SET. OTHER MEDIA SET. AND MASS STORAGE DEVICES. SERVICE LETTER INFORMATIONAL 20-SEP-1999 MOS - (s) SI. 737-SL-00-017 AVAILABILITY OF BOEING DISKETTE COPY PROCESS AND TOOL SET. (SUPERSEDED BY SL 737-SL-00-017 REV. A). SUPERSEDED SERVICE LETTER MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 207 Of 748 @ Camp Systems EFTA00618498 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SL 737-SL-00-017 REV. A AVAILABILITY OF BOEING DISKETTE COPY PROCESS AND TOOL SET. SERVICE LETTER RECOMMENDED MOS 17-OCT-2012 SL 737-SL-00-019 SUSPECT DISCREPANCY REPORT PROCESS (SUPERSEDED BY SL 737-SL-00-019 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-00-019 REV. A SUSPECT DISCREPANCY REPORT PROCESS. SERVICE LETTER RECOMMENDED MOS I3-NOV-2012 SL 737-SL-00-020 PROCEDURES FOR SEEKING ALTERNATE METHOD OF COMPLIANCE APPROVAL. SERVICE LETTER MOS 24-JAN-2007 SL 737-SL-00-022 BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL OBJECTION (NTO). ACCEPTABLE. AND APPROVED (8100-9) DATA. SERVICE LETTER MOS 10-JAN-2008 SL 737-SL-00-022 REV. A BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL OBJECTION (NTO). ACCEPTABLE. AND APPROVED (8100-9) DATA. SERVICE LETTER MOS 12-MAR-2008 SI. 737-SL-00-022 REV. 8 BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL OBJECTION (NTO). ACCEPTABLE. AND APPROVED (8100-9) DATA (SUPERSEDED BY SL 737-SL-00-022 REV. C). SERVICE LETTER MOS INFORMATIONAL INFORMATIONAL INFORMATIONAL SUPERSEDED SL 737-SL-00-022 REV. C BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL SUPERSEDED OBJECTIONS. FAA 8100-9 FORMS. AND REPAIR AND DEVIATION RECORDS (SUPERSEDED BY SL 737-SL-00-022 REV. D), SERVICE LETTER MOS SL 737-SL-00-022 REV. D BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL RECOMMENDED OBJECTIONS. FAA 8100-9 FORMS. AND REPAIR AND DEVIATION RECORDS. SERVICE LETTER MOS I6-JUL-2013 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 208 Of 748 @ Camp Systems EFTA00618499 CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SL 737-SL-00-023 SMOKE AND BURNING ODOR (SBO) EVENT SUMMARY. SERVICE LETTER INFORMATIONAL MOS 22-FEB-2008 • SL 737-SL-00-023 REV. A SMOKE AND BURNING ODOR (SBO) EVENT SUMMARY. SERVICE LETTER INFORMATIONAL MOS 24-NOv-2008 SL 737-SL-00-023 REV. B SMOKE AND BURNING ODOR (SBO) EVENT SUMMARY. SERVICE LETTER INFORMATIONAL MOS 17-DEC-2009 SL 737-SL-00-024 BOEING TECHNICAL COMMUNICATIONS (SUPERSEDED BY SL 737-SL-00-024 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-00-024 REV. A BOEING TECHNICAL COMMUNICATIONS. SERVICE LETTER RECOMMENDED MOS 11-APR-2011 SL 737-SL-00-025 DISCONTINUED USE OF 3.5 INCH FLOPPY DISKETTES FOR ONBOARD LOADABLE LRLI'S (SUPERSEDED BY SL SUPERSEDED 737-SL-00-025 REV. A). SERVICE LETTER MOS SL 737-SL-00-025 REV. A DISCONTINUED USE OF 3 5 INCH FLOPPY DISKETTES FOR ONBOARD LOADABLE LRUS (SUPERSEDED BY SL SUPERSEDED 737-SL-00-025 REV B). SERVICE LETTER MOS SL 737-SL-00-025 REV. B DISCONTINUED USE OF 3.5 INCH FLOPPY DISKETTES FOR ON BOARD LOADABLE LRUS (SUPERSEDED BY SL 737-SL-00-025 REV. C). SERVICE LETTER MOS SL 737-SL-00-025 REV. C DISCONTINUED USE OF 3 5 INCH FLOPPY DISKETTES FOR ONBOARD LOADABLE LRU.S. SERVICE LETTER MOS 23-JUL-2014 SL 737-SL-00-026 OPERATOR CORRECTION OF ERRORS IN THE LIFE LIMITED PART LIST AND AIRCRAFT READINESS LOG. SERVICE LETTER MOS 17-JAN.2014 SUPERSEDED RECOMMENDED RECOMMENDED ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time 209 Of 748 11 Camp Systems EFTA00618500 COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SL 737-SL-02-002 IN-FIGHT AIRFRAME VIBRATION. SERVICE LETTER INFORMATIONAL MOS 28-JUL-1987 - Is) St 737-SL-02-002 REV. A IN-FIGHT AIRFRAME VIBRATION. SERVICE LETTER INFORMATIONAL MOS 09-AUG-1995 - (s) St 737-SL-02-002 REV. B IN-FIGHT AIRFRAME VIBRATION. SERVICE LETTER INFORMATIONAL MOS I I -SEP-1996 - Is) St 737-SL-02-002 REV. C IN-FIGHT AIRFRAME VIBRATION. SERVICE LETTER INFORMATIONAL MOS 28-APR-1999 - Is) St 737-SL-02-002 REV. D IN FLIGHT AIRFRAME VIBRATION.. SERVICE LETTER INFORMATIONAL MOS 03-JUL-2001 - (s) St 737-SL-02-008 PASSENGER CARRY ON ELECTRONIC DEVICES (SUPERSEDED BY SL 737-SL-02-058 REV. A). SERVICE LETTER SUPERSEDED MOS 04-JUL-I 993 - (s) St 737-SL-02-008 REV. A PASSENGER CARRY ON ELECTRONIC DEVICES (SUPERSEDED BY SL 737-SL-02-058 REV. B). SERVICE LETTER SUPERSEDED MOS - (s) St 737-SL-02-008 REV. B PASSENGER CARRY ON ELECTRONIC DEVICES (SUPERSEDED BY SL 737-SL-02-058 REV. C), SERVICE LETTER SUPERSEDED MOS - St 737-SL-02-008 REV. C PASSENGER CARRY ON ELECTRONIC DEVICES (SUPERSEDED BY SL 737-SL-02-058 REV. D), SERVICE LETTER SUPERSEDED MOS - Is) St 737-SL-02-008 REV. D PASSENGER CARRY-ON ELECTRONIC DEVICES (SUPERSEDED BY 51 737-SL-02-008 REV. E), SERVICE LETTER SUPERSEDED MOS St 737-SL-02-008 REV. E PASSENGER CARRY-ON ELECTRONIC DEVICES (SUPERSEDED BY St 737-SL-02-008 REV. F). SERVICE LETTER SUPERSEDED MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 210 Of 748 @ Camp Systems EFTA [truncated]