EFTA02714500

1 OF 2 150526 WRO F381 PIC0092015 WORK REQUEST ORDER PICTON II LTD VP-BBJ 16737-72U I SN 29273 I YG006 NC I E2T I E2C I APUT I APUC I TO: Seyidi Ersevik COMPANY: hit Aviation Geneva FAX NUMBER: EMAIL ADDRESS: FROM (CAM): Steve Wilson DATED: 76.05.7014 QUOTATION REFERENCE: NJA WORK REQUEST ORDER NUMBER: P1C0092015 ITEM DESCRIPTION W/O ENTRY SIGNATURE 1. Comply with 1A/2A CAMP WO attached - -VP-BB) 2A Check 2015". Comply with Due Maintenance CAMP WO attached - "VP-BB) Due MX Jun 2015". 2. Compliance with AD 2012.24.08 / SB 737-30A1063 R2 NOTE: KITS provided as ordered with Jet Aviation. AMOC Letters to be referred if SB 737.30A1063 is not possible to install as is. (AMOC letters: I. GAMOC_1305-13-254 2. GAMOC_1305.14-66 3. SB-737-30A1063-02-AMOC-01 = 36 Months 3. Compliance with Task 28-AWL-05 and any other A/R applicable task after AD 2012-24.08 C/W. 4. Compliance with AD 2010-24-11 / SB 737.57A1279 consumables to be ordered ASAP. NOTE: A/R Tasks (MPD) to be verified N/A before access closure. S. Compliance with AD 2012-25-05 N/A by PN installed. Please check aircraft and record in WO accordingly. 6. Compliance with SB 737-28A1206 R3. Revision 2 previously C/W. 7. THANK YOU EXPECTED ARRIVAL: 15.06.2015 REQUESTED AVAILABILITY: 26.06.2015 CONTINUED AIRWORTHINESS MANAGEMENT (on behalf of PICTON II Ltd) Qjet Aero I Switzerland I [email protected] I Tel: +41 76 510 2654 EFTA_R1_02140495 EFTA02714500 150526 WRO F381 PIC0092015 WORK REQUEST ORDER INSTRUCTIONS RELEVANT - CERTIFICATE OF RELEASE TO SERVICE (CRS) 1. After entry of Work Request Items into MRO system, Planning or Technical Support shall sign in the allocated space. Signature indicates that request(s) have been transferred to the actual project. 2. Item numbers showing "*" have been amended/added after original order was issued. 3. Certificate of Release to Service (CRS) shall refer Work Request Order Number and encompass all requested items unless otherwise specified or communicated. 4. Work Order entries (items) shall detail maintenance reference/specific chapters in all cases. Generic references and vague statements will not be accepted. AMM revision status shall also be indicated. 5. CRS shall comprise Flight Log Entry/Stamp/Signature and printed Certificate for Aircraft/Engine/APU Logbook(s). INSTRUCTIONS RELEVANT - CONTINUED AIRWORTHINESS MANAGEMENT 1. Before aircraft departure CRS, WO and Flight Log Entry shall be scanned and sent to the Continued Airworthiness Manager (CAM) for review. 2. After project closing, all CAMP Cards including CRS shall be scanned and sent to CAMP SYSTEMS for update within 5 working days. 3. Original Work Package documents shall be handed to the Operator or CAM as arranged. Note: There is no requirement for originals/copies of procedures used during maintenance to be provided. CONTINUED AIRWORTHINESS MANAGEMENT (on behalf of PICTON II Ltd) Qjet Aero I Switzerland I [email protected] I Tel: +41 76 510 2654 EFTA_R1_02140498 EFTA02714501 CAMP A^....P•••••••••••ey Work Order Contents Report SERIAL : 29273 (YG006) REGNO : VP-BBJ MODEL NAME : BBJ 737-700IGW/-800/-900ER DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : WORK ORDER A: VP-BB.1 2A CHECK 2015 SERVICE CENTER : JET AVIATION (GENEVE) S.A. SORT ITEM NO DESCRIPTION STATUS 1.0 050020 1.1 352003 1.2 352004 1.3 21-88)-01 1.4 21-88)-02 1.5 33-090-00 1.6 25-020-00 COMPLIANCE NEXT DUE TIME REMAINING A-2 CHECK OPEN VISUAL INSPECTION OXYGEN SYS. BOX(S) OPEN VISUAL INSPECTION OXYGEN SYS MASK(S) OPEN INSPECT AND CLEAN OR REPLACE THE LEFT HAND NC COALESCER BAG OPEN INSPECT AND CLEAN OR REPLACE THE RIGHT HAND NC COALESCER BAG OPEN GENERAL VISUAL INSPECTION OF THE TRANSPARENT FAIRING LENS LOCATED ON THE FORWARD LEADING OPEN EDGE OF THE WINGLET, LEFT AND RIGHT DETAIL INSPECTION OF PIE CAPTAIN, FIRST OFFICER, FIRST OBSERVER AND SECOND OBSERVER (IF OPEN INSTALLED) SEAT HARNESSES, CROTCH STRAPS, AND SHOULDER BELTS (AS APPLICABLE) FOR WEAR, CONDITION AND SECURITY. 1.7 28-20-01 PATS OPERATIONAL CHECK OF THE AUXILIARY FUEL CONTROL UNIT OPEN 1.8 23-110-00 (FAR 91.207) INSPECT (FIXED) EMERGENCY LOCATOR TRANSMITTER TAW FAR 91.207(D) OPEN 1.9 54.090-01 FUNCTIONALLY CHECK THE LEFT ENGINE FORWARD STRUT AND AFT STRUT MIRING DRAINS. OPEN 1.10 54-090-02 FUNCTIONALLY CHECK THE RIGHT ENGINE FORWARD STRUT AND AFT STRUT MIRING DRAINS. OPEN 1.11 385015 CLEAN AFT GALLEY SINK DRAIN FILTER OPEN 1.12 21-140-01 CHECK THE LEFT WATER SEPARATOR INDICATION DISK (WITH THE AIR CONDITIONING SYSTEM OPERATING) OPEN 1.13 21.140.02 CHECK THE RIGHT WATER SEPARATOR INDICATION DISK (WITH THE AIRCONDITIONING SYSTEM OPERATING) OPEN 1.14 23-040-00 OPERATIONAL CHECK OF THE VOICE RECORDER AND RECORDER INDEPENDENT POWER OPEN SUPPLY (RIPS) (IF INSTALLED). 1.15 27-102-00 LUBRICATE STABILIZER TRIM ACTUATOR AND ACTUATOR GIMBAL PINS AND BALLNUT OPEN 1.16 27-170-01 LUBRICATE LEFT WING TRAILING EDGE FLAP ACTUATION MECHANISM OPEN 1.17 27-170-02 WBRICATE RIGHT WING TRAILING EDGE FLAP ACTUATION MECHANISM OPEN L18 32-010-01 CLEAN LEFT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN 1.19 32-010-02 CLEAN RIGHT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN 1.20 32-020-01 SERVICE LEFT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN 1.21 32-020-02 SERVICE RIGHT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN 1.22 32-030-01 LUBRICATE LEFT MAIN LANDING GEAR ASSEMBLY OPEN 1.23 32-030-02 WBRICATE RIGHT MAIN LANDING GEAR ASSEMBLY OPEN 1.24 32-060-00 CLEAN NOSE LANDING GEAR SHOCK STRUT OPEN 1.25 32-070-00 SERVICE NOSE LANDING GEAR SHOCK STRUT OPEN 1.26 32-080-00 LUBRICATE NOSE LANDING GEAR ASSEMBLY OPEN 1.27 32-270-01 VISUAL CHECK LEFT BRAKE WEAR PINS FOR MINIMUM EXTENSION OPEN 1.28 32-270-02 VISUAL CHECK RIGHT BRAKE WEAR PINS FOR MINIMUM EXTENSION OPEN 1.29 32-800-00 EXTERNAL ZONAL INSPECTION (GV) NOSE LANDING GEAR AND LANDING GEAR DOORS (FROM GROUND) OPEN PERFORM AN EXTERNAL ZONAL INSPECTION (GV) Of THE NOSE LANDING GEAR AND LANDING GEAR DOORS. INSPECTION IS ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. (EZAP) 1.30 32.804.01 EXTERNAL ZONAL INSPECTION (GV) LEFT MAIN LANDING GEAR AND LANDING GEAR DOORS (FROM GROUND) OPEN PERFORM AN EXTERNAL ZONAL INSPECTION (GV) OF THE LEFT MAIN LANDING GEAR AND LANDING GEAR DOORS. INSPECTION IS ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS 1.31 32.808.02 EXTERNAL ZONAL INSPECTION (GV) RIGHT MAIN LANDING GEAR AND LANDING GEAR DOORS (FROM GROUND) OPEN PERFORM AN EXTERNAL ZONAL INSPECTION (GV) OF THE RIGHT MAIN LANDING GEAR AND LANDING GEAR DOORS. INSPECTION IS ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS 26-MAY-2015 © CAMP SYSTEMS I of 3 EFTA_R1_02140497 EFTA02714502 CAMP A^....P•••••••••••ey Work Order Contents Report SERIAL : 29273 (YG006) REGNO : VP-BB) MODEL NAME : 68) 737.700IGW/-800/-900ER DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : WORK ORDER At: VP-B8) 2A CHECK 2015 SERVICE CENTER : JET AVIATION (GENEVE) S.A. SORT ITEM NO DESCRIPTION STATUS 1.32 33-010-00 1.33 53-800-00 1.34 53.81200 1.35 53-830-00 1.36 53.84400 1.37 53-894-00 1.38 55-800-00 1.39 57.802-01 1.40 57-872-02 1.41 70-803-01 1.42 70-810-02 1.43 52-150-00 1.44 26-450-00 1.45 050010 1.46 257001 1.47 257002 1.48 257003 1.49 257004 1.50 257005 1.51 257006 1.52 257007 1.53 257011 1.54 352002 1.55 381120 1.56 385010 1.57 57-950-01 1.58 57-952-01 1.59 57-960-02 COMPLIANCE NEXT DUE TIME REMAINING OPERATIONAL CHECK EMERGENCY LIGHTS OPEN EXTERNAL ZONAL INSPECTION (GV) OF THE LOWER FUSELAGE. THE NOSE LANDING GEAR WHEEL WELL AND OPEN MAIN LANDING GEAR WHEEL WELL ARE ALSO INCLUDED. INSPECTION IS ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED (EZAP) INTERNAL ZONAL INSPECTION (GV) FORWARD CARGO COMPARTMENT - SECTION 43, STATION 396 TO OPEN FORWARD CARGO COMPARTMENT AFT BULKHEAD INTERNAL ZONAL INSPECTION (GV) AFT CARGO COMPARTMENT - SECTION 46 AND 47 (PART), STATION 727 OPEN TO STATION 947.5 EXTERNAL ZONAL INSPECTION (GV) OF THE WING TO BODY FAIRING. INSPECTION IS ACCOMPLISHED FROM OPEN THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRE EXTERNAL ZONAL INSPECTION (GV) OF 711E FUSELAGE. INSPECTION IS ACCOMPLISHED FROM THE GROUND, OPEN WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED EXTERNAL ZONAL INSPECTION (GV) VERTICAL FIN AND HORIZONTAL STABILIZER. INSPECTION IS OPEN ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED EXTERNAL ZONAL INSPECTION (GV) LEFT WING INSPECTION IS ACCOMPLISHED FROM THE GROUND, WITHOUT OPEN THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED. EXTERNAL ZONAL INSPECTION (GV) RIGHT WING INSPECTION IS ACCOMPLISHED FROM THE GROUND, OPEN WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED. EXTERNAL ZONAL INSPECTION (GV) NO. 1 ENGINE STRUT FAIRINGS. INSPECTION IS ACCOMPLISHED FROM OPEN THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED. EXTERNAL ZONAL INSPECTION (GV) NO. 2 ENGINE STRUT FAIRINGS INSPECTION IS ACCOMPLISHED FROM OPEN THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED LUBRICATE AIRSTAIR DOOR SYSTEM (INCLUDES TWO ROLLERS, CARRIAGE DRIVE BEARING, DRIVE NUT IN OPEN JACK SCREW, LOCK PIN GREASE FITTING AND FOUR BEARINGS IN THE CARRIAGE ROLLERS). INSPECT (DETAILED) THE PORTABLE HALON FIRE EXTINGUISHERS FOR PROPER PRESSURE (IF GAUGE OPEN INSTALLED), WEIGHT AND CONDITION. A- I CHECK OPEN GENERAL VISUAL INSPECTION HEADLINER CEILING PANELS OPEN GENERAL VISUAL INSPECTION INTERIOR BULKHEADS OPEN GENERAL VISUAL INSPECTION COMPARTMENT DOORS OPEN GENERAL VISUAL INSPECTION SEATS ANDTABLES OPEN GENERAL VISUAL INSPECTION CLOSET AND CABINETS OPEN GENERAL VISUAL INSPECTION CLOSET AND CABINET DOORS OPEN GENERAL VISUAL INSPECTION BED AND DIVANS OPEN CHECK SAFETY BELTS OPEN GENERAL VISUAL INSPECTION CHEMICAL 02 MASK OPEN CHECK WATER/WASTE DRAIN LINES OPEN CLEAN WATER/WASTE INSIDE FILTER OPEN EXTERNAL ZONAL INSPECTION OF THE LEFT WINGLET OPEN INTERNAL ZONAL INSPECTION LEFT WINGLET OPEN EXTERNAL ZONAL INSPECTION OF THE RIGHT WINGLET OPEN 26-MAY-2015 © CAMP SYSTEMS 2 of 3 EFTA_R1_02140498 EFTA02714503 CAMP A^....P•••••••••••ey Work Order Contents Report SERIAL : 29273 (YG006) REGNO : VP-BB) MODEL NAME : 88) 737.700IGW/-800/-900ER WORK ORDER At: VP-88) 2A CHECK 2015 DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A. SORT ITEM NO DESCRIPTION STATUS COMPLIANCE NEXT DUE TIME REMAINING 1.60 57-962-02 INTERNAL ZONAL INSPECTION OF THE RIGHT WINGLET OPEN 1.61 33-055-00 FUNCTIONAL CHECK THE EMERGENCY LIGHTING BATTERY PACKS FOR CAPACITY (15 MIN. MINIMUM) AND ONE OPEN COMPLETE DEEP CYCLE. 1.62 72-020-01 DETAILED INSPECTION OF LEFT ENGINE INLET AND FAN BLADES. OPEN 1.63 72-020-02 DETAILED INSPECTION OF RIGHT ENGINE INLET AND FAN BLADES OPEN Prepared By: Approved By: Date: Date: 26-MAY-2015 © CAMP SYSTEMS 3 of 3 EFTA_R1_02140499 EFTA02714504 CAMP A^....P••••••••••ey Work Order Contents Report SERIAL : 29273 (YG006) REGNO : VP-BEJ MODEL NAME : BB) 737.700IGW/-8001.900ER DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : WORK ORDER At: VP-B8) DUE MX )UN. 2015 SERVICE CENTER : JET AVIATION (GENEVE) S.A. SORT ITEM NO DESCRIPTION STATUS COMPLIANCE NEXT DUE TIME REMAINING 1.0 737-28A1206 R3 FUEL - DISTRIBUTION - CENTER FUEL TANK BOOST PUMP AUTO SHUTOFF AND MASTER CAUTION LOGIC OPEN CHANGE, SERVICE BULLETIN 2.0 252501 VISUALLY CHECK FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER OPEN PRESSURE 3.0 252502 VISUALLY CHECK FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER OPEN PRESSURE 4.0 252503 VISUALLY CHECK AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER PRESSURE OPEN 5.0 252504 VISUALLY CHECK AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER PRESSURE OPEN 6.0 FM 2005-18-23 CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL OPEN 7.0 FM 2006-21-01 PART 1 FLIGHT CONTROLS AILERON AND AILERON TRIM CONTROL SYSTEM MEASURE THE FREEPLAY OF BOTH OPEN AILERON CONTROL BALANCE TABS 8.0 FM 2006-21-01 PART 2 FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - REPETATIVE LUBRICATION OPEN 9.0 FM 2011.27-03 PAM (6)(1)(1)(1) DETAILED INSPECTION TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE OPEN BALLSCREW IN THE DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAR AND FAILURE OF THE SECONDARY LOAD PATH IN ACCORDANCE WITH SERVICE BUITIN 737-27A1277 R2 10.0 29-230-03 OPERATIONAL CHECK STANDBY RUDDER SYSTEM TO INCLUDE OBSERVING LOW PRESSURE LIGHT OPEN ILLUMINATION AND THEN EXTINGUISHING. 11.0 24-120-00 (001.1) RESTORE MAIN BATTERY OPEN 12.0 24-120-00(002.1) RESTORE AUXILIARY BATTERY OPEN 13.0 254206 LAERDAL HEARTSTART FR DEFIBRILLATOR PADS OPEN 14.0 081001 WEIGHT CHECK OF AIRCRAFT OPEN 15.0 252901 CAPTAIN LIFE JACKET OPEN 16.0 252902 FIRST OFFICER LIFE JACKET OPEN 17.0 252903 FIRST OBSERVER LIFE JACKET OPEN 18.0 252904 NO. 1 FORWARD FLIGHT ATTENDANT LIFE JACKET OPEN 19.0 252905 NO. 2 FORWARD FLIGHT ATTENDANT LIFE JACKET OPEN 20.0 252906 NO. 1 AFT FLIGHT ATTENDANT UFE JACKET OPEN 21.0 252907 NO. 2 AFT FLIGHT ATTENDANT LIFE JACKET OPEN 22.0 252909 SECOND OBSERVER LIFE JACKET OPEN 23.0 256323 (001.1) OPERATIONAL CHECK OF THE NO. 1 FORWARD EMERGENCY FLASHUGHT OPEN 24.0 256323 (002,1) OPERATIONAL CHECK OF THE NO. 2 FORWARD EMERGENCY FLASHUGHT OPEN 25.0 256323 (003.1) OPERATIONAL CHECK OF THE NO. 1 COCKPIT FLASHLIGHT OPEN 26.0 256323 (004.1) OPERATIONAL CHECK OF THE NO. 2 COCKPIT FLASHUGHT OPEN 27.0 256323 (005.1) OPERATIONAL CHECK OF THE NO. 1 AFT EMERGENCY FLASHUGHT OPEN 28.0 256325 (003.1) OPERATIONAL CHECK OF THE CARGO NET OPEN 29.0 347105 (1) BIANNUAL CHECK EGPWS TERRAIN DATABASE VERSION STATUS OPEN 30.0 33.06600 RESTORE EMERGENCY LIGHTING BATTERY PACK (TWO OR MORE COMPLETE DEEP CYCLES) BATTERY CAPACITY OPEN TO REQUIRED STANDARD 31.0 25-310-00 (002.1) RESTORE NO. 2 LIFE RAFT PRESSURE BOTTLE OPEN 32.0 25-420-03 (001.1) RESTORE FORWARD FIRST AID KIT OPEN 33.0 25-420-00 (002.1) RESTORE AFT FIRST AID KIT OPEN 34.0 25-430-00 (001.1) RESTORE MEDAIRE - BLUE FIRST AID MEDICAL KIT OPEN 26-MAY-2015 © CAMP SYSTEMS 1 of 2 EFTA_R1_02140500 EFTA02714505 CAMP A^....P••••der...4 .• Work Order Contents Report SERIAL : 29273 (YG006) REGNO : VP-BB) MODEL NAME : 88) 737.700IGW/-800/-900ER DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : WORK ORDER At: VP-B8.1 DUE MX )UN. 2015 SERVICE CENTER : JET AVIATION (GENEVE) S.A. SORT ITEM NO DESCRIPTION STATUS 35.0 38-040-00 36.0 FM 2015-04-02 37.0 FM 2015-04-02 COMPLIANCE NEXT DUE TIME REMAINING RESTORE WASTE DRAIN BALL VALVE THE WASTE DRAIN BALL-VALVE BY REPLACING SEALS (2) (OFF OPEN AIRCRAFT) NO. 1 ENGINE - ENGINE FUEL AND CONTROL - MODIFY THE ENGINE BY REMOVING FULL AUTHORITY DIGITAL OPEN ENGINE CONTROL (FADEC) SOFTWARE, VERSION 7.B.V4 OR EARUER, INSTALLED IN THE ELECTRONIC ENGINE CONTROL (EEC) NO. 2 ENGINE - ENGINE FUEL AND CONTROL - MODIFY THE ENGINE BY REMOVING FULL AUTHORITY DIGITAL OPEN ENGINE CONTROL (FADEC) SOFTWARE, VERSION 7.B.V4 OR EARLIER, INSTALLED IN THE ELECTRONIC ENGINE CONTROL (EEC) 38.0 25-300-00 (002.1) INSPECT AFT LIFE RAFT OPEN 39.0 25-300-00 (003.1) INSPECT NO. 3 LIFE RAFT OPEN 40.0 26-330-00 (002.1) REPLACE (LIID2) CARGO FIRE EXTINGUISHER BOTTLE AFT SQUIB OPEN 41.0 25-60-00 GENERAL VISUAL INSPECTION OF ALL COCKPIT / CABIN EMERGENCY EQUIPMENT OPEN 42.0 28-054-00 OPERATIONAL CHECK (BITE) THE FUEL PUMP GFI RELAY OPEN 43.0 28-056-00 FUNCTIONALLY CHECK THE CENTER TANK FUEL BOOST PUMP POWER FAILED ON PROTECTION SYSTEM OPEN 44.0 28-115-00 FUNCTIONALLY CHECK THE CENTER TANK BOOST PUMP AUTO SHUTOFF SYSTEM OPEN 45.0 28-AWL-19 REVIEW CENTER TANK FUEL BOOST PUMP AUTOMATIC SHUTOFF SYSTEM OPEN 46.0 28-AWL-20 REVIEW OVER-CURRENT AND ARCING PROTECTION ELECTRICAL DESIGN FEATURES OPERATION - BOOST PUMP OPEN GROUND FAULT INTERRUPTER (CFI) 47.0 28-AWL-23 FUNCTIONALLY TEST CENTER TANK FUEL BOOST PUMP POWER FAILED ON PROTECTION SYSTEM. OPEN 48.0 737015 (I) ANNUAL CHECK OF EEC# I & EEC#2 SOFTWARE ENGINE FUEL AND CONTROL ECU SOFTWARE STATUS OPEN 49.0 FM 2011.27-03 PAM (G)(1XI)(2) LUBRICATE TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE 8A11FrREW IN THE OPEN DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAR AND FAILURE OF THE SECONDARY LOAD PATH IN ACCORDANCE SERVICE BULLETIN 737-27A1277 R2 50.0 347101 UPDATE NAV DATABASE OPEN Prepared By: Date: Approved By: Date: 26-MAY-2015 © CAMP SYSTEMS 2 of 2 EFTA_R1_02140501 EFTA02714506