EFTA01734493

Date

Unknown

Source

DOJ Data Set 10

Reference

efta-01734493

Pages

102

Persons

Integrity

Summary

Ask AI about this document

Search 264K+ documents with AI-powered analysis

0upvotesShare

Post Reddit

Save Post Watch

Extracted Text (OCR)

EFTA Disclosure

Text extracted via OCR from the original document. May contain errors from the scanning process.

NC: A6DFR EIC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB FJC Description: Print Date 07/09/2016 13:59 Page: 1 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information BC: 1974-08-09 39-9680 Category: AD Status: OPEN Rev: 16 25120-00-01 25-130-00-01 25400-60020 254000-DVI.10000.1 254000-DVI.10010.1 254012-0080 WASTE RECEPTACLE DOOR INSPECTION. 1000 Hrs Recur EARLIEST 632:35 20/07/2017 WO 50175 22/08/2015 Rev: 16 NC Total Hours: 5786:05 NC Total Cycles: 2071 254100-01000 Freq: i 74.08-09R2 74.08-09R3 A122540 EIC: 1987-08-09 AMM 12-15-51 INFLATION OF TIRES WITH NITROGEN Manual Compliance 01/06/1987 Rev: 2 39-5613 NC Total Hours: 0:00 NC Total Cycles: 0 THIS TASK IS CONTROLLED THROUGH DAILY Category: AD CHECK. Status: TERMINATED REF DAILY CHECK TASK CARD.. Rev: 2 EARLIEST Reason Freq: 1 COVERED BY DAILY CHECK TASK 05-010-01-AF, WORK STEP 8 . 32-BBJ-01.00 E/C: 1989-18-12 1991-10-02 CLASS B MAIN DECK CARGO 39-6557 COMPARTMENT Category: AD Status: N/A Rev: 2 Superseded By: 1991.1042 EARLIEST Reason Frog: I AD NOT APPLICABLE AS NC IS NOT EQUIPPED WITH WITH A CLASS B MAIN DECK CARGO COMPARTMENT. EFTA_R1_00012761 EFTA01734493 NC: A6DFR E/C (Category: AD) Ament NO A/C Actual Compliance Last Type/Series: 8737.700438,11 Document/SB NC SIN: 30884 E/C Description: Print Date 07/09/2016 13:59 Page: 2 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! HrslCyslDyslDte Next Due Last Compliance Information BC: 1990-25-01 Category: AD Status: OPEN Rev: 0 0626A001-MRBR CORROSION PREVENTION CONTROL PROGRAM Reason Freq: 1 FAA AMOC 120549487 DTD. 4-FEB-2010, APPROVES MRB COMPLIANCE WITH CPCP, REQUIREMENTS INCORPORATED INTO AMP. Once EARLIEST E/C: 1991-10-02 394986 Category: AD Status: N/A Rev: 2 1989-18.12 CLASS B MAIN DECK CARGO COMPARTMENT Superseded Sy: 1993-07-15 Reason Frog: I AD NOT APPLICABLE. NO CLASS B MAIN DECK CARGO COMPARTIMENT INSTALLED. EARLIEST E/C: 1993-07-15 39-8547 Category: AD Status: N/A Rev: 2 1989-18.12 1991-1002 CLASS B MAIN DECK CARGO COMPARTMENT Reason Freq: 1 THE AIRCRAFT IS NOT EQUIPPED WITH CLASS B MAIN DECK CARGO COMPARTMENT. HENCE, AD IS WA. LATEST BC: 1997-22.07 Category: AD Status: N/A Rev: 1 TO PREVENT SUDDEN DECOPMRESSION OF THE AIRPLANE Reason Freq: 1 SUPERSEDED BY AD 2002-07-08 EARLIEST EFTA_R1_00012762 EFTA01734494 NC: A6DFR EIC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DoeumenVSB BC Description: Print Date 07/09/2016 13:59 Page: 3 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/CyslDyslDte Next Due Last Compliance Information BC: 1998-02-01 Category: AD Status: N/A Rev: 1 UNCOMMANDED YAWING OF AIRCRAFT Reason Freq: I AD AFFECT MODEL 737-100, -200. - 300, -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 1998-02-51 Category: AD Status: N/A Rev: 1 INSPECTION OF HORZ STAB FOR STRUCTURAL INTEGRITY Reason Freq: 1 AD AFFECT MODEL 737-300. -400. -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST BC: 1998-03-09 Category: AD Status: N/A Rev: 1 DEFECTIVE AILERONS INSPECTION Reason Frog: 1 AD AFFECT MODEL 737-100, -200. - 300, -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 1998-03-10 39-10079 Category: AD Status: N/A Rev: 2 737-25-1334 PILOTS SEAT LOCK .4 SEAT TRACK OPERATIONS CHK. Reason Frog: I AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-25-1334 EARLIEST EFTA_R1_00012763 EFTA01734495 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DoeumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 4 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 1998-04.41 Category: AD Status: N/A Rev: 1 MAIN DECK CARGO DOOR & FUSE UPPER JAMB INSPECTION Reason Freq: I AD AFFECT MODEL 737-200. -300 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 1998-07-16 Category: AD Status: N/A Rev: 1 INTERCHANGING LOCATION OF HYD FUSE & FLOW LIMITER. Reason Freq: 1 AD AFFECT MODEL 737-300. -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST E/C: 1998-10-51 Category: AD Status: N/A Rev: 2 INSP OF FUEL BOOST PUMP WIRING IN THE FUEL TANKS Superseded By: 1998.11.51 Reason Frog: 1 AD AFFECT MODEL 737-100, -200. -200C, - 300. -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737.700 AIRCRAFT EARLIEST E/C: 1998-10-511 Category: AD Status: N/A Rev: 1 FUEL BOOST PUMP WIRING IN FUEL TANKS INSPECTION Reason Freq: i N/A - BY ACFT MODEL. APPL TO B737-100 TO -500. EARLIEST EFTA_R1_00012764 EFTA01734496 NC: A6DFR E/C (Category: AD) AmeM NO A/C Actual Compliance Last Type/Series: 8737.7001138J1 Document/SB NC SIN: 30884 EIC Description: Print Date 07/09/2016 13:59 Page: 5 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/CyslDyslDte Next Due Last Compliance Information EIC: 1998-11-04 Category: AD Status: N/A Rev: 02 ENSURE THE CONTINUED STRUCTURAL INTERGRITY Reason Freq: 1 AD AFFECT MODEL 737.100, -200 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT LATEST EIC: 1998-11-51 Category: AD Status: N/A Rev: 2 REMOVAL OF FUEL BOOST PUMP WIRING & DVL Reason Frog: 1 AD AFFECT MODEL 737.100. -200. •200C. • 300. -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 1998-11-51T Category: AO Status: N/A Rev: 01 REMOVAL OF FUEL BOOST PUMP WIRING & DVI. Reason Frog; 1 N/A - BY ACFT MODEL. APPLICABLE TO 5737-100 TO -500. EARLIEST EIC: 1998-11.52 Category: AD Status: N/A Rev: 1 REMOVAL OF FUEL BOOST PUMP WIRING. Reason Freq: I AD AFFECT MODEL 737-100. -200, -200C. - 300. -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-7® AIRCRAFT EARLIEST EFTA_R1_00012765 EFTA01734497 NC: A6DFR EIC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DoeumenVSB EJC Description: Print Date 07/09/2016 13:59 Page: 6 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 1998-13-12 Category: AD Status: N/A Rev: 01 PREVENT LOSS OF RUDDER CONTROL. Reason Freq: I AD AFFECT MODEL 737-100. -200. -200C. - 300, -400, AND -500 SERIES AIRPLANES. THE AD IS NIA FOR 737-700 AIRCRAFT EARLIEST E/C: 1998-14-09 Category: AD Status: N/A Rev: 1 FWD ENGINE MOUNTS SUPPORT FITTING & ATTACHEMENTS Reason Freq: 1 AD AFFECT MODEL 737-100. -200. 200C SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST BC: 1998-18-20 Category: AD Status: N/A Rev: 1 REPLACE JC CARTER FUEL S/OFF VALVE. Reason Frog: 1 THE AIRCRAFT IS NOT FITTED WITH CARTER FUEL VALVES P/N 40574-5 OR -5. AD IS N/A BY INSTALLED P/N. EARLIEST BC: 1998-19-09 Category: AD Status: CANCEL Rev: 1 FUEL BOOST PUMP & WIRING CHAFING CHK. Superseded By: 1999-21-15 Reason Frog: 1 AD AFFECT MODEL 737-200, - 300, -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EFTA_R1_00012766 EFTA01734498 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700IBB/1 NC S/N: 30884 EIC (Category: AD) Anent NO DocumenVSB FJC Description: Print Date 07/09/2016 13:59 Page: 7 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 1998-21-11 Category: AD Status: N/A Rev: 1 APU & ENGINES FIRE DETECTOR ASSEMBLIES Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD LINE NUMBER EFFECTIVITY LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST E/C: 1998-22-10 Category: AD Status: N/A Rev: 1 FUSE FWD SERVICE DOORWAY. AFT FRAME INSPECTION Reason Freq: 1 AD AFFECT MODEL 737-100. -200. -200C.- 300, AND -400 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 1998-25-06 Category: AD Status: N/A Rev: 1 DOOR FRAME & CROSS BEAMS OF AFT CARGO DOOR INSP. Superseded By: 2000.06.13 Reason Freq: 1 AD AFFECT MODEL 737-200. • 300. -400 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EFTA_R1_00012767 EFTA01734499 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 DoeumenVSB EJC Description: Print Date 07/09/2016 13:59 Page: 8 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information BC: 1998-26-24 Category: AD Status: N/A Rev: 1 TO PREVENT FAILURE OF THE WHEEL FLANGES Reason Freq: I AD AFFECT MODEL 737-100, -200 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST E/C: 1999-01-16 Category: AD Status: N/A Rev: 1 TO PREVENT DAMAGE TO AIRFRAME. HSTAB, ENGINES. Reason Freq: 1 AD AFFECT MODEL 737-100. -200. - 300. -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST E/C: 1999-03-04 Category: AD Status: N/A Rev: 1 TO PREVENT POSSIBLE IGNITION OF FUEL VAPOURS. Reason Frog: 1 AD AFFECT MODEL 737-100, -200. - 300, -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 1999-03-08 Category: AD Status: N/A Rev: 01 SB737-73A1011 FUEL HOSE QUICK DISCONNECT-INSPECTION 1 TERMINATION Superseded By: 2002.1421 Reason Frog: I AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-73A1011 EARLIEST EFTA_R1_00012768 EFTA01734500 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Salves: B737.700IBBJ1 NC SIN: 30884 DoeumenVSB FJC Description: Print Date 07/09/2016 13:59 Page: 9 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/DyslDte Next Due Last Compliance Information E/C: 1999-04-11 Category: AD Status: N/A Rev: 1 TO PREVENT DAMAGE OF AFT STRUT INSUL BLANKETS. Superseded By: 2008.21.02 Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD LINE NUMBER EFFECTIVITY LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST Ex: 1999-04-23 BROKEN BOLTS THAT ATTACH THE TERMINAL SUPPORT FITTING Category: AD Status: N/A Rev: 1 EARLIEST Reason Freq: i AD AFFECT MODEL 737-100. -200. -300 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT E/C: 1999-05-12 CENTER FUEL TANK WIRING Category: AD Status: N/A Rev: 1 EARLIEST Reason Freq: 1 AD AFFECT MODEL 737-100. -200. - 300. -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EFTA_R1_00012769 EFTA01734501 NC: A6DER E/C (Category: AD) Anent NO A/C Actual Compliance Last Type/Series: B737-70043BJ1 NC S/N: 30884 Document/SB E/C Description: Print Date 07/09:2016 13.59 Page: 10 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information EX: 1999-05-15 Category: AD Status: N/A Rev: 1 ELEVATOR TAB PUSH ROD. Reason Freq: 1 AD AFFECT MODEL 737-100. -200. - 300, -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EX: 1999-08-03 Category: AD Status: N/A Rev: 01 SB 737-24-1128 PANELS POWER DISTRIBUTION P91 & P92 - PREVENTION OF FAILURE Reason Freq: 1 AD IS N/A BY THE EFFECTMTY LIST OF BOEING SB 737-24-1128 EARLIEST EIC: 1999-08-21 39-11130 Category: AD Status: N/A Rev: 3 PAX 02 MASKS & PORTABLE 02 MASKS Reason Free: 1 THE AIRCRAFT IS NOT FITTED WITH PURITAN BENNET OXYGEN MASKS . AD IS N/A BY INSTALLED P/N. EARLIEST EIC: 1999-08-23 Category: AD Status: NIA Rev: 1 TO DETECT & CORRECT FATIGUE CRACKING Reason Freq: I AD AFFECT MODEL 737-100. -200. -200C. - 300. -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-7® AIRCRAFT EARLIEST EFTA_R1_00012770 EFTA01734502 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB FJC Description: Print Date 07/09/2016 13:59 Page: 11 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 1999-10-12 Category: AD Status: N/A Rev: 1 TO DETECT 8 CORRECT CORROSION AND CRACKING Reason Freq: I AD AFFECT MODEL 737-100. -200. -200C. - 300, -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST E/C: 1999-10-13 Category: AD Status: N/A Rev: 2 SE1737-27A1228 S245 TRAILING EDGE FLAP LIMIT SWITCH Reason Frog: 1 INFOR AD IS NOT APPLICABPLE TO THIS NC EFFECTIVITY OF SB AND YG039 IN NOT AFFECTED BY SB EARLIEST E/C: 1999-11-05 39-11175 Category: AD Status: TERMINATED Rev: 2 737-27A1222 RUDDER PCU SECONDARY SLIDE DISPLACEMENT TEST Frog: 1 LATEST Manual Compliance 26/02/2001 Rev: 2 NC Total Hours: 1103:35 NC Total Cycles: 595 FOUND ACCOMPLISHED ON 26/02/2001 AS PER LHT REPORT AT DELIVERY BC: 1999-12-08 Category: AD Status: N/A Rev: 01 TO PREVENT OPENING OR LOSS OF THE CARGO DOOR Reason Frog: 1 AD AFFECT MODEL 737-200C SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EFTA_R1_00012771 EFTA01734503 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SS EJC Description: Print Date 07/09/2016 13:59 Page: 12 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 1999-13-51 Category: AD Status: N/A Rev: 01 CN1999-259-IMP(B SB 737-55A1068 TO PREVENT REDUCED CONTROLLABILITY OF ACFT EARLIEST Reason Freq: I AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-55A1068 E/C: 1999-15-09 TO PREVENT LOSS OF CONTROLLABILITY OF THE AIRPLANE Category: AD Status: N/A Rev: 1 EARLIEST Reason Froq: 1 THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 1999-15-09 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. E/C: 1999-16-11 ENGINE SQUIB CIRCUIT TEST Category: AD Status: N/A Rev: 1 EARLIEST Reason Frog: 1 THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 1999.16.11 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EFTA_R1_00012772 EFTA01734504 NC: A6DER UC (Category: AD) Anent NO A/C Actual Compliance Last Type/Series: B737-700188,11 NC SIN: 30884 Document/SR EJC Description: Print Date 07/09:2016 13.59 Page: 13 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/CyslDyslDte Next Due Last Compliance Information FJC: 1999-18-01 Category: AD Status: N/A Rev: 1 ELEVATOR TAB Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 1999-18-01 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST EIC: 1999-18-17 PREVENTION OF FAILURE OF ALL ELECTRICALLY POWERD AIRPLANE SYSTEMS Category: AD Status: N/A Rev: 1 EARLIEST Reason Freq: I AD AFFECT MODEL 737-100. -200, - 300. -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT BC: 1999-19-27 TO PREVENT FAILURE OF MULTIPLE TIE BOLTS Category: AU Status: N'A Rev: 1 EARLIEST Reason Frog: t AD AFFECT MODEL 737-100. -200. - 300. -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EFTA_R1_00012773 EFTA01734505 NC: A6DFR EIC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 DocumenVSB FJC Description: Print Date 07/09/2016 13:59 Page: 14 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/DyslDte Next Due Last Compliance Information E/C: 1999-21-15 Category: AD Status: N/A Rev: 1 TO DETECT 8 CORRECT CHAFING & PREVENT ELECTRICAL Reason Freq: I AD AFFECT MODEL 737-100, -200. - 300, -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST E/C: 1999-22-16 Category: AD Status: N/A Rev: 01 SB 737-52-1137 FLIGHT DECK DOOR • DECOMPRESSION PANEL Reason Freq: 1 AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-52-1137 EARLIEST EJC: 1999-23-20 Category: AD Status: N/A Rev: 1 TO PREVENT A SHORT CIRCUIT Reason Frog: t AD AFFECT MODEL 737-100, -200, - 300, -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST PC: 1999-23-22 Category: AD Status: N/A Rev: 2 PREVENTION OF FALSE ADVISORIES DUE TO INACCURATE AIRPLANE ALTITUDE REPOARTING EARLIEST Reason Freq: 1 THE AIRCRAFT IS NOT FITTED WITH ATC TRANSPONDERS P/N 522-2703-XXX SERIES. HENCE THE AD IS N/A BY INSTALLED P/N. EFTA_R1_00012774 EFTA01734506 NC: A6DFR EIC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DoeumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 15 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/DyslDte Next Due Last Compliance Information BC: 1999-24-06 Category: AD Status: N/A Rev: 1 INSPJREPL. OF BREATHER PLUG IN FUEL TANK BOOST PUMPS Reason Freq: I AD AFFECT MODEL 737-100, -200. - 300, -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 1999-24.08 Category: AD Status: N/A Rev: 1 PREVENTION OF FAILURE OF ALL ELECTRICALLY POWERD AIRPLANE SYSTEMS Reason Freq: 1 AD AFFECT MODEL 737-100. -200. - 300. -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 1999-25-02 Category: AD Status: N/A Rev: 1 TO PREVENT THE LINKAGE BETWEEN THE RATIO CHANGER I Reason Frog: 1 AD AFFECT MODEL 737-100, -200. - 300, -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 1999-26-07 Category: AD Status: N/A Rev: 1 TO PREVENT FAILURE OF THE SECONDARY SUPPORT TO SU Reason Freq: I AD AFFECT MODEL 737-100, -200, AND -200C SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EFTA_R1_00012775 EFTA01734507 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SS EJC Description: Print Date 07/09/2016 13:59 Page: 16 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/DysIDte Next Due Last Compliance Information BC: 1999-26-10 Cate gory: AD Status: N/A Rev: 1 PREVENTION OF WATER ACCUMLATION IN THE LOWER CORNERS OF THE FLIGHT DECK EMERGNCY EXITS. Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 1999-26-10 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST BC: 1999-26-21 Category: AD Status: N/A Rev: 02 SB737.29A1077 INSP/REPL OF WIRE BUNDLES AND HYDRULIC HOSES Reason Freq: i AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-29A1077 EARLIEST E/C: 2000-02-03 Category: AD Status: N/A Rev: 1 TO PREVENT FATIGUE CRACKING OF THE ROD ENDS ON THE Reason Frog: 1 AD AFFECT MODEL 737-300, -400. -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST BC: 2000-02-18 Category: AD Status: N/A Rev: 1 TO PREVENT A REDUCED RATE OF MOVEMENT OF THE ELEV Reason Frog: I AD AFFECT MODEL 737-100, -200. - 300, -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EFTA_R1_00012776 EFTA01734508 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 DoeumenVSB FJC Description: Print Date 07/09/2016 13:59 Page: 17 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/DysIDte Next Due Last Compliance Information E/C: 2000-03-05 Category: AD Status: N/A Rev: 1 REPLACEMENT OF THE EMERGENCY FLOOR PATH LIGHTING SYSTEM Reason Freq: I AD AFFECT MODEL 737-200 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 2000-04-02 Category: AD Status: N/A Rev: 1 TO PREVENT FUEL SUCTION FEED OPERATION ON BOTH ENGI Reason Freq: 1 AD AFFECT MODEL 737-100. -200. - 300. -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST E/C: 2000-04-08 Category: AD Status: N/A Rev: 1 TO DETECT & CORRECT CRACKING IN CERTAIN FUSELAGE F Reason Frew 1 AD AFFECT MODEL 737-200C SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 2000-05-13 Category: AD Status: N/A Rev: 1 TO PREVENT FRACTURE OF THE MLG AXLE 8 THE SEPARAT Reason Frog: I AD AFFECT MODEL 737-100, -200, -200C. - 300, -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EFTA_R1_00012777 EFTA01734509 NC: A60FR E/C (Category: AD) Anent NO A/C Actual Compliance Last Type/Series: 8737-700/3Bit NC SIN: 30884 Document/SB BC Description: Print Date 07/09:2016 13.59 Page: 18 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information EIC: 2000-05-29 Category: AD TO DETECT FATIGUE CRACKING OF THE FORWARD PRESSUR Status: N/A Rev: 1 EARLIEST Reason Free: I AD AFFECT MODEL 737-100. -200. •2000. • 300. -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT E/C: 2000-06-13 TO PREVENT FATIGUE CRACKING OF THE CORNERS OF THE Category: AD Status: N/A Rev: 1 EARLIEST Reason Free: I AD AFFECT MODEL 737.100. -200. •2000. • 300, AND -400 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT E/C. 2000-07-06 TO PREVENT FATIGUE CRACKING OF THE LOWER CORNERS O Category: AO Status: N/A Rev: I EARLIEST Reason Fres: 1 AD AFFECT MODEL 737-100. -200. -200C. - 300, -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EFTA_R1_00012778 EFTA01734510 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SS EJC Description: Print Date 07/09/2016 13:59 Page: 19 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information BC: 2000-07-09 Category: AD Status: N/A Rev: 01 M-7200-00-00931 SWCB73-27-001 ELEVATOR PCU INSPECTION Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD LINE NUMBER EFFECTIVITY LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST E/C: 2000-07-27 Category: AD Status: N/A Rev: 1 HG2030AD-34-A0009 HG2050AC-34-A0008 ADIRU MOD STATUS CONFIRMATION Reason Freq: i THE AIRCRAFT IS NOT FITTED WITH AFFECTED HONEYWELL ADIRU P/N AND SIN. AD IS N/A BY INSTALLED P/N AND SM. EARLIEST E/C: 2000-080 (8) Category: AD Status: CANCEL Rev: 2 MODE NC AND S TRANSPONDER Superseded By: 2008-0285 Freq: 1 EARLIEST E/C: 2000-08-08 Category: AD Status: N/A Rev: 01 M-7200-00-01063 SB 737-57-1253 REAR SPAR INSPECTION AND MODIFICATION Reason Freq: 1 THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 2000-08-08 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST EFTA_R1_00012779 EFTA01734511 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 DoeumenVSB EJC Description: Print Date 07/09/2016 13:59 Page: 20 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/0812016 Schedule Remaining/ HrfaCysalysiDte Next Due Last Compliance Information BC: 2000-08-17 Category: AD Status: N/A Rev: 1 TO PREVENT DAMAGE TO THE TAXI FIGHT ASSEMBLY Reason Freq: I AD AFFECT MODEL 737-100, -200. - 300, -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EIC: 2000-10-21 Category: AD Status: N/A Rev: 1 M-720040-01370 FLIGHT CREW SEATS Reason Freq: 1 AD AFFECT MODEL 737-300. -400. -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST E/C: 2000-13-51 Category: AD Status: N/A Rev: 1 MAIN DECK CARGO DOOR FRAMES Reason Free: 1 AD AFFECT MODEL 737-200, - 300 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST BC: 2000-14-02 Category: AD Status: N/A Rev: 01 M-7200-00-01744 SB 737-23A1170 PLACARD INSTALLATION PREVENT LOSS OF VHF COMM. Reason Free: 1 AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-23A1170 EARLIEST EFTA_R1_00012780 EFTA01734512 NC: A60FR E/C (Category: AD) Anent NO A/C Actual Compliance Last Type/Series: 8737-700438,H NC S/N: 30884 Document/SB E/C Description: Print Date 07/09:2016 13.59 Page: 21 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information EX: 2000-14-13 Category: AD Status: N/A Rev: 1 DOOR HANDLE Reason Freq: I AD AFFECT MODEL 737-200, - 300. -400. AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EX: 2000-15-12 Category: AD Status: N/A Rev: 1 737-55A1071 HORZ STAB FRONT SPAR INSP. Reason Frog: 1 AD AFFECT MODEL 737-100. -200 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST E/C: 2000-15-16 Category: AO Status: N/A Rev: 1 737.35.1049 PAX OXY MASK Reason Freq: 1 AD IS N/A BY THE EFFECTMTY LIST OF BOEING SB 737-35-1049 EARLIEST E/C: 2000-15.18 Category: AD Status: N/A Rev: 1 KRUGER FLAP INSPECTION Reason Freq: .1 AD AFFECT MODEL 737-100. -200 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EFTA_R1_00012781 EFTA01734513 NC: A60FR E/C (Category: AD) Anent NO A/C Actual Compliance Last Type/Series: 8737-700/SEW NC S/N: 30884 Document/SS E/C Description: Print Date 07/09:2016 13.59 Page: 22 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information EX: 2000-19-05 Category: AD Status: N/A Rev: 1 ELEVATOR TAB PUSH ROD Reason Freq: 1 AD AFFECT MODEL 737-100, -200. -200C, • 300, -400, AND -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST EX: 2000-22.02 Category: AD Status: TERMINATED Rev: 2 2000-22-02 R1 SWCB73-00-001 UNCOMMANDED RUDDER NON-NORMAL PROCEDURE Fin: 1 EARLIEST Manual Compliance 23/10/2010 Rev: 2 NC Total Hours: 2223:50 NC Total Cycles: 998 PF REMARK: THE INTENT OF THIS AD HAS BEEN INCORPORATED INTO AFM. REFER TO LHT AD STATUS. EJC: 2000-23-34 Category: AD Status: N/A Rev: 1 PREVENT SEVERE ASSYMETFtIC THRUST CONDITION DURING FLIGHT Reason Free: 1 AD AFFECT MODEL 737-300, -400. -500 SERIES AIRPLANES. THE AD IS N/A FOR 737-700 AIRCRAFT EARLIEST E/C: 2000-25-07 Category: AD Status: N/A Rev: 1 OUTBOARD FLAP, INBOARD FLAP TRACK INSPECTION Reason From: 1 AD AFFECT MODEL 737-100, -200, -200C SERIES AIRPLANES. THE AD IS N/A FOR 737.700 AIRCRAFT EARLIEST EFTA_R1_00012782 EFTA01734514 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700/BBJ1 EIC (Category: AD) Arrant NO Document/SB NC S/N: 30884 FJC Description: Print Date 07/09/2016 13:59 Page: 23 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/CyslDyslDte Next Due Last Compliance Information E/C: 2001-01-13 Category: AD Status: N/A Rev: 1 TO DETECT 8 CORRECT CHAFING & TO PREVENT ELECTRICL Reason Freq: I NOT AFFECTED TO NC MODEL B737-600...-900 EARLIEST E/C: 2001-02-01 Category: AD Status: N/A Rev: 1 FWD PRESSURE BLKHEAD INSP Reason Froq: 1 AD AFFECT MODEL 737-100, -200, -200C. - 300. -400, AND .500 SERIES AIRPLANES. THE AD IS N/A FOR 737.700 AIRCRAFT EARLIEST E/C: 2001.023(AB) Category: AD Status: TERMINATED Rev: 2 CN 2001-023(AB) CN2001-023(AB) FM IMMUNITY Reason Frog: 1 VOR (P/N 822-0297-001) AND ILS (P/N 822-1152-002) INSTALLED ON THIS AIRCRAFT ARE FULLY COMPLIANT WITH FM IMMUNITY. EARLIEST Manual Compliance 12/01/2001 Rev: 2 NC Total Hours: 1103:35 NC Total Cycles: 595 ALL RJ EQUIPMENT COMPLIES WITH THE FM IMMUNITY REQUIREMENTS. E/C: 2001.04.08 Category: AD Status: CANCEL Rev: 01 EC 83-55A1072 SB737-55A1072 SWC 87355001 INSPECTION OF ELEVATOR TAB HINGE & ELEVATOR TAB CONTROL MECHANISM Superseded By: 2001-08-09 Frog: i EARLIEST EFTA_R1_00012783 EFTA01734515 NC Actual Compliance Last NC: A6DFR Type/Series: 8737.700IBBJ1 NC SIN: 30884 EIC (Category: AD) Anent NO Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 24 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys!Dte Next Due Last Compliance Information BC: 2001-06-08 Category: AD Status: N/A Rev: 01 SB 737-55-1067 INPEC OF ELEVATOR HINGE PLATE Superseded By: 2001.23.01 Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 2001-06-08 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST E/C: 2001-06-15 Category: AD Status: N/A Rev: 1 737-55A1064 INSP OF FASTENERS IN THE ELEVATOR BALANCE PANEL ASSEMBLIES. Reason Freq: AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-55A1064 EARLIEST E/C: 2001.08.07 Category: AD Status: N/A Rev: 1 TO DET & CORRCT CRACKING OF UPORTION M/DECK CGO Reason Frog: 1 SUPERSEDE BY AD 2004-03-23 EARLIEST EIC: 2001.08.09 39-12186 Category: AD Status: TERMINATED Rev: 2 BO NO: B3.55A1072 SB 737-55A1072 SWC 87355001 INSPECTION OF ELEVATOR TAB HINGE & ELEVATOR TAB CONTROL MECHANISM Frog: I EARLIEST Manual Compliance 01/12/2002 Rev: 2 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED WITH AMOC SB 737.55A1080 BY BACR668L (AD 2003-03-22) REFER TO LMT AD STATUS AT DELIVERY EFTA_R1_00012784 EFTA01734516 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Salves: B737.700/BBJ1 NC SIN: 30884 Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 25 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2001-08-24 Category: AD Status: TERMINATED Rev: 1 SWCB73-28-002 REVISE FLIGHT MANUAL TO PROHIBIT EXTENDED DRY OPERATION OF Center Tank Fuel Pumps Freq: I EARLIEST Manual Compliance 19/11/2002 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED BY BOEING REPAIR STATION BACR668L, REFER TO LHT AD STATUS AT DELIVERY E/C: 2001-09-15 Category: AD Status: N/A Rev: 1 TO PREVENT INFLIGHT SEPERATION OF THE M/D CGO DOOR Reason Freq: 1 N/A - BY ACFT MODEL. APPLICABLE ON B737-200/-300. EARLIEST E/C: 2001.09.51 Category: AD Status: TERMINATED Rev: 01 SB 737-27A1245 ELEVATOR TAB CONTROL RODS Frog: 1 EARLIEST Manual Compliance 14/03/2002 Rev: 01 NC Total Hours: 1103:35 NC Total Cycles: 595 ACTION TAKEN DURING CABIN COMPLETION. ACCOMPLISHED ON 14 MAR. 2002. REFER LHT AD STATUS AT DELIVERY. EIC: 2001.10.14 Category: AD Status: N/A Rev: 2 B3-35-1077 M7200-00-02474 SWCB73-35-003 INSP OF CHEM OXYGEN GEN 8/OR PAX. ATTENDANT OR LAV SERVICE UNIT ASSEMBLIES Reason Freq: 1 NOT APPLICABLE ACC. BOEING REPAIRE STATION BACR668L LOG BOOK ENTRIES FOR NON APPLICABLE AD'S. REFER LHT DELIVERY EARLIEST EFTA_R1_00012785 EFTA01734517 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 EIC (Category: AD) Anent NO Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 26 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys!Dte Next Due Last Compliance Information E/C: 2001-11-07 Category: AD Status: N/A Rev: 01 B3-29A1081 SB737.29A1082 INSP REPLACEMENT OF MOTOR-OPERATED HYDRAULIC SHUTOFF VALVES Reason Freq: I AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-29A1082 EARLIEST E/C: 2001-11-11 Category: AD Status: N/A Rev: 1 737-25-1371 737-25-1407 PREVENTION OF UNRESTRAINED MOVEMENT OF PASSENGER Reason Froq: 1 AD IS NIA BY THE EFFECTIVITY LIST OF BOEING SB 737-25-1371 AND SB 737-25-1407 EARLIEST E/C: 2001.12.51 39-12294 Category: AD Status: N/A Rev: 2 REV TO AFM TO PROHIBIT AIRPLANE SPEEDS ABOVE 300K Reason Frog: AD 2001-12-51 AFFECT B737-800 AIRCRAFT ONLY. AD IS N/A TO ROYAL JET BBJS BY AIRCRAFT MODEL EARLIEST E/C: 2001-13-07 39-12287 Category: AD Status: N/A Rev: 01 SB737-28-1180 TEST ELECTRICAL CIRCUITS THAT CLOSE WITH SPAR SOV Reason Freq: 1 AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-28-1160 EARLIEST EFTA_R1_00012786 EFTA01734518 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SS FJC Description: Print Date 07/09/2016 13:59 Page: 27 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information BC: 2001-13-23 39-12305 Category: AD Status: N/A Rev: 01 M-7200-O1.01608 SB 737-53-1212 BOLT ATTACH AFT PRESS BULKHEAD Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 2001-13-23 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST E/C: 2001-14-05 Category: AD Status: TERMINATED Rev: 1 M-7200-01-00756 ELEVATOR TAB REPAIR LIMITS/PROCEDURE Freq: i EARLIEST Manual Compliance 01/12/2002 Rev: 1 NC Total Hours: 1103:35 A/C Total Cycles: 595 CO IE WITH AMOC SB & AD 2003M PL22D RE -03- . FER LHT AD STATUS AT 737-55A10 DELIVERY BC: 2001-14-06 Category: AO Status: N/A Rev: 1 TO DETECT & CORRECT DISCRP LOCATED IN WN/W Reason Freq: 1 SUPERSEDED NOT AFFECTED TO NC MODEL EARLIEST BC: 2001.14.10 Category: AD Status: N/A Rev: 1 REMOVE ELECTRICAL POWER FROM IFE SYS WHEN NECESS Reason Frog: I NOT AFFECTED TO NC MODEL B737-600...-900 EARLIEST EFTA_R1_00012787 EFTA01734519 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DocumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 28 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2001-14-12 Category: AD Status: N/A Rev: 1 M-7200-01-01648 ST09104AC-D STC ST09100AC-D STC ST09105AC-D STC ST09106AC-D PES MODIFICATION Reason Frog: 1 THIS AIRCRAFT IS NOT MODIFED BY BY THE STC LISTED IN THE AD. HENCE AD IS N/A BY THE EFFECTIVITY LIST. EARLIEST E/C: 2001-14-20 Category: AD Status: N/A Rev: 1 WINGS CENTER WING BOX FLOOR BEAM INSP & MOD REP Reason Freq: 1 NOT AFFECTED TO NC MODEL B737-600...-900 EARLIEST E/C: 2001.15.01 39-12335 Category: AD Status: N/A Rev: 2 737-25-1403 737-25-1404 ESCAPE SLIDE Reason Frog: i AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-25-1403 AND SB 737.25.1404 EARLIEST E/C: 2001-16-06 Category: AD Status: N/A Rev: 1 WINGS SPARS POSSIBLE CRACKING AND CORROSION EARLIEST Reason Freq: 1 NOT AFFECTED TO NC MODEL B737-600...-900 EFTA_R1_00012788 EFTA01734520 NC: A6DFR E/C (Category: AD) Anent NO NC Actual Compliance Last Type/Series: 6737-700/BBJ1 NC SIN: 30884 DocumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 29 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2001-16-11 Category: AD Status: N/A Rev: 1 OUTBOARD MIDFLAP ASYMMETRY PREVENSION Reason Freq: I NOT AFFECTED TO NC MODEL B737-600...-900 EARLIEST E/C: 2001-17-02 63-53-1233 KEEL BEAM SPLICES INSPECTION FOR B3-531000 CORROSION AND CRACKING Category: AD S6737-53-1233 Status: N/A Rev: 01 EARLIEST Reason Froq: 1 THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 2001.17-02 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. E/C: 2001.20.10 737-SL-24.1116 PREV CHAFING WIRE BUNDLE -4 X JUNG B3-24-1113 BOX-WHEEL WELL Category: AD Status: N/A Rev: 01 EARLIEST Reason Frog: 1 THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 2001.20.10 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EFTA_R1_00012789 EFTA01734521 NC: A6DFR EIC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DoeumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 30 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys!Dte Next Due Last Compliance Information BC: 2001-21-51 Category: AD Status: N/A Rev: 01 B3-53A1238 BS 1016 AFT PRESSURE BULKHEAD INSPECTION Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 2001-21-51 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST E/C: 2001-22-11 Category: AD Status: N/A Rev: 1 737-24-1128 PDP INSPECTION/REPLACEMENT Reason Freq: 1 AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-24-1128 EARLIEST E/C: 2001.22.13 39-12492 Category: AD Status: N/A Rev: 4 747-27A2373 98-13-12R1 REPLACEMENT OF THE RUDDER PEDAL PUSHROD FASTENERS Reason Frog: 1 B737-700 AIRCRAFT ARE NOT AFFECTED BY AD 2001.22.13. AD IS N/A BY AIRCRAFT MODEL NUMBER. LATEST EFTA_R1_00012790 EFTA01734522 NC: A6DFR EIC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Doeument/SB FJC Description: Print Date 07/09/2016 13:59 Page: 31 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information BC: 2001-23-01 Category: AD Status: N/A Rev: 1 737-55-1067 INSPECTION/REPAIR OF ELEVATOR HINGE PLATES Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 2001-23-01 LINE NUMBER LIST. AD IS N/A BY AIRCRAFT LINE NUMBER. EARLIEST E/C: 2001-24-33 Category: AD Status: N/A Rev: 1 ELECT/AUX PWR GENERATOR FEEDER WIRE BUNDLE INSP Reason Freq: 1 NOT AFFECTED TO NC MODEL B737-600 -900 EARLIEST E/C: 2002-01.01 Category: AD Status: N/A Rev: 1 ELEV TAB ASSY INSP OF ELEV TAB HINGE 8 CONTRL MECH Reason Frog: 1 SUPERSEDED NC MODEL NOT AFFECTED EARLIEST EIC: 2002.02.08 Category: AD Status: N/A Rev: 1 WING MLG SUPPT BEAM RETAINING PIN BOLT REPLACEMNT Reason Frog: I NOT AFFECTED TO NC MODEL B737-600 -900 EARLIEST EFTA_R1_00012791 EFTA01734523 NC: A6DFR E/C (Category: AD) Arrant NO NC Actual Compliance Last Type/Salves: B737.700IBBJ1 NC SIN: 30884 DocumanVSB EJC Description: Print Date 07/09/2016 13:59 Page: 32 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Nrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2002-04-08 39-12665 Category: AD Status: N/A Rev: 2 B25A1383 SB 737-25A1383 INSPECTION/REPLACEMENT OF FASTENERS IN RUDDER PEDAL HOUSINGS Reason Freq: I NOT APPLICABLE PER LINE NUMBER. (1-295 ONLY) REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. LATEST E/C: 2002-05-07 Category: AD Status: N/A Rev: 1 OUTBOARD FLAP INSPECTION Reason Frog: 1 NOT AFFECTED TO NC MODEL B737-600 -900 EARLIEST EJC: 2002.06.03 39-12679 Category: AD Status: N/A Rev: 01 SB737-27A1234 MEASUREMENT OF CLEARANCE BETWEEN BRACKET FOR ELEVATOR PCU AND QUADRANT OF PCU Reason Frog: 1 NOT APPLICABLE PER LINE NUMBER REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. LATEST E/C: 2002-06-05 Category: AD Status: N/A Rev: 2 ATC TRANSPONDERS P/N 522-2703-XXX EARLIEST Reason Freq: 1 NOT APPLICABLE, AFFECTED P/N NOT INSTALLED. REFER TO LHT AD STATUS AT DELIVERY EFTA_R1_00012792 EFTA01734524 NC: A6DFR EX (Category: AD) Ament NO A/C Actual Compliance Last Type/Series: 8737.700/SEW NC S/N: 30884 Document/SB E/C Description: Print Date 07/09:2016 13.59 Page: 33 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information EC: 2002-07-08 Category: AD Status: N/A Rev: 1 FUSELAGE LAP JOINT CRACKING Reason Freq: 1 NOT AFFECTED TO A/C MODEL 8737-600 -900 EARLIEST E/C: 2002-07-10 Category: AD Status: N/A Rev: 1 FUSELAGE LAP JOINT PREMATURE CRACKING Reason From 1 NOT AFFECTED TO NC MODEL 8737.600_. 900 EARLIEST E/C: 2002-07-11 Category: AD Status: N/A Rev: 1 FUSELAGE LAP JOINT CRACKING Reason Freq: I NOT AFFECTED TO NC MODEL 8737.600_..-900 EARLIEST E/C: 2002.08.20 Category: AD Status: TERMINATED Rev: 1 B3-20020820 ELEVATOR TAB CLEANING Frog: 1 EARLIEST Manual Compliance 01/12/2002 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED BY BOEING REPAIR STATION BACR668L BY AMOV SB 737-55A1080 E AD 2003-03-22. REFER LHT REPORT AT DELIVERY. EFTA_R1_00012793 EFTA01734525 NC Actual Compliance Last NC: A6DFR Type/Series: 6737-700/BBJ1 E/C (Category: AD) Arrant NO Document/SB NC SIN: 30884 E/C Description: Print Date 07/09/2016 13:59 Page: 34 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/CyslDyslDte Next Due Last Compliance Information E/C: 2002-08-52 Category: AD Status: TERMINATED Rev: 1 FIT MANUAL REV TO PROHIBIT OPERATING SPEEDS Freq: I EARLIEST Manual Compliance 01/12/2002 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED BY BOEING REPAIR STATION BACR668L AMOC SB 737.55M080. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. E/C: 2002-10-11 Category: AD Status: N/A Rev: 1 FUELAGE AFT PRESS BLKHEAD INSP. MOD 8 REP BS 1016 Reason Frog: 1 NOT AFFECTED TO NC MODEL B737-600....-900 EARLIEST SC: 2002.10.12 Category: AD Status: N/A Rev: 1 AILERON TAB CNTRL ROD BARREL INSP OR REPLACEMENT Reason Frog: 1 NOT AFFECTED TO NC MODEL 6737.600....-900 EARLIEST BC: 2002-14-19 Category: AD Status: N/A Rev: 2 ROCKWELL COLLINS ADC Reason Freq: 1 THE AIRCRAFT IS NOT FITTED WITH ROCKWELL COLLINS ADC COMPUTER AFFECTED BY THE AD. AD IS N/A BY INSTALLED P/N. EARLIEST EFTA_R1_00012794 EFTA01734526 NC Actual Compliance Last NC: A6DFR Type/Series: 6737-700/BBJ1 E/C (Category: AD) Arrant NO Document/SB NC S/N: 30884 FJC Description: Print Date 07/0912016 13:59 Page: 35 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2002-14-20 Category: AD Status: TERMINATED Rev: 1 B3-24A1150 PITOT PROBES - PREVENT ICING CONDITION Manual Compliance 16/04/2002 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 ACCOMPLISHED UAW SB 737-24A1150 OM 16/04/2002. REFER LHT AD REPORT AT DELIVERY TO AMIRI FLIGHT. EARLIEST Freq: I E1C: 2002-14-21 SB 737-73A1011 QUICK DISCONNECT COUPLING ON THE ENGINE FUEL HOSE Category: AD Status: N/A Rev: 1 EARLIEST Reason Freq: 1 NOT AFFECTED TO LINE NO. E/C: 2002-16-03 737-24A1148 CORROSION PROT OF W/WELL 39-12842 B3-24A1148 CONNECTORS. Category: AD SB 737-24A1148 Status: CANCEL Rev: 03 Superseded By: 2005-18-23 EARLIEST Freq: 1 E/C: 2002-16-23 Category: AD Status: N/A Rev: 1 RUDDRE FEEL 8 CTR UNIT Reason Freq: I THE AIRCRAFT LINE NUMBER IS NOT INCLUDED IN THE AD 2002-16-23 LINE NUMBER LIST. AD IS N/A BY AIRCRAF LINE NUMBER. EARLIEST EFTA_R1_00012795 EFTA01734527 NC Actual Compliance Last NC: A6DFR Type/Series: B737-700IBBJ1 EIC (Category: AD) Amant NO Document/SB NC SIN: 30884 FJC Description: Print Date 07/09/2016 13:59 Page: 36 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2002-18-02 Category: AD Status: N/A Rev: 1 LATERAL TRFER MECH LWR BEARING SUPPORT INSP/MOD Reason Freq: I NOT AFFECTED TO NC MODEL 8737-600....-900 EARLIEST E/C: 2002-18-52 2002-19-52 CENTER WING TANK FUEL PUMP - 2002-24-51 EMERGENCY AIRWORTHINESS DIRECTIVE Category: AD 737-28A1197 Status: CANCEL 747-28A2248 Rev: 1 Superseded By: 2002-19-52 EARLIEST Reason Frog: I SUPERSEDED BY FAA AD 2002-19-52 E/C: 2002.19.51 2002-19-51R1 FLIGHT CONTROL MODULE RETURN M-7200-02-01435 PASSAGE BLOCKAGE Category: AD Status: N/A Rev: 01 LATEST Reason Frog: I NOT AFFECTED BY SERIAL NUMBERS OF FLIGHT CONTROL MODULE. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. EIC: 2002-19-52 2002-18-52 OPERATING RESTRICTIONS FOR Manual Compliance 12/03/2003 Rev: 3 39-12900 2002-24-51 MAINTAINING MINIMUM FUEL LEVELS. AIRPLANE FLT MAN REVN & PLACARD NC Total Hours: 1103:35 NC Total Cycles: 595 CIW PARAGRAPH (G) ONLY BY X-RAYING PUMPS Category: AD 737-28A1197 INSTL PER SB 737-28A1197 & CRAINE-HYDRO AIRE SB Status: TERMINATED 747-28-2269 28-01. REFER LHT AD STATUS ST DELIVERY TO Rev: 3 747-28A2248 AMIRI FLIGHT. B3-20021952 LATEST EO 136291 Frog: 1 EFTA_R1_00012796 EFTA01734528 NC: A6DFR E/C (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 37 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/0812016 Schedule Remaining/ Hrs/Cys/DysIDte Next Due Last Compliance Information SC: 2002-20-07 39-12903 Category: AD Status: CANCEL Rev: 01 2007-03-07 737.27.1247RI 737-27-1253 INSTALLATION OF AN ENHANCED RUDDER CONTROL SYSTEM Reason Freq: I SUPERSEDED BY AD 2002-20-07 LATEST E/C: 2002-21-01 Category: AD Status: N/A Rev: 2 REPL WIRING ON BRITAX SELL WATER BOILERS BEV MKRS Reason Freq: 1 AD IS N/A BY THE EFFECTIVITY LIST OF AD 2002-21-01 EARLIEST E/C: 2002.22.05 Category: AD Status: N/A Rev: 1 CARRIAGE SPINDLE INSPECTION Reason Freq: 1 SUPERSEDED BY AD 2003-24-08 EARLIEST E/C: 2002.24.51 39-12992 Category: AD Status: TERMINATED Rev: 1 AD 2002-24-51 OPERATIONAL RESTRICTIONS FOR AIRPLANES WITH CRANE HYDRO-AIRE FUEL PUMPS Frog: 1 EARLIEST Manual Compliance 26/11(2002 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED WITH AD INSERTED INTO AFM BY BOEING REPAIR STATION BACR688L PER EMERGENCY AD 2002-24-51. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. EFTA_R1_00012797 EFTA01734529 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.7001BBJ1 NC SIN: 30884 Document/SS EJC Description: Print Date 07/09/2016 13:59 Page: 38 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys!Dte Next Due Last Compliance Information SC: 2002-26-18 39-13006 Category: AD Status: TERMINATED Rev: 2 737-28A1142R3 B3-28A1142 PREVENT FLUID CONTAMINATION OF FUELING FLOAT SWITCH AND CONDUIT ASSYS. Freq: I EARLIEST Manual Compliance 06/05/2003 Rev: 2 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED BY BOEING REPAIR STATION BACR668L ACCOMPLISHED SB 737-28A1142. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. ESC: 2003-03-01 Category: AD Status: TERMINATED Rev: 2 2011.18.10 737-71A1462 AFT ENGINE MOUNT. CENTER LINK ASSY INSTALLATION INSPECTION Superseded By: 2011-18-10 Freq: 1 EARLIEST Manual Compliance 09/05/2003 Rev: 2 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED BY BOEING REPAIR STATION BACR668L RECORDS WERE REVIEWED NO ENGINE CHANGE OCCURED. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. ESC: 2003-03-05 Category: AD Status: N/A Rev: 1 WINGS LE SLATS ACTUATOR REPLACEMENT Reason Freq: 1 N/A - BY ACFT MODEL. APPLICABLE ON B737-300 TO -500. LATEST E1C: 2003-03-11 Category: AD Status: WA Rev: 1 SLIDE RAFT SYSTEM - NOT APPLICABLE TO AF Superseded By: 2004-03-01 Reason Freq: 1 AD NOT APPLICABLE AS AFFECTED SLIDE RAFT SYSTEM NOT INSTALLED. EARLIEST EFTA_R1_00012798 EFTA01734530 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DocumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 39 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hre/Cys/Dys/Dte Next Due Last Compliance Information BC: 2003-03-22 Category: AD Status: TERMINATED Rev: 1 B3-11A1109 SB 737-11A1109 SPEEDBRAKE FLIGHT DETENT-SPEED LIMITATION Freq: I EARLIEST Manual Compliance 01/12/2002 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED BY BOEING REPAIR STATION BACR668L SB 737-55A1080. REFER LHT AD STSTUS AT DELIVERY TO AMIRI FLIGHT. SC: 2003-07-12 Category: AD Status: N/A Rev: 1 LANDING GEAR LIFE LIMITED PARTS Reason Freq: 1 NOT AFFECTED TO NC MODEL B737-600....-900 EARLIEST E/C: 2003-08-15 Category: AD Status: N/A Rev: 1 FUSELAGE SKIN INSPECTION OF CROWN SKIN LAP JOINT Reason Freq: 1 NOT AFFECTED TO NC MODEL B737.600....-900 EARLIEST BC: 2003-11-03 Category: AD Status: N/A Rev: 1 HYD ACCUMULATORS INSP TO DETERMINE THE P/N Reason Freq: 1 N/A - BY ACFT MODEL. APPLICABLE TO 8737-100/-200. LATEST EFTA_R1_00012799 EFTA01734531 NC: A6DFR E/C (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 DoeumenVS8 FJC Description: Print Date 07/09/2016 13:59 Page: 40 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys!Dte Next Due Last Compliance Information EC: 2003-14-04 Category: AD Status: N/A Rev: 1 MODIFICATION OF THE REINFORCED FLIGHT DECK DOOR Superseded By: 2005-12-05 MOD Reason Freq: i SUPERSEDED BY AD 2005-12-05 EARLIEST E/C: 2003-14-06 INSP FOR CRACKING OF LAP SPLICES 8 CORRECTIVE Category: AD Status: N/A Rev: 1 EARLIEST Reason Freq: 1 NOT AFFECTED TO NC MODEL B737-600....-900 E/C: 2003-14-08 2006-13-13 AIRPLANE FLIGHT MANUAL - CABIN Manual Compliance 05/08/2003 Rev: 1 2008-23-07 ALTITUDE WARNING - DONNING OF NC Total Hours: 1103:35 NC Total Cycles: 595 OXYGEN MASKS COMPLIED WITH BOEING FLIGHT TEST BY Category: AD SWCB73-00-003 INSERTING AD IN THE AFM. REFER LHT AD STSTUS Status: TERMINATED SWCB76-00-001 AT DELIVERY TO AMIRI FLIGHT. Rev: 1 EARLIEST Frog: 1 EJC: 2003-20-13 B3-30-1054 WINDSHIELD WIPER MOTOR - WIRING Manual Compliance 22/10/2003 Rev: 2 SB 737-30-1054 CHANGE 8 CONVERTER REPLACEMENT NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED WITH SB 737-30-1054. REFER LHT AD Category: AD SB 737-30A1049 STATUS AT DELIVERY TO AMIRI FLIGHT. Status: TERMINATED Rev: 2 EARLIEST Freq: 1 EFTA_R1_00012800 EFTA01734532 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SB FJC Description: Print Date 07/09/2016 13:59 Page: 41 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2003-23-05 Category: AD Status: TERMINATED Rev: 1 B3-26A1109 EO F26-A0121 SB737.26A1109 ENGINES. APU & CARGO FIRE BOTTLE HOSES INSP Freq: i EARLIEST Manual Compliance 17/12/2003 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED WITH SB 26A1109R2. EFER REPORT AT DELIVERY TO AMIRI FRLIGHT. LHT AD EIC: 2003-26-12 Category: AD Status: N/A Rev: 1 737-23A1169 VIDEO DISTRIBUTION UNITS (VDU) CONNECTOR REPLACEMENT Reason Freq: 1 AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-23A1169 REVISION 02 EARLIEST E/C: 2003-26-14 Category: AD Status: TERMINATED Rev: 03 737-SL-26-043 RECALL OF KIDDE AEROSPACE PORTABLE HALON 1211 FIRE EXTINGUISHERS P/N 898052 Frog: 1 EARLIEST Manual Compliance 14/01/2004 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED BY BY REPLACED ALL 3 KIDDE HANDHELD HALON FIRE EXTING. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. EIC: 2004-03-01 Category: AD Status: N/A Rev: 1 AD 2004-03-01 AIR CRUISER SL/RAFTS - N/A TO AF Reason Freq: 1 THIS AIRCRAFT IS NOT FITTED WITH AIR CRUISER SLIDE/RAFTS. HENCE THE AD IS N/A BY INSTALLED SLIDE/RAFTS P/N. EARLIEST EFTA_R1_00012801 EFTA01734533 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700/BBJ1 EIC (Category: AD) Arrant NO Document/SS NC SIN: 30884 E/C Description: Print Date 07/0912016 13:59 Page: 42 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2004-05-19 39-13514 Category: AD Status: TERMINATED Rev: 4 737-55-1086 HORIZ STAB FRONT & REAR SPAR BOLT/PIN INSP Reason Free: I MOD ACCOMPLISHED 8-SEP-2008 AT KLM WITH WO #12142. EARLIEST E/C: 2004-05-19 DFR 737-55-1074 HORIZIZONTAL STABILIZER FRONT & REAR WO 12142 08/09/2008 Rev: 1 39-13514 737-55-1086 SPAR BOLT/PIN INSPECTION NC Total Hours: 1469:35 NC Total Cycles: 767 Category: AD 737-55-1086 OFR Status: TERMINATED Rev: 1 EARLIEST Frog: 1 E/C: 2004.07.10 SB737-32A1343 PSEU REPLACEMENT Manual Compliance 19/01/2005 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 COMPLIED lAW ED 142883 MOD. REFER LHT AD Category: AD STATUS AT DELIVERY TO AMIRI FLIGHT. Status: TERMINATED Rev: 1 EARLIEST Frog: 1 E/C: 2004.10.10 VSB1152426-49-08 SCU REPLACEMENT - TO AVOID Manual Compliance 06/11/2015 Rev: a 39-13640 CONNECTOR OVERHEATING NC Total Hours: 5817:55 NC Total Cycles: 2086 Category: AD REF EC ET49-1: DFR IS FITTED WITH 1152426-245, SERIES 7. Status: TERMINATED Rev: 4 EARLIEST Reason Frog: 1 REF EC ET49-1: DFR IS FITTED WITH 1152426-245, SERIES 7 EFTA_R1_00012802 EFTA01734534 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SB EJC Description: Print Date 07/09/2016 13:59 Page: 43 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2004-11-11 39-13657 Category: AD Status: TERMINATED Rev: 1 737-28A1148R1 73?-28A1148R2 AFT BOOST PUMP WIRING SUPPORT BRACKET INSTALLATION Freq: I EARLIEST Manual Compliance 12/11/2003 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 FIXED AS PER CAMP SYSTEM RECORDS ON 12.11.03. REFER LHT AD STATUS AT DELIVER TO AMIRI FLIGHT. E/C: 2004-18-02 39-13779 Category: AD Status: N/A Rev: 2 737-26A1118 HIGH ELECTRICAL RESISTANCE IN THE FIRE EXTENGUISHING SQUIB - GROUNDS INSPECTION/CHECK Reason Freq: 1 AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-26A1118 EARLIEST EIC: 2004.22.01 39-13829 Category: AD Status: N/A Rev: 1 1-46753136 CARGO RESTRAINT STRAP ASSEMBLIES Reason Frog: 1 THE AIRCRAFT IS NOT FITTED WITH CARGO RESTRAINT STRAP ASSEMBLIES P/N 1519-MCIDS. HENCE THE AD IS NIA BY INSTALLED P/N. EARLIEST BC: 2004.22.27 39-13855 Category: AD Status: TERMINATED Rev: 1 737.54.1039 737.54.103981 STRUT - APPLICATION OF SEALANT AT THE INTERFACE OF THE DIAGONAL BRACE FITTING AND THE AFT BULKHEAD Frog: I EARLIEST Manual Compliance 14/02/2003 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 NOT APPLICABLE ALRADY PERFORMED ACC. BACR668L. REFER LHT AD STATUS REPORT AT DELIVERY TO AMIRI FLIGHT. EFTA_R1_00012803 EFTA01734535 NC Actual Compliance Last NC: A6DFR Type/Series: 8737400/8B/1 E/C (Category: AD) Anent NO Document/SS NC S/N: 30884 FJC Description: Print Date 07/09/2016 13:59 Page: 44 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dysl0te Next Due Last Compliance Information E/C: 2004-23-10 39-13865 Category: AD Status: N/A Rev: 1 737-53-1256 INSPECTION FOR PITTING AND CRACKS OF THE LOWER SKIN PANEL Reason Freq: i AD IS N/A BY THE EFFECTIVITY LIST OF AD 2004-23-10 EARLIEST E/C: 2004-24-07 39-13883 Category: AD Status: TERMINATED Rev: 1 737-28-1190 737-28-1190R1 FOIS - CENTER FUEL TANK WIRE SUPPORT BRACKET REPLACEMENT Froq: 1 EARLIEST Manual Compliance 12/06/2003 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 AS PER CAMP REPORT SB 737-28-1190/01 FIXED. REFER LHT AD STATUS REPORT AT DELIVERY TO AMIRI FLIGHT. E/C: 2005-05-18 39-14007 Category: AD Status: OPEN Rev: 1 737-53-1251 INSPECTION OF THE WEBS OF THE AFT PRESSURE BULKHEAD FOR CRACKS 26000 Cys Recur EARLIEST 23797 02/11/2081 E/C: 2005-07-20 39-14045 Category: AD Status: CANCEL Rev: 0 AUTOFLIGHT - DIGITAL FLIGHT CONTROL SYSTEM - FLIGHT CONTROL COMPUTER OPERATIONAL PROGRAM SOFTWARE INSTALLATION - P2.0 Superseded By: 2012.21.08 Reason Frog: 1 NOT APPLICABLE AFFECTED P/NO NOT INSTALLED. EARLIEST EFTA_R1_00012804 EFTA01734536 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700/BBJ1 FJC (Category: AD) Ament NO DoeumenVSB NC SIN: 30884 FJC Description: Print Date 07/09/2016 13:59 Page: 45 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/CyslDyslDte Next Due Last Compliance Information SC: 2005-08-10 39-14062 Category: AD Status: N/A Rev: 0 737.54.1040R1 STRUT - APPLICATION OF SEALANT ON ENGINE STRUT STRUCTURE Reason Freq: I AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-54-1040 EARLIEST EIC: 2005-12-05 AMS 2003-14-04 REINFORCED FLIGHT DECK DOOR 39-14121 2005-12-05 CORRECTION Category: AD 2007-10-12 Status: CANCEL B221001-52-03 Rev: 2 B221200-52-01 ST01335LA Superseded By: 2007-10-12 EARLIEST Reason Froq: 1 SUPERSEDED BY AD 2007-10-12 E/C: 2005-12-05 MOD 2003-14-04 REINFORCED FLIGHT DECK DOOR 39-14121 2005-12-05 CORRECTION Category: AD 2007-10-12 Status: CANCEL B221001-52-03 Rev: 3 B221200-52-01 ST01335LA Superseded By: 2007-10-12 EARLIEST Reason Frog: 1 SUPERSEDED BY AD 2007-10-12 FJC: 2005-13-15 737-57-1250 CENTER WING BOX- INSP OF SECONDARY WO 12142 08/09/2008 Rev: 0 39-14152 FUEL VAPOR-BARRIER APPLICATION ON NC Total Hours: 1469:35 NC Total Cycles: 767 THE WING CNTR SECT TOP PANEL Terminating Action Has Been Performed Category: AD Status: TERMINATED Rev: 0 EARLIEST Frog: 1 EFTA_R1_00012805 EFTA01734537 NC: A6DFR E/C (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SS E/C Description: Print Date 07/09/2016 13:59 Page: 46 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2005-18-23 39-14264 Category: AD Status: OPEN Rev: 1 2002.16-03 737.24-01146 MLG ELECTRICAL CONNECTORS CORROSION PROTECTION Freq: I 730 Dys Recur EARLIEST 515 04/02/2018 WO 50505 05/0212016 Rev: 1 NC Total Hours: 5887:00 NC Total Cycles: 2120 E/C: 2005-19-19 39-14284 Category: AD Status: TERMINATED Rev: 0 737-34A1801 FMC: OPS CHANGE TO VERSION U10.5A Frog: 1 EARLIEST Manual Compliance 19/01/2005 Rev: 0 NC Total Hours: 1103:35 NC Total Cycles: 595 REQUIRED SB 737-34A1801 ALREADY PERFORMED IAW EO 144603. REFER LHT AD STATUS REPORT AT DELIVERY TO AMIRI FLIGHT. E/C: 2005-21-06 39-14344 Category: AD Status: OPEN Rev: 0 737-53A1248 BS 1016 AFT PRESS BLKHD WEB • INSP FOR CRACKS AT THE Y-CHORD Frog: 1 25000 Cys Recur EARLIEST 22797 06/02/2079 E/C: 2005-23-16 Category: AD Status: TERMINATED Rev: 0 737-28-1209 CWT: WIRE BUNDLE MODIFICATION Frog: 1 EARLIEST Manual Compliance 08/09/2008 Rev: 0 NC Total Hours: 1469:35 NC Total Cycles: 767 ACCOMPLISHMENT OF SB 737-28-1209, TERMINATES AD 2005-23-16 FOUND S8 DONE ON 08/09/08 WO 12142. EFTA_R1_00012806 EFTA01734538 NC Actual Compliance Last NC: A6DFR Type/Series: 6737-700/BBJ1 BC (Category: AD) Amant NO Document/SB NC SIN: 30884 E/C Description: Print Date 07/0912016 13:59 Page: 47 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2005-23-17 39-14375 Category: AD Status: TERMINATED Rev: 0 737-28-1200 P15 REFUEL PANEL WIRING INSPECTION/MODIFICATION Freq: I EARLIEST Manual Compliance 03/01/2006 Rev: 0 NC Total Hours: 1103:35 NC Total Cycles: 595 INSPECTION COMPLIED BY OPERATOR PER REF 01 OS SB AND AD COMPLIANCE TIME : 03-JAN-2006, 796FH, 465FC, REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. E/C: 2005-24-03 2005-24-03R1 NACELLE SUPPORT FITTING ATTACHMENT 25000 Hrs 18846:30 39-14955 737-57-1275 FASTENERS INSPECTION - MEASUREMENT 25000 Cys 22797 Category: AD Status: OPEN 26/06/2042 Rev: 1 Once EARLIEST Frog: 1 BC: 2005-25-03 2007-06-09 SECTION 41 CAB - POINT D SPLICE FITTING 39-14396 737-53A1222 REPLACEMENT Category: AD Status: CANCEL Rev: 1 Superseded By: 2007-06-09 EARLIEST Reason Frew 1 SUPERSEDED BY AD 2007-06-09 BC: 2005-26-03 39-14424 Category: AD Status: TERMINATED Rev: 0 737-27A1271 SWCB73-27-018 ELEVATOR INPUT TORQUE TUBE MODIFICATION Freq: EARLIEST Manual Compliance 03/08/2005 Rev: 0 NC Total Hours: 1103:35 NC Total Cycles: 595 MODIFIED IAW EO 146233. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. EFTA_R1_00012807 EFTA01734539 NC Actual Compliance Last NC: A6DFR Type/Series: B737.7001BBJ1 NC SIN: 30884 EIC (Category: AD) Arrant NO DocumenVSB EJC Description: Print Date 07/09/2016 13:59 Page: 48 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/CyslDyslDte Next Due Last Compliance Information E/C: 2006-0140-E Category: AD Status: TERMINATED Rev: 4 2006-0140R1 2006-0140R2 2006.0140R3 2006-0140R4 AIR CONDITIONING - ZONAL DRYING SYSTEM DEACTIVATION - EMERGENCY AIRWORTHINESS DIRECTIVE Freq: I EARLIEST WO 12893 09/10/2008 Rev: 1 NC Total Hours: 1490:00 NC Total Cycles: 771 ESC: 2006-0264 Category: AD Status: N/A Rev: 0 2001.11.11 747-25-3196 PASSENGER SEATS REAR FITTING ASSEMBLY ATTACHMENT REPLACEMENT Reason Freq: 1 THE AIRCRAFT IS NOT FITTED WITH AVIOINTERIORS PAX SEATS LISTED IN THE AD. HENCE THE AD IS N/A BY INSTALLED SEAT MODEL. EARLIEST EIC: 2006-0265 Category: AD Status: CANCEL Rev: 0 MODE S & C TRANSPONDERS • CHECK Superseded By: 2006-026SCN Freq: 1 EARLIEST SC: 2006-0265-CN Category: AD Status: CANCEL Rev: 0 NAVIGATION SYSTEMS - MODE S AND C TRANSPONDERS -CHECK Reason Freq: I EASA CANCEL AD 2006-0265 THROUGH AD CANCELATION NOTICE 2006-0265-CN. EARLIEST EFTA_R1_00012808 EFTA01734540 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 49 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information BC: 2006-0334 Category: AD Status: N/A Rev: 1 2006-0334 R01 THALES COMMUNICATION VHF DATA RADIO Reason Freq: 1 THE AIRCRAFT IS NOT FITTED WITH THALES VHF RADIOS. HENCE THE AD IS N/A BY INSTALLED VHF RADIOS P/N. EARLIEST E/C: 2006-04-04 SMOKE DETECTOR REPLACEMENT Category: AD Status: N/A Rev: 0 EARLIEST Reason Frog: 1 THIS AIRCRAFT IS NOT FITTED WITH MEGGITT 602 SMOKE DETECTOR. HENCE THE AD IS N/A BY INSTALLED SMOKE DETECTOR P/N. E/C: 2006-07-04 INSP 2006-07-04 FLUID ACCUMULATION IN ENGINE STRUT WO 19804 04/02/2014 Rev: 0 39-14531 2006-07-04 MOD AFT FAIRING - REPETITIVE INSPECTION NC Total Hours: 4841:40 NC Total Cycles: 1785 Category: AD 737-54-1041 Status: TERMINATED Rev: 0 EARLIEST Freq: 1 E/C: 2006-07-04 MOD 2006-07-04 FLUID ACCUMULATION IN ENGINE STRUT WO 16115 05/09/2011 Rev: 0 39-14531 200607.04 INSP AFT FAIRING - INSTALLATION OF NEW NC Total Hours: 2813:55 NC Total Cycles: 1178 ENGINE STRUT AFT FAIRING SEALS TERMINATING ACTION HAS BEEN PERFORMED Category: AD 737.54.1041 MODIFICATION PART OF SB 54-1041 PERFORMED Status: TERMINATED DURING C CHK AT TURKISH TCHNIC. REF WORK Rev: 0 ORDER 16115. EARLIEST Freq: 1 EFTA_R1_00012809 EFTA01734541 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 EIC (Category: AD) Anent NO Document/SB EJC Description: Print Date 07/09/2016 13:59 Page: 50 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/DysIDta Next Due Last Compliance Information BC: 2006-08-03 Category: AD Status: N/A Rev: 1 150-25-036 (SIGMA SB) 151-25-037 (SICMA SB) SICMAAEROSEAT CABIN ATTENDANT SEAT TYPE 150 & 151 Reason Freq: I THE AIRCRAFT IS NOT FITTED WITH SICMA FLIGHT ATTENDANT SEATS. HENCE THE AD IS NIA BY INSTALLED FLIGHT ATTENDANT SEAT EARLIEST E/C: 2006-10-17 39-14601 Category: AD Status: N/A Rev: 0 737-24A1141 P5 PANEL MODIFICATION Reason Freq: NOT APPLICABLE BY THE EFFECTIVITY LIST OF SB 737-24A1141 EARLIEST EIC: 2006-12-06 39-14631 Category: AD Status: N/A Rev: 0 737-25-1439 DRIESSEN GALLEYS: SPIRAL WRAP REPLACEMENT Reason Frog: 1 AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737.25.1439 EARLIEST E/C: 2006-12-11 Category: AD Status: TERMINATED Rev: 0 737-28-1199 ENGINE FUEL SHUTOFF VALVE WIRE & CONDUIT ASSY. REPLACEMENT Free: 1 EARLIEST Manual Compliance 03/08/2005 Rev: 0 NC Total Hours: 1103:35 NC Total Cycles: 595 SB 737-28-1199 REV. 00 FIXED 03.08.2005. THIS ACTION IS AN AMOC FOR AD 2006-12-11. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. EFTA_R1_00012810 EFTA01734542 NC: A6DFR E/C (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB FJC Description: Print Date 07/09/2016 13:59 Page: 51 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2006-13-13 39-14666 Category: AD Status: TERMINATED Rev: 1 2003-14-08 2008-23-07 AIRPLANE FLIGHT MANUAL AMENDMENT - CABIN PRESSURIZATION Freq: I EARLIEST Manual Compliance 31/07/2006 Rev: 1 NC Total Hours: 1103:35 NC Total Cycles: 595 AFM REVISION PFERFORM BY THE PREVIOUS CUSTOMER. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. E/C: 2006-15-18 Category: AD Status: TERMINATED Rev: 0 737-33-1133 M D & T WIRING SEPARATION Freq: 1 EARLIEST Manual Compliance 16/03/2003 Rev: 0 NC Total Hours: 1103:35 NC Total Cycles: 595 MODIFIED lAW SB 737-33-1133 BY BACR668L (BOEING) ACC. DELIVERY DOCUMENTS. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. E/C: 2006-16-11 39-14711 Category: AD Status: N/A Rev: 0 737-53-1236 AIRSTAIR DOORSTOP INTERCOSTAL - INSPECTION AND FASTENER REPLACEMENT Reason Freq: 1 NOT APPLICABLE ALREADY MODIFIED BY MANUFACTURE EARLIEST E/C: 2006-16-18 Category: AD Status: N/A Rev: 0 SANDEL AVIONICS INC. TAWS/RMI MODIFICATION Reason Freq: 1 THE AIRCRAFT IS NOT FITTED WITH SANDEL TWAS/RMI UNITS. HENCE THE AD IS N/A BY INSTALLED P/N LATEST EFTA_R1_00012811 EFTA01734543 NC: A6DFR E/C (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 52 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2006-17-13 Category: AD Status: N/A Rev: 2 3410-25MR477R3 RECARO MODEL 3410 SEATS : SEAT BELT ATTACHMENT BOLT REPLACEMENT Reason Freq: I THIS AIRCSRAFT IS NOT FITTED WITH RECARO MODEL 3410 PAX SEATS. HENCE THE AD IS N/A BY INSTALLED SEAT MODEL EARLIEST Sc: 2006-21-01 INSP 2006-21-01 LUBE AILERON BALANCE TAB FREEPLAY 8000 Hrs 7733:30 WO 50505 05/02/2016 Rev: 0 39-14784 Category: AD 737-27-1273 INSP 737-27-1273 LUBE INSPECTION 730 Dys 515 NC Total Hours: 5887:00 NC Total Cycles: 2120 Status: OPEN 04/02/2018 Rev: 0 Freq: 1 Recur EARLIEST E/C: 2006-21-01 LUBE 2006-2141 INSP AILERON BALANCE TAB HINGE BEARINGS 4000 Hrs 3632:35 WO 50175 22/08/2015 Rev: 0 39-14784 Category: AD 737-27-1273 INSP 737-27-1273 LUBE AND ROD END BEARINGS LUBRICATION 365 Dys -17 NC Total Hours: 5786:05 NC Total Cycles: 2071 Status: OPEN 21/08/2016 Rev: 0 Freq: 1 Recur EARLIEST E/C: 2006-26-01 39-14859 Category: AD Status: N/A Rev: 0 FUEL FILTER REPLACEMENT ( FOR PMA PARTS) Reason Freq: 1 FUEL FILTER PN WF337661, WF337017, 7595983.101, AND 7588133 NOT FITTED ON RJ ENGINES. HENCE AD IS N/A BY INSTALLED P/N. EARLIEST EFTA_R1_00012812 EFTA01734544 NC Actual Compliance Last NC: A6DFR Type/Series: 6737-700/BBJ1 EIC (Category: AD) Ament NO Document/SB NC S/N: 30884 FJC Description: Print Date 07/09/2016 13:59 Page: 53 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/CyslDyslDte Next Due Last Compliance Information E/C: 2007-02-14 39-14901 Category: AD 737-28-1225 INSPECTION / REPAIR OF ELECTRICAL BOND BETWEEN THE BULKHEAD FITTING FOR THE FUEL FEED LINE AND THE WING FRONT SPAR Manual Compliance 12/01/2007 Rev: 0 NC Total Hours: 1103:35 NC Total Cycles: 595 INSPECTED IAW EO 150722. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. Status: TERMINATED Rev: 0 EARLIEST Freq: I E/C: 2007-03-07 2002-20-07 RUDDER CONTROL SYSTEM - MAIN AND Manual Compliance 15/07/2007 Rev: 0 39-14918 737-27-1253 STANDBY RUDDER POWER CONTROL UNIT NC Total Hours: 1103:35 NC Total Cycles: 595 Category: AD 737-27A1280 FORCE FIGHT ACCOMPLISHED IAW E 152499. REFER LHT STATUS REPORT AT DELIVERY TO AMIRI FLIGHT AD. Status: TERMINATED 737-27A1280 STANDBY Rev: 0 SWCB73-27-021 EARLIEST Frog: 1 E/C: 2007-04-15 90-25-005 PASSENGER SEAT ASSEMBLY -AFT TRACK 39-14947 90-25-005 ISSUE 2 FITTING MODIFICATION Category: AD Status: N/A Rev: 0 EARLIEST Reason Frog: 1 THIS AIRCRAFT IS NOT FITTED WITH SICMA PAX SEATS. HENCE THE AD IS N/A BY INSTALLED SEAT MODEL E/C: 2007-06-09 2005-25-03 SECTION 41 CAB - POINT D SPLICE FITTING 737-53A1222 REPLACEMENT Category: AD Status: N/A Rev: 0 EARLIEST Reason Frog: 1 NOT APPLICABLE AD NOT AFFECTED TO THIS AIRCRAFT LINE NUMBER (SEE EFFECTIVITY PER SB 737-53A1222 REV 3) EFTA_R1_0001281 3 EFTA01734545 NC: A6DFR EIC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB SC Description: Print Date 07/09/2016 13:59 Page: 54 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2007-06-51 Category: AD Status: N/A Rev: 1 2007-06.52 EMERGENCY AIRWORTHINESS DIRECTIVE - FLIGHT SPOILER ACTUATOR JAM Superseded By: 2007-06-52 Reason Freq: i NOT APPLICALBE PER LISTED MSN IN SB 737-27A1283. EARLIEST E/C: 2007-06-52 Category: AD Status: N/A Rev: 1 2007-06-51 2007-15-04 EMERGENCY AIRWORTHINESS DIRECTIVE - FLIGHT SPOILER ACTUATOR JAM Superseded By: 2007-15-04 Reason Frog: 1 NOT APPLICALBE PER LISTED MSN IN SB 737-27A1283. EARLIEST E/C: 2007-07-02 39-15002 Category: AD Status: N/A Rev: 0 737-25-1545 PART 2 MODIFICATION OF THE OXYGEN ACTIVATION MECHANISM WITHIN THE PASSENGER SERVICE UNITS Reason Freq: i NOT APPLICABLE AFFECTED P/NO IS NOT FITTED EARLIEST E/C: 2007-10-12 Category: AD Status: N/A Rev: 1 2003-14-04 2005-12-05 AMS 2005-12-05 MOD INSPECTION OF DOOR WIRE HARNESSES ON AIRPLANES EQUIPPED WITH C 8 D ZODIAC RE-INFORCED FLIGHT DECK DOOR ASSEMBLY PN: B221001. Reason Frog: 1 NOT APPLICABLE AFFECTED P/NO IS NOT INSTALLED EARLIEST EFTA_R1_00012814 EFTA01734546 NC: A6DFR E/C (Category: AD) Ament NO A/C Actual Compliance Last Type/Series: B737-7001BBJ1 Document/SB NC SIN: 30884 E/C Description: Print Date 07i092016 13.59 Page: 55 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/CyslDyslDte Next Due Last Compliance Information E/C: 2007-15-04 2007-06.52 39-15133 Category: AD Status: N/A Rev: 0 FLIGHT SPOILER ACTUATOR EARLIEST Reason Freq: 1 THIS AD IS APPLICABLE TO 737-800 FLEET. HENCE THE AD IS N/A BY AIRCRAFT MODEL E/C: 2007-18-51 2007-18-52 EMERGENCY AIRWORTHINESS DIRECTIVE 737-SL-57-084 - INSPECTION OF SLAT TRACK DOWNSTOP ASSEMBLIES ON ALL LEADING EDGE Category: AD SLATS Status: CANCEL Rev: 2 Superseded By: 2007-18-52 EARLIEST E/C: 2007-18-52 1523812011.1 EMERGENCY AIRWORTHINESS DIRECTIVE Manual Compliance 01/09/2007 Rev: 0 1-527463441.1 - INSPECTION OF SLAT TRACK DOWNSTOP NC Total Hours: 1103:35 NC Total Cydes: 595 ASSEMBLIES ON ALL LEADING EDGE AD NOTE PERFORMED BY THE PREVIOUS OWNER Category: AD 2007-18-51 SLATS AT HAMBURG, ON 01/09/07. REFER ROYAL FLIGHT Status: CANCEL 2011-06-05 INSP TECH LOG 0411 Rev: 1 2011.06-05 MOD 737-SL-57-084 Superseded By: 2011.06-05 INSP EARLIEST Freq: 1 WC: 2007-19-13 EQUIPMENT/FURNISHINGS - B/E AEROSPACE SKYLUXE II (AA2) PASSENGER SEATS - INSP AND REORIENTATION OF Category: AD HYDROLOCK RETAINING PIN Status: N/A Rev: 0 LATEST Reason Frog: 1 THE AIRCRAFT IS NOT FITTED WITH WE AEROSPACE SKYLUXE II (M2) PAX SEATS. HENCE THE AD IS N/A BY INSTALLED SEAT MODEL EFTA_R1_00012815 EFTA01734547 NC Actual Compliance Last NC: A6DFR Type/Serlos: 6737-700/BBJ1 E/C (Category: AD) Amant NO Document/SB NC S/N: 30884 FJC Description: Print Date 07/09/2016 13:59 Page: 56 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/CyslDyslDte Next Due Last Compliance Information E/C: 2007-23-10 39-15256 Category: AD Status: N/A Rev: 0 WHEEL WELL CONNECTORS FILLET SEAL INSPECTION/MODIFICATION Reason Freq: I AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-24-1169 EARLIEST E/C: 2007-25-03 737-53A1253 FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING 15000 Cys 12797 Category: AD Status: OPEN 21109/2051 Rev: 0 Recur EARLIEST Froq: 1 E/C: 2008-0080 94-25-011 EQUIPMENT & FURNISHINGS - PASSENGER W-25-012 SEATS - INSPECTION/REPAIR/MODIFICATION Category: AD 94-25-013 Status: N/A Rev: 1 Superseded By: 2008-0097 LATEST Frew 1 BC: 2008-0097 94-25-011 EQUIPMENT & FURNISHINGS - PASSENGER 94.25-012 SEATS - INSPECTION/REPAIR/MODIFICATION Category: AD 94-25-013 Status: N/A Rev: 0 LATEST Reason Freq: 1 THIS AIRCRAFT IS NOT FITTED WITH SIGMA 94XX SERIES PAX SEATS. HENCE THE AD IS N/A BY INSTALLED SEAT MODEL EFTA_R1_00012816 EFTA01734548 NC: A6DFR EIC (Category: AD) Amant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 DoeumenVSB FJC Description: Print Date 07/09/2016 13:59 Page: 57 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information BC: 2008-01-01 Category: AD Status: N/A Rev: 1 FLIGHT DECK DOORS - MODIFICATION Reason Freq: I THIS AIRCRAFT IS NOT FITTED WITH JAMCO FLIGHT DECK DOORS. HENCE THE AD IS N/A BY INSTALLED FLIGHT DECK DOORS PIN. EARLIEST E/C: 2008-0135 12M/F68-06 EQUIPMENT/FURNISHINGS - PASSENGER 2006-0350 SEAT BACKREST • REPLACEMENT Category: AD Status: N/A Rev: 0 EARLIEST Reason Freq: i THIS AIRCRAFT IS NOT FITTED WITH AVIOINTERIORS SEATS PN: 12M SERIES. HENCE THE AD IS N/A BY INSTALLED SEAT MODEL. EIC: 2008-05-05 737.53A1242 STRUCTURE ATTACHMENT FITTINGS - Manual Compliance 09/04/2008 Rev: 0 INADEQUATE SEALING AROUND VERTICAL NC Total Hours: 1366:34 NC Total Cycles: 715 FIN LUGS SB 737-53A1242 C./OUT ON 28/03/03 BY BOEING Category: AD BACR668L. AD CLOSED. Status: TERMINATED Rev: 0 EARLIEST Freq: 1 E1C: 2008-06-03 AWL 2008-06-03 MOD ENGINE FUEL FEED SYSTEM • MOTOR Manual Compliance 28/06/2008 Rev: 0 39-15415 737-28A1207 OPERATED VALVE - AIRWORTHINESS NC Total Hours: 1455:09 NC Total Cycles: 764 LIMITATIONS SB 737-28A1207 CAN ON FLEET AND REQUIRED Category: AD AWLS' NOW INCORPORATED INTO THE AMS. AD Status: TERMINATED CLOSED. Rev: 0 EARLIEST Freq: 1 EFTA_R1_00012817 EFTA01734549 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SM: 30884 Document/SB EIC Description: Print Date 07/09/2016 13:59 Page: 58 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information BC: 2008-06-03 MOD 39-15415 Category: AD Status: TERMINATED Rev: 0 2008-06-03 AWL 737-28Al207 ENGINE FUEL FEED SYSTEM - MOTOR OPERATED VALVE - ACTUATOR REPLACEMENT Freq: I EARLIEST Manual Compliance 16/03/2008 Rev: 0 NC Total Hours: 1328:37 NC Total Cycles: 701 MOD PART OF AD CAN IAW SB 737-28Al207. REF TWO 12152 DTD 16/03/04. E/C: 2008-06-27 Category: AD Status: TERMINATED Rev: 3 25-343 EQUIPMENT/FURNISHINGS - EMERGENCY EVACUATION EQUIPMENT - SLIDE RAFTS - SHEAR PIN RESTRAINTS REPLACEMENT Reason Freq: 1 ALL SLIDES MODIFIED TO P/N 5A3307.7. EARLIEST EIC: 2008-08-22 Category: AD Status: TERMINATED Rev: 0 737-30-1056 GRAY WATER COMPOSITE DRAIN MAST BONDING JUMPER INSTALLATION Freq: 1 EARLIEST WO 12175 24/04/2008 Rev: 0 NC Total Hours: 1381:09 NC Total Cycles: 722 SB 737-30-1056 C/OUT ON 08/04/08. REF W/ORDER 12175 BC: 2008-08-24 Category: AD Status: TERMINATED Rev: 1 2012-23-08 737.54.1043 NACELLES/PYLONS - STRUT DRAINS AND SEALS -AFT FAIRING DRAIN TUBE ASSEMBLY REPLACEMENT Superseded By: 2012-23-08 Freq: 1 EARLIEST WO 13098 05/03/2009 Rev: 0 NC Total Hours: 1751:48 NC Total Cycles: 840 B3-54-1043 SB 737-54-1043 C/OUT DURING 2A CHK DTD 05/03/09. EFTA_R1_00012818 EFTA01734550 NC Actual Compliance Last NC: A6DFR Type/Series: 6737-700/BBJ1 E/C (Category: AD) Arrant NO Document/SB NC SIN: 30884 E/C Description: Print Date 07/0912016 13:59 Page: 59 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2008-09-14 39-15495 Category: AD Status: TERMINATED Rev: 1 737.28-1257 ENGINE FUEL FEED SYSTEM: BOOST PUMP CONTROL RELAY GROUND LOCATION CHANGE Free: I EARLIEST Manual Compliance 05/05/2008 Rev: 1 NC Total Hours: 1386:47 NC Total Cycles: 729 SB 737-28-1257 WAS CM' IAW EO 155809 BY LHT ON 15/07/07. REF DEL. DOGS. E/C: 2008-10-10AWL 2008-10.10 AMS REVISION TO INCLUDE AWL RELATED Manual Compliance 01/11/2009 Rev: 2 39-15516 2008-10-10INSP TO FUEL TANK SYSTEMS NC Total Hours: 1966:28 NC Total Cycles: 923 AMS ISSUE 14 REV. 0 DATED 01 NOV. 09 IS Category: AD 2008-10-10R1 ALREADY INCOPORTED WITH AWLS 28-AWL-21. Status: TERMINATED 28-AVVL-22 & 28-AVVL-24 ACTION REQUIRED BY Rev: 2 PARA (HX1) OF AD 2008-06-03. TERMINTES THE AD EARLIEST Reason Free: 1 AD COVERED WITH INTRODUCTION OF AWL ITEMS 28-AWL-01 TO 28-AWL-24 INTO THE MAINTENANCE PROGRAM. E/C: 2008-10-10INSP 2008-10-10 AMS REVISION TO INCLUDE AWL RELATED Manual Compliance 01/11/2009 Rev: 1 39-15516 2008-10-10AWL TO FUEL TANK SYSTEMS NC Total Hours: 1966:28 NC Total Cycles: 923 COVERED BY EC 2008-10-10-AWL COMPLIANCE - Category: AD 2008-10-10R1 AMS ISSUE 14 REV. 0 DATED 01 NOV. 09 IS Status: TERMINATED Rev: 1 ALREADY INCOPORTED WITH AWLS 28-AWL-21, 28-AWL-22 & 28-AWL-24 ACTION REQUIRED BY EARLIEST PARA (HX1) OF AD 2008-06-03. TERMINTES THE AD Reason Free: 1 INITIAL INSPECTION ACC. 28-AWL-03 PERFORMED. FINAL TERMINATION OF AD PER 2008-10-10AWL. E/C: 2008-11-08 737-56-1014 FLIGHT DECK NO Z 4, AND 5 WINDOWS - WO 50505 05/02/2016 Rev: 0 39-15530 737-56-1017 INSPECTION NC Total Hours: 5887:00 NC Total Cycles: 2120 Category: AD 737-56A1022 730 Dys 515 Status: OPEN SWCB73-56-001 04/02/2018 Rev: 0 Recur EARLIEST Frog: 1 EFTA_R1_00012819 EFTA01734551 NC: A6DFR E/C (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 DocumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 60 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2008-12-04 39-15547 Category: AD Status: OPEN Rev: 0 737-53-1232 FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION, REPAIR AND PREVENTIVE MODIFICATION Freq: I 35000 Cys Recur EARLIEST 32797 25/06/2106 E/C: 2008-16-13 39-15631 Category: AD Status: TERMINATED Rev: 0 737-27-1284 737-27-1284 IN 01 737-55A1080 FLIGHT CONTROLS - ELEVATOR AND TAB - LEFT AND RIGHT ELEVATOR TAB PUSHRODS REPLACEMENT Freq: 1 EARLIEST WO 13098 05/03/2009 Rev: 0 NC Total Hours: 1751:48 NC Total Cycles: 840 B3-27-1284 SB 737-27-1284 C/OUT DURING 2A CHK DTD 05/03/09. AD CLOSED. E/C: 2008-17-15 39-15653 Category: AD Status: N/A Rev: 0 INSTALL HOT SHORT PROTECTOR SUPPORT BRACKETS & EQUIPMENT FOR FOIS Reason Freq: 1 AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-28A1221 EARLIEST E/C: 2008.21.02 39-15686 Category: AD Status: TERMINATED Rev: 0 737.54.1045 NACELLES/PYLONS - HEAT INSULATION BLANKETS - REPLACEMENT Frog: 1 EARLIEST WO 13629 02/09/2009 Rev: 0 NC Total Hours: 1916:27 NC Total Cycles: 903 SB 737.54.1045 C/OUT DURING A CHK DTD 02/09/09. EFTA_R1_00012820 EFTA01734552 NC: A6DFR FJC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 61 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2008-22-01 AUX 39-15696 Category: AD Status: TERMINATED Rev: 2 2008-22-01 REPORT 2010-19-03 ST00936NY-D-28-S8-001 ST00936NY-D-28-SB-021 ST01384NY-D-28-SB-001 ST01384NY-D-28-SB-008 PREVENT USAGE OF AUXILIARY FUEL TANKS Freq: I EARLIEST WO 12640 16/08/2008 Rev: 2 NC Total Hours: 1469:35 NC Total Cycles: 767 ST00936NY-D-28-SB-001 AND ST00936NY-D-28-SB-021 C/OUT ON 16/08/2008 UNDER WORK ORDER 12640. AD TERMINATED. E/C: 2008-22-01 REPORT 39-15696 Category: AD Status: TERMINATED Rev: 0 2008-22-01 AUX 2010-19-03 ST00936NY-D-28-58.001 ST00936NY-D-28-SB-021 ST01384NY-D-28-58-001 ST01384NY-D-28-SB-008 PREVENT USAGE OF AUXILIARY FUEL TANKS Freq: 1 EARLIEST Manual Compliance 12/11/2008 Rev: 0 NC Total Hours: 1565:27 NC Total Cycles: 788 ETTER REF : QN120/0 BBJ PATS TANK STC /I USAGE INFORMATION NOTIFIED TO FM. BY QA ON 12/11/08. LETTER REF : ON120/08 E/C: 2008-23-07 39-15728 Category: AD Status: TERMINATED Rev: 0 2003-14-08 2006-13-13 AIRPLANE FLIGHT MANUAL REVISION - CABIN ALTITUDE WARNING Freq: 1 EARLIEST WO 12982 03/12/2008 Rev: 0 NC Total Hours: 1606:32 NC Total Cydes: 797 E/C: 2008-24-05 39-15745 Category: AD Status: TERMINATED Rev: 0 2003-20-13 737-30A1057 WINDSHILED WIPER MOTOR REPLACEMENT Freq: 1 EARLIEST WO 12229 11/01/2009 Rev: 0 NC Total Hours: 1655:45 NC Total Cycles: 813 SB 737-30A1057 C/OUT UNDER WORK ORDER 12229.P/N OF WIPER ASSY P/N CHANGED AS REQD. EFTA_R1_00012821 EFTA01734553 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC S/N: 30884 Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 62 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2008-24-08 Category: AD Status: TERMINATED Rev: 0 2001.15-01 2007-NM-228-AD 25-308 5A3307-25-309 5A3307.25.339 737-25-1404 737-25-1491 EQUIPMENT/FURNISHINGS - EMERGENCY - DOOR MOUNTED ESCAPE SYSTEM - CHANGE EVACUATION SLIDE INFLATION VALVE REGULATOR Free: I EARLIEST Manual Compliance 30/12/2008 Rev: 0 NC Total Hours: 1646:36 NC Total Cycles: 808 P/N 5A3307-5 FITTED TO NC SATISFIES THE REQUIREMENT OF THIS AD. AD CLOSED. E/C: 2008-24-51 1.1072186611.1 INSPECTION FOR MIS-WIRING AFTER WO 13014 19/11/2008 Rev: 2 39-15781 ACCOMPLISHMENT OF SB 737.28A1206 NC Total Hours: 1582:37 NC Total Cycles: 793 Category: AD Status: TERMINATED Rev: 3 EARLIEST Free: I EIC: 2009-01-02 737-25-1544 SUPPORT FITTING ASSEMBLY AIR 737-25-1544 R1 CONDITIONING EXTRUSIONS 36000 Cys 33797 REPLACEMENT Category: AD Status: OPEN 21/03/2109 Rev: 0 Once EARLIEST E/C: 2009-0251-E 2009-0278 FIRE PROTECTION - PORTABLE FIRE Manual Compliance 27/11/2009 Rev: 0 2009-39 EXTINGUISHERS - NC Total Hours: 1987:43 NC Total Cycles: 930 IDENTIFICATION/REPLACEMENT AD ACCOMPLISHED. NO AFFECTED P/N FOUND Category: AD FITTED TO AIRCRAFT. REF TLP 2198667 ITEM 7. Status: TERMINATED Rev: 1 EARLIEST Free: 1 EFTA_R1_00012822 EFTA01734554 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC S/N: 30884 Document/SS EJC Description: Print Date 07/09/2016 13:59 Page: 63 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/DyslDte Next Due Last Compliance Information E/C: 2009-0262 Category: AD Status: TERMINATED Rev: 2 2009-0251-E 2009-0262 R1 2009-0278 2009-39 ASB26-115 ASB26-115 ISS C FIRE PROTECTION - PORTABLE FIRE EXTINGUISHERS - IDENTIFICATION/REPLACEMENT EARLIEST WO 14291 28/12/2009 Rev: 0 NC Total Hours: 2012:21 NC Total Cycles: 936 FOUND AFFECTED FIRE EXT P/N & S/N NOT FITTED TO AIRCRAFT. REF SWCG26-003, W/O # 14291 Freq: I E/C: 2009-0278 2009-0251-E FIRE PROTECTION - PORTABLE HALON WO 14291 28/12/2009 Rev: 0 2009-0262 1211 FIRE EXTINGUISHERS - NC Total Hours: 2012:21 NC Total Cycles: 936 Category: AD Status: TERMINATED Rev: 1 IDENTIFICATION/REPLACEMENT Freq: 1 EARLIEST FOUND AFFECTED PORTABLE FIRE EXT P/N & S/N NOT FITTED. REF. SWCG26-004 W/O # 14291 E/C: 2009-12-06 737.24.1147 IFES LOAD SHED Manual Compliance 19804 04/02/2014 Rev: 0 39-15929 737IGW-24-03 NC Total Hours: 4841:40 NC Total Cycles: 1785 Category: AD Status: TERMINATED Rev: 0 Freq: 1 EARLIEST E/C: 2009-19-02 39-16019 Category: AD Status: N/A Rev: 3 RUDDER FEEL AND CENTERING UNIT - INSPECTION. TEST AND REPLACEMENT OF SPRING ASSEMBLY Reason Freq: I THIS AD IS N/A BY INSTALLED FEEL AND CENTERING UNITS P/N EARLIEST EFTA_R1_00012823 EFTA01734555 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700/BBJ1 E/C (Category: AD) Anent NO Document/SB NC SIN: 30884 E/C Description: Print Date 07/09/2016 13:59 Page: 64 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2009-21-10 39-16049 Category: AD Status: N/A Rev: 3 2009.21.10 R1 AVOX SYSTEMS AND 8/E AEROSPACE OXYGEN CYLINDER ASSEMBLIES Reason Freq: I THIS AD IS N/A BY INSTALLED OXYGEN CYLINDER ASSEMBLY S/N . EARLIEST E/C: 2009-24-07 2009-26-04 INSP MAIN LANDING GEAR - FORWARD 39-16095 2009-26-04 LOBE TRUNNION PIN INSPECTION AND REPLACEMENT Category: AD 737-32-1376 INSP Status: N/A 737-32-1376 LUBE Rev: 0 EARLIEST Reason Froq: 1 AD IS N/A BY THE EFFECTIVITY LIST OF BOEING SB 737-32-1402 E/C: 2009-26-03 737-24-1165R1 ELECTRICAL POWER: STANDBY STATIC Manual Compliance 02/02/2010 Rev: 0 39-16138 INVERTER MODIFICATION NC Total Hours: 2030:34 NC Total Cycles: 940 SB 737-24-1165 FOUND PERFORMED AS PER LHT Category: AD SB SUMMARY AT TIME OF DEL. TO PF. AD CLOSED. Status: TERMINATED Rev: 0 EARLIEST Freq: 1 BC: 2009-26-04 INSP 1.43710731 MAIN LANDING GEAR • FORWARD Manual Compliance 02/02/2010 Rev: 1 39-16139 2009-24-07 TRUNNION PIN INSPECTION AND REPLACEMENT NC Total Hours: 2030:34 NC Total Cycles: 940 SB 737-32-1376 FOUND COMPLIED WITH AND Category: AD 2009-26-04 LUBE CLOSED AS PER LHT SB SUMMARY LIST AT TIME Status: TERMINATED 737-32-1376 INSP OF DELIVERY TO AMIRI FLIGHT. AD CLOSED. Rev: 1 737-32-1376 LUBE 737-32-1376R1 EARLIEST 737-32-1376R2 Freq: 1 SWCB73-32-009 EFTA_R1_00012824 EFTA01734556 NC: A6DFR FJC (Category: AD) Ament NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SS FJC Description: Print Date 07/09/2016 13:59 Page: 65 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2009-26-04 LUBE 39-16139 Cat egory: AD 1.43710731 2009-24-07 2009-26-04 INSP MAIN LANDING GEAR - FORWARD TRUNNION PIN LUBRICATION WO 02/02/2010 Rev: 0 NC Total Hours: 2030:34 NC Total Cycles: 940 Terminating Action Has Been Performed Status: TERMINATED 737-32-1376 INSP Rev: 0 737-32-1376 LUBE 737-32-1376R1 EARLIEST 737-32-1376R2 Freq: I SWCB73-32•009 E/C: 2010-0062 2009-0251-E FIRE PROTECTION - HALON 1211 FIRE 2010-0062 R1 EXTINGUISHERS - IDENTIFICATION/REPLACEMENT Category: AD 26-116 Status: N/A 26-116 ISSU B Rev: 1 EARLIEST Reason Freq: 1 THIS NC IS NOT FITTED WITH FIRE EXTINGUSHER P/N LISTED IN THE FFE SB 28-116. AD IS N/A BY INSTALLED P/N. E/C: 2010-01.03 2009-0251-E PORTABLE HALON 1211 (BCF) FIRE Manual Compliance 01/02/2010 Rev: 0 2009-0262 EXTINGUISHERS MANUFACTURED BY FFE NC Total Hours: 2030:34 NC Total Cycles: 940 EASA AD 2009-0251-E AND 2009-0262 ARE Category: AD COMPLIED WITH WHICH WILL SATISFY THE Status: TERMINATED REQUIREMENT OF THIS FAA AD. REF ENG. Rev: 0 REMARKS IN EC. AD CLOSED. EARLIEST Frog: 1 E/C: 2010-01.08 737-57A1294 WINGS - WING CENTER SECTION - UPPER AND LOWER STRINGERS - DRILL START INSPECTION AND REPAIR Category: AD Status: N/A Rev: 0 LATEST Reason Frog: 1 AD IS NIA BY THE EFFECTIVITY LIST OF BOEING SB 737-57A1294 EFTA_R1_00012825 EFTA01734557 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700/BBJ1 EIC (Category: AD) Arrant NO Documant/SB NC SIN: 30884 E/C Description: Print Date 07/09/2016 13:59 Page: 66 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2010-0152 Category: AD Status: N/A Rev: 0 EASA AD 2010-0152 EQUIPMENT/FURNISHINGS - OXYGEN MASK REGULATOR - MODIFICATION Reason Frog: I AD IS N/A BY INSTALLED OXYGEN MASK REGULATOR P/N. EARLIEST E/C: 2010-0204 2010-0204 CORRECTION MODE S TRANSPONDER - MODIFICATION/REPLACEMENT Category: AD Status: N/A Rev: 1 EARLIEST Reason Froq: 1 THIS NC IS NOT FITTED WITH TDR-94 AND TDR-94D TRANSPONDERS. HENCE THE AD IS N/A BY INSTALLED P/N. E/C: 2010-02-04 125334D-28-02 ENGINE FUEL FEED - MAIN TANKS ENGINE WO 16115 16/09/2011 Rev: 1 737-28-1272 FUEL SPAR VALVE BODY REPLACEMENT NC Total Hours: 2813:55 NC Total Cycles: 1178 Category: AD 747-SL-28-106 Terminating Action Has Been Performed Status: TERMINATED SB125334D-28-02 Rev: 1 EARLIEST From t E/C: 2010-02-06 92-25-005 EQUIPMENT/FURNISHINGS- SIGMA AERO SEATS 90XX AND 92XX SERIES PASSENGER SEATS Category: AD Status: N/A Rev: 0 EARLIEST Reason Friuli I THE AIRCRAFT IS NOT FITTED WITH SICMA 90XX AND 92XX SERIES PAX SEATS. HENCE THE AD IS N/A BY INSTALLED SEAT MODEL EFTA_R1_00012826 EFTA01734558 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB FJC Description: Print Date 07/09/2016 13:59 Page: 67 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2010-0244-INSP Category: AD Status: CANCEL Rev: 1 2010-0244-MOD 2010-0244R1•INSP 2012•05•02-INSP 737-78-1079 737-78-1082 737-78-1088 EXHAUST - THRUST REVERSER INNER WALL - INSPECTION / REPAIR Superseded By: 2012•05•02•INSP Freq: I EARLIEST E/C: 2010-0244-MOD 2010-0244-INSP EXHAUST - THRUST REVERSER INNER WO 17373 20/0212012 Rev: 1 2010-0244-R1-MOD WALL — MODIFICATION NC Total Hours: 3055:15 A/C Total Cycles: 1262 Category: AD 2012-05-02-MOD Status: CANCEL 737-78-1079 Rev: 2 737-78-1082 737-78-1088 Superseded By: 2012-05-02-MOD EARLIEST Freq: 1 EIC: 2010-04-16 2009-0251-E FIRE PROTECTION - PORTABLE HALON 2009-0262 1211 FIRE EXTINGUISHERS • IDENTIFICATION/REPLACEMENT Category: AD 2009-0278 Status: N/A Rev: 0 EARLIEST Reason Freq: 1 AD IS N/A BY INSTALLED PORTABLE FIRE EXTINGUISHERS S/N EIC: 2010-06-51 737-27A1296 EMERGENCY AIRWORTHINESS DIRECTIVE Manual Compliance 14/04/2010 Rev: 0 - ELEVATOR TAB CONTROL MECHANISM NC Total Hours: 2030:34 NC Total Cycles: 940 DETAILED INSPECTION TERMINATED 15/04/10 BY ACCOMPLISHMENT OF Category: AD SB 737-27A1296. REF: WO14633 Status: TERMINATED Rev: 0 Superseded By: 2010-17-19 EARLIEST Reason Frog: 1 TERMINATED 15104/10 BY ACCOMPLISHMENT OF SB 737-27A1296. EFTA_R1_00012827 EFTA01734559 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SB EJC Description: Print Date 07/09/2016 13:59 Page: 68 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2010-09-05 Category: AD Status: CANCEL Rev: 1 2010-06.51 737.27-01296 737-27A1297 ELEVATOR TAB CONTROL MECHANISM DETAILED INSPECTION Superseded By: 2010-17-19 Freq: I EARLIEST E1C: 2010-17-05 737-28A1201 FUEL PUMP CONTROL GROUND FAULT WO 13629 07/0912010 Rev: 0 39-16395 Category: AD Status: TERMINATED Rev: 0 INTERRUPTER (GFI) RELAY INSTALLATION Freq: 1 EARLIEST NC Total Hours: 2127:50 NC Total Cycles: 971 C/OUT IAW B3-28A1201R1 13629 DTD 02/09/2009 UNDER WORK ORDER E/C: 2010-17-19 2010-09-05 ELEVATOR TAB CONTROL MECHANISM WO 18673 29/01/2013 Rev: 1 39-16413 737-27-1300 DETAILED INSPECTION NC Total Hours: 4026:35 NC Total Cycles: 1550 Category: AD 737-27A1296 Status: CANCEL 737-27A1297 Rev: 2 737-27A1297R1 737-27A1299 Superseded By: 2013-06-05 EARLIEST Freq: 1 E/C: 2010-19-03 39-16431 Category: AD Status: TERMINATED Rev: 1 2008-22-01 AUX 2008-22-01 REPORT ST00936NY-D-28-SB-001 ST00936NY.D.28-SB-021 PREVENT USAGE OF AUXILIARY FUEL TANKS OR MODIFY AUXILIARY FUEL SYSTEM Freq: 1 EARLIEST WO 12640 24/10/2010 Rev: 1 NC Total Hours: 2223:50 NC Total Cycles: 998 SB ST00936NY-0-28-SB-001 AND D-28-SB-021 C/OUT UNDER WO 12640 DTD 16/08/08. EFTA_R1_00012828 EFTA01734560 NC Actual Compliance Last NC: A6DFR Type/Series: 6737•700/BBJ1 E/C (Category: AD) Arrant NO Document/SB NC SIN: 30884 FJC Description: Print Date 07/09/2016 13:59 Page: 69 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/CyslDyslDte Next Due Last Compliance Information BC: 2010-24-11 39-16530 Category: AD 737-57A1279 CENTER AND OUTER WING - FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL INSPECTION WO 16115 16/09/2011 Rev. 0 NC Total Hours: 2813:55 NC Total Cycles: 1178 SB 737-57A1279 GOUT UNDER WO 16115 DTD 16/09/2011. Status: TERMINATED Rev: 0 Freq: I EARLIEST E/C: 2010-26-06 PART 1 2010-26-06 PART 2 737-53A1289 PART-1 FUSELAGE - SKIN - INSPECTION OF THE SKIN FOR SCRIBE LINES • PART 1 (SKIN LAP JOINTS. CIRCUMFERENTIAL BUTT 40000 Cys 37797 Category: AD Status: OPEN 737-53A1289 PART-2 JOINTS, INTERNAL APPROVED REPAIRS) 03103/2120 Rev: 0 Once EARLIEST E/C: 2010-26-06 PART 2 2010-26-06 PART 1 737-53A1289 PART-1 FUSELAGE - SKIN - INSPECTION OF THE SKIN FOR SCRIBE LINES • PART 2 (DECALS AND EXTERNAL APPROVED REPAIRS) 20000 Cys 17797 Category: AD Status: OPEN 737-53A1289 PART-2 30/05/2065 Rev: 0 Freq: 1 Once EARLIEST BC: 2011-0043 Category: AD Status: N/A Rev: 0 MODE S TRANSPONDER CONTROL PANELS - MODIFICATION Reason Freq: I THIS AIRCRAFT IS NOT FITTED WITH GABLES G7490, G7492 OR G7493 CONTROL PANELS. HENCE THE AD IS N/A BY INSTALLED P/N. EARLIEST EFTA_R1_00012829 EFTA01734561 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737-700/BBJ 1 NC S/N: 30884 DocumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 70 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/DyslDte Next Due Last Compliance Information E/C: 2011-0093 Category: AD Status: N/A Rev: 0 2011-0103 EQUIPMENT / FURNISHINGS - EMERGENCY LOCATOR TRANSMITTER (ELT) ANTENNA - MODIFICATION / REPLACEMENT Superseded By: 2011.0103 Frog: I EARLIEST E/C: 2011-0094 Category: AD Status: N/A Rev: 0 SB 25.65.24 EQUIPMENT/FURNISHINGS - LIFE JACKET VACUUM BAG - MODIFICATION Reason Frew 1 AD IS N/A BY INSTALLED P/N. EARLIEST E/C: 2011-0098 Category: AD Status: N/A Rev: 1 2011.12-O1 EQUIPMENT/FURNISHINGS - PASSENGER SEAT - REPLACEMENT Reason Frew 1 THIS AIRCRAFT IS NOT FITTED WIHT KOITO SEATS. HENCE THE AD IS N/A BY INSTALLED SEAT MODEL. EARLIEST E/C: 2011-0103 Category: AD Status: N/A Rev: 0 2011.0093 ATA 25: EQUIPMENT /FURNISHING - EMERGENCY LOCATOR TRANSMITTER(ELT) ANTENNA-MODIFICATION REPLACEMENT Reason Freq: 1 THIS AIRCRAFT IS NOT FITTED WITH CHELTON ELT ANTENNA P/N 21.41. HENCE THE AD IS N/A BY INSTALLED P/N. EARLIEST EFTA_R1_00012830 EFTA01734562 NC Actual Compliance Last NC: A6DFR Type/Series: B737-700/BBJ1 SC (Category: AD) Anent NO Document/SB NC SIN: 30884 E/C Description: Print Date 07/09/2016 13:59 Page: 71 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2011-01-09 Category: AD Status: N/A Rev: 01 119003-35-5 119003-35-6 EMERGENCY EQUIPMENT - WE AEROSPACE PROTECTIVE BREATHING EQUIPMENT Reason Freq: 1 THIS AIRCRAFT IS NOT FITTED WITH B/E AEROSPACE PBE PN: 119003-11. HENCE THE AD IS N/A BY INSTALLED P/N. EARLIEST SC: 2011-04-09 OXYGEN - PASSENGER OXYGEN SYSTEM - LAVATORY SERVICE UNITS Category: AD Status: N/A Rev: 1 Superseded By: 2012-11-09 EARLIEST Reason Frog: 1 NOT APPLICABLE FOR NC OPERATED IN THE UAE. E/C: 2011-06-05 INSP 1-523812011-1 INSPECTION OF SLAT TRACK DOWNSTOP WO 16115 16/09/2011 Rev: 0 1-527463441-1 ASSEMBLIES ON ALL LEADING EDGE NC Total Hours: 2813:55 NC Total Cycles: 1178 SLATS Terminating Action Has Been Performed Category: AD 2007-18-51 Status: TERMINATED 2007-18-52 Rev: 0 2011-06-05 MOD 737-57A1302 EARLIEST 737-SL-57-084 Frog: 1 SC: 2011-06-05 MOD 1-523812011-1 MODIFICATION OF SLAT TRACK WO 16115 16/09/2011 Rev: 0 1-527463441-1 DOWNSTOP ASSEMBLIES ON ALL LEADING NC Total Hours: 2813:55 NC Total Cycles: 1178 EDGE SLATS Terminating Action Has Been Performed Category: AD 2007-18-51 Status: TERMINATED 2007.18.52 Rev: 0 2011-06-05 INSP 737-57A1302 EARLIEST 737-SL-57-084 Frog: 1 EFTA_R1_00012831 EFTA01734563 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 72 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys!Dte Next Due Last Compliance Information E/C: 2011-07-05 Category: AD Status: N/A Rev: 01 2001-605(AB) 90-25.012 SICMAAERO SEATS - INSPECTION OF BACKREST LINKS FOR CRACKS Superseded By: 2014-20-11 Reason Freq: I AD NOT APPLICABLE. AFFECTED SEATS NOT INSTALLED. EARLIEST E/C: 2011-12-01 EQUIPMENT/FURNISHINGS - PASSENGER SEATS - KOITO SEATS - NON CONFORMITY TO CERTAIN FLAMMABILITY, STATIC Category: AD STRENGTH AND DYNAMIC STRENGTH Status: N/A CRITERIA Rev: 01 EARLIEST Reason Froq: 1 THIS AIRCRAFT IS NOT FITTED WIHT KOITO SEATS. HENCE THE AD IS N/A BY INSTALLED SEAT MODEL. E/C: 2011.12.13 737-27-1289 STABILIZER TAKEOFF WARNING SWITCHES 750 Hrs 483:30 WO 50505 05/02/2016 Rev: 0 39-16720 - TEST OF THE TAKEOFF WARNING INDICATION NC Total Hours: 5887:00 NC Total Cycles: 2120 Category: AD Status: OPEN 06/05/2017 Rev: 0 Recur EARLIEST Frog: i E/C: 2011.14-08 174080-35-04 OXYGEN - CONTINUOUS FLOW 2007-26-06 PASSENGER OXYGEN MASK ASSEMBLY - INSPECTION Category: AD 2008-12-05 Status: N/A 2010-0165 Rev: 0 EARLIEST Reason Frew I VTHIS NC IS NOT FITTED WITH PAX 02 MASKS LISTED IN VSB 174080-35-04. HENCE THE AD IS N/A BY P/N EFFECTIVITY. EFTA_R1_00012832 EFTA01734564 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 DoeumenVSB SC Description: Print Date 07/09/2016 13:59 Page: 73 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2011-18-03 Category: AD Status: TERMINATED Rev: 0 2001-08-24 2002-19-52 2002.24.51 737.28Al206 737-28A1248 INSTALLATION OF AN AUTOMATIC SHUTOFF SYSTEM FOR THE CENTER TANK FUEL BOOST PUMPS. AND INSTALLATION OF A PLACARD IN THE AIRPLANE FLIGHT DECK IF NECESSARY. WO 16920 04/10/2011 Rev: 0 NC Total Hours: 2820:50 NC Total Cycles: 1182 EARLIEST Freq: I SC: 2011-18-10 2003-03-01 AFT ENGINE MOUNT • CENTER LINK ASSY • Manual Compliance 05/1172015 Rev: 3 39-16792 737-71A1462 INSPECTION TO ENSURE CORRECT INSTALLATION NC Total Hours: 5817:55 NC Total Cycles: 2086 DURING ENGINE CHANGE (REF WON15766 DT: Category: AD 737-71A1462-1 26-MAY-2011) SB HANGAR FITTING WAS MARKED Status: TERMINATED I.A.W. SB 737-71A1462 R3 Rev: 3 EARLIEST Reason Frog: 1 REFER THE ENGINE AD STATUS COMMENT E/C: 2011.20-07 737-28Al201 FUEL PUMP CONTROL GROUND FAULT WO 13629 02/10/2011 Rev: 0 39-16816 INTERRUPTER (GFI) RELAY INSTALLATION NC Total Hours: 2820:30 NC Total Cycles: 1181 SB 737-28Al201R1 C/OUT ON 02/0972009 UNDER Category: AD WORK ORDER 13629 Status: TERMINATED Rev: 1 EARLIEST Frog: 1 SC: 2011.20.10 737-27-1282 RUDDER & RUDDER TRIM CONTROL WO 12252 09/10/2011 Rev: 0 39-16823 SYSTEM: WIRE BUNDLE W 443 AND LEFT NC Total Hours: 2820:50 NC Total Cycles: 1182 FWD. RUDDER QUADRANT CLEARANCE SB 737-27-1282 C/OUT UNDER WO 12252 Category: AD INSPECTION Status: TERMINATED Rev: 0 EARLIEST Freq: 1 EFTA_R1_00012833 EFTA01734565 NC: A6DFR EC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB EIC Description: Print Date 07/09/2016 13:59 Page: 74 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2011-21-08 Category: AD Status: N/A Rev: 0 2001.0613 SB 90-25-013 ISS 4 EQUIPMENT/FURNISHINGS - SICMAAERO SEATS - INSPECTION OF BACKREST LINKS Reason Freq: I THE AFFECTED SICMA SEATS ARE NOT INSTALLED ON THIS A/C AND HENCE THIS AD IS NOT APPLICABLE BY THE INSTALLED SEAT MODEL EARLIEST EIC: 2011-26-09 737-54-1046 NACELLES/PYLONS - STRUT TO WING WO 20202 0810812014 Rev: 0 Cate gory: AD FAIRINGS - THUMBNAIL FAIRING EDGE SEAL REPLACEMENT NC Total Hours: 5107:40 A/C Total Cycles: 1870 Status: TERMINATED Rev: 0 EARLIEST Freq: i FJC: 2011-27-03 WP1 2011-27-03 WP2 HORIZONTAL STABILIZER TRIM CONTROL 1600 Hrs 1232:35 WO 50175 22/0812015 Rev: 0 2011-27-03 WP3 SYSTEM - BALLSCREW AND NUT INSPECTION AND LUBRICATION - NC Total Hours: 5786:05 NC Total Cycles: 2071 Category: AD 737-27A1277 WP1 WORKAGE PACKAGE 1 365 Dys -17 Status: OPEN 21/08/2016 Rev: 0 Recur EARLIEST Freq: 1 EIC: 2011-27-03 WP2 Category: AD Status: OPEN Rev: 0 2011-27-03 WP1 2011.27-O3 WP3 27-108-00-01 737-27A1277 WP2 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM • STABILIZER TRIM ACTUATOR MODIFICATION • WORK PACKAGE 2 Freq: 1 25000 Hrs Once EARLIEST 18846:30 26/06/2042 EFTA_R1_00012834 EFTA01734566 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB EJC Description: Print Date 07/09/2016 13:59 Page: 75 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/CysloyelDte Next Due Last Compliance Information SC: 2011-27-03 WP3 39-16904 Category: AD Status: OPEN Rev: 0 2011.27-03 WP1 2011.27-03 WP2 27-108-00-01 737-27A1277 WP3 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - STABILIZER TRIM ACTUATOR OVERHAUL • WORK PACKAGE 3 25000 Hrs Recur EARLIEST 18846:30 26/06/2042 Freq: I E/C: 2012-0037 A26-081 FIRE PROTECTION - HAND OPERATED FIRE A26-081 RI EXTINGUISHER - MODIFICATION Category: AD Status: N/A Rev: 00 EARLIEST Reason Frog: 1 THE AFFECTED FIRE EXTINGUSHER P/N ARE NOT INSTALLED ON THIS NC AND HENCE THIS AD IS NOT APPLICABLE BY THE INSTALLED PIN EIC: 2012-0038 2001-605(AB) EQUIPMENT & FURNISHINGS - 90-25-012 PASSENGER SEAT BACKREST LINK - INSPECTION/REPLACEMENT Category: AD Status: N/A Rev: 0 EARLIEST Reason Frog: 1 THE AFFECTED SICMA SEATS ARE NOT INSTALLED ON THIS A/C AND HENCE THIS AD IS NOT APPLICABLE BY THE INSTALLED SEAT MODEL EIC: 2012-02-14 737-78-1074 THRUST REVERSER • BLOCKER DOOR Manual Compliance 25/02/2012 Rev: 00 39-16937 AERO/FIRE SEAL - INSPECTION / NC Total Hours: 3059:20 NC Total Cycles: 1263 REPLACEMENT SB 737-78-1074 PREV C/W.REF WORK ORDER Category: AD 13578 DTD 15/04/2010 Status: TERMINATED Rev: 00 EARLIEST Freq: 1 EFTA_R1_00012835 EFTA01734567 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Salves: B737.700IBBJ1 NC SIN: 30884 Document/SB EJC Description: Print Date 07/09/2016 13:59 Page: 76 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dta Next Due Last Compliance Information SC: 2012-05-02-INSP 2010-0244-INSP 2010-0244R14NSP EXHAUST - THRUST REVERSER INNER WALL - INSPECTION / REPAIR WO 17759 10/08/2012 Rev: 0 NC Total Hours: 3530:40 NC Total Cycles: 1392 Category: AD 737-78-1069 Status: TERMINATED 737-78-1079 Rev: 1 737-78-1082 737-78-1088 EARLIEST Freq: I E/C: 2012-05-02-MOD 2010-0244-MOD EXHAUST — THRUST REVERSER INNER Manual Compliance 27/09/2015 Rev: 2 2010-0244-R1-MOD WALL - MODIFICATION NC Total Hours: 5801:10 NC Total Cycles: 2082 ACCOMPLISHED 2010-0244MOD AS PER WO 17373 Category: AD 737-78-1063 DATED 20 FEB 2012. Status: TERMINATED 737-78-1079 Rev: 2 737-78-1082 CFM56.78.73.0135 EARLIEST Freq: 1 EIC: 2012-09-06 737-25-1598 REPLACEMENT OF THE SEAT TRACK PIVOT 737-25-1599 LINK ASSEMBLIES Category: AD 737-53-1286 Status: N/A Rev: 00 EARLIEST Reason Freq: 1 THIS AD IS NOT APPLICABLE BY THE EFFECTIVITY LIST OF SB 737-53-1286; 737-25-1598; 737-25-1599 EIC: 2012-11-09 2012-11-09 R1 INSTALLING A SUPPLEMENTAL OXYGEN SYSTEM IN AFFECTED LAVATORIES Category: AD Status: N/A Rev: 01 LATEST Reason Freq: 1 N/A DUE DOES NOT FALL INTO THE OPERATING CATEGORY (CFR PART 121; OR U.S. REGISTERED AND OPTG UNDER PART 129). EFTA_R1_00012836 EFTA01734568 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DocumenVSB EJC Description: Print Date 07/09/2016 13:59 Page: 77 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2012-19-11 Category: AD Status: OPEN Rev: 01 737.21.1165 737.31A1332 Incorporating design changes to improve the reliability Superseded By: 2015-16-01 Freq: 1 2190 Dys Once EARLIEST 790 06/11/2018 ESC: 2012-21-08 39-17224 Cat egory: AD Status: N/A Rev: 0 737-22A1211 FAA AD 2012-21-08 AUTOFLIGHT: DETECT AND CORRECT AN UNSAFE CONDITION DUE TO A DEFECTIVE RADIO ALTIMETER CHANNEL Reason Freq: 1 THIS AD IS NOT APPLICABLE BY THE EFFECTIVITY LIST OF 737-22A1211 EARLIEST BC: 2012.23.08 Category: AD Status: OPEN Rev: 00A 2008-08-24 737-54-1043 R2 NACELLES/PYLONS - STRUT DRAINS AND SEALS -AFT FAIRING DRAIN TUBE ASSEMBLY REPLACEMENT Frog: 1 1825 Dys Once EARLIEST 478 29/12/2017 EIC: 2012-24-08 Category: AD Status: TERMINATED Rev: 02 737-30A1063 Prevent ice from forming on air data system sensors Freq: 1 EARLIEST WO 20202 08/08/2014 Rev: 02 NC Total Hours: 5107:40 NC Total Cycles: 1870 EFTA_R1_00012837 EFTA01734569 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 E/C (Category: AD) Arrant NO Document/SB FJC Description: Print Date 07/09/2016 13:59 Page: 78 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2012-25-05 Category: AD Status: TERMINATED Rev: 00 2008-24-08 25-349 SA3307-25-389 EQUIPMENT/FURNISHINGS - ESCAPE SLIDE/RAFT - MODIFICATION Reason Freq: I ALL SLIDES MODIFIED ACCORDING TO VSB 5A3307-25-389. EARLIEST Manual Compliance 05/11/2015 Rev: 00 NC Total Hours: 5817:55 NC Total Cycles: 2086 VSB 5A3307-25-389 HAS BEEN COMPLIED TO ALL SLIDES. E/C: 2013-0020 Category: AD Status: N/A Rev: 06 2013-0020 R1 2013-0020 R2 2013-0020 R3 2013-0020 R4 2013-0020 R4 CORRECTION EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSPECTION / REPLACEMENT Reason Froq: I AFFECTED SEAT BELTS NOT FITTED PER AIRCRAFT RECORDS EARLIEST E/C: 2013-02-05 39-17326 Category: AD Status: TERMINATED Rev: 0 2003-14-08 2006-13-13 2008-23-07 737-31A1332 AURAL WARNING SYSTEM: INSTALLATION OF CABIN ALTITUDE WARNING SYSTEM & TAKEOFF CONFIGURATION WARNING SYSTEM LIGHTS Freq: 1 EARLIEST WO 20202 08/08/2014 Rev: 0 NC Total Hours: 5107:40 NC Total Cycles: 1870 BC: 2013-02-07 Category: AD Status: N/A Rev: 00 737-25-1641 737-25-1641 R1 737-25-1641 R2 EQUIPMENT / FURNISHINGS - PASSENGER CABIN PARTITIONS AND COMPARTMENTS - CENTER OVERHEAD STOWAGE BOX WITH LIFERAFT PROVISIONS - 9G TIE ROD ATTACHMENT CHANGE Reason Frog: 1 N/A BY VARIABLE NUMBER OF THE AIRCRAFT IN THE SB EFFECTIVITY LATEST EFTA_R1_00012838 EFTA01734570 NC: A60FR E/C (Category: AD) Ament NO A/C Actual Compliance Last Type/Series: Et737.70043BJ1 NC SIN: 30884 Document/SB BC Description: Print Date 07/092016 13.59 Page: 79 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information BC: 2013-04-11 Category: AD Status: NIA Rev: 00 737-28-1303 FAA AD 2013-04-11 Prevent electrical arcing and a potential ignition source within the ECS bay Reason Free: t N/A BY VARIABLE NUMBER OF THE AIRCRAFT IN THE SB EFFECTIVITY LATEST BC: 2013-06-05 INSP 2010-17-19 DETAILED INSPECTION OF THE INBOARD 1800 Hrs 754:10 WO 20202 08/0812014 Rev: 2 39-16270 737-27-1300 AND OUTBOARD AFT ATTACH LUGS OF THE LEFT AND RIGHT ELEVATOR TAB CONTROL NC Total Hours: 5107:40 NC Total Cycles: 1870 Category: AD 737-27A1297 MECHANISMS Status: OPEN 737-27A1297R1 19/09/2017 Rev: 2 737-27A1297R2 Recur 737-27A1299 LATEST Frog: 1 E/C: 2013-06.05 MOD 2010-17-19 REPLACE THE LEFTAND RIGHT ELEVATOR 2013-06-05 INSP TAB MECHANISMS WITH ELEVATOR TAB CONTROL MECAHNISMS THAT HAVE NEW Category: AD 737-27-1300 MACHINED AFT ATTACH LUGS Status: OPEN 737-27A1297 09105/2018 Dte 09/05/2018 Rev: 0 7S7-Y7Al299 Once EARLIEST Frog: 1 E/C: 2013-07-07 2014-05-30 STABILIZERS - HORIZONTAL STABILIZER 737-55-1093 REAR SPAR ATTACH PINS - INSPECTION/REPLACEMENT Category: AD Status: CANCEL RIM 01 Superseded By: 2014-05-30 EARLIEST Frog: 1 EFTA_R1_00012839 EFTA01734571 NC: A6DFR EIC (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SB FJC Description: Print Date 07/09/2016 13:59 Page: 80 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2013-07-09 Category: AD Status: N/A Rev: 00 737-35A1121 MXP1 /4-35-175 OXYGEN - FLIGHT CREW OXYGEN MASK STOWAGE BOX - TO PREVENT AN IGNITION SOURCE Reason Free: I THIS AD IS NOT APPLICABLE BY THE EFFECTIVITY LIST OF 737-35A1121 EARLIEST EIC: 2013-08-01 39-17418 Category: AD Status: TERMINATED Rev: 0 737-78-1086 Thrust Reverser - Upper Fire Seal Damage Froq: 1 EARLIEST WO 20202 08/08/2014 Rev: 0 NC Total Hours: 5107:40 NC Total Cycles: 1870 Terminating Action Has Been Performed E/C: 2013-08-16 Category: AD Status: OPEN Rev: 00 737-53-1310 FUSELAGE - SKIN - CHEM MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND MODIFICATION Frog: 1 43000 Cys Recur EARLIEST 40797 20/05/2128 EIC: 2013-08-18 Category: AD Status: TERMINATED Rev: 00 737-57-1293 WINGS - LEADING EDGE AND LEADING EDGE DEVICES - FUEL DRAIN PATH MODIFICATION Frog: 1 EARLIEST WO 19498 23/09/2013 Rev: 00 NC Total Hours: 4627:55 NC Total Cycles: 1706 REF WORK ORDER 19498 EFTA_R1_00012840 EFTA01734572 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.7001BBJ1 NC SIN: 30884 DocumenVSB EJC Description: Print Date 07/09/2016 13:59 Page: 81 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2013-15-16 737-52A1167 Category: AD Status: OPEN Rev: 0 DOORS - MAIN LANDING GEAR - INBOARD DOORS - INSPECTION OF INBOARD MLG DOOR HINGE FITTINGS FOR FATIGUE CRACKING Freq: I 10000 Cys 7797 12/01/2038 Recur EARLIEST E/C: 2013-15-17 AMP 2013-15-17 OPS TEST DETECT AND CORRECT LOSS OF THE Manual Compliance 25/11/2013 Rev: 00 28-050.00-01 ENGINE FUEL SUCTION FEED CAPABILITY NC Total Hours: 4737:05 NC Total Cycles: 1747 Category: AD 28-AWL-101-01 AD HAS BEEN COMPLIED AS PER AMP. Status: OPEN 28-AWL-101-02 Rev: 00 Recur EARLIEST Freq: 1 EIC: 2013-15-17 OPS TEST 2013-15-17 AMP Detect and correct loss of the engine fuel 7500 Hrs 6454:10 WO 20186 08/0812014 Rev: 00 28-050-00-01 suction feed capability NC Total Hours: 5107:40 NC Total Cycles: 1870 Category: AD 28-AWL-101-01 1095 Dys 334 8- TASK WORK ORDER 20186.-00-01 UNDER ROUTINE REF TO TASK 737-2050 Status: OPEN 28-AWL-101.02 07/08/2017 Rev: 00 Recur EARLIEST Freq: 1 E/C: 2013-18-09 Category: AD Status: N/A Rev: 03 1152682-23-A22 1152682-23-A22 R01 CF-2013-25 DETECT AND CORRECT DISCREPANCIES OF THE BATTERY WIRING INSTALLATION INSIDE THE ELT TRANSMITTER UNIT Superseded By: 2014-17-02 Reason Frog: AD NOT APPLICABLE. AFFECTED P/N NOT INSTALLED. EARLIEST EFTA_R1_00012841 EFTA01734573 NC Actual Compliance Last NC: A6DFR Type/Serlos: 6737-700/66J1 EIC (Category: AD) Arrant NO Doeument/SB NC S/N: 30884 E/C Description: Print Date 07/09/2016 13:59 Page: 82 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2013-t9-03 Cate gory: AD Status: N/A Rev: 00 737-29-1113 Detect and correct possible damage caused by insufficient separation between the wire bundles and hydraulic tubing Reason Freq: I NOT APPLICABLE FOR THIS AIRCRAFT BY THE EFFECTIVITY LIST OF SB 737-29-1113 EARLIEST EC: 2013-19-04 Category: AD Status: OPEN Rev: 00 737-53-1294 FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BS 540 - SKIN INSPECTION. CHORD SPLICE INSTALLATION AND SKIN REPAIR Froq: 1 18000 Cys Recur EARLIEST 15797 08112/2059 E/C: 2013-19-23 Category: AD Status: TERMINATED Rev: 00 FAA AD 2013-19-23 UPDATE INSPECTION REQUIREMENTS TO DETECT FATIGUE CRACKING OF PRINCIPAL STRUCTURAL ELEMENTS (PSE) Reason Freq: 1 AD COMPLIED WITH ON THE NEW AMP REVISION (SEP 2014). EARLIEST Manual Compliance 05/10/2013 Rev: 00 NC Total Hours: 4631:15 NC Total Cycles: 1710 AD REQUIREMENT HAS BEEN INCORPORATED IN 737 AMP REV01. EIC: 2013-23-04 Category: AD Status: OPEN Rev: 00 737-53-1296 FUSELAGE - PASSENGER CABIN FLOORS - STATION 7276 SPLICE STRAP 7000 Cys INSTALLATION Once EARLIEST Freq: 1 4797 26/10/2029 EFTA_R1_00012842 EFTA01734574 NC Actual Compliance Last NC: A6DFR Type/Series: B737.700IBBJ1 EIC (Category: AD) Arrant NO DoeumenVSB NC S/N: 30884 E/C Description: Print Date 07/09/2016 13:59 Page: 83 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2013-24-13 Category: AD Status: TERMINATED Rev: 01 737-53-1244 737-53-1244 RI 737-53-1244 R2 737.53.1244 R3 737-53-1244 R4 737-53-1244 R5 PASSENGER CABIN FLOORS - STA 520 TO 540 - PIVOT LINK ASSEMBLY REPAIR/REPLACE Superseded By: 2015-02-26 EARLIEST WO 13578 05/12/2013 Rev: 00 NC Total Hours: 4753:45 NC Total Cycles: 1755 PART A AND B OF SB 737-53-1244 CARRIED OUT UNDER WORK ORDER 13578 DTD 15/04/2010. Freq: I EIC: 2013-26-08 737-30-1058 ARCING. SMOKE. AND FIRE IN THE FLIGHT WO 19804 04/02/2014 Rev: 00 737-30-1058R04 DECK. NC Total Hours: 4841:40 A/C Total Cycles: 1785 Category: AD 737-30-1058R05 Terminating Action Has Been Performed Status: TERMINATED Rev: 00 EARLIEST Freq: 1 EIC: 2014-0142 2011-0090 OXYGEN - OXYGEN MASK REGULATOR 2014.0142 R1 INFLATABLE HARNESS/INFLATION HOSE - IDENTIFICATION / REPLACEMENT Category: AD MC10.35.274 Status: N/A Rev: 01 LATEST Reason Freq: 1 N/A BY INSTALLED PART NUMBER BC: 2014-03-19 Category: AD Status: N/A Rev: 00 BOEING SB B737-53-0011 FAA 2014-03-19 FUSELAGE - CORRECT CRACKS IN THE IN-FLIGHT ENTERTAINMENT SYSTEM RADOME ASSEMBLY Reason Freq: I N/A- THE AIRCRAFT IS NOT MODIFIED BY STC ST0028480 AND ST02887AT LATEST EFTA_R1_00012843 EFTA01734575 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DoeumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 84 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/DysIDte Next Due Last Compliance Information E/C: 2014-05-27 Category: AD Status: N/A Rev: 00 Testing and calibration of the alignment of the transponders Reason Freq: I AFFECTED P/N NOT INSTALLED. EARLIEST E/C: 2014-05-30 2013-07-07 STABILIZERS - HORIZONTAL STABILIZER 737-55-1093 REAR SPAR ATTACH PINS - INSPECTION/REPLACEMENT 56000 Cys 53797 Category: AD Status: OPEN 23112/2163 Rev: 00 Once EARLIEST Freq: 1 E/C: 2014-08-11 737-32-1376 INSP MAIN LANDING GEAR - FORWARD 737-32-1448 INSP TRUNNION PIN INSPECTION AND REPLACEMENT Category: AD Status: N/A Rev: 00 LATEST Reason Freq: 1 N/A BY VARIABLE NUMBER OF THE AIRCRAFT IN THE SB EFFECTIVITY E/C: 2014.13.07 737-33-1146 PREVENT DIRECT LIGHTNING STRIKE. Category: AD 2190 Dys 1440 Status: OPEN 17/08/2020 Rev: 00 Once EARLIEST Freq: 1 EFTA_R1_00012844 EFTA01734576 NC: A6DER E/C (Category: AD) Anent NO A/C Actual Compliance Last Type/Series: 8737-70043Bit NC S/N: 30884 Document/SB EIC Description: Print Date 07/09:2016 13.59 Page: 85 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information EJC 2014-13-10 Category: AD Status: NIA Rev: 0 737-28-1312 INSTALLATION OF INCORRECT WIRE SUPPORT CLAMPS WITHIN THE BAY AREA OF THE LEFT AND RIGHT ENVIRONMENTAL CONTROL SYSTEMS (ECS) - INSPECTION / REPLACEMENT Reason Freq: I N/A BY VARIABLE NUMBER OF THE AIRCRAFT IN THE SB EFFECTIVITY LATEST EJC: 2014-15.12 Category: AD Status: OPEN Rev: 00 737-55-1090 STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR TERMINATION FITTING - INSPECTION Frog: 1 36000 Cys Once EARLIEST 33797 21/03/2109 E!C: 201416.14 Category: AD Status: TERMINATED Rev: 0 737-22A1215 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 22, AUTO FLIGHT.AUTOTHROTTLE TO ENTER LANDING FLARE RETARD MODE PREMATURELY ON APPROACH. Rev 1 EARLIEST WO 20202 2510812014 Rev: 0 NC Total Hours: 5133:25 NC Total Cycles: 1878 SB737-22A1215 C/OUT ON 08/08/2014 UNDER WO 20202 EIC: 2014-17-02 Category: AD Status: N/A Rev-. 00 1152682-23-A22 2013-15-07 2013-18-09 HONEYWELL ELTS MODEL RESCU 406AF AND 406AFN WITH PINS 1152682-1, -2, AND -3. Reason Fres: 1 THE NC IS NOT FITTED WITH HONEYWELL ELTS PINS 1152682-1, -2, AND -3 AS LISTED IN THE AD. THE AD IS N/A BY INSTALLED P/N EARLIEST EFTA_R1_00012845 EFTA01734577 NC Actual Compliance Last NC: A6DFR Type/Series: 6737-700/BBJ1 EIC (Category: AD) Arrant NO Document/SB NC SIN: 30884 E!C Description: Print Date 07/09/2016 13:59 Page: 86 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2014-20-06 Category: AD Status: TERMINATED Rev: 0 737.31.1471 Prevent loss of flight-critical information displayed to the flightcrew Freq: I EARLIEST WO 20138 15/10/2014 Rev: 0 NC Total Hours: 5239:40 NC Total Cycles: 1901 SB 737-31-1471 CARRIED OUT ON 01/03/2014. REF WORK ORDER 20138. ESC: 2014-20-11 Category: AD Status: N/A Rev: 00 2011-07-05 2012-0038 90-25-2012 EQUIPMENT/FURNISHINGS - SICMA SEATS - DETECT AND CORRECT CRACKS IN THE BACKREST LINKS. Reason Freq: 1 N/A BY SEAT MODEL INSTALLED LATEST ESC: 2015-0093 Category: AD Status: N/A Rev: 00 EASA AD NO. 2015-0093 NAVIGATION - ATTITUDE HEADING REFERENCE SYSTEM - MODIFICATION / REPLACEMENT Reason Freq: 1 THIS AD IS NOT APPLICABLE BY THE PART NUMBER OF THE INSTALLED COMPONENTS. LATEST E/C: 2015-02-26 Category: AD Status: TERMINATED Rev: 0 737-53-1244 737-53-1244 RS PASSENGER CABIN FLOORS - STA 520 TO 540 - PIVOT LINK ASSEMBLY REPAIR! REPLACEMENT Reason Freq: 1 TERMINATED PER SB 737.53.1244 /AD 2013.24.13 WITH WO 13578 ON 12 MAI 2013. EARLIEST Manual Compliance 25/02/2015 Rev: 0 NC Total Hours: 5472:20 NC Total Cycles: 1975 TERMINATED: COMPLIED THE FOLLOWING SB 737-53-1244 / AD2013-24-13 AS PER WO13578 DATED 12 MAY 2013 EFTA_R1_00012846 EFTA01734578 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 DocumenVSB E/C Description: Print Date 07/09/2016 13:59 Page: 87 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2015-08-07 Category: AD Status: OPEN Rev: 00 MXH-35-240 OXYGEN SYSTEM - FLIGHT CREW OXYGEN MASK REGULATOR INFLATABLE HARNESS/HOSE • INSPECTION/REPLACEMENT Frew I 730 Dys 15(06/2017 Dte Once EARLIEST 281 15/06/2017 E/C: 2015-08-09 Category: AD Status: N/A Rev: 00 737-53A1325 FUSELAGE - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION/MOD Reason Free: 1 N/A BY VARIABLE NUMBER PER SB 737-53A1325 EFFECTIVITY LIST. LATEST EX: 2015-10-51 3418183 Category: AD Status: N/A Rev: 00 AD 2015-10-51 AVIDYNE !FOS DISPLAYING INCORRECT COURSE DEVIATION INDICATION INFORMATION DURING GPS APPROACHES Reason Frew I AD 2015-10-51 IS NOT APPLICABLE TO THIS AIRCRAFT BY THE INSTALLED PART NUMBER EARLIEST E/C: 2015-16-01 39-18226 Category: AD Status: TERMINATED Rev: 00A 737-21-1165 737-31A1332 AD 2012-19-11 LOSS OF CABIN ALTITUDE WARNING DURING A LACK OF CABIN PRESSURIZATION Superseded By: 2015.21.11 Frog: 1 LATEST EFTA_R1_00012847 EFTA01734579 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB FJC Description: Print Date 07/09/2016 13:59 Page: 88 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 2015-16-04 39-18229 Category: AD Status: N/A Rev: 00 AD 2015-16-04 KIDDE GRAVINER HAND-OPERATED FIRE EXTINGUISHERS Reason Freq: I THIS NC IS NOT FITTED WITH KIDDE GRAVINER FIRE EXTINGUISHERS PN 56412-0011-002,56411-001. AD IS NA BY INSTALLED P/N EARLIEST EIC: 2015-19-03 Category: AD Status: CANCEL Rev: 01 2015.21.10 28-AWL-MOV AD 2015-19-03 ENGINE FUEL SHUTOFF VALVE - POSITION INDICATION OPERATIONAL CHECK Superseded By: 2015.21.10 Reason Free: i AIRWORTHINESS LIMITATIONS SECTION 28-AWL-MOV UPDATE REQUIREMENT EARLIEST E/C: 2015.21.08 39-18301 Category: AD Status: N/A Rev: 00 DETECT AND CORRECT CRACKS IN THE INSPAR UPPER SKIN AND REAR SPAR UPPER CHORD Reason Free: 1 THE AD IS APPLICABLE TO 737-100. -200, -200C, -300. -400. AND -500. HENCE NA FOR THIS AIRCRAFT EARLIEST E/C: 2015.21.10 Category: AD Status: TERMINATED Rev: 00 28-AWL-MOV 737-28-1314 AD 2015-21-10 ENGINE FUEL SHUTOFF VALVE - POSITION INDICATION OPERATIONAL CHECK Freq: i EARLIEST Manual Compliance 22/11/2015 Rev: 00 NC Total Hours: 5827:25 NC Total Cycles: 2098 AMP 28-AWL-MOV IS INCLUDED IN AMP REV 04 DATED NOVEMBER 2015 BUT SET TO NOT APPLICABLE AS SB 737-28-1314 WAS ALREADY INCORPORATED UNDER WO 50175 ON 22-AUG-2015. EFTA_R1_00012848 EFTA01734580 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB E/C Description: Print Date 07/09/2016 13:59 Page: 89 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dta Next Due Last Compliance Information E/C: 2015-21-11 39-18304 Category: AD Status: TERMINATED Rev: 00 2012.19.11 2015-16-01 737.21.116583 737-31A1332R4 AD 2015-21.11 LOSS OF CABIN ALTITUDE WARNING DURING A LACK OF CABIN PRESSURIZATION Freq: I LATEST Manual Compliance 12/11/2015 Rev 00 NC Total Hours: 5817:55 NC Total Cycles: 2086 TERMINATED: RELATED SB 737-31A1332 HAS BEEN INCORPORATED AS PER W020202 DTD 8/8/2014. E/C: 2015-23-09 Category: AD Status: TERMINATED Rev: OOA MCF-SBU-35-001 OXYGEN - OXYGEN MASK REGULATOR - INSPECTION FOR POTENTIAL DEFAULT CALIBRATION Reason Frog: 1 ALL AFFECTED REGULATORS INSPECTED PER VSB MCF-SBU-35-001 AND ADJUSTED IF NECESSARY. EARLIEST Manual Compliance 02/02/2016 Rev: OOA NC Total Hours: 5887:00 NC Total Cycles: 2120 ALL AFFECTED REGULATORS HAS BEEN INSPECTED AS PER VSB MCF-SBU-35-001. E/C: 2016-0024 Category: AD Status: N/A Rev: 00 FIRE PROTECTION - OPTICAL AND AMBIENT SMOKE DETECTORS - IDENTIFICATION / REPLACEMENT Reason Freq: 1 N/A BY INSTALLED PART NUMBER. EARLIEST E/C: 2016-0044 Category: AD Status: N/A Rev: 00 FIRE PROTECTION - ENGINE AND AUXILIARY POWER UNIT AUTOMATIC FIRE EXTINGUISHERS - INSPECTION/OVERHAUL Reason Freq: 1 P/N NOT INSTALLED. LATEST EFTA_R1_00012849 EFTA01734581 NC: A6DFR E/C (Category: AD) Anent NO NC Actual Compliance Last Type/Series: B737.700IBBJ1 NC SIN: 30884 Document/SS FJC Description: Print Date 07/09/2016 13:59 Page: 90 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2016-04-06 39-18400 Category: AD Status: OPEN Rev: 00 DETECTION AND CORRECTION OF LATENT EQUIPMENT COOLING SYSTEM AND LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM FAILURES Freq: I 01/02/2017 Dte Recur EARLIEST 01/02/2017 E/C: 2016-04-20 Category: AD Status: TERMINATED Rev: 00 ENGINE FUEL FEED SYSTEM - MOTOR OPERATED VALVE P/N MA20A1001.1 REPLACEMENT Reason Freq: 1 RECORDS CHECKED: P/N MA20A1001.1 NOT INSTALLED AND DEACTIVATED FROM TRAX. EARLIEST Manual Compliance 26/05/2016 Rev: 00 NC Total Hours: 6068:15 A/C Total Cycles: 2179 PN: MA20A1001-1 IS NOT INSTALLED AND DEACTIVATED FROM TRAX EIC: 2016-07-16 39-17717 Category: AD Status: OPEN Rev: 00 2013-26-08 737-30-1058R05 ICE AND RAIN PROTECTION - ARCING, SMOKE. AND FIRE IN THE FLIGHT DECK IN WINDOW NUMBER 2 Freq: 1 09/02/2018 Dte Once EARLIEST 09/02/2018 E/C: 2016-11-20 39-18547 Category: AD Status: N/A Rev: 00 OXYGEN SYSTEM - PROTECTIVE BREATHING EQUIPMENT (PBE) P/N 119003-11 - INSPECTION/REPLACEMENT Reason Free: 1 THE ACFT IS NOT FITTED WITH PBE P/N 119003.11. AD IS N/A BY PART NUMBER INSTALLED. LATEST EFTA_R1_00012850 EFTA01734582 NC: A6DFR EIC (Category: AD) Arrant NO NC Actual Compliance Last Type/Series: B737.700/BBJ1 NC SIN: 30884 Document/SB EJC Description: Print Date 07/09/2016 13:59 Page: 91 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 2016-13-16-HFEC Category: AD Status: OPEN Rev: 00 2016-13.16 737.SSA1097 STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR UPPER CHORD - (G) (2) HIGH FREQUENCY EDDY CURRENT (HFEC) 11/08/2017 Dte Recur EARLIEST 11/08/2017 E/C: 2016-13-16-INS Category: AD Status: OPEN Rev: 00 2016-13-16 737-55A1097 STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR UPPER CHORD - (G) (1) INSPECTION FOR CONFIGURATION Freq: 1 11/08/2017 Dte Once EARLIEST 11/08/2017 WO 50505 07/02/2016 Rev: 00 NC Total Hours: 5887:00 NC Total Cycles: 2120 737-55A1097-INS HFEC INSPECTION PERFORMED UNDER EC 737-55A1097-INS / WO 50505 DURING THE A CHECK ON 07-02-2016 AND FOUND SATISFACTORY EIC: 2016-18-01 INSP Category: AD Status: OPEN Rev: 0 737-32-1448 INSP TO DETECT AND CORRECT HEAVY CORROSION AND CHROME DAMAGE OF THE FORWARD AND AFT TRUNNION PIN ASSEMBLIES AND THE RIGHT AND LEFT MLGS. WHICH COULD RESULT IN CRACKING OF THESE ASSEMBLIES AND COLLAPSE OF THE MLGS Freq: 1 Recur EARLIEST EIC: 2016-18-01 LUBE Category: AD Status: OPEN Rev: 0 737-32-1448 LUBE TO DETECT AND CORRECT HEAVY CORROSION AND CHROME DAMAGE OF THE FORWARD AND AFT TRUNNION PIN ASSEMBLIES AND THE RIGHT AND LEFT MLGS, WHICH COULD RESULT IN CRACKING OF THESE ASSEMBLIES AND COLLAPSE OF THE MLGS Freq: I Recur EARLIEST EFTA_R1_00012851 EFTA01734583 NC Actual Compliance Last NC: A6DFR Type/Series: B737.7001BBJ1 NC SIN: 30884 EC (Category: AD) Arrant NO Document/SS E/C Description: Print Date 07/09/2016 13:59 Page: 92 of 92 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 Schedule Remaining! Hrs/CysiDysiDte Next Due Last Compliance Information EC: 2016-18-01 MOD Category: AD Status: PENDING Rev: 0 TO DETECT AND CORRECT HEAVY CORROSION AND CHROME DAMAGE OF THE FORWARD AND AFT TRUNNION PIN ASSEMBLIES AND THE RIGHT AND LEFT MLGS. WHICH COULD RESULT IN CRACKING OF THESE ASSEMBLIES AND COLLAPSE OF THE MLGS Freq: I Recur EARLIEST EFTA_R1_00012852 EFTA01734584 P/N Compliance Print PIN: CFM56.7-827/83 PIN Description: GE AIRCRAFT ENGINE CFM! P/N SIN: 876170 Installed NC: A6DFR Amont NO Document/SB SC Description: PIN Hours: 12214:09 PIN Cycles: 4113 Schedule Remaining/ HrslCyslDyslDte Next Due Print Date 10105/2016 11 37 Page: 1 of 5 Days: 5830 Installed Date: 05/08/2013 Compliance Document Remarks 1998-14-51T Category: AD Status: N/A Rev: 00 CFP.156-7B-72-130 CFM56.78-72-132 STARTER GEARSHAFT REPLACEMENT AND MCD INSPECTION Reason NM AS THIS ENGINE IS NOT IN THE AFFECTED ENGINE ON LIST LATEST 1998-18-51 1958-21-23 UNCOMMANDED ENG ACCELERATION I INFLT SHUTDOWN 98-18.51 Category: AD TERMINATED CN 98.350 Superseded By: 1908-21-23 Status: CN T98-350 Reason Rev: 0 SB 72-0130, S80132 SUPERSEDED BY 1998.21.23 LAI b S 1 T98-18-51 1998-19-20 89-162(8) STARTER GrelaSHAFT REPLACEMENT AND hICO INSPECTION Category: AD Status: NIA Reason Rev: 00 NABY MAU PN EA11LIESI 1998-21-23 CFM56-7B-73-A024 EEC SOFTWARE VER 7B.11(7838) Category: AD Status: NIA Reason Rev: 1 N/A BY EEC SOFTWARE PN EARLIEST 2000-12.01 2002-13-03 CFM56 SELECTED CRITICAL LIFE LIMITED PARTS INSP Category: AD Status: TERMINATED Superseded By: 2002-13-03 Rev: 3 EARLIEST 2001-02-12 SB CFM58-78 72-0075 INSPECT PS3 LINE FITTING WO 2104 11102/2001 Rev: 1 Hours Cycles Days Category: AD EIC Reset At: 0:00 0 0 Status: TERMINATED CFM58-78-VS8-75-005 INSPECTED IAW Rev: 01 CFM56-78-VS8-75-005 ON EARLIEST 11/02/2001 REFER TWO 2104 EFTA_R1_00012853 EFTA01734585 P/N Compliance Print P/N: CFM56.7-B27/83 PIN Description; GE AIRCRAFT ENGINE CFM! P/N S/N: 876170 Installed NC: ABDFR Ament NO Document/SB BC Description: PIN Hours: 12214:09 PIN Cycles: 4113 Schedule Remaining/ Hrs/CyslDyslDte Next Due Print Date 10105/2016 11 37 Page: 2 of 5 Days: 5830 Installed Date: 05/08/2013 Compliance Document Remarks 2001-11-05 Category: AD Status: NIA Rev: 1 SB 72.0329 REPLACEMENT OF NO.4 ROLLER BEARING P/N 305-355.717-0 IN DEFECTIVE BATCH Reason WA BY ENGINE SW LARLi6ST 2002-13.03 Category: AD Status: OPEN Rev: 2A CFMS6.76-72.241 LIFE LIMITED ROTATING PART FAILURE Reason NEXT PIECE PART OPPORTUNITY Recur 29/08/2002 Rev: 2 Hours Cycles Days E/C Reset At: 0:00 0 0 TR 05-0035:0036.0037 AND 0038 TO TIME LIMITS CD INSERTED IN NC LAPTOP BAG ALONG WITH BOOKLINK CD. REF TRANSMITTAL LETTER. 2002-16-18 39-12857 Category: AD Status: TERMINATED Rev: I CFM56-78-72-241 REPLACEMENT OF 2ND AND 3RD STAGE LOW PRESSURE TURBINE NOZZLE SEGMENTS LARLIEST EARLIEST RO 49757 07/04/2013 Rev: 1 Hours Cycles Days E/C Reset At: 10375:39 3530 4703 RECEIVING PROCESS SB 72-0241 FOUND EMBODIED DURING SHOP VISIT DTD MARCH 2013. 2003-03-01 Category: AD Status: TERMINATED Rev: 2 2006.26-01 39.14859 Category: AD Status: N/A Rev: 0 2011-18-10 737.7181462 AFT ENGINE MOUNT. CENTER LINK ASSY INSTALLATION INSPECTION Superseded By: 201148-10 24/12/2003 Rev: 2 Hours Cycles Days E/C Reset At: 0:00 0 0 C/OUT DURING IC CHK AT KLM. REF TO FILE #3 OF CHK PACK 24/12/2003 Rev: 2 Hours Cycles Days E/C Reset At: 0:00 0 0 60 8-71A1462 C/OT DURING "I C" CHECK AT KLM. REF TO FILE NO 3 OF CHK PACK (KLM JOB CARD NO 90-M90003C) FUEL FILTER REPLACEMENT ( FOR PIA PARTS) EARLIEST EFTA_R1_00012854 EFTA01734586 P/N Compliance Print P/N: CFM56-7-B27/B3 PIN Description: GE AIRCRAFT ENGINE CFM: P/N SIN: 876170 Installed NC: A6DFR Ament NO Document/SB SC Description: PIN Hours: 12214:09 P/N Cycles: 4113 Schedule Remaining/ HrsiCyslDyslDte Next Due Print Date 10105/2016 11 37 Page: 3 of 5 Days: 5830 Installed Date: 05/08/2013 Compliance Document Remarks 2008-03-09 2007-0104 TRF WITH TANGENTIAL STRUTS - MANDATORY INSPECTIONS - LIFE TIMES 19/02/2008 Rev: 2 39-15359 CFM56.7E-72-0558 19000 Cys 18510 Hours Cycles Days Category: AD CFP.1S6.7B-72.0579 E/C Reset At: 0:00 0 0 Status: OPEN 13/01/2067 AD REPEAT INSPECTION Rev: 3 Recur IS BEING CONTROLLED EARUEST THROUGH SB CFM56-78-72-0579. AD CLOSED. 20094009 2010-01-05 LPT REAR FRAME - LIFE LIMIT / MANDATORY INSPECTION CFM56-76-72-0558 19000 Cys 18510 Category: AD CFA,I56-7B-72-0579 Status: OPEN 13/01/2067 Rev: 1 Recur EARLIEST 2009-0270 CFM56-7B-72-0743 LPT ROTOR STATOR ASSEMBLY - REPLACEMENT Category: AD Status: N/A Reason Rev: 0 LPT STD 3 DISK INSTALLED IS NOT AFFECTED BY THIS AD EARLIEST 2010-13.09 CFM56-7B-72-0743 LPT DISK • REMOVE FROM SERVICE SUSPECT 39-16340 DISKS Category: AD Status: N/A Reason Rev: 0 LPT DISKS INSTALLED IN PPRJ ENGINES ARE NOT AFFECTED EARUEST EFTA_R1_00012855 EFTA01734587 P/N Compliance Print PIN: CR156-7-627/83 PIN Description: GE AIRCRAFT ENGINE CFM! P/N SIN: 876170 Installed NC: A6DFR Ament NO Document/SB E/C Description: PIN Hours: 12214:09 P/N Cycles: 4113 Schedule Remaining/ HrslCysiDyslDte Next Due Print Date 10/0512016 11 37 Page: 4 of 5 Days: 5830 Installed Date: 05/080013 Compliance Document Remarks 2011-18-10 39-16792 Category: AD Status: TERMINATED Rev: 3 2003-02-01 737-71A1462 737.71A1462-1 AFT ENGINE MOUNT -CENTER LINK ASSY • INSPECTION TO ENSURE CORRECT INSTALLATION Reason DURING ENGINE CHANGE (REF INOPISM4 OT. 26-MAY-201I) S8 liANGAFt MMHG WAS NARKED IA.W. SS 737.71A1482 R3 EARLIEST 12110/2011 Rev: 0 Hours Cycles Days E/C Reset At: 9388:29 320500 4331 DETAILED INSPECTION IN ACCORDANCE WITH SB 737-71A1462, TO DETERMINE IF THE CENTER LINK ASSEMBLY OF THE AFT ENGINE MOUNT IS INSTALLED CORRECTLY. HAS BEEN ACCOMPLISHED ON PFIRJ ENGINES AS FOLLOWS: 6- ESN 876170 - CPAI DURING 1C CHECKAT KLM - REF FILE #3 OF CHECK PACKAGE DT: 24-DEC-2003 NO FURTHER ACTION IS REQUIRED. 2012-0209 Category: AD Status: OPEN Rev: 0 2013-26-01 CFM56-78-72-0564 CFM56-7B-72-0879 ACCESSORY GEARBOX (AGB) HANDCRANKING PAD MODIFICATION Once EARLIEST 2013-26-01 Category: AD Status: N/A Rev: 0 2012-0209 CFM56-7B-72-0564 CFM56-7B-72.0879 INDEPENDENT INSPECTION OF THE AGB HANDCRANKING PAD COVER R oston NOT AFFECTED DUE TO CURRENTLY HAVING INSTALLED AGES Pal 340846.50,10 2014-0130 Category: AO Status: N/A Rev: 0 CFM56-76 ESPJ Time Limits- Engine Stationary Pans - Life Limits! Mandatory Inspections Reason NO CFM56-IS STATIONARY PART IN PF OR RJ FLEET HAS PREVIOUSLY OPERATED ON ENGINE TYPE OR MODEL WITH DIFFERENT LIFE LIMIT EARLIEST EFTA_R1_00012856 EFTA01734588 P/N Compliance Print PIN: CFM1156.7-B27/83 PIN Description; GE AIRCRAFT ENGINE CFM; PIN SIN: 876170 Installed NC: A6DFR Amen/ NO Document/SB ec Description: PIN Hours: 12214:09 P/N Cycles: 4113 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Print Date 10/05/2016 11 37 Page: 5 of 5 Days: 5830 Installed Date: 05/08/2013 Compliance Document Remarks 2014-0261 Category: AD Status: TERMINATED Rev: 01 CR156-79-73-0204 ENGINE FUEL & CONTROL - ENGINE ELECTRONIC CONTROL - SOFTWARE UPDATE Reason FADEC SW UPGRADE IS DONE PER CFIA:45-78-73-0204 SATISFIES THE INTENT OF THIS AD EARLIEST 2015-0133 Category: AD Status: NIA Rev: 00A CFM56-7B-72-0964 ENGINE - ACCESSORY GEARBOX GEARSHAFT - NSPECTION I FtEPLACEMENT Reason THE ENGINE IS NOT INCLUDED IN THE AFFECTED ENGINE SN UST OF THE AD EARUEST 2015-04.02 Category: AD Status: TERMINATED Rev: 00 CFM56-715-73-0204 DUAL ENGINE THRUST INSTABILITY EVENT Reason CFM56-76-734204 COMPLIED (INSTALUWEIN OF LATEST FADEC SOFTWARE VERSION T.E.WF2) SATISFY THE AD REQUIREMENT LATEST 2015-18-04 Category: AD Status: N/A Rev: 01 CFM56-7B-72.0964 73-TOOTH GEARSHAFT LOCATED IN THE ENGINE ACCESSORY GEARBOX (AGB) Reason THE ENGINE is NOT INCLUDED IN THE EFFECTED UST PER CCM 58 72-0904 LATEST EFTA_R1_00012857 EFTA01734589 P/N Compliance Print P/N: CFM56.7-827/83 PIN Description: GE AIRCRAFT ENGINE CFM! PIN SIN: 889151 Installed NC: A6DFR Amon/ NO Document/SB SC Description: PIN Hours: 5999:05 P/N Cycles: 2160 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Print Date 10/05/2016 11:35 Page: 1 05 Days: 5597 Installed Date: 12/01/2001 Compliance Document Remarks 1998-14-51T Category: AD Status: N/A Rev: 00 CFP.156-7B-72-130 CFM56.78-72-132 STARTER GEARSHAFT REPLACEMENT AND MCD INSPECTION Reason WA AS THIS ENGINE IS NOT IN THE AFFECTED ENGINE SM LIST LATEST 1998-18-51 1958-21-23 UNCOMMANDED ENG ACCELERATION I INFLT SHUTDOWN 98-18.51 Category: AD TERMINATED CN 98.350 Superseded By: 1908-21-23 Status: CN T98-350 Reason Rev: 0 SB 72-0130, 580132 SUPERSEDED BY 1998.21.23 LAIEST T38-18-51 1998-19-20 89-162(8) STARTER Grol2SHAFT REPLACEMENT AND MCD INSPECTION Category: AD Status: NIA Rev: 00 EAMLIESI 1998-21-23 CFM56-7B-73-A024 EEC SOFTWARE VER 78.11(7838) Category: AD Status: NIA Reason Rev: 1 WA BY EEC SOFTWARE PN EARLIEST 2000-12.01 2002-13-03 CFM56 SELECTED CRITICAL LIFE LIMITED PARTS INSP Category: AD Status: TERMINATED Superseded By: 2002-13-03 Rev: 3 EARLIEST 2001-02-12 SB CFM56-78 72-0075 INSPECT PS3 LINE FITTING Category: AD Status: N/A Rev: 01 EARLIEST EFTA_R1_00012858 EFTA01734590 P/N Compliance Print P/N: CFM56.7-B27/83 PIN Description: GE AIRCRAFT ENGINE CFM! PIN SIN: 889151 Installed NC: ABDFR Anent NO Print Date 10/05/2016 11:35 Page: 2 or 5 Schedule Remaining/ Document/SB BC Description: HrslCys/Dys/Dte Next Due Compliance Document Remarks PIN Hours: 5999:05 P/N Cycles: 2160 Days: 5597 Installed Date: 12/01/2001 2001-11-05 Category: AD Status: NIA Rev: 1 SB 72.0329 REPLACEMENT OF NO.4 ROLLER BEARING PIN 305-355.717-0 IN DEFECTIVE BATCH Reason WA BY ENGINE SIN LARLILSI 2002-13.03 Category: AD Status: OPEN Rev: 2A CFM56.76-72.241 LIFE LIMITED ROTATING PART FAILURE Recur 2002-16-18 39-12857 Category: AD Status: N/A Rev: 1 CFM56-7B-72-241 REPLACEMENT OF 2ND AND 3RD STAGE LOW PRESSURE TURBINE NOZZLE SEGMENTS EARLIEST 2003-03-01 Category: AD Status: TERMINATED Rev: 2 2011.18.10 737-71A1462 AFT ENGINE MOUNT. CENTER LINK ASSY INSTALLATION INSPECTION Superseded By: 2011.18.10 EARLIEST 09/05/2003 Rev: 2 Hours Cycles Days EIC Reset At 1103:35 595.00 847 COMPLIED BY BOEING REPAIR STATION BACR668L. RECORDS WERE REVIEWED NO ENGINE CHANGE OCCURED. REFER U17 AC/ STATEMENT AT DELIVERY TO PRESIDENTIAL FLIGHT. 2006.2601 39.14859 Category: AD Status: NIA Rev: 0 FUEL FILTER REPLACEMENT ( FOR PMA PARTS) EARLIEST EFTA_R1_00012859 EFTA01734591 P/N Compliance Print P/N: CFM56-7-B27/83 PIN Description: GE AIRCRAFT ENGINE CFM; PIN S/N: 889151 Installed NC: A6DFR Amen NO Document/SB E/C Description: PIN Hours: 5999:05 P/N Cycles: 2160 Schedule Remaining/ Hrs/Cys/Dys/Dte Next Due Print Date 10/05/2016 11:35 Page: 3 of 5 Days: 5597 Installed Date: 12/01/2001 Compliance Document Remarks 2008-03-09 39-15359 Category: AD Status: OPEN Rev: 3 2007-0104 CHASE-78-72-0558 CFMS6.78-72.0579 TRF WITH TANGENTIAL STRUTS - MANDATORY INSPECTIONS - LIFE TIMES 19000 Cys Recur EARLIEST 16840 18/06/2062 19/02/2008 Rev: 2 Hours Cycles Days E/C Reset At: 1294:57 687.00 2594 AD REPEAT INSPECTION IS BEING CONTROLLED THROUGH SB CFM56-78-72-0579. AD CLOSED. 2009-0009 Category: AD Status: N/A Rev: 1 2010-01.05 CFM56-76-72-0558 CFM56-7B-72.0579 LPT REAR FRAME - LIFE LIMIT !MANDATORY INSPECTION Reason LPT REAR FRAME RN 340-186-206-0 INSTALLED IS NOT AFFECTED BY THIS AD EARLIEST 2009-0270 Category: AD Status: N/A Rev: 0 CFM56-78-72-0743 LPT ROTOR STATOR ASSEMBLY • REPLACEMENT Reason LPT STG 3 DISK INSTALLED IS NOT AFFECTED BY THIS AD EARUEST 2010-13-09 39-16340 Category: AD Status: N/A Rev: 0 CFM56-78-72-0743 LPT DISK - REMOVE FROM SERVICE SUSPECT DISKS Reason tPT DISKS INSTALLED IN PE/RI ENGINES ARE NOT AFFECTED EARLIEST EFTA_R1_00012860 EFTA01734592 PIN: CFM1156-74127433 Amens NO P/N Compliance Print PIN Description: GE AIRCRAFT ENGINE CFM! PIN SIN: 889151 Installed NC: A6DFR Document/SB BC Description: AFT ENGINE MOUNT - CENTER LINK ASSY • INSPECTION TO ENSURE CORRECT INSTALLATION Print Date 10/05/2016 11:35 Page: 4 of 5 Schedule Remaining/ HrslCyslDyslDte Next Due Compliance Document Remarks PIN Hours: 5999:05 PIN Cycles: 2160 Days: 5597 Installed Date: 12/0112001 2011-18-10 39-16792 Category: AD Status: TERMINATED Rev: 3 2012-0209 Category: AD Status: OPEN Rev: 0 2013-26.01 2003-03-01 737-71A1462 737.71A1462-1 Reason COMPLIANCE OF AD 20030341. ENGINE HAS NOT BEEN CHANGED EARLIEST 2013-26-01 CFM56.76-72-0564 CFM56.76-72.0879 ACCESSORY GEARBOX (AGO) HAND-CRANKING PAD MODIFICATION Once Category: AD Status: TERMINATED Rev: 0 2014-0130 Category: AO Status: N/A Rev: 0 2012-0209 CFM56.78.72-0564 CFM56-78-72-0879 INDEPENDENT INSPECTION OF THE AGO HANDCRANKING PAD COVER Reason AD SATISFIED BY AIAMENOINO AFFECTED ALP TASK (72.320-01O2 AND 72.070-01102) TO INCLUDE INDEPENDENT INSPECTION TO VERIFY Tyne Lints - Engine Stationary Pans - Life Limits I Mandatory Inspections CROSS-2B ESM EARLIEST Reason NO EflA56-78 STATIONARY PART IN PF OR RJ FLEET HAS PREVIOUSLY OPERATED ON ENGINE TYPE OR MODEL DEFERENT LIFE umiT EARLIEST 12110/2011 Rev: 0 Hours Cycles Days E/C Reset At: 2824:25 1186.00 3925 DETAILED INSPECTION IN ACCORDANCE WITH SB 737-71A1462, TO DETERMINE IF THE CENTER LINK ASSEMBLY OF THE AFT ENGINE MOUNT IS INSTALLED CORRECTLY. HAS BEEN ACCOMPLISHED ON PFIRJ ENGINES AS FOLLOWS: 12-ESN 889151 - CM UNDER TFtAX WO # 12361 DT: 29-APR-2008 NO FURTHER ACTION IS REQUIRED. EFTA_R1_00012861 EFTA01734593 P/N Compliance Print PIN: CFM1156.7-B27/83 PIN Description: GE AIRCRAFT ENGINE CFM; P/N SIN: 869151 Installed NC: A6DFR Amen/ NO Document/SB ec Description: PIN Hours: 5999:05 P/N Cycles: 2160 Schedule Remaining/ HrslCys/Dys/Dte Next Due Print Date 10/05/2016 11:35 Page: 5 of 5 Days: 5597 Installed Date: 12/01/2001 Compliance Document Remarks 2014-0261 Category: AD Status: TERMINATED Rev: 01 CR156-78-73-0204 ENGINE FUEL & CONTROL - ENGINE ELECTRONIC CONTROL - SOFTWARE UPDATE Reason FADEC SW UPGRADE IS DONE PER CFM5648-734204 SATISFIES THE INTENT OF THIS AD EARLIEST 2015-0133 Category: AD Status: NIA Rev: 00A CFM56-7B-72-0964 ENGINE - ACCESSORY GEARBOX GEARSHAFT - NSPECTION I FtEPLACEMENT Reason THE ENGINE IS NOT INCLUDED IN THE AFFECTED ENGINE SAN UST OF THE AD EARUEST 2015-04.02 Category: AD Status: TERMINATED Rev: 00 CFM56-78-73-0204 DUAL ENGINE THRUST INSTABILITY EVENT Reason CFM56-76-734204 COMPLIED (INSTALULTION OF LATEST FADEC SOFTWARE VERSION 7.0.WF2) SATISFY THE AD REQUIREMENT LATEST 2015-18-04 Category: AD Status: N/A Rev: 01 CFM56-7B-72.0964 73-TOOTH GEARSHAFT LOCATED IN THE ENGINE ACCESSORY GEARBOX (AGB) Reason THE ENGINE IS NOT INCLUDED IN THE EFFECTED UST PER CCM 58 72-0544 LATEST EFTA_R1_00012862 EFTA01734594

Forum Discussions

This document was digitized, indexed, and cross-referenced with 1,400+ persons in the Epstein files. 100% free, ad-free, and independent.

Donate More ways to support →

Annotations powered by Hypothesis. Select any text on this page to annotate or highlight it.