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NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Ament NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
BC: 1974-08-09 25120-00-01 WASTE RECEPTACLE DOOR INSPECTION. 1000 Hrs 632:35 WO 50175 22/08/2015 Rev: 16
39-9680 25-130-00-01 NC Total Hours: 5786:05 NC Total Cycles: 2071
Category: AD 25400-60020
Status: OPEN 254000-DVI.10000.1 20/07/2017
Rev: 16 254000-DVI.10010.1 Recur
EARLIEST
254012-0080
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
EARLIEST
Superseded By: 1991.1042
Reason Frog: I
AD NOT APPLICABLE AS NC IS NOT
EQUIPPED WITH WITH A CLASS B MAIN
DECK CARGO COMPARTMENT.
EFTA_R1_00012761
EFTA01734493
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NC: A6DFR Type/Series: 8737.700438,11 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Ament NO Document/SB E/C Description: HrslCyslDyslDte Next Due Last Compliance Information
BC: 1990-25-01 0626A001-MRBR CORROSION PREVENTION CONTROL
PROGRAM
Category: AD
Status: OPEN
Rev: 0 Once
EARLIEST
Reason Freq: 1
FAA AMOC 120549487 DTD. 4-FEB-2010,
APPROVES MRB COMPLIANCE WITH
CPCP, REQUIREMENTS INCORPORATED
INTO AMP.
E/C: 1991-10-02 1989-18.12 CLASS B MAIN DECK CARGO
394986 COMPARTMENT
Category: AD
Status: N/A
Rev: 2
EARLIEST
Superseded Sy: 1993-07-15
Reason Frog: I
AD NOT APPLICABLE. NO CLASS B MAIN
DECK CARGO COMPARTIMENT
INSTALLED.
E/C: 1993-07-15 1989-18.12 CLASS B MAIN DECK CARGO
39-8547 1991-1002 COMPARTMENT
Category: AD
Status: N/A
Rev: 2
LATEST
Reason Freq: 1
THE AIRCRAFT IS NOT EQUIPPED WITH
CLASS B MAIN DECK CARGO
COMPARTMENT. HENCE, AD IS WA.
BC: 1997-22.07 TO PREVENT SUDDEN DECOPMRESSION
OF THE AIRPLANE
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
SUPERSEDED BY AD 2002-07-08
EFTA_R1_00012762
EFTA01734494
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NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Ament NO DoeumenVSB BC Description: Hrs/CyslDyslDte Next Due Last Compliance Information
BC: 1998-02-01 UNCOMMANDED YAWING OF AIRCRAFT
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
EIC: 1998-02-51 INSPECTION OF HORZ STAB FOR
STRUCTURAL INTEGRITY
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
AD AFFECT MODEL 737-300. -400. -500
SERIES AIRPLANES. THE AD IS N/A FOR
737-700 AIRCRAFT
BC: 1998-03-09 DEFECTIVE AILERONS INSPECTION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
AD AFFECT MODEL 737-100, -200. - 300,
-400. AND -500 SERIES AIRPLANES. THE AD
IS N/A FOR 737-700 AIRCRAFT
EIC: 1998-03-10 737-25-1334 PILOTS SEAT LOCK .4 SEAT TRACK
39-10079 OPERATIONS CHK.
Category: AD
Status: N/A
Rev: 2
EARLIEST
Reason Frog: I
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-25-1334
EFTA_R1_00012763
EFTA01734495
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NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO DoeumenVSB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 1998-04.41 MAIN DECK CARGO DOOR & FUSE UPPER
JAMB INSPECTION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
AD AFFECT MODEL 737-200. -300 SERIES
AIRPLANES. THE AD IS N/A FOR 737-700
AIRCRAFT
EIC: 1998-07-16 INTERCHANGING LOCATION OF HYD FUSE
& FLOW LIMITER.
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
AD AFFECT MODEL 737-300. -400. AND -500
SERIES AIRPLANES. THE AD IS N/A FOR
737-700 AIRCRAFT
E/C: 1998-10-51 INSP OF FUEL BOOST PUMP WIRING IN THE
FUEL TANKS
Category: AD
Status: N/A
Rev: 2
EARLIEST
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
E/C: 1998-10-511 FUEL BOOST PUMP WIRING IN FUEL TANKS
INSPECTION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: i
N/A - BY ACFT MODEL. APPL TO B737-100
TO -500.
EFTA_R1_00012764
EFTA01734496
Print Date 07/09/2016 13:59
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NC: A6DFR Type/Series: 8737.7001138J1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
AmeM NO Document/SB EIC Description: Hrs/CyslDyslDte Next Due Last Compliance Information
EIC: 1998-11-04 ENSURE THE CONTINUED STRUCTURAL
INTERGRITY
Category: AD
Status: N/A
Rev: 02
LATEST
Reason Freq: 1
AD AFFECT MODEL 737.100, -200 SERIES
AIRPLANES. THE AD IS N/A FOR 737-700
AIRCRAFT
EIC: 1998-11-51 REMOVAL OF FUEL BOOST PUMP WIRING &
DVL
Category: AD
Status: N/A
Rev: 2
EARLIEST
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
EIC: 1998-11-51T REMOVAL OF FUEL BOOST PUMP WIRING &
DVI.
Category: AO
Status: N/A
Rev: 01
EARLIEST
Reason Frog; 1
N/A - BY ACFT MODEL. APPLICABLE TO
5737-100 TO -500.
EIC: 1998-11.52 REMOVAL OF FUEL BOOST PUMP WIRING.
Category: AD
Status: N/A
Rev: 1
EARLIEST
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
EFTA_R1_00012765
EFTA01734497
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NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Ament NO DoeumenVSB EJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 1998-13-12 PREVENT LOSS OF RUDDER CONTROL.
Category: AD
Status: N/A
Rev: 01
EARLIEST
Reason Freq: I
AD AFFECT MODEL 737-100. -200. -200C. -
300, -400, AND -500 SERIES AIRPLANES.
THE AD IS NIA FOR 737-700 AIRCRAFT
E/C: 1998-14-09 FWD ENGINE MOUNTS SUPPORT FITTING &
ATTACHEMENTS
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
AD AFFECT MODEL 737-100. -200. 200C
SERIES AIRPLANES. THE AD IS N/A FOR
737-700 AIRCRAFT
BC: 1998-18-20 REPLACE JC CARTER FUEL S/OFF VALVE.
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
BC: 1998-19-09 FUEL BOOST PUMP & WIRING CHAFING
CHK.
Category: AD
Status: CANCEL
Rev: 1
EARLIEST
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
EFTA_R1_00012766
EFTA01734498
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NC Actual Compliance Last Page: 7 of 92
NC: A6DFR Type/Series: B737.700IBB/1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO DocumenVSB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 1998-21-11 APU & ENGINES FIRE DETECTOR
ASSEMBLIES
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
E/C: 1998-22-10 FUSE FWD SERVICE DOORWAY. AFT
FRAME INSPECTION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
AD AFFECT MODEL 737-100. -200. -200C.-
300, AND -400 SERIES AIRPLANES. THE AD
IS N/A FOR 737-700 AIRCRAFT
EIC: 1998-25-06 DOOR FRAME & CROSS BEAMS OF AFT
CARGO DOOR INSP.
Category: AD
Status: N/A
Rev: 1
EARLIEST
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
EFTA_R1_00012767
EFTA01734499
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NC Actual Compliance Last Page: 8 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO DoeumenVSB EJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
BC: 1998-26-24 TO PREVENT FAILURE OF THE WHEEL
FLANGES
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
AD AFFECT MODEL 737-100, -200 SERIES
AIRPLANES. THE AD IS N/A FOR 737-700
AIRCRAFT
E/C: 1999-01-16 TO PREVENT DAMAGE TO AIRFRAME.
HSTAB, ENGINES.
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
E/C: 1999-03-04 TO PREVENT POSSIBLE IGNITION OF FUEL
VAPOURS.
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
AD AFFECT MODEL 737-100, -200. - 300,
-400. AND -500 SERIES AIRPLANES. THE AD
IS N/A FOR 737-700 AIRCRAFT
EIC: 1999-03-08 SB737-73A1011 FUEL HOSE QUICK
DISCONNECT-INSPECTION 1 TERMINATION
Category: AD
Status: N/A
Rev: 01
EARLIEST
Superseded By: 2002.1421
Reason Frog: I
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-73A1011
EFTA_R1_00012768
EFTA01734500
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NC: A6DFR Type/Salves: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO DoeumenVSB FJC Description: Hrs/Cys/DyslDte Next Due Last Compliance Information
E/C: 1999-04-11 TO PREVENT DAMAGE OF AFT STRUT
INSUL BLANKETS.
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
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
Print Date 07/09:2016 13.59
A/C Actual Compliance Last Page: 10 of 92
NC: A6DER Type/Series: B737-70043BJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Anent NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
EX: 1999-05-15 ELEVATOR TAB PUSH ROD.
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
EX: 1999-08-03 SB 737-24-1128 PANELS POWER DISTRIBUTION P91 & P92 -
PREVENTION OF FAILURE
Category: AD
Status: N/A
Rev: 01
EARLIEST
Reason Freq: 1
AD IS N/A BY THE EFFECTMTY LIST OF
BOEING SB 737-24-1128
EIC: 1999-08-21 PAX 02 MASKS & PORTABLE 02 MASKS
39-11130
Category: AD
Status: N/A
Rev: 3
EARLIEST
Reason Free: 1
THE AIRCRAFT IS NOT FITTED WITH
PURITAN BENNET OXYGEN MASKS . AD IS
N/A BY INSTALLED P/N.
EIC: 1999-08-23 TO DETECT & CORRECT FATIGUE
CRACKING
Category: AD
Status: NIA
Rev: 1
EARLIEST
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
EFTA_R1_00012770
EFTA01734502
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NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 1999-10-12 TO DETECT 8 CORRECT CORROSION AND
CRACKING
Category: AD
Status: N/A
Rev: 1
EARLIEST
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
E/C: 1999-10-13 SE1737-27A1228 S245 TRAILING EDGE FLAP LIMIT SWITCH
Category: AD
Status: N/A
Rev: 2
EARLIEST
Reason Frog: 1
INFOR AD IS NOT APPLICABPLE TO THIS
NC EFFECTIVITY OF SB AND YG039 IN NOT
AFFECTED BY SB
E/C: 1999-11-05 737-27A1222 RUDDER PCU SECONDARY SLIDE Manual Compliance 26/02/2001 Rev: 2
39-11175 DISPLACEMENT TEST NC Total Hours: 1103:35 NC Total Cycles: 595
FOUND ACCOMPLISHED ON 26/02/2001 AS PER
Category: AD LHT REPORT AT DELIVERY
Status: TERMINATED
Rev: 2
LATEST
Frog: 1
BC: 1999-12-08 TO PREVENT OPENING OR LOSS OF THE
CARGO DOOR
Category: AD
Status: N/A
Rev: 01
EARLIEST
Reason Frog: 1
AD AFFECT MODEL 737-200C SERIES
AIRPLANES. THE AD IS N/A FOR 737-700
AIRCRAFT
EFTA_R1_00012771
EFTA01734503
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NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO Document/SS EJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 1999-13-51 CN1999-259-IMP(B TO PREVENT REDUCED CONTROLLABILITY
SB 737-55A1068 OF ACFT
Category: AD
Status: N/A
Rev: 01
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
Print Date 07/09:2016 13.59
A/C Actual Compliance Last Page: 13 of 92
NC: A6DER Type/Series: B737-700188,11 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
UC (Category: AD) Schedule Remaining!
Anent NO Document/SR EJC Description: Hrs/CyslDyslDte Next Due Last Compliance Information
FJC: 1999-18-01 ELEVATOR TAB
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 14 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Ament NO DocumenVSB FJC Description: Hrs/Cys/DyslDte Next Due Last Compliance Information
E/C: 1999-21-15 TO DETECT 8 CORRECT CHAFING &
PREVENT ELECTRICAL
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
E/C: 1999-22-16 SB 737-52-1137 FLIGHT DECK DOOR • DECOMPRESSION
PANEL
Category: AD
Status: N/A
Rev: 01
EARLIEST
Reason Freq: 1
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-52-1137
EJC: 1999-23-20 TO PREVENT A SHORT CIRCUIT
Category: AD
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
PC: 1999-23-22 PREVENTION OF FALSE ADVISORIES DUE
TO INACCURATE AIRPLANE ALTITUDE
REPOARTING
Category: AD
Status: N/A
Rev: 2
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 15 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Ament NO DoeumenVSB E/C Description: Hrs/Cys/DyslDte Next Due Last Compliance Information
BC: 1999-24-06 INSPJREPL. OF BREATHER PLUG IN FUEL
TANK BOOST PUMPS
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
EIC: 1999-24.08 PREVENTION OF FAILURE OF ALL
ELECTRICALLY POWERD AIRPLANE
SYSTEMS
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
EIC: 1999-25-02 TO PREVENT THE LINKAGE BETWEEN THE
RATIO CHANGER I
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
AD AFFECT MODEL 737-100, -200. - 300,
-400. AND -500 SERIES AIRPLANES. THE AD
IS N/A FOR 737-700 AIRCRAFT
EIC: 1999-26-07 TO PREVENT FAILURE OF THE
SECONDARY SUPPORT TO SU
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
AD AFFECT MODEL 737-100, -200, AND
-200C SERIES AIRPLANES. THE AD IS N/A
FOR 737-700 AIRCRAFT
EFTA_R1_00012775
EFTA01734507
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 16 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO Document/SS EJC Description: Hrs/Cys/DysIDte Next Due Last Compliance Information
BC: 1999-26-10 PREVENTION OF WATER ACCUMLATION IN
THE LOWER CORNERS OF THE FLIGHT
DECK EMERGNCY EXITS.
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
BC: 1999-26-21 SB737.29A1077 INSP/REPL OF WIRE BUNDLES AND
HYDRULIC HOSES
Category: AD
Status: N/A
Rev: 02
EARLIEST
Reason Freq: i
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-29A1077
E/C: 2000-02-03 TO PREVENT FATIGUE CRACKING OF THE
ROD ENDS ON THE
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
AD AFFECT MODEL 737-300, -400. -500
SERIES AIRPLANES. THE AD IS N/A FOR
737-700 AIRCRAFT
BC: 2000-02-18 TO PREVENT A REDUCED RATE OF
MOVEMENT OF THE ELEV
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: I
AD AFFECT MODEL 737-100, -200. - 300,
-400, AND -500 SERIES AIRPLANES. THE AD
IS N/A FOR 737-700 AIRCRAFT
EFTA_R1_00012776
EFTA01734508
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 17 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO DoeumenVSB FJC Description: Hrs/Cys/DysIDte Next Due Last Compliance Information
E/C: 2000-03-05 REPLACEMENT OF THE EMERGENCY
FLOOR PATH LIGHTING
SYSTEM
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
AD AFFECT MODEL 737-200 SERIES
AIRPLANES. THE AD IS N/A FOR 737-700
AIRCRAFT
EIC: 2000-04-02 TO PREVENT FUEL SUCTION FEED
OPERATION ON BOTH ENGI
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
E/C: 2000-04-08 TO DETECT & CORRECT CRACKING IN
CERTAIN FUSELAGE F
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frew 1
AD AFFECT MODEL 737-200C SERIES
AIRPLANES. THE AD IS N/A FOR 737-700
AIRCRAFT
EIC: 2000-05-13 TO PREVENT FRACTURE OF THE MLG AXLE
8 THE SEPARAT
Category: AD
Status: N/A
Rev: 1
EARLIEST
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
EFTA_R1_00012777
EFTA01734509
Print Date 07/09:2016 13.59
A/C Actual Compliance Last Page: 18 of 92
NC: A60FR Type/Series: 8737-700/3Bit NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Anent NO Document/SB BC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
EIC: 2000-05-29 TO DETECT FATIGUE CRACKING OF THE
FORWARD PRESSUR
Category: AD
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 19 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO Document/SS EJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
BC: 2000-07-09 M-7200-00-00931 ELEVATOR PCU INSPECTION
SWCB73-27-001
Category: AD
Status: N/A
Rev: 01
EARLIEST
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.
E/C: 2000-07-27 HG2030AD-34-A0009 ADIRU MOD STATUS CONFIRMATION
HG2050AC-34-A0008
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
E/C: 2000-080 (8) MODE NC AND S TRANSPONDER
Category: AD
Status: CANCEL
Rev: 2
EARLIEST
Superseded By: 2008-0285
Freq: 1
E/C: 2000-08-08 M-7200-00-01063 REAR SPAR INSPECTION AND
SB 737-57-1253 MODIFICATION
Category: AD
Status: N/A
Rev: 01
EARLIEST
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.
EFTA_R1_00012779
EFTA01734511
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 20 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/0812016
EIC (Category: AD) Schedule Remaining/
Anent NO DoeumenVSB EJC Description: HrfaCysalysiDte Next Due Last Compliance Information
BC: 2000-08-17 TO PREVENT DAMAGE TO THE TAXI FIGHT
ASSEMBLY
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
EIC: 2000-10-21 M-720040-01370 FLIGHT CREW SEATS
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
AD AFFECT MODEL 737-300. -400. -500
SERIES AIRPLANES. THE AD IS N/A FOR
737-700 AIRCRAFT
E/C: 2000-13-51 MAIN DECK CARGO DOOR FRAMES
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Free: 1
AD AFFECT MODEL 737-200, - 300 SERIES
AIRPLANES. THE AD IS N/A FOR 737-700
AIRCRAFT
BC: 2000-14-02 M-7200-00-01744 PLACARD INSTALLATION PREVENT LOSS
SB 737-23A1170 OF VHF COMM.
Category: AD
Status: N/A
Rev: 01
EARLIEST
Reason Free: 1
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-23A1170
EFTA_R1_00012780
EFTA01734512
Print Date 07/09:2016 13.59
A/C Actual Compliance Last Page: 21 of 92
NC: A60FR Type/Series: 8737-700438,H NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Anent NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
EX: 2000-14-13 DOOR HANDLE
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
AD AFFECT MODEL 737-200, - 300. -400.
AND -500 SERIES AIRPLANES. THE AD IS
N/A FOR 737-700 AIRCRAFT
EX: 2000-15-12 737-55A1071 HORZ STAB FRONT SPAR INSP.
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
AD AFFECT MODEL 737-100. -200 SERIES
AIRPLANES. THE AD IS N/A FOR 737-700
AIRCRAFT
E/C: 2000-15-16 737.35.1049 PAX OXY MASK
Category: AO
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
AD IS N/A BY THE EFFECTMTY LIST OF
BOEING SB 737-35-1049
E/C: 2000-15.18 KRUGER FLAP INSPECTION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: .1
AD AFFECT MODEL 737-100. -200 SERIES
AIRPLANES. THE AD IS N/A FOR 737-700
AIRCRAFT
EFTA_R1_00012781
EFTA01734513
Print Date 07/09:2016 13.59
A/C Actual Compliance Last Page: 22 of 92
NC: A60FR Type/Series: 8737-700/SEW NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Anent NO Document/SS E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
EX: 2000-19-05 ELEVATOR TAB PUSH ROD
Category: AD
Status: N/A
Rev: 1
EARLIEST
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
EX: 2000-22.02 2000-22-02 R1 UNCOMMANDED RUDDER NON-NORMAL Manual Compliance 23/10/2010 Rev: 2
SWCB73-00-001 PROCEDURE NC Total Hours: 2223:50 NC Total Cycles: 998
PF REMARK: THE INTENT OF THIS AD HAS BEEN
Category: AD INCORPORATED INTO AFM. REFER TO LHT AD
Status: TERMINATED STATUS.
Rev: 2
EARLIEST
Fin: 1
EJC: 2000-23-34 PREVENT SEVERE ASSYMETFtIC THRUST
CONDITION DURING FLIGHT
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Free: 1
AD AFFECT MODEL 737-300, -400. -500
SERIES AIRPLANES. THE AD IS N/A FOR
737-700 AIRCRAFT
E/C: 2000-25-07 OUTBOARD FLAP, INBOARD FLAP TRACK
INSPECTION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason From: 1
AD AFFECT MODEL 737-100, -200, -200C
SERIES AIRPLANES. THE AD IS N/A FOR
737.700 AIRCRAFT
EFTA_R1_00012782
EFTA01734514
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 23 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB FJC Description: Hrs/CyslDyslDte Next Due Last Compliance Information
E/C: 2001-01-13 TO DETECT 8 CORRECT CHAFING & TO
PREVENT ELECTRICL
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
NOT AFFECTED TO NC MODEL
B737-600...-900
E/C: 2001-02-01 FWD PRESSURE BLKHEAD INSP
Category: AD
Status: N/A
Rev: 1
EARLIEST
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
E/C: 2001.023(AB) CN 2001-023(AB) FM IMMUNITY Manual Compliance 12/01/2001 Rev: 2
CN2001-023(AB) NC Total Hours: 1103:35 NC Total Cycles: 595
ALL RJ EQUIPMENT COMPLIES WITH THE FM
Category: AD IMMUNITY REQUIREMENTS.
Status: TERMINATED
Rev: 2
EARLIEST
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.
E/C: 2001.04.08 EC 83-55A1072 INSPECTION OF ELEVATOR TAB HINGE &
SB737-55A1072 ELEVATOR TAB CONTROL MECHANISM
Category: AD SWC 87355001
Status: CANCEL
Rev: 01
EARLIEST
Superseded By: 2001-08-09
Frog: i
EFTA_R1_00012783
EFTA01734515
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 24 of 92
NC: A6DFR Type/Series: 8737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO Document/SB E/C Description: Hrs/Cys/Dys!Dte Next Due Last Compliance Information
BC: 2001-06-08 SB 737-55-1067 INPEC OF ELEVATOR HINGE PLATE
Category: AD
Status: N/A
Rev: 01
EARLIEST
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.
E/C: 2001-06-15 737-55A1064 INSP OF FASTENERS IN THE ELEVATOR
BALANCE PANEL ASSEMBLIES.
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq:
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-55A1064
E/C: 2001.08.07 TO DET & CORRCT CRACKING OF
UPORTION M/DECK CGO
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
SUPERSEDE BY AD 2004-03-23
EIC: 2001.08.09 BO NO: B3.55A1072 INSPECTION OF ELEVATOR TAB HINGE & Manual Compliance 01/12/2002 Rev: 2
39-12186 SB 737-55A1072 ELEVATOR TAB CONTROL MECHANISM NC Total Hours: 1103:35 NC Total Cycles: 595
COMPLIED WITH AMOC SB 737.55A1080 BY
Category: AD SWC 87355001 BACR668L (AD 2003-03-22) REFER TO LMT AD
Status: TERMINATED STATUS AT DELIVERY
Rev: 2
EARLIEST
Frog: I
EFTA_R1_00012784
EFTA01734516
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 25 of 92
NC: A6DFR Type/Salves: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2001-08-24 SWCB73-28-002 REVISE FLIGHT MANUAL TO PROHIBIT Manual Compliance 19/11/2002 Rev: 1
EXTENDED DRY OPERATION OF Center NC Total Hours: 1103:35 NC Total Cycles: 595
Tank Fuel Pumps COMPLIED BY BOEING REPAIR STATION
Category: AD BACR668L, REFER TO LHT AD STATUS AT DELIVERY
Status: TERMINATED
Rev: 1
EARLIEST
Freq: I
E/C: 2001-09-15 TO PREVENT INFLIGHT SEPERATION OF
THE M/D CGO DOOR
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
N/A - BY ACFT MODEL. APPLICABLE ON
B737-200/-300.
E/C: 2001.09.51 SB 737-27A1245 ELEVATOR TAB CONTROL RODS Manual Compliance 14/03/2002 Rev: 01
NC Total Hours: 1103:35 NC Total Cycles: 595
ACTION TAKEN DURING CABIN COMPLETION.
Category: AD ACCOMPLISHED ON 14 MAR. 2002. REFER LHT AD
Status: TERMINATED STATUS AT DELIVERY.
Rev: 01
EARLIEST
Frog: 1
EIC: 2001.10.14 B3-35-1077 INSP OF CHEM OXYGEN GEN 8/OR PAX.
ATTENDANT OR LAV SERVICE UNIT
M7200-00-02474
ASSEMBLIES
Category: AD SWCB73-35-003
Status: N/A
Rev: 2
EARLIEST
Reason Freq: 1
NOT APPLICABLE ACC. BOEING REPAIRE
STATION BACR668L LOG BOOK ENTRIES
FOR NON APPLICABLE AD'S. REFER LHT
DELIVERY
EFTA_R1_00012785
EFTA01734517
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 26 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO Document/SB E/C Description: Hrs/Cys/Dys!Dte Next Due Last Compliance Information
E/C: 2001-11-07 B3-29A1081 INSP REPLACEMENT OF
SB737.29A1082 MOTOR-OPERATED HYDRAULIC SHUTOFF
VALVES
Category: AD
Status: N/A
Rev: 01
EARLIEST
Reason Freq: I
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-29A1082
E/C: 2001-11-11 737-25-1371 PREVENTION OF UNRESTRAINED
737-25-1407 MOVEMENT OF PASSENGER
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Froq: 1
AD IS NIA BY THE EFFECTIVITY LIST OF
BOEING SB 737-25-1371 AND SB
737-25-1407
E/C: 2001.12.51 REV TO AFM TO PROHIBIT AIRPLANE
SPEEDS ABOVE 300K
39-12294
Category: AD
Status: N/A
Rev: 2
EARLIEST
Reason Frog:
AD 2001-12-51 AFFECT B737-800 AIRCRAFT
ONLY. AD IS N/A TO ROYAL JET BBJS BY
AIRCRAFT MODEL
E/C: 2001-13-07 SB737-28-1180 TEST ELECTRICAL CIRCUITS THAT CLOSE
WITH SPAR SOV
39-12287
Category: AD
Status: N/A
Rev: 01
EARLIEST
Reason Freq: 1
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-28-1160
EFTA_R1_00012786
EFTA01734518
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 27 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO Document/SS FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
BC: 2001-13-23 M-7200-O1.01608 BOLT ATTACH AFT PRESS BULKHEAD
39-12305 SB 737-53-1212
Category: AD
Status: N/A
Rev: 01
EARLIEST
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.
E/C: 2001-14-05 M-7200-01-00756 ELEVATOR TAB REPAIR Manual Compliance 01/12/2002 Rev: 1
LIMITS/PROCEDURE NC Total Hours: 1103:35 A/C Total Cycles: 595
CO IE WITH AMOC SB & AD
Category: AD 2003M
-03-
PL22D. REFER LHT AD STATUS
737-55A10
ATDELIVERY
Status: TERMINATED
Rev: 1
EARLIEST
Freq: i
BC: 2001-14-06 TO DETECT & CORRECT DISCRP LOCATED
IN WN/W
Category: AO
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
SUPERSEDED NOT AFFECTED TO NC
MODEL
BC: 2001.14.10 REMOVE ELECTRICAL POWER FROM IFE
SYS WHEN NECESS
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: I
NOT AFFECTED TO NC MODEL
B737-600...-900
EFTA_R1_00012787
EFTA01734519
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 28 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO DocumenVSB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2001-14-12 M-7200-01-01648 PES MODIFICATION
ST09104AC-D
Category: AD STC ST09100AC-D
Status: N/A STC ST09105AC-D
Rev: 1 STC ST09106AC-D
EARLIEST
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.
E/C: 2001-14-20 WINGS CENTER WING BOX FLOOR BEAM
INSP & MOD REP
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
NOT AFFECTED TO NC MODEL
B737-600...-900
E/C: 2001.15.01 737-25-1403 ESCAPE SLIDE
39-12335 737-25-1404
Category: AD
Status: N/A
Rev: 2
EARLIEST
Reason Frog: i
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-25-1403 AND SB
737.25.1404
E/C: 2001-16-06 WINGS SPARS POSSIBLE CRACKING AND
CORROSION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
NOT AFFECTED TO NC MODEL
B737-600...-900
EFTA_R1_00012788
EFTA01734520
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 29 of 92
NC: A6DFR Type/Series: 6737-700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Anent NO DocumenVSB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2001-16-11 OUTBOARD MIDFLAP ASYMMETRY
PREVENSION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
NOT AFFECTED TO NC MODEL
B737-600...-900
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 30 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Ament NO DoeumenVSB E/C Description: Hrs/Cys/Dys!Dte Next Due Last Compliance Information
BC: 2001-21-51 B3-53A1238 BS 1016 AFT PRESSURE BULKHEAD
INSPECTION
Category: AD
Status: N/A
Rev: 01
EARLIEST
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.
E/C: 2001-22-11 737-24-1128 PDP INSPECTION/REPLACEMENT
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-24-1128
E/C: 2001.22.13 747-27A2373 REPLACEMENT OF THE RUDDER PEDAL
39-12492 98-13-12R1 PUSHROD FASTENERS
Category: AD
Status: N/A
Rev: 4
LATEST
Reason Frog: 1
B737-700 AIRCRAFT ARE NOT AFFECTED
BY AD 2001.22.13. AD IS N/A BY AIRCRAFT
MODEL NUMBER.
EFTA_R1_00012790
EFTA01734522
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 31 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Ament NO Doeument/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
BC: 2001-23-01 737-55-1067 INSPECTION/REPAIR OF ELEVATOR HINGE
PLATES
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
E/C: 2001-24-33 ELECT/AUX PWR GENERATOR FEEDER
WIRE BUNDLE INSP
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
NOT AFFECTED TO NC MODEL
B737-600 -900
E/C: 2002-01.01 ELEV TAB ASSY INSP OF ELEV TAB HINGE 8
CONTRL MECH
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
SUPERSEDED NC MODEL NOT AFFECTED
EIC: 2002.02.08 WING MLG SUPPT BEAM RETAINING PIN
BOLT REPLACEMNT
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: I
NOT AFFECTED TO NC MODEL
B737-600 -900
EFTA_R1_00012791
EFTA01734523
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 32 of 92
NC: A6DFR Type/Salves: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Arrant NO DocumanVSB EJC Description: Nrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2002-04-08 B25A1383 INSPECTION/REPLACEMENT OF
39-12665 SB 737-25A1383 FASTENERS IN RUDDER PEDAL HOUSINGS
Category: AD
Status: N/A
Rev: 2
LATEST
Reason Freq: I
NOT APPLICABLE PER LINE NUMBER.
(1-295 ONLY) REFER LHT AD STATUS AT
DELIVERY TO AMIRI FLIGHT.
E/C: 2002-05-07 OUTBOARD FLAP INSPECTION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
NOT AFFECTED TO NC MODEL
B737-600 -900
EJC: 2002.06.03 SB737-27A1234 MEASUREMENT OF CLEARANCE BETWEEN
39-12679 BRACKET FOR ELEVATOR PCU AND
QUADRANT OF PCU
Category: AD
Status: N/A
Rev: 01
LATEST
Reason Frog: 1
NOT APPLICABLE PER LINE NUMBER
REFER LHT AD STATUS AT DELIVERY TO
AMIRI FLIGHT.
E/C: 2002-06-05 ATC TRANSPONDERS P/N 522-2703-XXX
Category: AD
Status: N/A
Rev: 2
EARLIEST
Reason Freq: 1
NOT APPLICABLE, AFFECTED P/N NOT
INSTALLED. REFER TO LHT AD STATUS AT
DELIVERY
EFTA_R1_00012792
EFTA01734524
Print Date 07/09:2016 13.59
A/C Actual Compliance Last Page: 33 of 92
NC: A6DFR Type/Series: 8737.700/SEW NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EX (Category: AD) Schedule Remaining!
Ament NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
EC: 2002-07-08 FUSELAGE LAP JOINT CRACKING
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
NOT AFFECTED TO A/C MODEL
8737-600 -900
E/C: 2002-07-10 FUSELAGE LAP JOINT PREMATURE
CRACKING
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason From 1
NOT AFFECTED TO NC MODEL
8737.600_. 900
E/C: 2002-07-11 FUSELAGE LAP JOINT CRACKING
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
NOT AFFECTED TO NC MODEL
8737.600_..-900
E/C: 2002.08.20 B3-20020820 ELEVATOR TAB CLEANING Manual Compliance 01/12/2002 Rev: 1
NC Total Hours: 1103:35 NC Total Cycles: 595
COMPLIED BY BOEING REPAIR STATION BACR668L
Category: AD BY AMOV SB 737-55A1080 E AD 2003-03-22. REFER
Status: TERMINATED LHT REPORT AT DELIVERY.
Rev: 1
EARLIEST
Frog: 1
EFTA_R1_00012793
EFTA01734525
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 34 of 92
NC: A6DFR Type/Series: 6737-700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Arrant NO Document/SB E/C Description: Hrs/CyslDyslDte Next Due Last Compliance Information
E/C: 2002-08-52 FIT MANUAL REV TO PROHIBIT OPERATING Manual Compliance 01/12/2002 Rev: 1
SPEEDS NC Total Hours: 1103:35 NC Total Cycles: 595
COMPLIED BY BOEING REPAIR STATION BACR668L
Category: AD AMOC SB 737.55M080. REFER LHT AD STATUS AT
Status: TERMINATED DELIVERY TO AMIRI FLIGHT.
Rev: 1
EARLIEST
Freq: I
E/C: 2002-10-11 FUELAGE AFT PRESS BLKHEAD INSP. MOD
8 REP BS 1016
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
NOT AFFECTED TO NC MODEL
B737-600....-900
SC: 2002.10.12 AILERON TAB CNTRL ROD BARREL INSP OR
REPLACEMENT
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
NOT AFFECTED TO NC MODEL
6737.600....-900
BC: 2002-14-19 ROCKWELL COLLINS ADC
Category: AD
Status: N/A
Rev: 2
EARLIEST
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.
EFTA_R1_00012794
EFTA01734526
Print Date 07/0912016 13:59
NC Actual Compliance Last Page: 35 of 92
NC: A6DFR Type/Series: 6737-700/BBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Arrant NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2002-14-20 B3-24A1150 PITOT PROBES - PREVENT ICING Manual Compliance 16/04/2002 Rev: 1
CONDITION NC Total Hours: 1103:35 NC Total Cycles: 595
ACCOMPLISHED UAW SB 737-24A1150 OM
Category: AD 16/04/2002. REFER LHT AD REPORT AT DELIVERY
Status: TERMINATED TO AMIRI FLIGHT.
Rev: 1
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
EARLIEST
Superseded By: 2005-18-23
Freq: 1
E/C: 2002-16-23 RUDDRE FEEL 8 CTR UNIT
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
EFTA_R1_00012795
EFTA01734527
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 36 of 92
NC: A6DFR Type/Series: B737-700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Amant NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2002-18-02 LATERAL TRFER MECH LWR BEARING
SUPPORT INSP/MOD
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
NOT AFFECTED TO NC MODEL
8737-600....-900
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
EARLIEST
Superseded By: 2002-19-52
Reason Frog: I
SUPERSEDED BY FAA AD 2002-19-52
E/C: 2002.19.51 2002-19-51R1 FLIGHT CONTROL MODULE RETURN
PASSAGE BLOCKAGE
M-7200-02-01435
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. NC Total Hours: 1103:35 NC Total Cycles: 595
AIRPLANE FLT MAN REVN & PLACARD 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.
LATEST
B3-20021952
EO 136291 Frog: 1
EFTA_R1_00012796
EFTA01734528
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 37 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/0812016
E/C (Category: AD) Schedule Remaining/
Anent NO Document/SB E/C Description: Hrs/Cys/DysIDte Next Due Last Compliance Information
SC: 2002-20-07 2007-03-07 INSTALLATION OF AN ENHANCED RUDDER
39-12903 737.27.1247RI CONTROL SYSTEM
Category: AD 737-27-1253
Status: CANCEL
Rev: 01
LATEST
Reason Freq: I
SUPERSEDED BY AD 2002-20-07
E/C: 2002-21-01 REPL WIRING ON BRITAX SELL WATER
BOILERS BEV MKRS
Category: AD
Status: N/A
Rev: 2
EARLIEST
Reason Freq: 1
AD IS N/A BY THE EFFECTIVITY LIST OF AD
2002-21-01
E/C: 2002.22.05 CARRIAGE SPINDLE INSPECTION
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
SUPERSEDED BY AD 2003-24-08
E/C: 2002.24.51 AD 2002-24-51 OPERATIONAL RESTRICTIONS FOR Manual Compliance 26/11(2002 Rev: 1
39-12992 AIRPLANES WITH CRANE HYDRO-AIRE NC Total Hours: 1103:35 NC Total Cycles: 595
FUEL PUMPS COMPLIED WITH AD INSERTED INTO AFM BY
Category: AD BOEING REPAIR STATION BACR688L PER
Status: TERMINATED EMERGENCY AD 2002-24-51. REFER LHT AD
Rev: 1 STATUS AT DELIVERY TO AMIRI FLIGHT.
EARLIEST
Frog: 1
EFTA_R1_00012797
EFTA01734529
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 38 of 92
NC: A6DFR Type/Series: B737.7001BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SS EJC Description: Hrs/Cys/Dys!Dte Next Due Last Compliance Information
SC: 2002-26-18 737-28A1142R3 PREVENT FLUID CONTAMINATION OF Manual Compliance 06/05/2003 Rev: 2
39-13006 B3-28A1142 FUELING FLOAT SWITCH AND CONDUIT NC Total Hours: 1103:35 NC Total Cycles: 595
ASSYS. COMPLIED BY BOEING REPAIR STATION BACR668L
Category: AD ACCOMPLISHED SB 737-28A1142. REFER LHT AD
Status: TERMINATED STATUS AT DELIVERY TO AMIRI FLIGHT.
Rev: 2
EARLIEST
Freq: I
ESC: 2003-03-01 2011.18.10 AFT ENGINE MOUNT. CENTER LINK ASSY Manual Compliance 09/05/2003 Rev: 2
737-71A1462 INSTALLATION INSPECTION NC Total Hours: 1103:35 NC Total Cycles: 595
COMPLIED BY BOEING REPAIR STATION BACR668L
Category: AD RECORDS WERE REVIEWED NO ENGINE CHANGE
Status: TERMINATED OCCURED. REFER LHT AD STATUS AT DELIVERY
Rev: 2 TO AMIRI FLIGHT.
EARLIEST
Superseded By: 2011-18-10
Freq: 1
ESC: 2003-03-05 WINGS LE SLATS ACTUATOR
REPLACEMENT
Category: AD
Status: N/A
Rev: 1
LATEST
Reason Freq: 1
N/A - BY ACFT MODEL. APPLICABLE ON
B737-300 TO -500.
E1C: 2003-03-11 SLIDE RAFT SYSTEM - NOT APPLICABLE TO
AF
Category: AD
Status: WA
Rev: 1
EARLIEST
Superseded By: 2004-03-01
Reason Freq: 1
AD NOT APPLICABLE AS AFFECTED SLIDE
RAFT SYSTEM NOT INSTALLED.
EFTA_R1_00012798
EFTA01734530
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 39 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO DocumenVSB E/C Description: Hre/Cys/Dys/Dte Next Due Last Compliance Information
BC: 2003-03-22 B3-11A1109 SPEEDBRAKE FLIGHT DETENT-SPEED Manual Compliance 01/12/2002 Rev: 1
SB 737-11A1109 LIMITATION NC Total Hours: 1103:35 NC Total Cycles: 595
COMPLIED BY BOEING REPAIR STATION BACR668L
Category: AD SB 737-55A1080. REFER LHT AD STSTUS AT
Status: TERMINATED DELIVERY TO AMIRI FLIGHT.
Rev: 1
EARLIEST
Freq: I
SC: 2003-07-12 LANDING GEAR LIFE LIMITED PARTS
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
NOT AFFECTED TO NC MODEL
B737-600....-900
E/C: 2003-08-15 FUSELAGE SKIN INSPECTION OF CROWN
SKIN LAP JOINT
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
NOT AFFECTED TO NC MODEL
B737.600....-900
BC: 2003-11-03 HYD ACCUMULATORS INSP TO DETERMINE
THE P/N
Category: AD
Status: N/A
Rev: 1
LATEST
Reason Freq: 1
N/A - BY ACFT MODEL. APPLICABLE TO
8737-100/-200.
EFTA_R1_00012799
EFTA01734531
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 40 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Ament NO DoeumenVS8 FJC Description: Hrs/Cys/Dys!Dte Next Due Last Compliance Information
EC: 2003-14-04 MODIFICATION OF THE REINFORCED
FLIGHT DECK DOOR
Category: AD
Status: N/A
Rev: 1
EARLIEST
Superseded By: 2005-12-05 MOD
Reason Freq: i
SUPERSEDED BY AD 2005-12-05
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
ALTITUDE WARNING - DONNING OF NC Total Hours: 1103:35 NC Total Cycles: 595
2008-23-07
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 41 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2003-23-05 B3-26A1109 ENGINES. APU & CARGO FIRE BOTTLE Manual Compliance 17/12/2003 Rev: 1
EO F26-A0121 HOSES INSP NC Total Hours: 1103:35 NC Total Cycles: 595
COMPLIED WITH SB 26A1109R2. EFER LHT AD
Category: AD SB737.26A1109 REPORT AT DELIVERY TO AMIRI FRLIGHT.
Status: TERMINATED
Rev: 1
EARLIEST
Freq: i
EIC: 2003-26-12 737-23A1169 VIDEO DISTRIBUTION UNITS (VDU)
CONNECTOR REPLACEMENT
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-23A1169 REVISION 02
E/C: 2003-26-14 737-SL-26-043 RECALL OF KIDDE AEROSPACE PORTABLE Manual Compliance 14/01/2004 Rev: 1
HALON 1211 FIRE EXTINGUISHERS P/N NC Total Hours: 1103:35 NC Total Cycles: 595
898052 COMPLIED BY BY REPLACED ALL 3 KIDDE
Category: AD HANDHELD HALON FIRE EXTING. REFER LHT AD
Status: TERMINATED STATUS AT DELIVERY TO AMIRI FLIGHT.
Rev: 03
EARLIEST
Frog: 1
EIC: 2004-03-01 AD 2004-03-01 AIR CRUISER SL/RAFTS - N/A TO AF
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
EFTA_R1_00012801
EFTA01734533
Print Date 07/0912016 13:59
NC Actual Compliance Last Page: 42 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SS E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2004-05-19 737-55-1086 HORIZ STAB FRONT & REAR SPAR
39-13514 BOLT/PIN INSP
Category: AD
Status: TERMINATED
Rev: 4
EARLIEST
Reason Free: I
MOD ACCOMPLISHED 8-SEP-2008 AT KLM
WITH WO #12142.
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
REF EC ET49-1: DFR IS FITTED WITH 1152426-245,
Category: AD 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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 43 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB EJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2004-11-11 737-28A1148R1 AFT BOOST PUMP WIRING SUPPORT Manual Compliance 12/11/2003 Rev: 1
39-13657 73?-28A1148R2 BRACKET INSTALLATION NC Total Hours: 1103:35 NC Total Cycles: 595
FIXED AS PER CAMP SYSTEM RECORDS ON
Category: AD 12.11.03. REFER LHT AD STATUS AT DELIVER TO
Status: TERMINATED AMIRI FLIGHT.
Rev: 1
EARLIEST
Freq: I
E/C: 2004-18-02 737-26A1118 HIGH ELECTRICAL RESISTANCE IN THE
39-13779 FIRE EXTENGUISHING SQUIB - GROUNDS
INSPECTION/CHECK
Category: AD
Status: N/A
Rev: 2
EARLIEST
Reason Freq: 1
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-26A1118
EIC: 2004.22.01 1-46753136 CARGO RESTRAINT STRAP ASSEMBLIES
39-13829
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
BC: 2004.22.27 737.54.1039 STRUT - APPLICATION OF SEALANT AT THE Manual Compliance 14/02/2003 Rev: 1
39-13855 737.54.103981 INTERFACE OF THE DIAGONAL BRACE NC Total Hours: 1103:35 NC Total Cycles: 595
FITTING AND THE AFT BULKHEAD NOT APPLICABLE ALRADY PERFORMED ACC.
Category: AD BACR668L. REFER LHT AD STATUS REPORT AT
Status: TERMINATED DELIVERY TO AMIRI FLIGHT.
Rev: 1
EARLIEST
Frog: I
EFTA_R1_00012803
EFTA01734535
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 44 of 92
NC: A6DFR Type/Series: 8737400/8B/1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Anent NO Document/SS FJC Description: Hrs/Cys/Dysl0te Next Due Last Compliance Information
E/C: 2004-23-10 737-53-1256 INSPECTION FOR PITTING AND CRACKS OF
39-13865 THE LOWER SKIN PANEL
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: i
AD IS N/A BY THE EFFECTIVITY LIST OF AD
2004-23-10
E/C: 2004-24-07 737-28-1190 FOIS - CENTER FUEL TANK WIRE SUPPORT Manual Compliance 12/06/2003 Rev: 1
39-13883 737-28-1190R1 BRACKET REPLACEMENT NC Total Hours: 1103:35 NC Total Cycles: 595
AS PER CAMP REPORT SB 737-28-1190/01 FIXED.
Category: AD REFER LHT AD STATUS REPORT AT DELIVERY TO
Status: TERMINATED AMIRI FLIGHT.
Rev: 1
EARLIEST
Froq: 1
E/C: 2005-05-18 737-53-1251 INSPECTION OF THE WEBS OF THE AFT
PRESSURE BULKHEAD FOR CRACKS 23797
39-14007 26000 Cys
Category: AD
Status: OPEN 02/11/2081
Rev: 1 Recur
EARLIEST
E/C: 2005-07-20 AUTOFLIGHT - DIGITAL FLIGHT CONTROL
39-14045 SYSTEM - FLIGHT CONTROL COMPUTER
OPERATIONAL PROGRAM SOFTWARE
Category: AD INSTALLATION - P2.0
Status: CANCEL
Rev: 0
EARLIEST
Superseded By: 2012.21.08
Reason Frog: 1
NOT APPLICABLE AFFECTED P/NO NOT
INSTALLED.
EFTA_R1_00012804
EFTA01734536
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 45 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
FJC (Category: AD) Schedule Remaining/
Ament NO DoeumenVSB FJC Description: Hrs/CyslDyslDte Next Due Last Compliance Information
SC: 2005-08-10 737.54.1040R1 STRUT - APPLICATION OF SEALANT ON
39-14062 ENGINE STRUT STRUCTURE
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Freq: I
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-54-1040
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
EARLIEST
ST01335LA Superseded By: 2007-10-12
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
EARLIEST
ST01335LA Superseded By: 2007-10-12
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 46 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Arrant NO Document/SS E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2005-18-23 2002.16-03 MLG ELECTRICAL CONNECTORS WO 50505 05/0212016 Rev: 1
39-14264 737.24-01146 CORROSION PROTECTION NC Total Hours: 5887:00 NC Total Cycles: 2120
Category: AD 730 Dys 515
Status: OPEN 04/02/2018
Rev: 1 Recur
EARLIEST
Freq: I
E/C: 2005-19-19 737-34A1801 FMC: OPS CHANGE TO VERSION U10.5A Manual Compliance 19/01/2005 Rev: 0
39-14284 NC Total Hours: 1103:35 NC Total Cycles: 595
REQUIRED SB 737-34A1801 ALREADY PERFORMED
Category: AD IAW EO 144603. REFER LHT AD STATUS REPORT AT
Status: TERMINATED DELIVERY TO AMIRI FLIGHT.
Rev: 0
EARLIEST
Frog: 1
E/C: 2005-21-06 737-53A1248 BS 1016 AFT PRESS BLKHD WEB • INSP
39-14344 FOR CRACKS AT THE Y-CHORD 25000 Cys 22797
Category: AD
Status: OPEN 06/02/2079
Rev: 0 Recur
EARLIEST
Frog: 1
E/C: 2005-23-16 737-28-1209 CWT: WIRE BUNDLE MODIFICATION Manual Compliance 08/09/2008 Rev: 0
NC Total Hours: 1469:35 NC Total Cycles: 767
ACCOMPLISHMENT OF SB 737-28-1209,
Category: AD TERMINATES AD 2005-23-16 FOUND S8 DONE ON
Status: TERMINATED 08/09/08 WO 12142.
Rev: 0
EARLIEST
Frog: 1
EFTA_R1_00012806
EFTA01734538
Print Date 07/0912016 13:59
NC Actual Compliance Last Page: 47 of 92
NC: A6DFR Type/Series: 6737-700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
BC (Category: AD) Schedule Remaining/
Amant NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2005-23-17 737-28-1200 P15 REFUEL PANEL WIRING Manual Compliance 03/01/2006 Rev: 0
39-14375 INSPECTION/MODIFICATION NC Total Hours: 1103:35 NC Total Cycles: 595
INSPECTION COMPLIED BY OPERATOR PER REF
Category: AD 01 OS SB AND AD COMPLIANCE TIME : 03-JAN-2006,
Status: TERMINATED 796FH, 465FC, REFER LHT AD STATUS AT DELIVERY
Rev: 0 TO AMIRI FLIGHT.
EARLIEST
Freq: I
E/C: 2005-24-03 2005-24-03R1 NACELLE SUPPORT FITTING ATTACHMENT 25000 Hrs 18846:30
39-14955 737-57-1275 FASTENERS INSPECTION - MEASUREMENT 22797
25000 Cys
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
EARLIEST
Superseded By: 2007-06-09
Reason Frew 1
SUPERSEDED BY AD 2007-06-09
BC: 2005-26-03 737-27A1271 ELEVATOR INPUT TORQUE TUBE Manual Compliance 03/08/2005 Rev: 0
39-14424 SWCB73-27-018 MODIFICATION NC Total Hours: 1103:35 NC Total Cycles: 595
MODIFIED IAW EO 146233. REFER LHT AD STATUS
Category: AD AT DELIVERY TO AMIRI FLIGHT.
Status: TERMINATED
Rev: 0
EARLIEST
Freq:
EFTA_R1_00012807
EFTA01734539
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 48 of 92
NC: A6DFR Type/Series: B737.7001BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining!
Arrant NO DocumenVSB EJC Description: Hrs/CyslDyslDte Next Due Last Compliance Information
E/C: 2006-0140-E 2006-0140R1 AIR CONDITIONING - ZONAL DRYING WO 12893 09/10/2008 Rev: 1
2006-0140R2 SYSTEM DEACTIVATION - EMERGENCY NC Total Hours: 1490:00 NC Total Cycles: 771
AIRWORTHINESS DIRECTIVE
Category: AD 2006.0140R3
Status: TERMINATED 2006-0140R4
Rev: 4
EARLIEST
Freq: I
ESC: 2006-0264 2001.11.11 PASSENGER SEATS REAR FITTING
747-25-3196 ASSEMBLY ATTACHMENT REPLACEMENT
Category: AD
Status: N/A
Rev: 0
EARLIEST
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.
EIC: 2006-0265 MODE S & C TRANSPONDERS • CHECK
Category: AD
Status: CANCEL
Rev: 0
EARLIEST
Superseded By: 2006-026SCN
Freq: 1
SC: 2006-0265-CN NAVIGATION SYSTEMS - MODE S AND C
TRANSPONDERS -CHECK
Category: AD
Status: CANCEL
Rev: 0
EARLIEST
Reason Freq: I
EASA CANCEL AD 2006-0265 THROUGH AD
CANCELATION NOTICE 2006-0265-CN.
EFTA_R1_00012808
EFTA01734540
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 49 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
BC: 2006-0334 2006-0334 R01 THALES COMMUNICATION VHF DATA RADIO
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: 1
THE AIRCRAFT IS NOT FITTED WITH
THALES VHF RADIOS. HENCE THE AD IS
N/A BY INSTALLED VHF RADIOS P/N.
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 50 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO Document/SB EJC Description: Hrs/Cys/DysIDta Next Due Last Compliance Information
BC: 2006-08-03 150-25-036 (SIGMA SB) SICMAAEROSEAT CABIN ATTENDANT SEAT
151-25-037 (SICMA SB) TYPE 150 & 151
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Freq: I
THE AIRCRAFT IS NOT FITTED WITH SICMA
FLIGHT ATTENDANT SEATS. HENCE THE
AD IS NIA BY INSTALLED FLIGHT
ATTENDANT SEAT
E/C: 2006-10-17 737-24A1141 P5 PANEL MODIFICATION
39-14601
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Freq:
NOT APPLICABLE BY THE EFFECTIVITY
LIST OF SB 737-24A1141
EIC: 2006-12-06 737-25-1439 DRIESSEN GALLEYS: SPIRAL WRAP
39-14631 REPLACEMENT
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Frog: 1
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737.25.1439
E/C: 2006-12-11 737-28-1199 ENGINE FUEL SHUTOFF VALVE WIRE & Manual Compliance 03/08/2005 Rev: 0
CONDUIT ASSY. REPLACEMENT NC Total Hours: 1103:35 NC Total Cycles: 595
SB 737-28-1199 REV. 00 FIXED 03.08.2005. THIS
Category: AD ACTION IS AN AMOC FOR AD 2006-12-11. REFER
Status: TERMINATED LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT.
Rev: 0
EARLIEST
Free: 1
EFTA_R1_00012810
EFTA01734542
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 51 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Arrant NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2006-13-13 2003-14-08 AIRPLANE FLIGHT MANUAL AMENDMENT - Manual Compliance 31/07/2006 Rev: 1
39-14666 2008-23-07 CABIN PRESSURIZATION NC Total Hours: 1103:35 NC Total Cycles: 595
AFM REVISION PFERFORM BY THE PREVIOUS
Category: AD CUSTOMER. REFER LHT AD STATUS AT DELIVERY
Status: TERMINATED TO AMIRI FLIGHT.
Rev: 1
EARLIEST
Freq: I
E/C: 2006-15-18 737-33-1133 M D & T WIRING SEPARATION Manual Compliance 16/03/2003 Rev: 0
NC Total Hours: 1103:35 NC Total Cycles: 595
MODIFIED lAW SB 737-33-1133 BY BACR668L
Category: AD (BOEING) ACC. DELIVERY DOCUMENTS. REFER LHT
Status: TERMINATED AD STATUS AT DELIVERY TO AMIRI FLIGHT.
Rev: 0
EARLIEST
Freq: 1
E/C: 2006-16-11 737-53-1236 AIRSTAIR DOORSTOP INTERCOSTAL -
39-14711 INSPECTION AND FASTENER
REPLACEMENT
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Freq: 1
NOT APPLICABLE ALREADY MODIFIED BY
MANUFACTURE
E/C: 2006-16-18 SANDEL AVIONICS INC. TAWS/RMI
MODIFICATION
Category: AD
Status: N/A
Rev: 0
LATEST
Reason Freq: 1
THE AIRCRAFT IS NOT FITTED WITH
SANDEL TWAS/RMI UNITS. HENCE THE AD
IS N/A BY INSTALLED P/N
EFTA_R1_00012811
EFTA01734543
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 52 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Anent NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2006-17-13 3410-25MR477R3 RECARO MODEL 3410 SEATS : SEAT BELT
ATTACHMENT BOLT REPLACEMENT
Category: AD
Status: N/A
Rev: 2
EARLIEST
Reason Freq: I
THIS AIRCSRAFT IS NOT FITTED WITH
RECARO MODEL 3410 PAX SEATS. HENCE
THE AD IS N/A BY INSTALLED SEAT MODEL
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 737-27-1273 INSP INSPECTION NC Total Hours: 5887:00 NC Total Cycles: 2120
Category: AD 737-27-1273 LUBE 730 Dys 515
Status: OPEN 04/02/2018
Rev: 0 Recur
EARLIEST
Freq: 1
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 737-27-1273 INSP AND ROD END BEARINGS LUBRICATION NC Total Hours: 5786:05 NC Total Cycles: 2071
Category: AD 737-27-1273 LUBE 365 Dys -17
Status: OPEN 21/08/2016
Rev: 0 Recur
EARLIEST
Freq: 1
E/C: 2006-26-01 FUEL FILTER REPLACEMENT ( FOR PMA
39-14859 PARTS)
Category: AD
Status: N/A
Rev: 0
EARLIEST
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.
EFTA_R1_00012812
EFTA01734544
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 53 of 92
NC: A6DFR Type/Series: 6737-700/BBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Ament NO Document/SB FJC Description: Hrs/CyslDyslDte Next Due Last Compliance Information
E/C: 2007-02-14 737-28-1225 INSPECTION / REPAIR OF ELECTRICAL Manual Compliance 12/01/2007 Rev: 0
39-14901 BOND BETWEEN THE BULKHEAD FITTING NC Total Hours: 1103:35 NC Total Cycles: 595
FOR THE FUEL FEED LINE AND THE WING INSPECTED IAW EO 150722. REFER LHT AD
Category: AD FRONT SPAR 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
ACCOMPLISHED IAW E 152499. REFER LHT
Category: AD 737-27A1280 FORCE FIGHT 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_00012813
EFTA01734545
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 54 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Ament NO Document/SB SC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2007-06-51 2007-06.52 EMERGENCY AIRWORTHINESS DIRECTIVE
- FLIGHT SPOILER ACTUATOR JAM
Category: AD
Status: N/A
Rev: 1
EARLIEST
Superseded By: 2007-06-52
Reason Freq: i
NOT APPLICALBE PER LISTED MSN IN SB
737-27A1283.
E/C: 2007-06-52 2007-06-51 EMERGENCY AIRWORTHINESS DIRECTIVE
2007-15-04 - FLIGHT SPOILER ACTUATOR JAM
Category: AD
Status: N/A
Rev: 1
EARLIEST
Superseded By: 2007-15-04
Reason Frog: 1
NOT APPLICALBE PER LISTED MSN IN SB
737-27A1283.
E/C: 2007-07-02 737-25-1545 PART 2 MODIFICATION OF THE OXYGEN
39-15002 ACTIVATION MECHANISM WITHIN THE
PASSENGER SERVICE UNITS
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Freq: i
NOT APPLICABLE AFFECTED P/NO IS NOT
FITTED
E/C: 2007-10-12 2003-14-04 INSPECTION OF DOOR WIRE HARNESSES
ON AIRPLANES EQUIPPED WITH C 8 D
2005-12-05 AMS
ZODIAC RE-INFORCED FLIGHT DECK DOOR
Category: AD 2005-12-05 MOD ASSEMBLY PN: B221001.
Status: N/A
Rev: 1
EARLIEST
Reason Frog: 1
NOT APPLICABLE AFFECTED P/NO IS NOT
INSTALLED
EFTA_R1_00012814
EFTA01734546
Print Date 07i092016 13.59
A/C Actual Compliance Last Page: 55 of 92
NC: A6DFR Type/Series: B737-7001BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Ament NO Document/SB E/C Description: Hrs/CyslDyslDte Next Due Last Compliance Information
E/C: 2007-15-04 2007-06.52 FLIGHT SPOILER ACTUATOR
39-15133
Category: AD
Status: N/A
Rev: 0
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
- INSPECTION OF SLAT TRACK DOWNSTOP
737-SL-57-084
ASSEMBLIES ON ALL LEADING EDGE
Category: AD SLATS
Status: CANCEL
Rev: 2
EARLIEST
Superseded By: 2007-18-52
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
EARLIEST
737-SL-57-084 Superseded By: 2011.06-05 INSP
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 56 of 92
NC: A6DFR Type/Serlos: 6737-700/BBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Amant NO Document/SB FJC Description: Hrs/CyslDyslDte Next Due Last Compliance Information
E/C: 2007-23-10 WHEEL WELL CONNECTORS FILLET SEAL
39-15256 INSPECTION/MODIFICATION
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Freq: I
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-24-1169
E/C: 2007-25-03 737-53A1253 FUSELAGE - GENERAL - STATION 1016 AFT
PRESSURE BULKHEAD - INSPECTION FOR 12797
15000 Cys
WEB OIL CANNING
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
LATEST
Superseded By: 2008-0097
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 57 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining!
Amant NO DoeumenVSB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
BC: 2008-01-01 FLIGHT DECK DOORS - MODIFICATION
Category: AD
Status: N/A
Rev: 1
EARLIEST
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.
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 58 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SM: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB EIC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
BC: 2008-06-03 MOD 2008-06-03 AWL ENGINE FUEL FEED SYSTEM - MOTOR Manual Compliance 16/03/2008 Rev: 0
39-15415 737-28Al207 OPERATED VALVE - ACTUATOR NC Total Hours: 1328:37 NC Total Cycles: 701
REPLACEMENT MOD PART OF AD CAN IAW SB 737-28Al207. REF
Category: AD TWO 12152 DTD 16/03/04.
Status: TERMINATED
Rev: 0
EARLIEST
Freq: I
E/C: 2008-06-27 25-343 EQUIPMENT/FURNISHINGS - EMERGENCY
EVACUATION EQUIPMENT - SLIDE RAFTS -
SHEAR PIN RESTRAINTS REPLACEMENT
Category: AD
Status: TERMINATED
Rev: 3
EARLIEST
Reason Freq: 1
ALL SLIDES MODIFIED TO P/N 5A3307.7.
EIC: 2008-08-22 737-30-1056 GRAY WATER COMPOSITE DRAIN MAST WO 12175 24/04/2008 Rev: 0
BONDING JUMPER INSTALLATION NC Total Hours: 1381:09 NC Total Cycles: 722
SB 737-30-1056 C/OUT ON 08/04/08. REF W/ORDER
Category: AD 12175
Status: TERMINATED
Rev: 0
EARLIEST
Freq: 1
BC: 2008-08-24 2012-23-08 NACELLES/PYLONS - STRUT DRAINS AND WO 13098 05/03/2009 Rev: 0
737.54.1043 SEALS -AFT FAIRING DRAIN TUBE NC Total Hours: 1751:48 NC Total Cycles: 840
ASSEMBLY REPLACEMENT B3-54-1043 SB 737-54-1043 C/OUT DURING 2A CHK
Category: AD DTD 05/03/09.
Status: TERMINATED
Rev: 1
EARLIEST
Superseded By: 2012-23-08
Freq: 1
EFTA_R1_00012818
EFTA01734550
Print Date 07/0912016 13:59
NC Actual Compliance Last Page: 59 of 92
NC: A6DFR Type/Series: 6737-700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Arrant NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2008-09-14 737.28-1257 ENGINE FUEL FEED SYSTEM: BOOST PUMP Manual Compliance 05/05/2008 Rev: 1
39-15495 CONTROL RELAY GROUND LOCATION NC Total Hours: 1386:47 NC Total Cycles: 729
CHANGE SB 737-28-1257 WAS CM' IAW EO 155809 BY LHT
Category: AD ON 15/07/07. REF DEL. DOGS.
Status: TERMINATED
Rev: 1
EARLIEST
Free: I
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 ALREADY INCOPORTED WITH AWLS 28-AWL-21,
Rev: 1 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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 60 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Anent NO DocumenVSB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2008-12-04 737-53-1232 FUSELAGE - SKIN - CHEMICALLY MILLED
39-15547 STEPS - INSPECTION, REPAIR AND 32797
35000 Cys
PREVENTIVE MODIFICATION
Category: AD
Status: OPEN 25/06/2106
Rev: 0 Recur
EARLIEST
Freq: I
E/C: 2008-16-13 737-27-1284 FLIGHT CONTROLS - ELEVATOR AND TAB - WO 13098 05/03/2009 Rev: 0
39-15631 737-27-1284 IN 01 LEFT AND RIGHT ELEVATOR TAB NC Total Hours: 1751:48 NC Total Cycles: 840
PUSHRODS REPLACEMENT B3-27-1284 SB 737-27-1284 C/OUT DURING 2A CHK
Category: AD 737-55A1080 DTD 05/03/09.
Status: TERMINATED AD CLOSED.
Rev: 0
EARLIEST
Freq: 1
E/C: 2008-17-15 INSTALL HOT SHORT PROTECTOR
39-15653 SUPPORT BRACKETS & EQUIPMENT FOR
FOIS
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Freq: 1
AD IS N/A BY THE EFFECTIVITY LIST OF
BOEING SB 737-28A1221
E/C: 2008.21.02 737.54.1045 NACELLES/PYLONS - HEAT INSULATION WO 13629 02/09/2009 Rev: 0
39-15686 BLANKETS - REPLACEMENT NC Total Hours: 1916:27 NC Total Cycles: 903
SB 737.54.1045 C/OUT DURING A CHK DTD
Category: AD 02/09/09.
Status: TERMINATED
Rev: 0
EARLIEST
Frog: 1
EFTA_R1_00012820
EFTA01734552
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 61 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
FJC (Category: AD) Schedule Remaining/
Ament NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2008-22-01 AUX 2008-22-01 REPORT PREVENT USAGE OF AUXILIARY FUEL WO 12640 16/08/2008 Rev: 2
39-15696 2010-19-03 TANKS NC Total Hours: 1469:35 NC Total Cycles: 767
ST00936NY-D-28-SB-001 AND
Category: AD ST00936NY-D-28-S8-001 ST00936NY-D-28-SB-021 C/OUT ON 16/08/2008
Status: TERMINATED ST00936NY-D-28-SB-021 UNDER WORK ORDER 12640. AD TERMINATED.
Rev: 2 ST01384NY-D-28-SB-001
ST01384NY-D-28-SB-008 EARLIEST
Freq: I
E/C: 2008-22-01 REPORT 2008-22-01 AUX PREVENT USAGE OF AUXILIARY FUEL Manual Compliance 12/11/2008 Rev: 0
39-15696 2010-19-03 TANKS NC Total Hours: 1565:27 NC Total Cycles: 788
ETTER REF : QN120/0 BBJ PATS TANK STC /I
Category: AD ST00936NY-D-28-58.001 USAGE INFORMATION NOTIFIED TO FM. BY QA ON
Status: TERMINATED ST00936NY-D-28-SB-021 12/11/08. LETTER REF : ON120/08
Rev: 0 ST01384NY-D-28-58-001
EARLIEST
ST01384NY-D-28-SB-008
Freq: 1
E/C: 2008-23-07 2003-14-08 AIRPLANE FLIGHT MANUAL REVISION - WO 12982 03/12/2008 Rev: 0
39-15728 2006-13-13 CABIN ALTITUDE WARNING NC Total Hours: 1606:32 NC Total Cydes: 797
Category: AD
Status: TERMINATED
Rev: 0
EARLIEST
Freq: 1
E/C: 2008-24-05 2003-20-13 WINDSHILED WIPER MOTOR WO 12229 11/01/2009 Rev: 0
39-15745 737-30A1057 REPLACEMENT NC Total Hours: 1655:45 NC Total Cycles: 813
SB 737-30A1057 C/OUT UNDER WORK ORDER
Category: AD 12229.P/N OF WIPER ASSY P/N CHANGED AS REQD.
Status: TERMINATED
Rev: 0
EARLIEST
Freq: 1
EFTA_R1_00012821
EFTA01734553
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 62 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2008-24-08 2001.15-01 EQUIPMENT/FURNISHINGS - EMERGENCY - Manual Compliance 30/12/2008 Rev: 0
2007-NM-228-AD DOOR MOUNTED ESCAPE SYSTEM - NC Total Hours: 1646:36 NC Total Cycles: 808
CHANGE EVACUATION SLIDE INFLATION P/N 5A3307-5 FITTED TO NC SATISFIES THE
Category: AD 25-308 VALVE REGULATOR REQUIREMENT OF THIS AD. AD CLOSED.
Status: TERMINATED 5A3307-25-309
Rev: 0 5A3307.25.339
737-25-1404 EARLIEST
737-25-1491 Free: I
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 33797
36000 Cys
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 63 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining!
Arrant NO Document/SS EJC Description: Hrs/Cys/DyslDte Next Due Last Compliance Information
E/C: 2009-0262 2009-0251-E FIRE PROTECTION - PORTABLE FIRE WO 14291 28/12/2009 Rev: 0
2009-0262 R1 EXTINGUISHERS - NC Total Hours: 2012:21 NC Total Cycles: 936
IDENTIFICATION/REPLACEMENT FOUND AFFECTED FIRE EXT P/N & S/N NOT FITTED
Category: AD 2009-0278 TO AIRCRAFT. REF SWCG26-003, W/O # 14291
Status: TERMINATED 2009-39
Rev: 2 ASB26-115
EARLIEST
ASB26-115 ISS C
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
IDENTIFICATION/REPLACEMENT FOUND AFFECTED PORTABLE FIRE EXT P/N & S/N
Category: AD NOT FITTED. REF. SWCG26-004 W/O # 14291
Status: TERMINATED
Rev: 1
EARLIEST
Freq: 1
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
EARLIEST
Freq: 1
E/C: 2009-19-02 RUDDER FEEL AND CENTERING UNIT -
INSPECTION. TEST AND REPLACEMENT OF
39-16019
SPRING ASSEMBLY
Category: AD
Status: N/A
Rev: 3
EARLIEST
Reason Freq: I
THIS AD IS N/A BY INSTALLED FEEL AND
CENTERING UNITS P/N
EFTA_R1_00012823
EFTA01734555
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 64 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Anent NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2009-21-10 2009.21.10 R1 AVOX SYSTEMS AND 8/E AEROSPACE
39-16049 OXYGEN CYLINDER ASSEMBLIES
Category: AD
Status: N/A
Rev: 3
EARLIEST
Reason Freq: I
THIS AD IS N/A BY INSTALLED OXYGEN
CYLINDER ASSEMBLY S/N .
E/C: 2009-24-07 2009-26-04 INSP MAIN LANDING GEAR - FORWARD
TRUNNION PIN INSPECTION AND
39-16095 2009-26-04 LOBE
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
INVERTER MODIFICATION NC Total Hours: 2030:34 NC Total Cycles: 940
39-16138
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
TRUNNION PIN INSPECTION AND NC Total Hours: 2030:34 NC Total Cycles: 940
39-16139 2009-24-07 REPLACEMENT 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
EARLIEST
737-32-1376R1
737-32-1376R2 Freq: 1
SWCB73-32-009
EFTA_R1_00012824
EFTA01734556
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 65 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
FJC (Category: AD) Schedule Remaining/
Ament NO Document/SS FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2009-26-04 LUBE 1.43710731 MAIN LANDING GEAR - FORWARD WO 02/02/2010 Rev: 0
TRUNNION PIN LUBRICATION NC Total Hours: 2030:34 NC Total Cycles: 940
39-16139 2009-24-07
Terminating Action Has Been Performed
Category: AD 2009-26-04 INSP
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 66 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Documant/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2010-0152 EASA AD 2010-0152 EQUIPMENT/FURNISHINGS - OXYGEN
MASK REGULATOR - MODIFICATION
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Frog: I
AD IS N/A BY INSTALLED OXYGEN MASK
REGULATOR P/N.
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
Terminating Action Has Been Performed
Category: AD 747-SL-28-106
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 67 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2010-0244-INSP 2010-0244-MOD EXHAUST - THRUST REVERSER INNER
2010-0244R1•INSP WALL - INSPECTION / REPAIR
Category: AD 2012•05•02-INSP
Status: CANCEL 737-78-1079
Rev: 1 737-78-1082
EARLIEST
737-78-1088 Superseded By: 2012•05•02•INSP
Freq: I
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
EARLIEST
737-78-1088 Superseded By: 2012-05-02-MOD
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
EARLIEST
Superseded By: 2010-17-19
Reason Frog: 1
TERMINATED 15104/10 BY
ACCOMPLISHMENT OF SB 737-27A1296.
EFTA_R1_00012827
EFTA01734559
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 68 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining!
Arrant NO Document/SB EJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2010-09-05 2010-06.51 ELEVATOR TAB CONTROL MECHANISM
737.27-01296 DETAILED INSPECTION
Category: AD 737-27A1297
Status: CANCEL
Rev: 1
EARLIEST
Superseded By: 2010-17-19
Freq: I
E1C: 2010-17-05 737-28A1201 FUEL PUMP CONTROL GROUND FAULT WO 13629 07/0912010 Rev: 0
INTERRUPTER (GFI) RELAY INSTALLATION NC Total Hours: 2127:50 NC Total Cycles: 971
39-16395
C/OUT IAW B3-28A1201R1 UNDER WORK ORDER
Category: AD 13629 DTD 02/09/2009
Status: TERMINATED
Rev: 0
EARLIEST
Freq: 1
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
EARLIEST
737-27A1299 Superseded By: 2013-06-05
Freq: 1
E/C: 2010-19-03 2008-22-01 AUX PREVENT USAGE OF AUXILIARY FUEL WO 12640 24/10/2010 Rev: 1
39-16431 2008-22-01 REPORT TANKS OR MODIFY AUXILIARY FUEL NC Total Hours: 2223:50 NC Total Cycles: 998
SYSTEM SB ST00936NY-0-28-SB-001 AND D-28-SB-021
Category: AD ST00936NY-D-28-SB-001 C/OUT UNDER WO 12640 DTD 16/08/08.
Status: TERMINATED ST00936NY.D.28-SB-021
Rev: 1
EARLIEST
Freq: 1
EFTA_R1_00012828
EFTA01734560
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 69 of 92
NC: A6DFR Type/Series: 6737•700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Arrant NO Document/SB FJC Description: Hrs/CyslDyslDte Next Due Last Compliance Information
BC: 2010-24-11 737-57A1279 CENTER AND OUTER WING - FASTENER WO 16115 16/09/2011 Rev. 0
39-16530 SEALING AND WIRE BUNDLE SUPPORT NC Total Hours: 2813:55 NC Total Cycles: 1178
GENERAL VISUAL INSPECTION SB 737-57A1279 GOUT UNDER WO 16115 DTD
Category: AD 16/09/2011.
Status: TERMINATED
Rev: 0
EARLIEST
Freq: I
E/C: 2010-26-06 PART 1 2010-26-06 PART 2 FUSELAGE - SKIN - INSPECTION OF THE
737-53A1289 PART-1 SKIN FOR SCRIBE LINES • PART 1 (SKIN 37797
40000 Cys
LAP JOINTS. CIRCUMFERENTIAL BUTT
Category: AD 737-53A1289 PART-2 JOINTS, INTERNAL APPROVED REPAIRS)
Status: OPEN 03103/2120
Rev: 0 Once
EARLIEST
E/C: 2010-26-06 PART 2 2010-26-06 PART 1 FUSELAGE - SKIN - INSPECTION OF THE
737-53A1289 PART-1 SKIN FOR SCRIBE LINES • PART 2 (DECALS 20000 Cys 17797
AND EXTERNAL APPROVED REPAIRS)
Category: AD 737-53A1289 PART-2
Status: OPEN 30/05/2065
Rev: 0 Once
EARLIEST
Freq: 1
BC: 2011-0043 MODE S TRANSPONDER CONTROL PANELS
- MODIFICATION
Category: AD
Status: N/A
Rev: 0
EARLIEST
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.
EFTA_R1_00012829
EFTA01734561
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 70 of 92
NC: A6DFR Type/Series: B737-700/BBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO DocumenVSB E/C Description: Hrs/Cys/DyslDte Next Due Last Compliance Information
E/C: 2011-0093 2011-0103 EQUIPMENT / FURNISHINGS - EMERGENCY
LOCATOR TRANSMITTER (ELT) ANTENNA -
MODIFICATION / REPLACEMENT
Category: AD
Status: N/A
Rev: 0
EARLIEST
Superseded By: 2011.0103
Frog: I
E/C: 2011-0094 SB 25.65.24 EQUIPMENT/FURNISHINGS - LIFE JACKET
VACUUM BAG - MODIFICATION
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Frew 1
AD IS N/A BY INSTALLED P/N.
E/C: 2011-0098 2011.12-O1 EQUIPMENT/FURNISHINGS - PASSENGER
SEAT - REPLACEMENT
Category: AD
Status: N/A
Rev: 1
EARLIEST
Reason Frew 1
THIS AIRCRAFT IS NOT FITTED WIHT
KOITO SEATS. HENCE THE AD IS N/A BY
INSTALLED SEAT MODEL.
E/C: 2011-0103 2011.0093 ATA 25: EQUIPMENT /FURNISHING -
EMERGENCY LOCATOR TRANSMITTER(ELT)
ANTENNA-MODIFICATION REPLACEMENT
Category: AD
Status: N/A
Rev: 0
EARLIEST
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.
EFTA_R1_00012830
EFTA01734562
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 71 of 92
NC: A6DFR Type/Series: B737-700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
SC (Category: AD) Schedule Remaining/
Anent NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2011-01-09 119003-35-5 EMERGENCY EQUIPMENT - WE
119003-35-6 AEROSPACE PROTECTIVE BREATHING
EQUIPMENT
Category: AD
Status: N/A
Rev: 01
EARLIEST
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.
SC: 2011-04-09 OXYGEN - PASSENGER OXYGEN SYSTEM -
LAVATORY SERVICE UNITS
Category: AD
Status: N/A
Rev: 1
EARLIEST
Superseded By: 2012-11-09
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
EARLIEST
737-57A1302
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
EARLIEST
737-57A1302
737-SL-57-084 Frog: 1
EFTA_R1_00012831
EFTA01734563
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 72 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB E/C Description: Hrs/Cys/Dys!Dte Next Due Last Compliance Information
E/C: 2011-07-05 2001-605(AB) SICMAAERO SEATS - INSPECTION OF
90-25.012 BACKREST LINKS FOR CRACKS
Category: AD
Status: N/A
Rev: 01
EARLIEST
Superseded By: 2014-20-11
Reason Freq: I
AD NOT APPLICABLE. AFFECTED SEATS
NOT INSTALLED.
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 NC Total Hours: 5887:00 NC Total Cycles: 2120
INDICATION
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 73 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO DoeumenVSB SC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2011-18-03 2001-08-24 INSTALLATION OF AN AUTOMATIC SHUTOFF WO 16920 04/10/2011 Rev: 0
2002-19-52 SYSTEM FOR THE CENTER TANK FUEL NC Total Hours: 2820:50 NC Total Cycles: 1182
BOOST PUMPS. AND INSTALLATION OF A
Category: AD 2002.24.51 PLACARD IN THE AIRPLANE FLIGHT DECK
Status: TERMINATED 737.28Al206 IF NECESSARY.
Rev: 0 737-28A1248
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 NC Total Hours: 5817:55 NC Total Cycles: 2086
INSTALLATION 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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 74 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EC (Category: AD) Schedule Remaining/
Arrant NO Document/SB EIC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2011-21-08 2001.0613 EQUIPMENT/FURNISHINGS - SICMAAERO
SB 90-25-013 ISS 4 SEATS - INSPECTION OF BACKREST LINKS
Category: AD
Status: N/A
Rev: 0
EARLIEST
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
EIC: 2011-26-09 737-54-1046 NACELLES/PYLONS - STRUT TO WING WO 20202 0810812014 Rev: 0
FAIRINGS - THUMBNAIL FAIRING EDGE NC Total Hours: 5107:40 A/C Total Cycles: 1870
SEAL REPLACEMENT
Category: AD
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 NC Total Hours: 5786:05 NC Total Cycles: 2071
INSPECTION AND LUBRICATION -
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 2011-27-03 WP1 HORIZONTAL STABILIZER TRIM CONTROL 25000 Hrs 18846:30
2011.27-O3 WP3 SYSTEM • STABILIZER TRIM ACTUATOR
MODIFICATION • WORK PACKAGE 2
Category: AD 27-108-00-01
Status: OPEN 737-27A1277 WP2 26/06/2042
Rev: 0 Once
EARLIEST
Freq: 1
EFTA_R1_00012834
EFTA01734566
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 75 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining!
Arrant NO Document/SB EJC Description: Hrs/CysloyelDte Next Due Last Compliance Information
SC: 2011-27-03 WP3 2011.27-03 WP1 HORIZONTAL STABILIZER TRIM CONTROL 25000 Hrs 18846:30
SYSTEM - STABILIZER TRIM ACTUATOR
39-16904 2011.27-03 WP2
OVERHAUL • WORK PACKAGE 3
Category: AD 27-108-00-01
Status: OPEN 737-27A1277 WP3 26/06/2042
Rev: 0 Recur
EARLIEST
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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 76 of 92
NC: A6DFR Type/Salves: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining!
Anent NO Document/SB EJC Description: Hrs/Cys/Dys/Dta Next Due Last Compliance Information
SC: 2012-05-02-INSP 2010-0244-INSP EXHAUST - THRUST REVERSER INNER WO 17759 10/08/2012 Rev: 0
2010-0244R14NSP WALL - INSPECTION / REPAIR 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
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 77 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO DocumenVSB EJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2012-19-11 737.21.1165 Incorporating design changes to improve the
737.31A1332 reliability
Category: AD 2190 Dys 790
Status: OPEN 06/11/2018
Rev: 01 Once
EARLIEST
Superseded By: 2015-16-01
Freq: 1
ESC: 2012-21-08 737-22A1211 AUTOFLIGHT: DETECT AND CORRECT AN
39-17224 FAA AD 2012-21-08 UNSAFE CONDITION DUE TO A DEFECTIVE
RADIO ALTIMETER CHANNEL
Category: AD
Status: N/A
Rev: 0
EARLIEST
Reason Freq: 1
THIS AD IS NOT APPLICABLE BY THE
EFFECTIVITY LIST OF 737-22A1211
BC: 2012.23.08 2008-08-24 NACELLES/PYLONS - STRUT DRAINS AND
737-54-1043 R2 SEALS -AFT FAIRING DRAIN TUBE
ASSEMBLY REPLACEMENT
Category: AD 1825 Dys 478
Status: OPEN 29/12/2017
Rev: 00A Once
EARLIEST
Frog: 1
EIC: 2012-24-08 737-30A1063 Prevent ice from forming on air data system WO 20202 08/08/2014 Rev: 02
sensors NC Total Hours: 5107:40 NC Total Cycles: 1870
Category: AD
Status: TERMINATED
Rev: 02
EARLIEST
Freq: 1
EFTA_R1_00012837
EFTA01734569
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 78 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Arrant NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2012-25-05 2008-24-08 EQUIPMENT/FURNISHINGS - ESCAPE Manual Compliance 05/11/2015 Rev: 00
25-349 SLIDE/RAFT - MODIFICATION NC Total Hours: 5817:55 NC Total Cycles: 2086
VSB 5A3307-25-389 HAS BEEN COMPLIED TO ALL
Category: AD SA3307-25-389 SLIDES.
Status: TERMINATED
Rev: 00
EARLIEST
Reason Freq: I
ALL SLIDES MODIFIED ACCORDING TO
VSB 5A3307-25-389.
E/C: 2013-0020 2013-0020 R1 EQUIPMENT & FURNISHINGS - SAFETY
2013-0020 R2 BELTS / TORSO RESTRAINT SYSTEMS -
INSPECTION / REPLACEMENT
Category: AD 2013-0020 R3
Status: N/A 2013-0020 R4
Rev: 06 2013-0020 R4 CORRECTION
EARLIEST
Reason Froq: I
AFFECTED SEAT BELTS NOT FITTED PER
AIRCRAFT RECORDS
E/C: 2013-02-05 2003-14-08 AURAL WARNING SYSTEM: INSTALLATION WO 20202 08/08/2014 Rev: 0
39-17326 2006-13-13 OF CABIN ALTITUDE WARNING SYSTEM & NC Total Hours: 5107:40 NC Total Cycles: 1870
TAKEOFF CONFIGURATION WARNING
Category: AD 2008-23-07 SYSTEM LIGHTS
Status: TERMINATED 737-31A1332
Rev: 0
EARLIEST
Freq: 1
BC: 2013-02-07 737-25-1641 EQUIPMENT / FURNISHINGS - PASSENGER
737-25-1641 R1 CABIN PARTITIONS AND COMPARTMENTS -
CENTER OVERHEAD STOWAGE BOX WITH
Category: AD 737-25-1641 R2 LIFERAFT PROVISIONS - 9G TIE ROD
Status: N/A ATTACHMENT CHANGE
Rev: 00
LATEST
Reason Frog: 1
N/A BY VARIABLE NUMBER OF THE
AIRCRAFT IN THE SB EFFECTIVITY
EFTA_R1_00012838
EFTA01734570
Print Date 07/092016 13.59
A/C Actual Compliance Last Page: 79 of 92
NC: A60FR Type/Series: Et737.70043BJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Ament NO Document/SB BC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
BC: 2013-04-11 737-28-1303 Prevent electrical arcing and a potential ignition
FAA AD 2013-04-11 source within the ECS bay
Category: AD
Status: NIA
Rev: 00
LATEST
Reason Free: t
N/A BY VARIABLE NUMBER OF THE
AIRCRAFT IN THE SB EFFECTIVITY
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 NC Total Hours: 5107:40 NC Total Cycles: 1870
LEFT AND RIGHT ELEVATOR TAB CONTROL
Category: AD 737-27A1297 MECHANISMS
Status: OPEN 737-27A1297R1 19/09/2017
Rev: 2 737-27A1297R2 Recur
LATEST
737-27A1299
Frog: 1
E/C: 2013-06.05 MOD 2010-17-19 REPLACE THE LEFTAND RIGHT ELEVATOR
TAB MECHANISMS WITH ELEVATOR TAB
2013-06-05 INSP
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
EARLIEST
Superseded By: 2014-05-30
Frog: 1
EFTA_R1_00012839
EFTA01734571
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 80 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Anent NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2013-07-09 737-35A1121 OXYGEN - FLIGHT CREW OXYGEN MASK
MXP1/4-35-175 STOWAGE BOX - TO PREVENT AN IGNITION
SOURCE
Category: AD
Status: N/A
Rev: 00
EARLIEST
Reason Free: I
THIS AD IS NOT APPLICABLE BY THE
EFFECTIVITY LIST OF 737-35A1121
EIC: 2013-08-01 737-78-1086 Thrust Reverser - Upper Fire Seal Damage WO 20202 08/08/2014 Rev: 0
39-17418 NC Total Hours: 5107:40 NC Total Cycles: 1870
Terminating Action Has Been Performed
Category: AD
Status: TERMINATED
Rev: 0
EARLIEST
Froq: 1
E/C: 2013-08-16 737-53-1310 FUSELAGE - SKIN - CHEM MILL STEPS IN
CROWN SKINS AT SPECIFIED LOCATIONS - 40797
43000 Cys
INSPECTION AND MODIFICATION
Category: AD
Status: OPEN 20/05/2128
Rev: 00 Recur
EARLIEST
Frog: 1
EIC: 2013-08-18 737-57-1293 WINGS - LEADING EDGE AND LEADING WO 19498 23/09/2013 Rev: 00
EDGE DEVICES - FUEL DRAIN PATH NC Total Hours: 4627:55 NC Total Cycles: 1706
MODIFICATION REF WORK ORDER 19498
Category: AD
Status: TERMINATED
Rev: 00
EARLIEST
Frog: 1
EFTA_R1_00012840
EFTA01734572
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 81 of 92
NC: A6DFR Type/Series: B737.7001BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO DocumenVSB EJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2013-15-16 737-52A1167 DOORS - MAIN LANDING GEAR - INBOARD
DOORS - INSPECTION OF INBOARD MLG 10000 Cys 7797
DOOR HINGE FITTINGS FOR FATIGUE
Category: AD CRACKING
Status: OPEN 12/01/2038
Rev: 0 Recur
EARLIEST
Freq: I
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
AD HAS BEEN COMPLIED AS PER AMP.
Category: AD 28-AWL-101-01
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
REF TO TASK 737-205020186.-00-01 UNDER ROUTINE
Category: AD 28-AWL-101-01 1095 Dys 334 TASK WORK ORDER8-
Status: OPEN 28-AWL-101.02 07/08/2017
Rev: 00 Recur
EARLIEST
Freq: 1
E/C: 2013-18-09 1152682-23-A22 DETECT AND CORRECT DISCREPANCIES
1152682-23-A22 R01 OF THE BATTERY WIRING INSTALLATION
INSIDE THE ELT TRANSMITTER UNIT
Category: AD CF-2013-25
Status: N/A
Rev: 03
EARLIEST
Superseded By: 2014-17-02
Reason Frog:
AD NOT APPLICABLE. AFFECTED P/N NOT
INSTALLED.
EFTA_R1_00012841
EFTA01734573
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 82 of 92
NC: A6DFR Type/Serlos: 6737-700/66J1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Doeument/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2013-t9-03 737-29-1113 Detect and correct possible damage caused by
insufficient separation between the wire
bundles and hydraulic tubing
Category: AD
Status: N/A
Rev: 00
EARLIEST
Reason Freq: I
NOT APPLICABLE FOR THIS AIRCRAFT BY
THE EFFECTIVITY LIST OF SB 737-29-1113
EC: 2013-19-04 737-53-1294 FUSELAGE - SKIN - LOWER BULKHEAD
CHORDS AT BS 540 - SKIN INSPECTION. 15797
18000 Cys
CHORD SPLICE INSTALLATION AND SKIN
Category: AD REPAIR
Status: OPEN 08112/2059
Rev: 00 Recur
EARLIEST
Froq: 1
E/C: 2013-19-23 FAA AD 2013-19-23 UPDATE INSPECTION REQUIREMENTS TO Manual Compliance 05/10/2013 Rev: 00
DETECT FATIGUE CRACKING OF PRINCIPAL NC Total Hours: 4631:15 NC Total Cycles: 1710
STRUCTURAL ELEMENTS (PSE) AD REQUIREMENT HAS BEEN INCORPORATED IN
Category: AD 737 AMP REV01.
Status: TERMINATED
Rev: 00
EARLIEST
Reason Freq: 1
AD COMPLIED WITH ON THE NEW AMP
REVISION (SEP 2014).
EIC: 2013-23-04 737-53-1296 FUSELAGE - PASSENGER CABIN FLOORS -
STATION 7276 SPLICE STRAP 4797
INSTALLATION 7000 Cys
Category: AD
Status: OPEN 26/10/2029
Rev: 00 Once
EARLIEST
Freq: 1
EFTA_R1_00012842
EFTA01734574
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 83 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO DoeumenVSB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2013-24-13 737-53-1244 PASSENGER CABIN FLOORS - STA 520 TO WO 13578 05/12/2013 Rev: 00
737-53-1244 RI 540 - PIVOT LINK ASSEMBLY NC Total Hours: 4753:45 NC Total Cycles: 1755
REPAIR/REPLACE PART A AND B OF SB 737-53-1244 CARRIED OUT
Category: AD 737-53-1244 R2 UNDER WORK ORDER 13578 DTD 15/04/2010.
Status: TERMINATED 737.53.1244 R3
Rev: 01 737-53-1244 R4
EARLIEST
737-53-1244 R5 Superseded By: 2015-02-26
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
Terminating Action Has Been Performed
Category: AD 737-30-1058R05
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 BOEING SB B737-53-0011 FUSELAGE - CORRECT CRACKS IN THE
FAA 2014-03-19 IN-FLIGHT ENTERTAINMENT SYSTEM
RADOME ASSEMBLY
Category: AD
Status: N/A
Rev: 00
LATEST
Reason Freq: I
N/A- THE AIRCRAFT IS NOT MODIFIED BY
STC ST0028480 AND ST02887AT
EFTA_R1_00012843
EFTA01734575
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 84 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO DoeumenVSB E/C Description: Hrs/Cys/DysIDte Next Due Last Compliance Information
E/C: 2014-05-27 Testing and calibration of the alignment of the
transponders
Category: AD
Status: N/A
Rev: 00
EARLIEST
Reason Freq: I
AFFECTED P/N NOT INSTALLED.
E/C: 2014-05-30 2013-07-07 STABILIZERS - HORIZONTAL STABILIZER
737-55-1093 REAR SPAR ATTACH PINS - 53797
56000 Cys
INSPECTION/REPLACEMENT
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
Print Date 07/09:2016 13.59
A/C Actual Compliance Last Page: 85 of 92
NC: A6DER Type/Series: 8737-70043Bit NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining!
Anent NO Document/SB EIC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
EJC 2014-13-10 737-28-1312 INSTALLATION OF INCORRECT WIRE
SUPPORT CLAMPS WITHIN THE BAY AREA
OF THE LEFT AND RIGHT ENVIRONMENTAL
Category: AD CONTROL SYSTEMS (ECS) - INSPECTION /
Status: NIA REPLACEMENT
Rev: 0
LATEST
Reason Freq: I
N/A BY VARIABLE NUMBER OF THE
AIRCRAFT IN THE SB EFFECTIVITY
EJC: 2014-15.12 737-55-1090 STABILIZERS - HORIZONTAL STABILIZER -
REAR SPAR TERMINATION FITTING - 33797
36000 Cys
INSPECTION
Category: AD
Status: OPEN 21/03/2109
Rev: 00 Once
EARLIEST
Frog: 1
E!C: 201416.14 737-22A1215 AIR TRANSPORT ASSOCIATION (ATA) OF WO 20202 2510812014 Rev: 0
AMERICA CODE 22, AUTO NC Total Hours: 5133:25 NC Total Cycles: 1878
FLIGHT.AUTOTHROTTLE TO ENTER SB737-22A1215 C/OUT ON 08/08/2014 UNDER WO
Category: AD LANDING FLARE RETARD MODE 20202
Status: TERMINATED PREMATURELY ON APPROACH.
Rev: 0
EARLIEST
Rev 1
EIC: 2014-17-02 1152682-23-A22 HONEYWELL ELTS MODEL RESCU 406AF
2013-15-07 AND 406AFN WITH PINS 1152682-1, -2, AND
-3.
Category: AD 2013-18-09
Status: N/A
Rev-. 00
EARLIEST
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
EFTA_R1_00012845
EFTA01734577
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 86 of 92
NC: A6DFR Type/Series: 6737-700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB E!C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2014-20-06 737.31.1471 Prevent loss of flight-critical information WO 20138 15/10/2014 Rev: 0
displayed to the flightcrew NC Total Hours: 5239:40 NC Total Cycles: 1901
SB 737-31-1471 CARRIED OUT ON 01/03/2014. REF
Category: AD WORK ORDER 20138.
Status: TERMINATED
Rev: 0
EARLIEST
Freq: I
ESC: 2014-20-11 2011-07-05 EQUIPMENT/FURNISHINGS - SICMA SEATS -
2012-0038 DETECT AND CORRECT CRACKS IN THE
BACKREST LINKS.
Category: AD 90-25-2012
Status: N/A
Rev: 00
LATEST
Reason Freq: 1
N/A BY SEAT MODEL INSTALLED
ESC: 2015-0093 EASA AD NO. 2015-0093 NAVIGATION - ATTITUDE HEADING
REFERENCE SYSTEM - MODIFICATION /
REPLACEMENT
Category: AD
Status: N/A
Rev: 00
LATEST
Reason Freq: 1
THIS AD IS NOT APPLICABLE BY THE PART
NUMBER OF THE INSTALLED
COMPONENTS.
E/C: 2015-02-26 737-53-1244 PASSENGER CABIN FLOORS - STA 520 TO Manual Compliance 25/02/2015 Rev: 0
737-53-1244 RS 540 - PIVOT LINK ASSEMBLY REPAIR! NC Total Hours: 5472:20 NC Total Cycles: 1975
REPLACEMENT TERMINATED: COMPLIED THE FOLLOWING SB
Category: AD 737-53-1244 / AD2013-24-13 AS PER WO13578 DATED
Status: TERMINATED 12 MAY 2013
Rev: 0
EARLIEST
Reason Freq: 1
TERMINATED PER SB 737.53.1244 /AD
2013.24.13 WITH WO 13578 ON 12 MAI 2013.
EFTA_R1_00012846
EFTA01734578
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 87 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO DocumenVSB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2015-08-07 MXH-35-240 OXYGEN SYSTEM - FLIGHT CREW OXYGEN
MASK REGULATOR INFLATABLE
HARNESS/HOSE •
Category: AD INSPECTION/REPLACEMENT 730 Dys 281
Status: OPEN 15(06/2017 Dte 15/06/2017
Rev: 00 Once
EARLIEST
Frew I
E/C: 2015-08-09 737-53A1325 FUSELAGE - BODY STATION (STA) 727
BULKHEAD LOWER FRAME WEB AND
INNER CHORD - INSPECTION/MOD
Category: AD
Status: N/A
Rev: 00
LATEST
Reason Free: 1
N/A BY VARIABLE NUMBER PER SB
737-53A1325 EFFECTIVITY LIST.
EX: 2015-10-51 AD 2015-10-51 AVIDYNE !FOS DISPLAYING INCORRECT
COURSE DEVIATION INDICATION
3418183
INFORMATION DURING GPS APPROACHES
Category: AD
Status: N/A
Rev: 00
EARLIEST
Reason Frew I
AD 2015-10-51 IS NOT APPLICABLE TO THIS
AIRCRAFT BY THE INSTALLED PART
NUMBER
E/C: 2015-16-01 737-21-1165 LOSS OF CABIN ALTITUDE WARNING
39-18226 737-31A1332 DURING A LACK OF CABIN
PRESSURIZATION
Category: AD AD 2012-19-11
Status: TERMINATED
Rev: 00A
LATEST
Superseded By: 2015.21.11
Frog: 1
EFTA_R1_00012847
EFTA01734579
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 88 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
E/C: 2015-16-04 AD 2015-16-04 KIDDE GRAVINER HAND-OPERATED FIRE
39-18229 EXTINGUISHERS
Category: AD
Status: N/A
Rev: 00
EARLIEST
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
EIC: 2015-19-03 2015.21.10 ENGINE FUEL SHUTOFF VALVE - POSITION
28-AWL-MOV INDICATION OPERATIONAL CHECK
Category: AD AD 2015-19-03
Status: CANCEL
Rev: 01
EARLIEST
Superseded By: 2015.21.10
Reason Free: i
AIRWORTHINESS LIMITATIONS SECTION
28-AWL-MOV UPDATE REQUIREMENT
E/C: 2015.21.08 DETECT AND CORRECT CRACKS IN THE
39-18301 INSPAR UPPER SKIN AND REAR SPAR
UPPER CHORD
Category: AD
Status: N/A
Rev: 00
EARLIEST
Reason Free: 1
THE AD IS APPLICABLE TO 737-100. -200,
-200C, -300. -400. AND -500. HENCE NA FOR
THIS AIRCRAFT
E/C: 2015.21.10 28-AWL-MOV ENGINE FUEL SHUTOFF VALVE - POSITION Manual Compliance 22/11/2015 Rev: 00
737-28-1314 INDICATION OPERATIONAL CHECK NC Total Hours: 5827:25 NC Total Cycles: 2098
AMP 28-AWL-MOV IS INCLUDED IN AMP REV 04
Category: AD AD 2015-21-10 DATED NOVEMBER 2015 BUT SET TO NOT
Status: TERMINATED APPLICABLE AS SB 737-28-1314 WAS ALREADY
Rev: 00 INCORPORATED UNDER WO 50175 ON 22-AUG-2015.
EARLIEST
Freq: i
EFTA_R1_00012848
EFTA01734580
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 89 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining/
Arrant NO Document/SB E/C Description: Hrs/Cys/Dys/Dta Next Due Last Compliance Information
E/C: 2015-21-11 2012.19.11 LOSS OF CABIN ALTITUDE WARNING Manual Compliance 12/11/2015 Rev 00
39-18304 2015-16-01 DURING A LACK OF CABIN NC Total Hours: 5817:55 NC Total Cycles: 2086
PRESSURIZATION TERMINATED: RELATED SB 737-31A1332 HAS
Category: AD 737.21.116583 BEEN INCORPORATED AS PER W020202 DTD
Status: TERMINATED 737-31A1332R4 8/8/2014.
Rev: 00 AD 2015-21.11
LATEST
Freq: I
E/C: 2015-23-09 MCF-SBU-35-001 OXYGEN - OXYGEN MASK REGULATOR - Manual Compliance 02/02/2016 Rev: OOA
INSPECTION FOR POTENTIAL DEFAULT NC Total Hours: 5887:00 NC Total Cycles: 2120
CALIBRATION ALL AFFECTED REGULATORS HAS BEEN
Category: AD INSPECTED AS PER VSB MCF-SBU-35-001.
Status: TERMINATED
Rev: OOA
EARLIEST
Reason Frog: 1
ALL AFFECTED REGULATORS INSPECTED
PER VSB MCF-SBU-35-001 AND ADJUSTED
IF NECESSARY.
E/C: 2016-0024 FIRE PROTECTION - OPTICAL AND
AMBIENT SMOKE DETECTORS -
IDENTIFICATION / REPLACEMENT
Category: AD
Status: N/A
Rev: 00
EARLIEST
Reason Freq: 1
N/A BY INSTALLED PART NUMBER.
E/C: 2016-0044 FIRE PROTECTION - ENGINE AND
AUXILIARY POWER UNIT AUTOMATIC FIRE
EXTINGUISHERS - INSPECTION/OVERHAUL
Category: AD
Status: N/A
Rev: 00
LATEST
Reason Freq: 1
P/N NOT INSTALLED.
EFTA_R1_00012849
EFTA01734581
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 90 of 92
NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
E/C (Category: AD) Schedule Remaining/
Anent NO Document/SS FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2016-04-06 DETECTION AND CORRECTION OF LATENT
39-18400 EQUIPMENT COOLING SYSTEM AND LOW
PRESSURE ENVIRONMENTAL CONTROL
Category: AD SYSTEM FAILURES
Status: OPEN 01/02/2017 Dte 01/02/2017
Rev: 00 Recur
EARLIEST
Freq: I
E/C: 2016-04-20 ENGINE FUEL FEED SYSTEM - MOTOR Manual Compliance 26/05/2016 Rev: 00
OPERATED VALVE P/N MA20A1001.1 NC Total Hours: 6068:15 A/C Total Cycles: 2179
REPLACEMENT PN: MA20A1001-1 IS NOT INSTALLED AND
Category: AD DEACTIVATED FROM TRAX
Status: TERMINATED
Rev: 00
EARLIEST
Reason Freq: 1
RECORDS CHECKED: P/N MA20A1001.1
NOT INSTALLED AND DEACTIVATED FROM
TRAX.
EIC: 2016-07-16 2013-26-08 ICE AND RAIN PROTECTION - ARCING,
39-17717 737-30-1058R05 SMOKE. AND FIRE IN THE FLIGHT DECK IN
WINDOW NUMBER 2
Category: AD
Status: OPEN 09/02/2018 Dte 09/02/2018
Rev: 00 Once
EARLIEST
Freq: 1
E/C: 2016-11-20 OXYGEN SYSTEM - PROTECTIVE
39-18547 BREATHING EQUIPMENT (PBE) P/N
119003-11 - INSPECTION/REPLACEMENT
Category: AD
Status: N/A
Rev: 00
LATEST
Reason Free: 1
THE ACFT IS NOT FITTED WITH PBE P/N
119003.11. AD IS N/A BY PART NUMBER
INSTALLED.
EFTA_R1_00012850
EFTA01734582
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 91 of 92
NC: A6DFR Type/Series: B737.700/BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EIC (Category: AD) Schedule Remaining!
Arrant NO Document/SB EJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information
SC: 2016-13-16-HFEC 2016-13.16 STABILIZERS - HORIZONTAL STABILIZER -
737.SSA1097 REAR SPAR UPPER CHORD - (G) (2) HIGH
FREQUENCY EDDY CURRENT (HFEC)
Category: AD
Status: OPEN 11/08/2017 Dte 11/08/2017
Rev: 00 Recur
EARLIEST
E/C: 2016-13-16-INS 2016-13-16 STABILIZERS - HORIZONTAL STABILIZER - WO 50505 07/02/2016 Rev: 00
737-55A1097 REAR SPAR UPPER CHORD - (G) (1) NC Total Hours: 5887:00 NC Total Cycles: 2120
INSPECTION FOR CONFIGURATION 737-55A1097-INS HFEC INSPECTION PERFORMED
Category: AD UNDER EC 737-55A1097-INS / WO 50505 DURING
Status: OPEN 11/08/2017 Dte 11/08/2017 THE A CHECK ON 07-02-2016 AND FOUND
Rev: 00 Once SATISFACTORY
EARLIEST
Freq: 1
EIC: 2016-18-01 INSP 737-32-1448 INSP TO DETECT AND CORRECT HEAVY
CORROSION AND CHROME DAMAGE OF
THE FORWARD AND AFT TRUNNION PIN
Category: AD ASSEMBLIES AND THE RIGHT AND LEFT
Status: OPEN MLGS. WHICH COULD RESULT IN
CRACKING OF THESE ASSEMBLIES AND Recur
Rev: 0
COLLAPSE OF THE MLGS
EARLIEST
Freq: 1
EIC: 2016-18-01 LUBE 737-32-1448 LUBE TO DETECT AND CORRECT HEAVY
CORROSION AND CHROME DAMAGE OF
THE FORWARD AND AFT TRUNNION PIN
Category: AD ASSEMBLIES AND THE RIGHT AND LEFT
Status: OPEN MLGS, WHICH COULD RESULT IN
CRACKING OF THESE ASSEMBLIES AND Recur
Rev: 0
COLLAPSE OF THE MLGS
EARLIEST
Freq: I
EFTA_R1_00012851
EFTA01734583
Print Date 07/09/2016 13:59
NC Actual Compliance Last Page: 92 of 92
NC: A6DFR Type/Series: B737.7001BBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016
EC (Category: AD) Schedule Remaining!
Arrant NO Document/SS E/C Description: Hrs/CysiDysiDte Next Due Last Compliance Information
EC: 2016-18-01 MOD TO DETECT AND CORRECT HEAVY
CORROSION AND CHROME DAMAGE OF
THE FORWARD AND AFT TRUNNION PIN
Category: AD ASSEMBLIES AND THE RIGHT AND LEFT
Status: PENDING MLGS. WHICH COULD RESULT IN
CRACKING OF THESE ASSEMBLIES AND Recur
Rev: 0
COLLAPSE OF THE MLGS
EARLIEST
Freq: I
EFTA_R1_00012852
EFTA01734584
P/N Compliance Print Print Date 10105/2016 11 37
Page: 1 of 5
PIN: CFM56.7-827/83 PIN Description: GE AIRCRAFT ENGINE CFM! P/N SIN: 876170 PIN Hours: 12214:09 PIN Cycles: 4113 Days: 5830
Installed NC: A6DFR Installed Date: 05/08/2013
Schedule Remaining/
Amont NO Document/SB SC Description: HrslCyslDyslDte Next Due Compliance Document Remarks
1998-14-51T CFP.156-7B-72-130 STARTER GEARSHAFT REPLACEMENT AND MCD
INSPECTION
CFM56.78-72-132
Category: AD
Status: N/A
Reason
Rev: 00 NM AS THIS ENGINE IS NOT IN THE AFFECTED ENGINE
ON LIST LATEST
1998-18-51 UNCOMMANDED ENG ACCELERATION I INFLT
1958-21-23
SHUTDOWN
98-18.51
Category: AD CN 98.350
Status: TERMINATED Superseded By: 1908-21-23
CN T98-350 Reason
Rev: 0 SUPERSEDED BY 1998.21.23
SB 72-0130, S80132 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 CFM56 SELECTED CRITICAL LIFE LIMITED PARTS
2002-13-03 INSP
Category: AD
Superseded By: 2002-13-03
Status: TERMINATED
Rev: 3
EARLIEST
2001-02-12 INSPECT PS3 LINE FITTING WO 2104 11102/2001 Rev: 1
SB CFM58-78 72-0075
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 Print Date 10105/2016 11 37
Page: 2 of 5
P/N: CFM56.7-B27/83 PIN Description; GE AIRCRAFT ENGINE CFM! P/N S/N: 876170 PIN Hours: 12214:09 PIN Cycles: 4113 Days: 5830
Installed NC: ABDFR Installed Date: 05/08/2013
Schedule Remaining/
Ament NO Document/SB BC Description: Hrs/CyslDyslDte Next Due Compliance Document Remarks
2001-11-05 SB 72.0329 REPLACEMENT OF NO.4 ROLLER BEARING P/N
305-355.717-0 IN DEFECTIVE BATCH
Category: AD
Status: NIA
Reason
Rev: 1 WA BY ENGINE SW LARLi6ST
2002-13.03 CFMS6.76-72.241 LIFE LIMITED ROTATING PART FAILURE 29/08/2002 Rev: 2
Hours Cycles Days
Category: AD E/C Reset At: 0:00 0 0
Status: OPEN TR 05-0035:0036.0037 AND
Reason 0038 TO TIME LIMITS CD
Rev: 2A Recur
NEXT PIECE PART OPPORTUNITY INSERTED IN NC LAPTOP
BAG ALONG WITH
BOOKLINK CD. REF
TRANSMITTAL LETTER.
2002-16-18 CFM56-78-72-241 REPLACEMENT OF 2ND AND 3RD STAGE LOW RO 49757 07/04/2013 Rev: 1
PRESSURE TURBINE NOZZLE SEGMENTS
39-12857 Hours Cycles Days
Category: AD E/C Reset At: 10375:39 3530 4703
Status: TERMINATED RECEIVING PROCESS
Rev: I SB 72-0241 FOUND
LARLIEST EMBODIED DURING SHOP
VISIT DTD MARCH 2013.
2003-03-01 2011-18-10 AFT ENGINE MOUNT. CENTER LINK ASSY 24/12/2003 Rev: 2
INSTALLATION INSPECTION
737.7181462 Hours Cycles Days
Category: AD E/C Reset At: 0:00 0 0
Status: TERMINATED Superseded By: 201148-10
C/OUT DURING IC CHK
Rev: 2 AT KLM. REF TO FILE #3
EARLIEST 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 "IC" CHECK
AT KLM. REF TO FILE NO
3 OF CHK PACK (KLM JOB
CARD NO 90-M90003C)
2006.26-01 FUEL FILTER REPLACEMENT ( FOR PIA PARTS)
39.14859
Category: AD
Status: N/A
Rev: 0
EARLIEST
EFTA_R1_00012854
EFTA01734586
P/N Compliance Print Print Date 10105/2016 11 37
Page: 3 of 5
P/N: CFM56-7-B27/B3 PIN Description: GE AIRCRAFT ENGINE CFM: P/N SIN: 876170 PIN Hours: 12214:09 P/N Cycles: 4113 Days: 5830
Installed NC: A6DFR Installed Date: 05/08/2013
Schedule Remaining/
Ament NO Document/SB SC Description: HrsiCyslDyslDte Next Due Compliance Document Remarks
2008-03-09 TRF WITH TANGENTIAL STRUTS - MANDATORY 19/02/2008 Rev: 2
2007-0104
INSPECTIONS - LIFE TIMES
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 LPT REAR FRAME - LIFE LIMIT / MANDATORY
2010-01-05
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 LPT DISK • REMOVE FROM SERVICE SUSPECT
CFM56-7B-72-0743 DISKS
39-16340
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 Print Date 10/0512016 11 37
Page: 4 of 5
PIN: CR156-7-627/83 PIN Description: GE AIRCRAFT ENGINE CFM! P/N SIN: 876170 PIN Hours: 12214:09 P/N Cycles: 4113 Days: 5830
Installed NC: A6DFR Installed Date: 05/080013
Schedule Remaining/
Ament NO Document/SB E/C Description: HrslCysiDyslDte Next Due Compliance Document Remarks
2011-18-10 2003-02-01 AFT ENGINE MOUNT -CENTER LINK ASSY • 12110/2011 Rev: 0
INSPECTION TO ENSURE CORRECT
39-16792 737-71A1462 INSTALLATION Hours Cycles Days
Category: AD 737.71A1462-1 E/C Reset At: 9388:29 320500 4331
Status: TERMINATED DETAILED INSPECTION IN
Rev: 3 Reason ACCORDANCE WITH SB
DURING ENGINE CHANGE (REF INOPISM4 OT. EARLIEST 737-71A1462, TO
26-MAY-201I) S8 liANGAFt MMHG WAS NARKED IA.W.
SS 737.71A1482 R3 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 ACCESSORY GEARBOX (AGB) HANDCRANKING
2013-26-01 PAD MODIFICATION
CFM56-78-72-0564
Category: AD CFM56-7B-72-0879
Status: OPEN
Rev: 0 Once
2013-26-01 INDEPENDENT INSPECTION OF THE AGB
2012-0209
HANDCRANKING PAD COVER
CFM56-7B-72-0564
Category: AD CFM56-7B-72.0879
Status: N/A
Roston
Rev: 0 NOT AFFECTED DUE TO CURRENTLY HAVING INSTALLED
AGES Pal 340846.50,10 EARLIEST
2014-0130 CFM56-76 ESPJ Time Limits- Engine Stationary Pans - Life Limits!
Mandatory Inspections
Category: AO
Status: N/A
Reason
Rev: 0
NO CFM56-IS STATIONARY PART IN PF OR RJ FLEET HAS EARLIEST
PREVIOUSLY OPERATED ON ENGINE TYPE OR MODEL
WITH DIFFERENT LIFE LIMIT
EFTA_R1_00012856
EFTA01734588
P/N Compliance Print Print Date 10/05/2016 11 37
Page: 5 of 5
PIN: CFM1156.7-B27/83 PIN Description; GE AIRCRAFT ENGINE CFM; PIN SIN: 876170 PIN Hours: 12214:09 P/N Cycles: 4113 Days: 5830
Installed NC: A6DFR Installed Date: 05/08/2013
Schedule Remaining/
Amen/ NO Document/SB ec Description: Hrs/Cys/Dys/Dte Next Due Compliance Document Remarks
2014-0261 CR156-79-73-0204 ENGINE FUEL & CONTROL - ENGINE
ELECTRONIC CONTROL - SOFTWARE UPDATE
Category: AD
Status: TERMINATED
Reason
Rev: 01
FADEC SW UPGRADE IS DONE PER CFIA:45-78-73-0204 EARLIEST
SATISFIES THE INTENT OF THIS AD
2015-0133 ENGINE - ACCESSORY GEARBOX GEARSHAFT -
CFM56-7B-72-0964
NSPECTION I FtEPLACEMENT
Category: AD
Status: NIA
Reason
Rev: 00A THE ENGINE IS NOT INCLUDED IN THE AFFECTED
ENGINE SN UST OF THE AD EARUEST
2015-04.02 CFM56-715-73-0204 DUAL ENGINE THRUST INSTABILITY EVENT
Category: AD
Status: TERMINATED
Reason
Rev: 00
CFM56-76-734204 COMPLIED (INSTALUWEIN OF LATEST LATEST
FADEC SOFTWARE VERSION T.E.WF2) SATISFY THE AD
REQUIREMENT
2015-18-04 CFM56-7B-72.0964 73-TOOTH GEARSHAFT LOCATED IN THE ENGINE
ACCESSORY GEARBOX (AGB)
Category: AD
Status: N/A
Reason
Rev: 01 THE ENGINE is NOT INCLUDED IN THE EFFECTED UST
PER CCM 58 72-0904 LATEST
EFTA_R1_00012857
EFTA01734589
P/N Compliance Print Print Date 10/05/2016 11:35
Page: 1 05
P/N: CFM56.7-827/83 PIN Description: GE AIRCRAFT ENGINE CFM! PIN SIN: 889151 PIN Hours: 5999:05 P/N Cycles: 2160 Days: 5597
Installed NC: A6DFR Installed Date: 12/01/2001
Schedule Remaining/
Amon/ NO Document/SB SC Description: Hrs/Cys/Dys/Dte Next Due Compliance Document Remarks
1998-14-51T CFP.156-7B-72-130 STARTER GEARSHAFT REPLACEMENT AND MCD
INSPECTION
CFM56.78-72-132
Category: AD
Status: N/A
Reason
Rev: 00 WA AS THIS ENGINE IS NOT IN THE AFFECTED ENGINE
SM LIST LATEST
1998-18-51 UNCOMMANDED ENG ACCELERATION I INFLT
1958-21-23
SHUTDOWN
98-18.51
Category: AD CN 98.350
Status: TERMINATED Superseded By: 1908-21-23
CN T98-350 Reason
Rev: 0 SUPERSEDED BY 1998.21.23
SB 72-0130, 580132 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 CFM56 SELECTED CRITICAL LIFE LIMITED PARTS
2002-13-03 INSP
Category: AD
Superseded By: 2002-13-03
Status: TERMINATED
Rev: 3
EARLIEST
2001-02-12 INSPECT PS3 LINE FITTING
SB CFM56-78 72-0075
Category: AD
Status: N/A
Rev: 01
EARLIEST
EFTA_R1_00012858
EFTA01734590
P/N Compliance Print Print Date 10/05/2016 11:35
Page: 2 or 5
P/N: CFM56.7-B27/83 PIN Description: GE AIRCRAFT ENGINE CFM! PIN SIN: 889151 PIN Hours: 5999:05 P/N Cycles: 2160 Days: 5597
Installed NC: ABDFR Installed Date: 12/01/2001
Schedule Remaining/
Anent NO Document/SB BC Description: HrslCys/Dys/Dte Next Due Compliance Document Remarks
2001-11-05 REPLACEMENT OF NO.4 ROLLER BEARING PIN
SB 72.0329
305-355.717-0 IN DEFECTIVE BATCH
Category: AD
Status: NIA
Reason
Rev: 1 WA BY ENGINE SIN LARLILSI
2002-13.03 CFM56.76-72.241 LIFE LIMITED ROTATING PART FAILURE
Category: AD
Status: OPEN
Rev: 2A Recur
2002-16-18 CFM56-7B-72-241 REPLACEMENT OF 2ND AND 3RD STAGE LOW
PRESSURE TURBINE NOZZLE SEGMENTS
39-12857
Category: AD
Status: N/A
Rev: 1
EARLIEST
2003-03-01 AFT ENGINE MOUNT. CENTER LINK ASSY 09/05/2003 Rev: 2
2011.18.10 INSTALLATION INSPECTION
737-71A1462 Hours Cycles Days
Category: AD EIC Reset At 1103:35 595.00 847
Superseded By: 2011.18.10
Status: TERMINATED COMPLIED BY BOEING
Rev: 2 REPAIR STATION
EARLIEST BACR668L. RECORDS
WERE REVIEWED NO
ENGINE CHANGE
OCCURED. REFER U17
AC/ STATEMENT AT
DELIVERY TO
PRESIDENTIAL FLIGHT.
2006.2601 FUEL FILTER REPLACEMENT ( FOR PMA PARTS)
39.14859
Category: AD
Status: NIA
Rev: 0
EARLIEST
EFTA_R1_00012859
EFTA01734591
P/N Compliance Print Print Date 10/05/2016 11:35
Page: 3 of 5
P/N: CFM56-7-B27/83 PIN Description: GE AIRCRAFT ENGINE CFM; PIN S/N: 889151 PIN Hours: 5999:05 P/N Cycles: 2160 Days: 5597
Installed NC: A6DFR Installed Date: 12/01/2001
Schedule Remaining/
Amen NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Compliance Document Remarks
2008-03-09 TRF WITH TANGENTIAL STRUTS - MANDATORY 19/02/2008 Rev: 2
2007-0104
INSPECTIONS - LIFE TIMES
39-15359 CHASE-78-72-0558 19000 Cys 16840 Hours Cycles Days
Category: AD CFMS6.78-72.0579 E/C Reset At: 1294:57 687.00 2594
Status: OPEN 18/06/2062 AD REPEAT INSPECTION
Rev: 3 Recur IS BEING CONTROLLED
EARLIEST THROUGH SB
CFM56-78-72-0579. AD
CLOSED.
2009-0009 LPT REAR FRAME - LIFE LIMIT !MANDATORY
2010-01.05
INSPECTION
CFM56-76-72-0558
Category: AD CFM56-7B-72.0579
Status: N/A
Reason
Rev: 1 LPT REAR FRAME RN 340-186-206-0 INSTALLED IS NOT
AFFECTED BY THIS AD EARLIEST
2009-0270 LPT ROTOR STATOR ASSEMBLY •
CFM56-78-72-0743
REPLACEMENT
Category: AD
Status: N/A
Reason
Rev: 0
LPT STG 3 DISK INSTALLED IS NOT AFFECTED BY THIS
AD EARUEST
2010-13-09 LPT DISK - REMOVE FROM SERVICE SUSPECT
CFM56-78-72-0743
DISKS
39-16340
Category: AD
Status: N/A
Reason
Rev: 0 tPT DISKS INSTALLED IN PE/RI ENGINES ARE NOT
AFFECTED EARLIEST
EFTA_R1_00012860
EFTA01734592
P/N Compliance Print Print Date 10/05/2016 11:35
Page: 4 of 5
PIN: CFM1156-74127433 PIN Description: GE AIRCRAFT ENGINE CFM! PIN SIN: 889151 PIN Hours: 5999:05 PIN Cycles: 2160 Days: 5597
Installed NC: A6DFR Installed Date: 12/0112001
Schedule Remaining/
Amens NO Document/SB BC Description: HrslCyslDyslDte Next Due Compliance Document Remarks
2011-18-10 AFT ENGINE MOUNT - CENTER LINK ASSY • 12110/2011 Rev: 0
2003-03-01
INSPECTION TO ENSURE CORRECT
39-16792 737-71A1462 INSTALLATION Hours Cycles Days
Category: AD 737.71A1462-1 E/C Reset At: 2824:25 1186.00 3925
Status: TERMINATED DETAILED INSPECTION IN
Reason ACCORDANCE WITH SB
Rev: 3 COMPLIANCE OF AD 20030341. ENGINE HAS NOT BEEN
EARLIEST 737-71A1462, TO
CHANGED
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.
2012-0209 2013-26-01 ACCESSORY GEARBOX (AGO) HAND-CRANKING
PAD MODIFICATION
CFM56.76-72-0564
Category: AD CFM56.76-72.0879
Status: OPEN
Rev: 0 Once
2013-26.01 2012-0209 INDEPENDENT INSPECTION OF THE AGO
HANDCRANKING PAD COVER
CFM56.78.72-0564
Category: AD CFM56-78-72-0879
Status: TERMINATED
Reason
Rev: 0 AD SATISFIED BY AIAMENOINO AFFECTED ALP TASK
(72.320-01O2 AND 72.070-01102) TO INCLUDE EARLIEST
INDEPENDENT INSPECTION TO VERIFY
2014-0130 Tyne Lints - Engine Stationary Pans - Life Limits I
CROSS-2B ESM
Mandatory Inspections
Category: AO
Status: N/A
Reason
Rev: 0 NO EflA56-78 STATIONARY PART IN PF OR RJ FLEET HAS
PREVIOUSLY OPERATED ON ENGINE TYPE OR MODEL EARLIEST
DEFERENT LIFE umiT
EFTA_R1_00012861
EFTA01734593
P/N Compliance Print Print Date 10/05/2016 11:35
Page: 5 of 5
PIN: CFM1156.7-B27/83 PIN Description: GE AIRCRAFT ENGINE CFM; P/N SIN: 869151 PIN Hours: 5999:05 P/N Cycles: 2160 Days: 5597
Installed NC: A6DFR Installed Date: 12/01/2001
Schedule Remaining/
Amen/ NO Document/SB ec Description: HrslCys/Dys/Dte Next Due Compliance Document Remarks
2014-0261 CR156-78-73-0204 ENGINE FUEL & CONTROL - ENGINE
ELECTRONIC CONTROL - SOFTWARE UPDATE
Category: AD
Status: TERMINATED
Reason
Rev: 01
FADEC SW UPGRADE IS DONE PER CFM5648-734204 EARLIEST
SATISFIES THE INTENT OF THIS AD
2015-0133 ENGINE - ACCESSORY GEARBOX GEARSHAFT -
CFM56-7B-72-0964
NSPECTION I FtEPLACEMENT
Category: AD
Status: NIA
Reason
Rev: 00A THE ENGINE IS NOT INCLUDED IN THE AFFECTED
ENGINE SAN UST OF THE AD EARUEST
2015-04.02 CFM56-78-73-0204 DUAL ENGINE THRUST INSTABILITY EVENT
Category: AD
Status: TERMINATED
Reason
Rev: 00
CFM56-76-734204 COMPLIED (INSTALULTION OF LATEST
FADEC SOFTWARE VERSION 7.0.WF2) SATISFY THE AD LATEST
REQUIREMENT
2015-18-04 CFM56-7B-72.0964 73-TOOTH GEARSHAFT LOCATED IN THE ENGINE
ACCESSORY GEARBOX (AGB)
Category: AD
Status: N/A
Reason
Rev: 01 THE ENGINE IS NOT INCLUDED IN THE EFFECTED UST
PER CCM 58 72-0544 LATEST
EFTA_R1_00012862
EFTA01734594