# N409AZ: 1990 Boeing 767-3P6

- Status: Valid registration
- Airframe: [Boeing 767-3P6](https://openairdocs.org/model/boeing-767-3p6) (registry code 1385105, 290 seats)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 24983
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 23, 1997
- Certificate issued: February 20, 2019
- Expires: February 28, 2029
- Mode S code: A4CE28
- Registered owner: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC)
- Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=409AZ
- Page: https://openairdocs.org/aircraft/N409AZ

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every GE CF6-80 model are included.

## ADs that may apply (OpenAirDocs): 61 in force

### Matched by airframe (Boeing 767-3P6)

None in force.

### Matched by engine (GE CF6-80 series)

- [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025
- [AD 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023
- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020
- [AD 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018
- [AD 2017-11-15](https://openairdocs.org/ad/2017-11-15): Turbine/ Turboprop Engine--Turbine Section · General Electric CF6-80C2L1F. Effective Jul 13, 2017
- [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016
- [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014
- [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013
- [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012
- [AD 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 2012
- [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009
- [AD 2009-14-08](https://openairdocs.org/ad/2009-14-08): High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts · General Electric CF6-80C2B5F. Effective Aug 5, 2009
- [AD 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor  
 disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009
- [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 2009
- [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009
- [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008
- [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-24-07](https://openairdocs.org/ad/2007-24-07): Thermal spray coating on certain stage 1 fan disks · General Electric CF6-80C2B1. Effective Jan 2, 2008
- [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007
- [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2001-06-09](https://openairdocs.org/ad/2001-06-09): Aft Engine Mount Link Assemblies · General Electric CF6-80A3. Effective May 1, 2001
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000
- [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996
- [AD 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995
- [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995
- [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994
- [AD 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 1994
- [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994

### Historical (superseded or no longer in force)

- [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020
- [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018
- [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009
- [AD 2007-12-07](https://openairdocs.org/ad/2007-12-07) (historical): Electronic control units (ECUs) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 5 more. Effective Jul 11, 2007
- [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004
- [AD 2003-01-05](https://openairdocs.org/ad/2003-01-05) (historical): Dovetail slots · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jan 28, 2003
- [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002
- [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001
- [AD 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000
- [AD 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 2000
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000
- [AD 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999
- [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999
- [AD 98-15-17](https://openairdocs.org/ad/98-15-17) (historical): Link Assembly · General Electric CF6-80A3. Effective Aug 7, 1998
- [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991
- [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990

All 80: https://openairdocs.org/aircraft/N409AZ/ads.md

## Information bulletins (advisory) (5 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010
- [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser  Transcowl Clevis Pin. Issued Sep 3, 2008
- [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006

## NTSB investigations

None matched to N409AZ.

## FAA accident and incident reports

None matched to N409AZ.

## Service difficulty reports (41)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR IXXA20260802067](https://openairdocs.org/sdr/IXXA20260802067), Aug 2, 2026: WINDOW. INOPERATIVE. FIRST OFFICERS WINDOW DOES NOT APPEAR TO MECHANICALLY CLOSE ALL THE WAY. ADJUSTED R2 WINODW IN ACCORDANCE WITH B767 AMM 56-11-02. OPERATIONAL CHECK GOOD. ACCOMP
- [SDR IXXA20260512001](https://openairdocs.org/sdr/IXXA20260512001), May 12, 2026: ANGLE. CRACKED. FOUND CRACK ON UPPER ANGLE ON FRONT SPAR ABOVE PDU LES150-148
- [SDR IXXA20260123006](https://openairdocs.org/sdr/IXXA20260123006), Jan 23, 2026: SLIDING WINDOW. OUT OF ALIGNMENT. L2 WINDOW OPENED BUT WILL NOT CLOSE. ACCOMPLISHED ADJUSTEMENT OF L2 WINDOW AND LUBED SEAL IN ACCORDANCE WITH B767 AIRCRAFT MAINTENANCE MANUAL 56-11-02. OPERATIO
- [SDR IXXA20250703003](https://openairdocs.org/sdr/IXXA20250703003), Jul 3, 2025: FAIRING. CHAFED. LT O/B FLAP FAIRING 573BB SEAL RETAINER AND SEAL ARE CHAFED
- [SDR IXXA20250703002](https://openairdocs.org/sdr/IXXA20250703002), Jul 3, 2025: BEAM. CRACKED. #1 PYLON AFT STINGER FAIRING INTERNAL I/B I-BEAM BROKEN PIECE
- [SDR IXXA20250703001](https://openairdocs.org/sdr/IXXA20250703001), Jul 3, 2025: SKIN. CHAFED. LEFT WING AFT FLAP L\E CHAFED BEYOND LIMITS
- [SDR IXXA20250702003](https://openairdocs.org/sdr/IXXA20250702003), Jul 2, 2025: RETAINER. CHAFED. RT I/B FLAP FAIRING 671DB I/B SEAL RETAINER AND SEAL ARE CHAFED
- [SDR IXXA20250702002](https://openairdocs.org/sdr/IXXA20250702002), Jul 2, 2025: SKIN. GOUGED. #1 SLAT I/B SURFACE GOUGED
- [SDR IXXA20250613002](https://openairdocs.org/sdr/IXXA20250613002), Jun 13, 2025: STRUCTURE. CRACKED. NUMBER 1 PYLON INTERNAL O/B CORD CRACKED AND BROKEN ON FWD AND AFT ENDS SEEN THROUGH ACCESS PANEL 436AL
- [SDR IXXA20250613001](https://openairdocs.org/sdr/IXXA20250613001), Jun 13, 2025: ANGLE. CRACKED. NUMBER 1 PYLON INTERNAL UPPER O/B ANGLE CRACKED AT TOP SIDE OF FRAME SEEN THROUGH O/B ACCESS PANEL 436AL
- [SDR IXXA20240510029](https://openairdocs.org/sdr/IXXA20240510029), May 7, 2024: FLAP SYSTEM. FAULTED. ON APPROACH TO KRFD CREW REPORTED EXECUTING GO-AROUND DUE TO WIND SHEAR/UNSTABLE APP. ON FLAP RETRACTION EICAS LE SLAT SYM. EXTRA CONTROL FORCES RIGHT YOKE TO R
- [SDR IXXA20240212004](https://openairdocs.org/sdr/IXXA20240212004), Feb 10, 2024: UNKNOWN. ODOR. DURING SCHEDULED INSPECTIONS LINE MAINTENANCE REPORTED WITH LEFT AND RIGHT PACKS IN OPERATION EXHAUST SMELLS IN THE THE FLIGHT DECK WERE NOTED. SMOKE OR FUMES I
- [SDR IXXA20240209003](https://openairdocs.org/sdr/IXXA20240209003), Feb 8, 2024: BATTERY. INOPERATIVE. DURING SCHEDULED INSPECTIONS LINE MAINTENANCE REPORTED, LEFT EMERGENCY LIGHTS INOPERATIVE. FORWARD EMERGENCY LIGHT BATTERY REMOVED AND REPLACED. OPERATIONAL CHE
- [SDR IXXA20230914062](https://openairdocs.org/sdr/IXXA20230914062), Sep 13, 2023: UNKNOWN. UNKNOWN. POST FLIGHT, CREW REPORTED EMERGENCY LIGHTS SWITCH COVER WILL NOT STAY CLOSED. REMOVED AND REPLACED EMERGENCY LIGHTS SWITCH GUARD IAW B767 SWPM 20-83-11. OPERAT
- [SDR IXXA2022071004](https://openairdocs.org/sdr/IXXA2022071004), Jul 10, 2023: COWLING. DAMAGED. #2 ENGINE I/B CORE COWL HAS A HOLE IN THE UPPER AFT EXTERIOR NAC 220-225
- [SDR IXXA2023070701](https://openairdocs.org/sdr/IXXA2023070701), Jul 7, 2023: SEAT TRACK. CRACKED. FIRST OFFICER INBOARD SEAT TRACK CRACKED.
- [SDR IXXA2023070203](https://openairdocs.org/sdr/IXXA2023070203), Jul 2, 2023: STRINGER. CRACKED. STRINGER CAP CRACKED @ STA 340,S24R
- [SDR IXXA2023070202](https://openairdocs.org/sdr/IXXA2023070202), Jul 2, 2023: SEAL DEPRESSOR. DAMAGED. MCD CUTOUT FORWARD LOWER CORNER DAMAGED
- [SDR IXXA2023070201](https://openairdocs.org/sdr/IXXA2023070201), Jul 2, 2023: SEAL DEPRESSOR. DAMAGED. MCD CUTOUT AFT LOWER CORNER DAMAGED
- [SDR IXXA2023071003](https://openairdocs.org/sdr/IXXA2023071003), Jun 28, 2023: SKIN. DAMAGED. LMLG WHEEL WELL FUSELAGE FORWARD OF BODY DOOR IS DAMAGED AT AND AROUND DOUBLER REPAIR
- [SDR IXXA202306280001](https://openairdocs.org/sdr/IXXA202306280001), Jun 28, 2023: SKIN. DAMAGED. LW LEADING EDGED HAS COMPOSITE DAMAGE.
- [SDR IXXA2023062703](https://openairdocs.org/sdr/IXXA2023062703), Jun 27, 2023: SKIN. ABNORMAL. HOLE IN SKIN FOUND @ STA 344, S21R
- [SDR IXXA2023062702](https://openairdocs.org/sdr/IXXA2023062702), Jun 27, 2023: SUPPORT. CRACKED. LW, T/E, I/B FLAP ANGLE GEARBOX SUPPORT PLATE CRACKED
- [SDR IXXA2023062701](https://openairdocs.org/sdr/IXXA2023062701), Jun 27, 2023: SEAT TRACK. CRACKED. FIRST OFFICERS FWD SEAT TRACK CRACKED
- [SDR IXXA2023071002](https://openairdocs.org/sdr/IXXA2023071002), Jun 14, 2023: SKIN. CRACKED. R1 DOOR CUTOUT AFT LOWER CORNER CRACKED
- [SDR IXXA2023071001](https://openairdocs.org/sdr/IXXA2023071001), Jun 14, 2023: SKIN. CRACKED. L1 DOOR CUTOUT AFT LOWER CORNER CRACKED
- [SDR IXXA20220707121](https://openairdocs.org/sdr/IXXA20220707121), Jul 4, 2022: WINDOW. INOPERATIVE. DURING ROUTINE MAINTENANCE, R2 WINDOW DIFFICULT TO CLOSE. ADJUSTED R2 WINDOW IAW B767 AMM 56-11-02. OPERATIONAL AND LEAK CHECK GOOD. FAULT NOT DUPLICATED.
- [SDR IXXA20211128072](https://openairdocs.org/sdr/IXXA20211128072), Nov 24, 2021: PANEL. FAULTY. POST FLIGHT, CREW REPORTED OVERHEAD EMERGENCY DOOR LIGHT KEEPS BLINKING/FLASHING ON AND OFF. NO EICAS MESSAGE INDICATIONS OR FAULTS WITH PRESSURIZATION NOTED. S
- [SDR IXXA20211109073](https://openairdocs.org/sdr/IXXA20211109073), Oct 29, 2021: BEAM. CORRODED. #2 PYLON OUTBOARD HYDRAULIC BAY DOOR CUTOUT LOWER BEAM FWD END NUT PLATE BROKEN AND BEAM CHAFFED. REMOVED AND REPLACED #2 PYLON OUTBOARD HYDRAULIC DOOR LOWER BE
- [SDR IXXA20210791109](https://openairdocs.org/sdr/IXXA20210791109), Oct 27, 2021: FLAP. DELAMINATED. UPPER SURFACE OFF TRAILING EDGE OUTBOARD FLAP DELAM AREA 46" INBOARD FROM OUTBOARD EDGE AND 10" FROM TRAILING EDGE. REPAIRED DAMAGE ON RIGHT WING OUTBOARD FLAP 
- [SDR IXXA20211109074](https://openairdocs.org/sdr/IXXA20211109074), Oct 27, 2021: PLATE. CRACKED. #2 PYLON STRINGER FAIRING 447DB FORWARD OUTBOARD ATTACH ANGLE FLANGE CRACKED LOWER ON PYLON. REMOVED AND REPLACED SPLICE FLANGE ON #2 PYLON V WEB IAW B767 SRM 5
- [SDR IXXA20211109072](https://openairdocs.org/sdr/IXXA20211109072), Oct 27, 2021: BRACKET. CRACKED. #2 PYLON INBOUND HYDRAULIC BAY DOOR 447BL ACCESS HYDRAULIC DRAIN LINE AFT SUPPORT BRACKET CRACKED. REMOVED AND REPLACED AFT HYDRAULIC DRAIN LINE SUPPORT IAW B76
- [SDR IXXA20211109071](https://openairdocs.org/sdr/IXXA20211109071), Oct 27, 2021: SPLICE PLATE. CHAFED. #2 PYLON OUTBOARD SIDE ACCESS 447AR PANEL AFT MATING FLANGE CHAFFED. REMOVED, FABBED AND INSTALLED REPLACEMENT AFT MATING FLANGE IAW B767 SRM 51-40-02 PARA 9 AN
- [SDR IXXA20211109077](https://openairdocs.org/sdr/IXXA20211109077), Oct 25, 2021: NONE. NONE. #12 SLAT HAS AREA OF DELAMINATION ON UPPER TRAILING EDGE WEDGE. REPAIRED AREA OF DELAMINATION ON #12 SLAT TRAILING EDGE WEDGE IAW B767 SRM 51-70-10.
- [SDR IXXA20211109075](https://openairdocs.org/sdr/IXXA20211109075), Oct 24, 2021: SLAT. CRACKED. GOUGE IN BOTTOM SIDE OF UPPER TRAILING EDGE OF LEFT WING NUMBER 3 SLAT LOCATED APPROXIMATELY AT OSS 734.74. REPAIRED BOTTOME SIDE OF THE UPPER TRAILING EDGE WED
- [SDR IXXA20211109070](https://openairdocs.org/sdr/IXXA20211109070), Oct 22, 2021: FRAME. CORRODED. T FRAME AT AFT END OF KEEL PANEL 139BL IS CORRODED. T FRAME BLENDED AND REPLACED AS REQUIRED IAW B767 SRM 53-50-12 ALLOWABLE DAMAGE 1 FIG 101 DETAIL VII B767 SR
- [SDR IXXA20211109078](https://openairdocs.org/sdr/IXXA20211109078), Oct 21, 2021: SLAT. DENTED. #1 SLAT HAS DENT ON UPPER TRAILING EDGE WEDGE. DENT REPAIRED AT 250 FARENHEIT UNDER VACCUM IAW B767 SRM 51-70-10. DENT LENGTH 8 INCHES BY 21 INCHES
- [SDR IXXA20211109076](https://openairdocs.org/sdr/IXXA20211109076), Oct 19, 2021: RIB. CRACKED. LEFT WING NOSE FORMER AT WING STATION 450 CRACKED. REMOVED AND REPLACED CRACKED FORMER AT LOWER STATION 450 IAW B767-300 SRM 51-40-02.
- [SDR IXXA20211109069](https://openairdocs.org/sdr/IXXA20211109069), Oct 18, 2021: BRACKET. CRACKED. FORWARD INBOARD UPPER ATTACH ANGLE IS CRACKED ON P34 PANEL IN MEC. REMOVED AND REPLACED MOUNTING BRACKET FWD INBD UPPER ON P34 PANEL IN MEC IAW B767 SRM 51-40-0
- [SDR IXXA20211028](https://openairdocs.org/sdr/IXXA20211028), Oct 12, 2021: FAIRING. CRACKED. DMI 26031, L/P 572823-5 FOUND ON WALK- FWD OF MLG DOOR, STA 599, CRACK 9 IN. LONG FILLER SHEET METAL. AWAITING EO REPAIR FROM ENGINEERING. AMES N/R 139923-0100-
- [SDR IXXA20211002048](https://openairdocs.org/sdr/IXXA20211002048), Oct 2, 2021: NONE. NONE. SUPPLEMENTAL-ENROUTE KTPA TO KILN, RIGHT ENGINE UNCOMMANDED SHUTDOWN. SUSPECTED OIL PRESSURE BELOW 10 PSI WINDMILL. ENGINE BOTTLE 2 DISCHARGE DUE TO LOOP FAIL A

## STCs that may be installed (OpenAirDocs) (6)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (GE CF6-80 series)

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic. Lists CF6-80A
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic. Lists CF6-80C2 Series
- [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc. Lists CF6-80A
- [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series
- [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc. Lists CF6-80C2A1
- [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc

## Related

- Other Boeing 767-3P6 aircraft: https://openairdocs.org/model/boeing-767-3p6/aircraft.md
- The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.md

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