# N449AZ: 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: 24985
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 27, 1997
- Certificate issued: February 15, 2019
- Expires: February 28, 2029
- Mode S code: A56C24
- 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=449AZ
- Page: https://openairdocs.org/aircraft/N449AZ

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/N449AZ/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 N449AZ.

## FAA accident and incident reports

None matched to N449AZ.

## Service difficulty reports (51, newest 50)

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 IXXA20251007062](https://openairdocs.org/sdr/IXXA20251007062), Oct 7, 2025: OIL SYSTEM. LEAKING. IN FLIGHT SHUT DOWN OF #1 ENGINE DUE TO LEFT OIL QUANTITY DEPLETED TO ZERO. LEFT OIL PRESSURE EICAS, LOWEST 10. AIRCRAFT GROUNDED FOR FURHTER INSPECTION AND MAI
- [SDR IXXA20250726037](https://openairdocs.org/sdr/IXXA20250726037), Jul 26, 2025: APU. SPARKS. UPON INITIAL WALK AROUND SPARKS WERE SEEN COMING OUT OF THE EXHAUST BEFORE APU SHUT DOWN. ACCOMPLISHED BORESCOPE FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS. REM
- [SDR IXXA2025021201](https://openairdocs.org/sdr/IXXA2025021201), Feb 12, 2025: BEAM. CRACKED. STUB BEAM CRACKED IN LOWER AREA OF RADIUS ON RIGHT SIDE
- [SDR IXXA20250208001](https://openairdocs.org/sdr/IXXA20250208001), Feb 8, 2025: STRUCTURE. CORRODED. CORROSION ON UNDER SIDE OF INNER CORD AT LOWER AFT CORNER OF FLC DOOR CUTOUT STA 612 RBL 45.
- [SDR IXXA2025020100000](https://openairdocs.org/sdr/IXXA2025020100000), Feb 1, 2025: SEAL. DAMAGED. #2 I/B T/R HAS 2 MISSDRILLED FASTENER HOLES
- [SDR IXXA20250201000](https://openairdocs.org/sdr/IXXA20250201000), Feb 1, 2025: THRUST REVERSER. MECHANIC ERROR. #2 I/B T/R HAS 2 MISSDRILLED FASTENER HOLES
- [SDR IXXA20250201001](https://openairdocs.org/sdr/IXXA20250201001), Feb 1, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON THE LOWER SURFACE OF THE BULK CARGO FLOOR PANEL SUPPORT, UNDER 3 NUTPLATES, FROM STA.1432 TO STA.1439, LBL42
- [SDR IXXA20231128084](https://openairdocs.org/sdr/IXXA20231128084), Nov 27, 2023: UNKNOWN. UNKNOWN. DURING SERVICE CHECK INSPECTIONS LINE MAINTENANCE IDENTIFIED EMERGENCY LIGHTS SWITCH GUARD NOT PULLING SWITCH TO ARMED POSITION. OVERHEAD PANEL SWITCH GUARD REM
- [SDR IXXA20231118001](https://openairdocs.org/sdr/IXXA20231118001), Nov 18, 2023: FAILSAFE. CORRODED. CORROSION ON FAILSAFE STRAP IN FLC DOOR CUTOUT
- [SDR IXXA2023112001](https://openairdocs.org/sdr/IXXA2023112001), Nov 14, 2023: SKIN. CRACKED. RI DOOR LOWER CORNER CRACKS ON FUSELAGE AND BEARSTRAP
- [SDR IXXA2023111701](https://openairdocs.org/sdr/IXXA2023111701), Nov 14, 2023: SKIN. CRACKED. FUSELAGE SKIN AND BEAR STRAP AT THE LOWER TWO HOLES OF THE R1 DOOR LOWER CORNER ARE CRACKED.
- [SDR IXXA2023110303](https://openairdocs.org/sdr/IXXA2023110303), Nov 3, 2023: SKIN. CRACKED. FUSELAGE SKIN AND BEAR STRAP IS CRACKED AT THE L1 DOOR LOWER CORNER.
- [SDR IXXA2023110301](https://openairdocs.org/sdr/IXXA2023110301), Nov 3, 2023: SKIN PANEL. DELAMINATED. RH SIDE OF VERTICAL STAB SKIN IS DELAMINATED.
- [SDR IXXA2023112002](https://openairdocs.org/sdr/IXXA2023112002), Oct 19, 2023: SHEAR TIE. CORRODED. SHEAR TIE AT STA 1562 BACK SIDE OF FRAME FOUND TO BE EXFOILATED OUT OF LIMITS
- [SDR IXXA20231015070](https://openairdocs.org/sdr/IXXA20231015070), Oct 11, 2023: UNKNOWN. UNKNOWN. POST FLIGHT CREW REPORTED, #6 INERTIAL REEL FELL OUT OF HOLDER. REMOVED INERTIAL REEL IAW B767 IAW SMM 25-61-03. SYSTEM FAULT TRANSFERRED TO DEFERRAL MAINTENANC
- [SDR IXXA20230416027](https://openairdocs.org/sdr/IXXA20230416027), Apr 16, 2023: SENSOR. INADEQUATE. CLIMB OUT OF 14,500 CLIMB 1 SETTING, RT ENG N1 FLUCTUATE APPROX 20% AFRAME VIB W/LOUD BANGING & YAWING. POSSIBLE COMPRESS STALL. AIR TURNBACK, EMERG DECLARED. L
- [SDR IXXA2022030501](https://openairdocs.org/sdr/IXXA2022030501), Mar 5, 2022: FAIRING. CRACKED. CORE COWL FAIRING CRACKED
- [SDR IXXA2022030403](https://openairdocs.org/sdr/IXXA2022030403), Mar 4, 2022: PANEL. DAMAGED. PYLON PANEL 446BR BACKING DAMAGED
- [SDR IXXA2022030402](https://openairdocs.org/sdr/IXXA2022030402), Mar 4, 2022: DRAIN LINE. CHAFED. DRAIN LINE CHAFED
- [SDR IXXA2022030401](https://openairdocs.org/sdr/IXXA2022030401), Mar 4, 2022: PANEL. CRACKED. PANEL 446CR CRACKED
- [SDR IXXA2022030304](https://openairdocs.org/sdr/IXXA2022030304), Mar 3, 2022: BRACKET. CRACKED. CRACKED SEAL BRACKET
- [SDR IXXA2022030303](https://openairdocs.org/sdr/IXXA2022030303), Mar 3, 2022: FAIRING. CRACKED. SKIRT FAIRING CRACKED
- [SDR IXXA2022030302](https://openairdocs.org/sdr/IXXA2022030302), Mar 3, 2022: BRACKET. CRACKED. SIDEWALL SUPPORT BRACKET CRACKED
- [SDR IXXA2022030301](https://openairdocs.org/sdr/IXXA2022030301), Mar 3, 2022: PANEL. CRACKED. P33 BACK PANEL CRACKED
- [SDR IXXA2022030211](https://openairdocs.org/sdr/IXXA2022030211), Mar 2, 2022: EXHAUST DUCT. CHAFED. CHAFE ON PRE-COOLER EXHAUST DUCT
- [SDR IXXA2022030210](https://openairdocs.org/sdr/IXXA2022030210), Mar 2, 2022: SEAL DEPRESSOR. DENTED. MDCD SEAL DEPRESSOR DENTED.
- [SDR IXXA2022030209](https://openairdocs.org/sdr/IXXA2022030209), Mar 2, 2022: ACCESS PANEL. CRACKED. #9 SLAT CONTROL ROD PANEL CRACKED.
- [SDR IXXA2022030208](https://openairdocs.org/sdr/IXXA2022030208), Mar 2, 2022: ACCESS PANEL. CRACKED. #10 SLAT CONTROL ROD PANEL CRACKED
- [SDR IXXA2022030207](https://openairdocs.org/sdr/IXXA2022030207), Mar 2, 2022: ACCESS PANEL. CRACKED. #11 SLAT CONTROL ROD PANEL CRACKED
- [SDR IXXA2022030206](https://openairdocs.org/sdr/IXXA2022030206), Mar 2, 2022: STRIP. CRACKED. STRIP CRACKED
- [SDR IXXA2022030205](https://openairdocs.org/sdr/IXXA2022030205), Mar 2, 2022: CHANNEL. CRACKED. PYLON PANEL 447DB HAS CRACKED CHANNEL
- [SDR IXXA2022030204](https://openairdocs.org/sdr/IXXA2022030204), Mar 2, 2022: ACCESS PANEL. TORN. PANEL 446CL SKIN IS TORN
- [SDR IXXA2022030203](https://openairdocs.org/sdr/IXXA2022030203), Mar 2, 2022: RETAINER SEAL. CRACKED. RIGHT FLAP O/B FAIRING SEAL SUPPORT CRACKED.
- [SDR IXXA2022030202](https://openairdocs.org/sdr/IXXA2022030202), Mar 2, 2022: STRINGER. CRACKED. RIGHT WING STRINGER L-9.5 STATION 976.2 CRACK INDICATION
- [SDR IXXA2022030201](https://openairdocs.org/sdr/IXXA2022030201), Mar 2, 2022: RETAINER SEAL. CRACKED. FLAP FAIRING I/B SEAL RETAINER CRACKED.
- [SDR IXXA2022022604](https://openairdocs.org/sdr/IXXA2022022604), Feb 26, 2022: ANGLE. CRACKED. SLAT ANGLE BRACKET CRACKED
- [SDR IXXA2022022603](https://openairdocs.org/sdr/IXXA2022022603), Feb 26, 2022: ATTACH ANGLE. CRACKED. SLAT ATTACH ANGLE CRACKED
- [SDR IXXA2022022602](https://openairdocs.org/sdr/IXXA2022022602), Feb 26, 2022: ANGLE. CRACKED. SLAT ANGLE CRACKED
- [SDR IXXA2022022601](https://openairdocs.org/sdr/IXXA2022022601), Feb 26, 2022: MOUNT BRACKET. CRACKED. PYLON PANEL HANGER CRACKED
- [SDR IXXA2022022504](https://openairdocs.org/sdr/IXXA2022022504), Feb 25, 2022: WEB. DAMAGED. PYLON STIFFENER DAMAGED.
- [SDR IXXA2022022503](https://openairdocs.org/sdr/IXXA2022022503), Feb 25, 2022: SEAL DEPRESSOR. CRACKED. SEAL DEPRESSOR CRACKED
- [SDR IXXA2022022502](https://openairdocs.org/sdr/IXXA2022022502), Feb 25, 2022: ATTACH ANGLE. CRACKED. CORE COWL ATTACH ANGLE BROKEN
- [SDR IXXA2022022501](https://openairdocs.org/sdr/IXXA2022022501), Feb 25, 2022: WEB. CRACKED. PYLON PANEL CRACKED V-WEB.
- [SDR IXXA2022022401](https://openairdocs.org/sdr/IXXA2022022401), Feb 24, 2022: ACCESS PANEL. DAMAGED. PYLON PANEL 441AT DAMAGED
- [SDR IXXA2022030305](https://openairdocs.org/sdr/IXXA2022030305), Feb 11, 2022: WEB. CORRODED. FLC BILGE PANEL @STA 610-632 LBL 12-36 FOUND TO BE CORRODED
- [SDR IXXA2022030404](https://openairdocs.org/sdr/IXXA2022030404), Feb 9, 2022: NONE. CRACKED. PANEL 446CR HAS LOWER CORNER OF PANEL BROKEN OFF
- [SDR IXXA2022022403](https://openairdocs.org/sdr/IXXA2022022403), Feb 9, 2022: ROD. CRACKED. #2 PYLON HYD BAY DOOR O/B HOLD OPEN ROD FOUND BROKEN
- [SDR IXXA2022022402](https://openairdocs.org/sdr/IXXA2022022402), Feb 9, 2022: PANEL. CHAFED. # 1 PYLON PANEL 437AL CHAFED
- [SDR IXXA20210729333](https://openairdocs.org/sdr/IXXA20210729333), Jul 25, 2021: ESCAPE REEL. UNWANTED DEPLOY. LINE MAINTENANCE REPORTS AFTER BLOCK IN,3 EMERGENCY DESCENT REELS DEPLOYED. WORK IN PROGRESS.
- [SDR IXXA20210522037](https://openairdocs.org/sdr/IXXA20210522037), May 18, 2021: WARNING LIGHT. ILLUMINATED. ENROUTE FROM KAFW TO KJFK LEFT ENGINE SHUTDOWN AND LEFT ENGINE FUEL VALVE EICAS MESSAGE DISPLAYED. AT FL210 (CLIMBOUT) EGT EXCEEDED AT 831, LEFT THRUST REVERSER

All 51: https://openairdocs.org/aircraft/N449AZ/reports.md

## 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

## Earlier aircraft with N449AZ

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N449AZ before.

- [Cancelled 2011-02-08](https://openairdocs.org/deregistered/N449AZ-2011-02-08): Puriton Frederick M PURITON RV-6A, S/N 23902, built 1999. Exported to South Africa. Owner: [Purinton Sylvia A](https://openairdocs.org/faa-owner/PURINTON%20SYLVIA%20A), [Prescott, AZ](https://openairdocs.org/faa-place/AZ/Prescott)

## 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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