# N1049A: 1999 Boeing 767-36N

- Status: Valid registration
- Airframe: [Boeing 767-36N](https://openairdocs.org/model/boeing-767-36n) (registry code 1385152, 290 seats)
- Engine: [GE CF6-80C2B7F](https://openairdocs.org/engine/ge-cf6-80c2b7f) (registry code 30114)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 30109
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 27, 2016
- Certificate issued: May 14, 2023
- Expires: May 31, 2030
- Mode S code: A01724
- Registered owner: [Andromeda Leasing II LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20II%20LLC)
- Location: [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase)
- Owner type: LLC
- Owner's area on the map: 41.0382° N, 73.7107° W: Placed by OpenAirDocs at the center of ZIP code 10577, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1049A
- Page: https://openairdocs.org/aircraft/N1049A

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.

## ADs that may apply (OpenAirDocs): 32 in force

### Matched by airframe (Boeing 767-36N)

None in force.

### Matched by engine (GE CF6-80C2B7F)

- [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 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 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 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 2009-07-03](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 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 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 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 2003-02-07](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 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 95-10-11](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 94-06-03](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
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993

### 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 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 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 2000-16-12](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 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999

## 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 N1049A.

## FAA accident and incident reports

None matched to N1049A.

## Service difficulty reports (198, 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 IXXA20260302019](https://openairdocs.org/sdr/IXXA20260302019), Mar 2, 2026: GUARD. BROKEN. CREW REPORTED ELT RED GUARD SWITCH COVER BROKEN. PLACED ON DEFERRAL 71102 MINIMUM EQUIPMENT LIST ATI-23-24-01-04 CATEGORY D. FOUND SWITCH GUARD WAS MISSING BREA
- [SDR IXXA20250819046](https://openairdocs.org/sdr/IXXA20250819046), Aug 19, 2025: COVER. OUT OF POSITION. EMERGENCY LIGHTS SWITCH COVER TURNS SWITCH OFF WHEN CLOSED. METAL BAR FOUND OUT OF POSITION AND WOULD FORCE SWITCH INTO OFF POSITION. ADJUSTED METAL BAR BACK IN
- [SDR IXXA2025061301](https://openairdocs.org/sdr/IXXA2025061301), Jun 13, 2025: DOOR. ERODED. #2 ENG IB TR INSIDE LIP ON THE IDG DOOR HAS CHAFFING WEAR ON LANDING
- [SDR IXXA202506132001](https://openairdocs.org/sdr/IXXA202506132001), Jun 12, 2025: HINGE. ELONGATED. #2 ENGINE PYLON HYD BAY ACCESS PANEL 447BR AFT HINGE HAS PLAY
- [SDR IXXA20250619003](https://openairdocs.org/sdr/IXXA20250619003), Jun 11, 2025: SKIN. DAMAGED. RUDDER HAS SEVERAL LIGHTNING STRIKES AFT OF SMILE RT SIDE. HAECO WO 320013 NON ROUTINE 39028
- [SDR IXXA20250609001](https://openairdocs.org/sdr/IXXA20250609001), Jun 9, 2025: WEB. DAMAGED. E&E DOOR UPPER AFT TRACK HAS DRILL START & GOUGE UNDER TRACK
- [SDR IXX2025F00010](https://openairdocs.org/sdr/IXX2025F00010), Jun 5, 2025: SKIN. GOUGED. #1 OB CORE COWL EXTERNAL SKIN IS GOUGED AT AFT LOWER EDGE
- [SDR IXXA2025060500003](https://openairdocs.org/sdr/IXXA2025060500003), Jun 4, 2025: STRUCTURE. CRACKED. #2 ENGINE PYLON INTERNAL OF ZONE 442 INBD UPPER CHORD IS CRACKED AT APPROX NAC STA 221.5
- [SDR IXXA20250604002](https://openairdocs.org/sdr/IXXA20250604002), Jun 4, 2025: SKIN. DENTED. L/H WING INBD AFT FLAP LOWER SURFACE OF THE L/E PANEL IS DENTED APPROX 4" OTBD OF THE OTBD TRACK FAIRING
- [SDR IXXA202506040001](https://openairdocs.org/sdr/IXXA202506040001), Jun 4, 2025: FAN COWL. DAMAGED. #1 ENG O/B FAN COWL DOOR FWD EDGE LANDING SHOWING COMPOSITES MISSING PROTECTIVE FINISH
- [SDR IXXA20250603004](https://openairdocs.org/sdr/IXXA20250603004), Jun 3, 2025: FAN COWL. ERODED. #1 ENG I/B FAN COWL DOOR FWD EDGE LANDING SHOWING COMPOSITE EROSION DAMAGE
- [SDR IXXA20250603003](https://openairdocs.org/sdr/IXXA20250603003), Jun 3, 2025: FAN COWL. DAMAGED. #2 ENG I/ FAN COWL DOOR FWD EDGE LANDING HAS COMPOSITES SHOWING PAINT MISSING AND WIRE MESH DAMAGE OUT OF LIMITS
- [SDR IXXA20250603002](https://openairdocs.org/sdr/IXXA20250603002), Jun 3, 2025: STOP FITTING. GOUGED. 119AL E&E DOOR FWD LH STOP FITTING HAS A GOUGE
- [SDR IXXA20250303001](https://openairdocs.org/sdr/IXXA20250303001), Jun 3, 2025: STOP FITTING. GOUGED. 119AL E&E DOOR FWD RH STOP HAS GOUGE
- [SDR IXXA20250602001](https://openairdocs.org/sdr/IXXA20250602001), Jun 2, 2025: STIFFENER. CRACKED. CRACK FOUND ON RIGHT HAND VERTICAL STIFFNER IN THE NOSE LANDING GEAR WHEEL WELL 10INCHES ABOVE ELECTRICAL PANEL BOX
- [SDR IXXA20250529002](https://openairdocs.org/sdr/IXXA20250529002), May 29, 2025: FRAME. GOUGED. O/B CORE COWL #1 ENG 2ND FRAME SUPPORT STRUCTURE FROM FWD HAS GOUGE
- [SDR IXXA20250529001](https://openairdocs.org/sdr/IXXA20250529001), May 29, 2025: SKIN. DELAMINATED. L/W O/B AILERON UPPER SURFACE HAS DAMAGED COMPOSITES AT O/B TRAILING EDGE
- [SDR IXXA20250524001](https://openairdocs.org/sdr/IXXA20250524001), May 15, 2025: BRACKET. CRACKED. #2 PYLON AFT FAIRING ASSY ATTACH ANGLE IS CRACKED ON O/B AFT UPPER CORNER STRUCTURE COMMON TO PANEL 447CR
- [SDR IXXA20250618001](https://openairdocs.org/sdr/IXXA20250618001), May 13, 2025: ATTACH ANGLE. DAMAGED. MAIN CARGO DOOR CUTOUT - LOWER SEAL DEPRESSOR ATTACH ANGLE ELONGATED HOLES ON FWD AND AFT ENDS
- [SDR IXXA20256018002](https://openairdocs.org/sdr/IXXA20256018002), May 5, 2025: COWLING. CHAFED. #2 ENG IB TR INSIDE LIP ON IDG DOOR HAS CHAFFING WEAR ON LANDING. HAECO WO 320013 NON ROUTINE 38713
- [SDR IXXA20250522002](https://openairdocs.org/sdr/IXXA20250522002), May 4, 2025: FITTING. CRACKED. LH WING INBD FLAP HINGE ARM FOR THE AFT FLAP IS CRACKED AT THE ATTACH FLANGE COMMON TO THE LOWER SURFACE SKIN
- [SDR IXXA20250616001](https://openairdocs.org/sdr/IXXA20250616001), May 3, 2025: RIB. WORN. RIGHT WING #8 SLAT OUTBOARD SIDE EDGE IS WORN IN 2 PLACES. HAECO SERVICE ORDER 320013, NR 38540
- [SDR IXXA20250523001](https://openairdocs.org/sdr/IXXA20250523001), May 3, 2025: SKIN SPLICE. CRACKED. RH WING FIXED LEADING EDGE SKIN PLATE IS CRACKED AT APPROX OFSS 505
- [SDR IXXA20250521003](https://openairdocs.org/sdr/IXXA20250521003), May 3, 2025: FORMER. CRACKED. RH WING FIXED LEADING EDGE SKIN FORMER IS CRACKED AT APPROX OFSS 490
- [SDR IXXA20250513002](https://openairdocs.org/sdr/IXXA20250513002), May 2, 2025: FORMER. CRACKED. LEFT WING FIXED LEADING-EDGE FORMER CRACKED AT APPROX OSS 490. HAECO SERVICE ORDER 320013 AND NR 38512
- [SDR IXXA20250513001](https://openairdocs.org/sdr/IXXA20250513001), May 2, 2025: FORMER. CRACKED. LEFT WING FIXED LEADING-EDGE FORMER IS CRACKED AT APPROX OSS 563. HAECO SERVICE ORDER 320013, NR 38499
- [SDR IXXA20250521002](https://openairdocs.org/sdr/IXXA20250521002), May 1, 2025: ATTACH BOLT. CRACKED. LH WING #6 SLAT AT OUTBD CONTROL ROD LOWER ATTACH L BRACKET IS CRACKED
- [SDR IXXA20250619002](https://openairdocs.org/sdr/IXXA20250619002), Apr 29, 2025: SKIN. CRACKED. CRACK INDICATION FOUND IN L1 FWD ENTRY DOOR CUTOUT LOWER AFT CORNER
- [SDR IXXA20250619001](https://openairdocs.org/sdr/IXXA20250619001), Apr 29, 2025: SKIN. CRACKED. R1 FWD SERVICE DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP HAS CRACK EXTENDING FROM SECOND LOWER FASTENER HOLE AS MARKED
- [SDR IXXA20241216083](https://openairdocs.org/sdr/IXXA20241216083), Dec 15, 2024: ACM. MALFUNCTIONED. ENROUTE FROM KCVG TO KBDL CREW REPORTED FWD EQPT OVHT EICAS MESSAGE. CREW COMPLIED WITH ATI QRH; CABIN STARTED TO CLIMB. DIVERTED TO KBUF & AN EMERG DESCENT. LA
- [SDR IXXA20240903060](https://openairdocs.org/sdr/IXXA20240903060), Aug 31, 2024: BATTERY. INOPERATIVE. POST FLIGHT CREW REPORTED, WITH EMERGENCY LIGHTS IN ARMED POSITION EMERGENCY LIGHTS TURN ON AND OFF INTERMITTENTLY (SUPERNUMERY AREA). FAULT TRANSFERRED TO DEFE
- [SDR IXXA20240903059](https://openairdocs.org/sdr/IXXA20240903059), Aug 31, 2024: BATTERY. INOPERATIVE. POST FLIGHT CREW REPORTED, WITH EMERGENCY LIGHTS IN ARMED POSITION EMERGENCY LIGHTS TURN ON AND OFF INTERMITTENTLY (SUPERNUMERY AREA). FAULT TRANSFERRED TO DEFE
- [SDR IXXA2024080902001](https://openairdocs.org/sdr/IXXA2024080902001), Aug 9, 2024: SKIN. DAMAGED. LH HORIZONTAL STAB UPPER BONDED PANEL JUST AFT OF L/E DAMAGED
- [SDR IXXA20240803055](https://openairdocs.org/sdr/IXXA20240803055), Jul 2, 2024: GENERATOR. FAULTED. ENROUTE FROM KCLT TO KSBD R GEN DRIVE MESSAGE DISPLAYED ON EICAS FL340. APU INOPERATIVE DUE TO SYSTEM ACTIVELY IN DEFERRED MAINTENANCE STATUS. PER ATI MINIMUM E
- [SDR IXXA20240613039](https://openairdocs.org/sdr/IXXA20240613039), Jun 13, 2024: BATTERY. NO TEST. FOLLOWING SCHEDULED CHECKS AND INSPECTIONS, LINE MAINTENANCE REPORTED BATHROOM WALL EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE ITEM-52497 PER ATI MINIMUM EQU
- [SDR IXXA20240612038](https://openairdocs.org/sdr/IXXA20240612038), Jun 11, 2024: BATTERY. NO TEST. FOLLOWING SCHEDULED CHECKS AND INSPECTIONS, LINE MAINTENANCE REPORTED CENTER PEDESTAL EMERGENCY FLASHLIGHT INOPERATIVE. CENTER PEDESTAL EMERGENCY FLASHLIGHT BAT
- [SDR IXXA2023090802](https://openairdocs.org/sdr/IXXA2023090802), Sep 8, 2023: SKIN. CRACKED. RH FWD SERVICE DOOR CUTOUT AFT LWR CORNER CRACKED.
- [SDR IXXA2023042701](https://openairdocs.org/sdr/IXXA2023042701), Apr 27, 2023: SEAT TRACK. CRACKED. FIRST OFFICERS FORWARD O/B SEAT TRACK IS CRACKED.
- [SDR IXXA2023042604](https://openairdocs.org/sdr/IXXA2023042604), Apr 26, 2023: ROLLER TRAY. CORRODED. ROLLER TRAY CORRODED
- [SDR IXXA2023042603](https://openairdocs.org/sdr/IXXA2023042603), Apr 26, 2023: WEB. CORRODED. FLOOR SUPPORT WEB CORRODED
- [SDR IXXA2023042602](https://openairdocs.org/sdr/IXXA2023042602), Apr 26, 2023: FAILSAFE. CRACKED. LH STA. 955 FAIL SAFE STRAP CRACKED
- [SDR IXXA2023042601](https://openairdocs.org/sdr/IXXA2023042601), Apr 26, 2023: PANEL. CRACKED. PANEL 521BB CRACKED.
- [SDR IXXA2023041501](https://openairdocs.org/sdr/IXXA2023041501), Apr 15, 2023: SEAT TRACK. CRACKED. CAPTIANS FORWARD O/B SEAT TRACK CRACKED.
- [SDR IXXA2023041202](https://openairdocs.org/sdr/IXXA2023041202), Apr 12, 2023: SEAT TRACK. CRACKED. CAPTAIN'S FORWARD IB SEAT TRACK IS CRACKED
- [SDR IXXA2023041201](https://openairdocs.org/sdr/IXXA2023041201), Apr 12, 2023: SEAT TRACK. CRACKED. FIRST OFFICERS FORWARD O/B SEAT TRACK CRACKED
- [SDR IXXA2023040803](https://openairdocs.org/sdr/IXXA2023040803), Apr 8, 2023: SEAT TRACK. WORN. CAPTAINS I/B AFT SEAT TRACK HOLE ELONGATED AND WEAR ON TOP FLANGE.
- [SDR IXXA2023040802](https://openairdocs.org/sdr/IXXA2023040802), Apr 8, 2023: SEAT TRACK. WORN. FO AFT I/B SEAT TRACK HOLES ELONGATED AND WEAR ON TOP FLANGE
- [SDR IXXA2023040801](https://openairdocs.org/sdr/IXXA2023040801), Apr 8, 2023: ROLLER TRAY. CORRODED. ROLLER TRAY CORRODED
- [SDR IXXA2023040104](https://openairdocs.org/sdr/IXXA2023040104), Apr 1, 2023: FITTING. CRACKED. CARGO HANDLING SUPPORT FITTING CRACKED
- [SDR IXXA202304010003](https://openairdocs.org/sdr/IXXA202304010003), Apr 1, 2023: ROLLER TRAY. CORRODED. ROLLER TRAY CORRODED

All 198: https://openairdocs.org/aircraft/N1049A/reports.md

## STCs that may be installed (OpenAirDocs) (5)

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 CF6-80C2B7F)

- [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
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic. Lists CF6-80C2 Series
- [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
- [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. Lists CF6-80 Series

## Earlier aircraft with N1049A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1049A before.

- [Cancelled 1997-02-19](https://openairdocs.org/deregistered/N1049A-1997-02-19): North American Medore T-6D, S/N 4134378. Triennial form not returned. Owner: [Avag Inc](https://openairdocs.org/faa-owner/AVAG%20INC), [Richvale, CA](https://openairdocs.org/faa-place/CA/Richvale)
- [Cancelled 1965-05-18](https://openairdocs.org/deregistered/N1049A-1965-05-18): Piper PA-18, S/N 18624. Owner: [Rothenberger E R](https://openairdocs.org/faa-owner/ROTHENBERGER%20E%20R), [Grant, NE](https://openairdocs.org/faa-place/NE/Grant)

## Related

- Other Boeing 767-36N aircraft: https://openairdocs.org/model/boeing-767-36n/aircraft.md
- The GE CF6-80C2B7F engine: https://openairdocs.org/engine/ge-cf6-80c2b7f.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.