# N649GT: 1992 Boeing 767-300ER - Status: Valid registration - Airframe: [Boeing 767-300ER](https://openairdocs.org/model/boeing-767-300er) (registry code 1385202, 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: 25864 - Year built: 1992 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 19, 2014 - Certificate issued: January 27, 2016 - Expires: January 31, 2029 - Mode S code: A88752 - Registered owner: [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC) - Location: [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase) - Owner type: Corporation - 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=649GT - Page: https://openairdocs.org/aircraft/N649GT 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 767-300ER) 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/N649GT/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 N649GT. ## FAA accident and incident reports None matched to N649GT. ## Service difficulty reports (574, 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 UIEA2026102300995](https://openairdocs.org/sdr/UIEA2026102300995), Oct 22, 2026: BATTERY. INOPERATIVE. EMERGENCY FLASHLIGHT NEXT TO LAV LED NOT FLASHING. R & R FLASHLIGHT BATTERY IAW AMM 25-64-02. OPS CHECK GOOD.

) - [SDR UIEA2026101500987](https://openairdocs.org/sdr/UIEA2026101500987), Oct 12, 2026: LIMIT SWITCH. FAILED. REJECTED T/O AT 60KTS DUE TO EICAS MESSAGE. UNSCHEDULED STAB TRIM MESSAGE ALSO APPEARED TWICE DURING TAXI OUT(

RIGHT STAB TRIM LIMIT SWITCH/POSITION INDICATOR - [SDR UIEA2026100900972](https://openairdocs.org/sdr/UIEA2026100900972), Oct 10, 2026: FAILSAFE. DAMAGED. DETECTED DEFECT INDICATION DURING EO 6753A070 (SB 767-53A0100 R3/AD 2021-09-04) STA 955 REAR SPAR BULKHEAD SIDE FITTING FAILSAFE STRAP ULTRASONIC INSPECTION. DE - [SDR UIEA2026100900973](https://openairdocs.org/sdr/UIEA2026100900973), Oct 10, 2026: SKIN. CRACKED. DURING EO 6753A070 (SB 767-53A0100 R3/AD 2012-09-04 TERMINATING ACTION) OPEN-HOLE HFEC AT STA 955 R/H, A CRACK INDICATION WAS FOUND AT THE FAIL-SAFE STRAP, AND - [SDR UIEA2026100900974](https://openairdocs.org/sdr/UIEA2026100900974), Oct 10, 2026: TEE FITTING. CRACKED. DURING EO 6753A070 PART 4 (SB 767-53A0100 R3 / AD 2012-09-04 TERMINATING ACTION) AT STA 955 R/H, CRACKS WERE FOUND AT THE 10 O'CLOCK (0.5€?) AND 4 O'CLOCK (NOT - [SDR UIEA2026100900975](https://openairdocs.org/sdr/UIEA2026100900975), Oct 10, 2026: SKIN. CORRODED. CORROSION FOUND ON R/H INBOARD MAIN FLAP LOWER SKIN (DAMAGE SIZE: L=11.2", W=1.7")(

REPAIRED THE R/H INBD MAIN FLAP LOWER PANEL (P/N 113T2243-2) SKIN IN ACCOR - [SDR UIEA2026100900976](https://openairdocs.org/sdr/UIEA2026100900976), Oct 10, 2026: STRUCTURE. CORRODED. CORROSION FOUND ON L/H INBOARD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=19")(

PER BOEING RDR SP1-TLS-26-0037-05B, INSTALLATION OF CHORD (P/N 113T2225-401) ON THE - [SDR UIEA2026100900977](https://openairdocs.org/sdr/UIEA2026100900977), Oct 10, 2026: FLAP. DAMAGED. CORROSION FOUND ON RT INBD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=12") REMOVED RT INBD MAIN FLAP LOWER CHORD AND REPLACED WITH NEW CHORD PER SRM 51-40-02. HOLE C - [SDR UIEA2026100900978](https://openairdocs.org/sdr/UIEA2026100900978), Oct 10, 2026: SKIN. CORRODED. L/H WING LEADING EDGE NR 1 SLAT SKIN, FOUND DENSE CORE CORROSION (DAMAGE SIZE: L = 2.5", W=5.4") REPAIRED LT WING LEADING EDGE NR 1 SLAT SKIN IAW SRM 51-70-10 A - [SDR UIEA2026072800658](https://openairdocs.org/sdr/UIEA2026072800658), Jul 27, 2026: SEAL. BROKEN. GALLEY ELT TAMPER TAPE BROKEN. REMOVED AND REPLACED GALLEY ELT IAW AMM 25-63-03. OPS CHK OK. - [SDR UIEA2026060900455](https://openairdocs.org/sdr/UIEA2026060900455), Jun 9, 2026: CIRCUIT CARD. FAULTED. RAT DEPLOYED RIGHT AFTER ROTATION ON TAKE-OFF. GREEN PRESSURE LIGHT ILLUMINATED(

REMOVED AND REPLACED LH ENG SPEED CARD & STOWED RAT PER AMM 73-21-54. NO - [SDR UIEA2026060300430](https://openairdocs.org/sdr/UIEA2026060300430), Jun 2, 2026: OXYGEN MASK. INOPERATIVE. CENTER SUPERNUMERARY SEAT O2 MASK INOPERATIVE. REMOVED AND REPLACED CENTER SUPERNUMERARY O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD. NO LEAKS NOTED. - [SDR UIEA2026060100424](https://openairdocs.org/sdr/UIEA2026060100424), May 30, 2026: STOWAGE BOX. NO TEST. CAPTAIN SIDE O2 MASK AUDIO INTERCOM WILL NOT TEST. R & R CAPT SIDE O2 MASK STOWAGE IAW AMM 35-11-51 AND IPC 35-11-52-15. OPS CHECK GOOD. NO DEFECTS NOTED. - [SDR UIEA2026052600364](https://openairdocs.org/sdr/UIEA2026052600364), May 26, 2026: TAG. BROKEN. FLIGHT DECK ELT RH DO NOT REMOVE TAG BROKEN (PORTABLE ELT)(

REMOVED AND REPLACED FLIGHT DECK RH PORTABLE ELT IAW B767 AMM 25-63-03 & AIPC 25-63-52-97 AND - [SDR UIEA2026051800341](https://openairdocs.org/sdr/UIEA2026051800341), May 16, 2026: WINDOW. NOISY. LOUD WHISTLING NOISES ON BOTTOM OF L1 WINDOW. PER CREW DEBRIEF, ACTUAL WINDOW IS L2 ( SLIDING WINDOW ). CLEANED AND INSPECTED L2 WINDOW AERODYNAMIC ALONG WITH L - [SDR UIEA2026040500127](https://openairdocs.org/sdr/UIEA2026040500127), Apr 5, 2026: FAN. VIBRATION. DURING CLIMB, RIGHT ENGINE FAN VIBRATION REACHED 4.3. DURING CRUISE, VIB 0.8. PERFORMED BLADE LUBE PER AMM 72-31-02. SPINNER RE-TORQUED PER AMM 72-31-01. TRIM B - [SDR UIEA2026032700110](https://openairdocs.org/sdr/UIEA2026032700110), Mar 27, 2026: HANDLE. OUT OF ADJUST. EMERGENCY WINDOW OUTSIDE HANDLE POPS OUT. ADJUSTED SPRING LOADED BALL LATCH OF WINDOW R2 EXTERIOR EMERGENCY ESCAPE HANDLE IAW AMM 56-11-04. OPS CHK GOOD AT THIS - [SDR UIEA2025111801297](https://openairdocs.org/sdr/UIEA2025111801297), Nov 16, 2025: LANYARD. UNSECURE. ELT BY LAVATORY HAS STRING HANGING. SECURED THE ELT STRING IAW AMM 25-63-03. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025102401278](https://openairdocs.org/sdr/UIEA2025102401278), Oct 24, 2025: SKIN. DAMAGED. AIRCRAFT STRUCK BY LIGHTNING. LIGHTNING STRIKE DAMAGE FOUND ON R/H INLET COWL 3:00 POSITION(

PERFORMED PHASE 1 LIGHTNING STRIKE INSPECTION IAW B767 AMM 05-51. - [SDR UIEA2025100401256](https://openairdocs.org/sdr/UIEA2025100401256), Oct 4, 2025: HF COMM. ABNORMAL. BOTH HF COMM RADIO INOP AND SELCAL INOP(

T/S WITH FIM 23-11 FT 804. RESECURED CONNECTIONS AT HF ANTENNA. OPS CHK GOOD PER AMM 23-11-00

) - [SDR UIEA2025092601246](https://openairdocs.org/sdr/UIEA2025092601246), Sep 26, 2025: COVER. DETACHED. EMERGENCY EXIT LIGHT COVER FELL OFF L1 DOOR. INSTALLED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-03. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025071400949](https://openairdocs.org/sdr/UIEA2025071400949), Jul 14, 2025: BRACKET. DAMAGED. FLIGHT DECK FIRE EXTINGUISHER HOLDING BRACKET INOPERATIVE. RE-ADJUSTED FLIGHT DECK FIRE EXTINGUISHING BRACKET IAW B767 AMM 26-26-02. OPS CHECK GOOD. NO FURTHER - [SDR UIEA2025062100789](https://openairdocs.org/sdr/UIEA2025062100789), Jun 19, 2025: LATCH. OUT OF ADJUST. ON LANDING, FO WINDOW NR 2 EXTERNAL EMERGENCY ESCAPE HANDLE UNLATCHING. ADJUSTED FO WINDOW #2 EMERGENCY ESCAPE HANDLE LATCH & PERFORMED SYSTEM OPS CHECK OF EXTE - [SDR UIEA2025052900705](https://openairdocs.org/sdr/UIEA2025052900705), Jun 7, 2025: SKIN. CRACKED. SERVICE DOOR CUTOUT, AFT LOWER CORNER FUSELAGE FOUND CRACKS INDICATION, ON OPEN HOLES: #4, POSITION 8 O'CLOCK (SKIN AND BEAR STRAP) APPROX AND HOLE #5, POSITION - [SDR UIEA2025052900706](https://openairdocs.org/sdr/UIEA2025052900706), Jun 7, 2025: BEAR STRAP. CRACKED. FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH TWO CRACK INDICATIONS AT HOLE #5: 1. ON SKIN AT 3 O´CLOCK POSITION. 2. ON BEAR STRAP AT 9 O´CLOCK POSITION.(

AFFECTED AREA WAS REPAIRED IN ACCORDANCE WITH B767 SRM 57-70-01-2R-1 - [SDR UIEA2025060300723](https://openairdocs.org/sdr/UIEA2025060300723), Jun 7, 2025: WEDGE. DAMAGED. LH WING, SLAT# 1, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(

LH WING, SLAT# 1, TRAILING WEDGE, UPPER SURFACE WITH DENTS (9 EAS) WERE EVALUATED AND FOUR DENTS WERE R - [SDR UIEA2025060300724](https://openairdocs.org/sdr/UIEA2025060300724), Jun 7, 2025: BUSHING. CORRODED. FRETTING CORROSION ON BUSHING P/N BACB28X20E085 INSTALLED IN THE FWD SHEAR PIN HOLE OF THE FWD ENGINE MOUNT (P/N 311T2211-7), RH SIDE.(

BUSHING WAS REPLACED ( - [SDR UIEA2025060300725](https://openairdocs.org/sdr/UIEA2025060300725), Jun 7, 2025: FUEL TANK. LEAKING. FUEL LEAK AT CENTER TANK BETWEEN STGR L-6 AND LBL 97.5.(

THE SEALANT IN THE FUEL TANK STRUCTURE WAS REPAIRED PER AMM 28-11-00-308-013. NO FURTHER DEFECTS NOTE - [SDR UIEA2025060300726](https://openairdocs.org/sdr/UIEA2025060300726), Jun 7, 2025: WEDGE. DAMAGED. LH WING, SLAT# 4, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(

LH WING, SLAT# 4, TRAILING WEDGE, UPPER SURFACE WITH DENTS (11 EAS) WERE EVALUATED AND FOUR DENTS WERE - [SDR UIEA2025060300728](https://openairdocs.org/sdr/UIEA2025060300728), Jun 7, 2025: WEDGE. DAMAGED. LH WING, SLAT# 3, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(

LH WING, SLAT# 3, TRAILING WEDGE, UPPER SURFACE WITH DENTS (7 EAS) WERE EVALUATED AND TWO DENTS WERE RE - [SDR UIEA2025060700735](https://openairdocs.org/sdr/UIEA2025060700735), Jun 7, 2025: SKIN. CORRODED. RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION.(

RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION LEVEL - [SDR UIEA2025060700736](https://openairdocs.org/sdr/UIEA2025060700736), Jun 7, 2025: SKIN. CORRODED. RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT FRONT SPAR FROM STA 0.0 TO STA 107.927, CORROSION AROUND FASTENERS. L= 6.0 IN W=1.5 IN.(

RH OUTBD HORIZONTAL - [SDR UIEA2025031700353](https://openairdocs.org/sdr/UIEA2025031700353), Mar 17, 2025: EVAS UNIT. INOPERATIVE. DURING EVAS OPS CHECK, FOUND CAPTAINS EVAS INOP (BLOWER INOP)(

REMOVED & REPLACED EVAS CAPTAINS SIDE AS PER B-767-300 AMM 25-60-99. OPS CHECK GOOD.

) - [SDR UIEA2025031200260](https://openairdocs.org/sdr/UIEA2025031200260), Mar 12, 2025: SKIN. NO DISCREPANCY. LIGHTNING STRIKE AT 17000 FT. SUSPECT STRIKE IMPACT ON CAPTAIN'S SIDE IN THE VICINITY OF THE NOSE.(

PERFORMED LIGHTNING STRIKE DAMAGE PHASE INSPECTION IAW B76 - [SDR UIEA2025021200132](https://openairdocs.org/sdr/UIEA2025021200132), Feb 12, 2025: WIRE HARNESS. DAMAGED. AIR TURN BACK DUE TO APU SHUTDOWN IN FLIGHT. LEFT GENERATOR ON MEL SO APU IS REQUIRED. APU RESTARTED ON 3RD ATTEMPT.(

PER ENGINEERING AND MANAGEMENT REQUEST, - [SDR UIEA2024122901187](https://openairdocs.org/sdr/UIEA2024122901187), Dec 30, 2024: TRANSCOWL. DAMAGED. LH ENG T/REV WIRE MESH DAMAGED AT 0700 O'CLOCK POSITION. C/W EO 6778A019 REV 5 PART 1 INTERIM REPAIR. C/W PART 2 PERMANENT REPAIR AT NEXT A-CHECK.(

REMOVED TR - [SDR UIEA2024122901188](https://openairdocs.org/sdr/UIEA2024122901188), Dec 30, 2024: RADOME. ERODED. FWD FUSELAGE RADOME SURFACE, FOUND SEVERAL AREAS OF EROSION.(

INSPECTED SURFACE DEFECT AT NOSE RADOME. FOUND EVIDENCE OF PEELING PAINT IAW B767 AMM 53-12-01 C - [SDR UIEA2024122901189](https://openairdocs.org/sdr/UIEA2024122901189), Dec 30, 2024: OXYGEN MASK. CONTAMINATED. LAV PORTABLE OXYGEN MASK CONTAMINATED.(

REMOVED AND REPLACED LAV PORTABLE OXYGEN MASK AS REQUIRED PER 767 AMM 35-31-01. OPS CHK GOOD.

) - [SDR UIEA2024122901190](https://openairdocs.org/sdr/UIEA2024122901190), Dec 30, 2024: PANEL. LOOSE. #2 ENGINE I/B CORECOWL HINGES DAMAGED, DIFFICULT TO OPEN AND CLOSE. REQUIRES EVALUATION.(

EVALUATED AND FOUND SKIRT PANEL WITH LOOSE AND MISSING FASTENERS. LO - [SDR UIEA2024122901191](https://openairdocs.org/sdr/UIEA2024122901191), Dec 30, 2024: CDU. INOPERATIVE. LEFT T/R INOP.(

REMOVED CENTER DRIVE UNIT AT LEFT ENGINE INBOARD SIDE AS PER REF B747 AMM 78-31-21. OK TO INSTALL. INSTALLED CENTER DRIVE UNIT AT LEFT ENGINE - [SDR UIEA2024120301158](https://openairdocs.org/sdr/UIEA2024120301158), Dec 3, 2024: SWITCH. FAULTED. UNSCHEDULED STAB TRIM MSG ON DECENT. CLEARED SHORTLY AFTER.(

R/R STAB TRIM LIMIT SWITCH MODULE ASSY IAW AMM 27-48-01. OPS CHECK GOOD NO DEFECTS NOTED. PERFORM - [SDR UIEA2024111301085](https://openairdocs.org/sdr/UIEA2024111301085), Nov 12, 2024: ELT. INOPERATIVE. REF W/O 138840, DURING OPS CHECK OF FIXED ELT FOUND TO BE INOPERATIVE.(

R/R FIXED ELT PER EO OT-23-0084. OPS CHECK GOOD. DMI 220446 CLOSED

) - [SDR UIEA2024082300843](https://openairdocs.org/sdr/UIEA2024082300843), Aug 23, 2024: SKIN. DAMAGED. RH OTBD AILERON TRAILING EDGE LIGHTNING STRIKE(

TRANSFER TO NON-MEL DMI 215328 DUE DATE 27AUG24.

/

LP 1872886 M1: C/W PART 3 PERMANENT REPAIR PER ATLAS - [SDR UIEA2024080200776](https://openairdocs.org/sdr/UIEA2024080200776), Aug 2, 2024: INDICATION SYS. FAULTED. AFTER LANDING O2 BOTTLE INDICATES 40 PSI. CONFIRMED EICAS IND INOP. REF DMI 213995 PER MEL 35-11-02-01 CAT B DUE DATE 8AUG24. MMP PERFORMED. BOTTLE #1 1400 PSI, - [SDR UIEA2024072600753](https://openairdocs.org/sdr/UIEA2024072600753), Jul 26, 2024: AVERAGING UNIT. FAULTED. ON GROUND OXYGEN PRESSURE SHOWS 40 PSI.(

R/R AVERAGING UNIT IAW AMM 35-11-06. OPS & LEAK CHECK GOOD. DMI 213524 CLOSED.

) - [SDR UIEA2024040800267](https://openairdocs.org/sdr/UIEA2024040800267), Apr 7, 2024: SHROUD. DAMAGED. L1 DOOR EMERGENCY ESCAPE ROPE SHROUD DAMAGED.(

PERFORMED TIME LIMITED REPAIR ON L1 DOOR ESCAPE ROPE RETAINER SHROUD IAW EA 6725A0025. TRANSFER TO NON-MEL DMI - [SDR UIEA2024021700090](https://openairdocs.org/sdr/UIEA2024021700090), Feb 17, 2024: ELT. UNKNOWN. DURING OPS CHECK OF FIXED ELT PER W/C # A-23--339-01(

TRANSFERRED TO MDDR 203168 PER DDG 25-63-10-02C CAT D DUE 16JUM24. MX ACTIONS C/W, PLACARDS INSTALLED. P - [SDR UIEA2024012400022](https://openairdocs.org/sdr/UIEA2024012400022), Jan 24, 2024: SENSOR. OUT OF TOLERANCE. MAIN CARGO DOOR SHOWS OPEN DURING CRUISE. INDICATION WENT OUT DURING DESCENT AT FL 340. "MAIN CARGO DOOR" EICAS MSG.(

FOUND MAIN CARGO DOOR LOCKED WARNING SEN - [SDR UIEA2023122201010](https://openairdocs.org/sdr/UIEA2023122201010), Dec 22, 2023: COMPUTER. UNKNOWN. RETURN TO BLOCK AFTER LOW SPEED RTO DUE MASTER CAUTION LIGHT AND BEEPER. "AUTOTHROTTLE DISCONNECT" EICAS MSG. SPED WAS AROUND 40KTS.(

DEFERRED IAW MEL 22-30-0 All 574: https://openairdocs.org/aircraft/N649GT/reports.md ## Service difficulty reports on N649GT not matched to an aircraft (1) They name N649GT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DU4R2021051700073](https://openairdocs.org/sdr/DU4R2021051700073), May 17, 2021: FLOOR PANEL. CORRODED. DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AFT CARGO COMPARTMENT FLOOR PANEL 1336X HAS MULTIPLE AREAS OF PITTING CORROSION. S/O 660006 N/R 38 ## 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 767-300ER aircraft: https://openairdocs.org/model/boeing-767-300er/aircraft.md - The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.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.