# N1361A: 1995 Boeing 767-31B - Status: Valid registration - Airframe: [Boeing 767-31B](https://openairdocs.org/model/boeing-767-31b) (registry code 1385190, 149 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: 26265 - Year built: 1995 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 30, 2017 - Certificate issued: October 17, 2017 - Expires: October 31, 2027 - Mode S code: A093F7 - Registered owner: [Msn 26265 LLC](https://openairdocs.org/faa-owner/MSN%2026265%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=1361A - Page: https://openairdocs.org/aircraft/N1361A 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 767-31B) 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/N1361A/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 N1361A. ## FAA accident and incident reports None matched to N1361A. ## Service difficulty reports (445, 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 ABXA20260926438](https://openairdocs.org/sdr/ABXA20260926438), Sep 26, 2026: FIRE WARNING. FALSE ACTIVATION. MAIN CARGO FIRE WARNING GOING ON AND OFF. PERFORMED MAIN CARGO INSPECTION IAW AMM 26-14-00 NO FIRE OR SMOKE NOTED PERFORMED FIRE WARNING OPS CHECK IAW AMM 26-14 - [SDR ABXA20260914403](https://openairdocs.org/sdr/ABXA20260914403), Sep 14, 2026: FIRE DETECTOR. FALSE ACTIVATION. HAD MAIN CARGO FIRE BELL/ LIGHTS, NO SMOKE OR FIRE, QRH COMPLETED, EXTERIOR INSPECTION OPS NORM, FIRE RESCUE WILL INSPECT WITH IR CAMERA. PERFORMED CARGO COMPAR - [SDR ABXA20260810352](https://openairdocs.org/sdr/ABXA20260810352), Aug 10, 2026: OXYGEN BOTTLE. LOW PRESSURE. DURING CREW PREDEPARTURE CHECK, EICAS PRESSURE INDICATION INOP READING 40 PSI. DEFERRED EICAS O2 PRESSOR INDICATION PER MEL 35-11-2-1 MX PROCEDURES COMPLY WITH - [SDR ABXA20260807351](https://openairdocs.org/sdr/ABXA20260807351), Aug 7, 2026: ELEC CONNECTOR. DEFECTIVE. ON PREDEPARTURE CHECK EICAS OXYGEN PRESS READS 40 PSI BOTTLE 1. ACTUAL READINGS BOTTLE #1 1850 PSI BOTTLE #2 1450 PSI. DEFERRED CREW BOTTLE #1 EICAS INDICATION - [SDR ABXA20260729338](https://openairdocs.org/sdr/ABXA20260729338), Jul 29, 2026: WARNING MESSAGE. FALSE ACTIVATION. LEFT ENG BLEED OFF EICAS MSG AFTER STARTING #1 ENGINE. ACCOMPLISHED 227 NNC AND ADVANCED THRUST TO 78% N2 DID NOT RESOLVE THE ISSUE. CREW RETURNED TO THE GATE ( - [SDR ABXA20260622283](https://openairdocs.org/sdr/ABXA20260622283), Jun 22, 2026: FLAP SYSTEM. WARNING MESSAGE. TRAILING EDGE FLAP DISAGREE DISPLAYED 5 TIMES DURING THE TAXI TO TAKEOFF AND THEN WENT AWAY. CREW ABORTED TAKEOFF (ATO) AND CONFERENCED WITH THE FOO AND MX. CAP - [SDR ABXA20260620270](https://openairdocs.org/sdr/ABXA20260620270), Jun 20, 2026: FSEU. MALFUNCTIONED. DURING TAXI OUT TO TAKE OFF T/E DISAGREE KEPT POPPING UP AND A/C RETURNED TO THE GATE AND MTX GROUNDED A/C . AFTER TROUBLR SHOOTING REMOVED AND REPLACED FSEU IA - [SDR ABXA20260516211](https://openairdocs.org/sdr/ABXA20260516211), May 16, 2026: GENERATOR. INOPERATIVE. ON T/O, RT GEN OFF ON THRUST ADVANCE. CREW DEFERRED IAW 24-00-1-1 AND PERFORMED AN ABORTED TAKE OFF (ATO). MTC DEFERRED PER MEL 24-00-1-1 MX PROCEDURES C/W PLAC - [SDR ABXA20260502183](https://openairdocs.org/sdr/ABXA20260502183), May 2, 2026: SMOKE DETECTOR. FALSE ACTIVATION. BATHROOM SMOKE DETECTOR WENT OFF TWICE IN FLIGHT NO EICAS OR OTHER INDICATION OF FIRE.AFTER LANDING DEFERRED LAVATORY SMOKE DETECTION SYSTEM IAW ABX MEL 26-26-3 - [SDR ABXA20260404145](https://openairdocs.org/sdr/ABXA20260404145), Apr 4, 2026: FIRE WARNING. FALSE ACTIVATION. MAIN CARGO FIRE MSG, MTX GROUNDED ACFT AND VERIFIED NO FIRE, PERFORMED OPS CHECK AND FOUND GOOD IAW AMM 26-14-00, ACFT REMAINS ETOPS 180. AND RETURNED ACFT TO S - [SDR ABXA20260330138](https://openairdocs.org/sdr/ABXA20260330138), Mar 30, 2026: ALTIMETER. FAULTED. ON APPROACH, GEAR NOT DOWN EICAS AND BELL AT 2500 FEET FOLLOWED BY LAND 2 NO LAND 3 ON ASA. ACCOMPLISHED LAST FLIGHT FAULTS ON MCDP AND RADIO ALTIMETER TESTS IA - [SDR ABXA20260327134](https://openairdocs.org/sdr/ABXA20260327134), Mar 27, 2026: RADIO ALTIMETER. FAULTED. DURING DESCENT, GEAR NOT DOWN RED EICAS MESSAGE CAME ON AROUND 5000FT ON THE ARRIVAL WITH FLAPS SET AT 1 SEVERAL TIMES WITH THROTTLES AT IDLE. C/W 30/40 TEST NO - [SDR ABXA20260318113](https://openairdocs.org/sdr/ABXA20260318113), Mar 18, 2026: STARTER. DEFECTIVE. DURING ENGINE START, L ENG STARTER EICAS MESSAGE, UNABLE TO START NO. 1 ENGINE, NO N2. AIRCRAFT RETURNED TO BLOCKS (BTB). T/S #1 ENG STARTER IAW B767 FIM 80-11 - [SDR ABXA20251231364](https://openairdocs.org/sdr/ABXA20251231364), Dec 31, 2025: ANTI-ICE VALVE. FAULTED. DURING TAXI OUT, AFTER L ENG START EICAS MESSAGE L ENG ANTI-ICE VALVE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED AND REPLACED L ENG TAI VALVE IAW A - [SDR ABXA20250918232](https://openairdocs.org/sdr/ABXA20250918232), Sep 18, 2025: A/C PACK. WARNING MESSAGE. ON TAXI OUT, L PACK TEMP EICAS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED L PACK PER MEL 21-51-1-1. MTX PROCEDURES CW. PLACARD - [SDR ABXA2025622134](https://openairdocs.org/sdr/ABXA2025622134), Jun 22, 2025: PITOT HEAD. DEFECTIVE. DURING TAXI, F/O'S PITOT LIGHT PROBE NOT WORKING. AIRCRAFT RETURNED TO BLOCKS. (BTB). REMOVED AND REPLACED THE F/O'S PITOT PROBE IAW B767 AMM 54-11-01. OPS CHEC - [SDR ABXA20250407071](https://openairdocs.org/sdr/ABXA20250407071), Apr 7, 2025: MODULE. MALFUNCTIONED. ON TAKEOFF, RIGHT N1 DID NOT ADVANCE MORE THAN 60%. RH ENG NOT MAKING TAKEOFF PWR. ABORTED TAKEOFF, RETURNED TO BLOCKS (BTB). PERFORMED B767 FIM 71-01 FT 810 (R - [SDR ABXA20250116013](https://openairdocs.org/sdr/ABXA20250116013), Jan 16, 2025: WARNING MESSAGE. FALSE ACTIVATION. AFTER BLOCKOUT AND BOTH ENGINES RUNNING AFT CABIN TEMP FWD CABIN TEMP, FLT DECK TEMP EICAS MESSAGES DISPLAYED WITH DISCRETE LIGHTS ILLUMINATE.AC RETURNED TO GAT - [SDR ABXA20241207246](https://openairdocs.org/sdr/ABXA20241207246), Dec 7, 2024: IRU. FAILED. AFTER PUSHBACK R IRS ALIGN EICAS AND DISCRETE LIGHT ILLUMINATED. PERFORMED QUICK ALIGN AND STATUS DID NOT CHANGE. AIIRCRAFT RETURNED TO GATE. MAINTENANCE GROUND - [SDR ABXA20241102211](https://openairdocs.org/sdr/ABXA20241102211), Nov 2, 2024: STEERING SYS. NO DISCREPANCY. TUG DRIVER OVERTORQUED NOSE GEAR ON PUSH BACK AC RETURNED TO THE GATE AND MTX GROUNDED AC . MTX EXECUTED A PHASE 1 CONDITIONAL INSPECTION OF THE NLG STEERING SY - [SDR UIEA2024072200713](https://openairdocs.org/sdr/UIEA2024072200713), Jul 28, 2024: HYDRAULIC LINE. TORN. TORN HYDRAULIC LINE TRUCK POSITIONER LEFT MAIN LANDING GEAR(

HYDRAULIC LINE TRUCK POSITIONER LEFT MAIN LANDING GEAR WAS REPLACED IAW AMM 32-32-18-404-024 REV - [SDR UIEA2024072200714](https://openairdocs.org/sdr/UIEA2024072200714), Jul 28, 2024: ROD. WORN. LH WING, INNER ACCESS PANEL 521QB, OUTBD REFUEL COUPLING, BEARING ROD ASSY WITH WORN(

LH WING INNER ACCESS PANEL 521QB OUTBD REFUEL COUPLING ROD WAS REPLACED - [SDR UIEA2024072200715](https://openairdocs.org/sdr/UIEA2024072200715), Jul 28, 2024: CHAIN. MISSING. LH WING, INNER ACCESS PANEL 521QB, ON BOTH REFUEL COUPLINGS, CHAINS MISSING(

THE CAPS ASSY OF REFUEL COUPLINGS WERE REPLACED IAW AMM 28-21-01-404-010 REV:142 - [SDR UIEA2024072200716](https://openairdocs.org/sdr/UIEA2024072200716), Jul 28, 2024: BRAKE PADS. WORN. NOSE LANDING GEAR WHEEL WELL, WEAR ON LEFT AND RIGHT SPIN BRAKES (PADS).(

NOSE LANDING GEAR WHEEL WELL, LEFT AND RIGHT SPIN BRAKES (PADS) WERE REPLACED IAW AM - [SDR UIEA2024072200717](https://openairdocs.org/sdr/UIEA2024072200717), Jul 28, 2024: PLACARD. DAMAGED. LOWER FUSELAGE EXTERNAL SKIN, ILLEGIBLE LABELS ON EMERGENCY ACCESS HANDLE OF RH COCKPIT WINDOW #2.(

LOWER FUSELAGE EXTERNAL SKIN, ON EMERGENCY ACCESS HANDLE O - [SDR UIEA2024072300732](https://openairdocs.org/sdr/UIEA2024072300732), Jul 28, 2024: ACCESS PANEL. LEAKING. RH WING, ACCESS PANEL 641BB, BASE OF FUEL STICK WITH LEAK(

RH WING, ACCESS PANEL 641BB, BASE OF FUEL STICK WAS REPLACED IAW AMM 28-44-01-404-033 REV 142 22-AP - [SDR UIEA2024072300733](https://openairdocs.org/sdr/UIEA2024072300733), Jul 28, 2024: SKIN. DELAMINATED. LH WING, SLAT #1, EXTERNAL SURFACE, MIDDLE SIDE WITH DELAMINATION(

LH WING, SLAT #1, EXTERNAL SURFACE WAS REPAIRED IAW SRM 57-43-02-2R-1 PAG 1-2 AND SRM 51-70 - [SDR UIEA2024072300734](https://openairdocs.org/sdr/UIEA2024072300734), Jul 28, 2024: TORQUE BOX. DELAMINATED. VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 185(

VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 185 WAS RE - [SDR UIEA2024072300735](https://openairdocs.org/sdr/UIEA2024072300735), Jul 28, 2024: TORQUE BOX. DELAMINATED. VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 169(

VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 169 WAS RE - [SDR UIEA2024072300736](https://openairdocs.org/sdr/UIEA2024072300736), Jul 28, 2024: SHIM. MIGRATED. FUEL TANK LEFT WING, INTERNAL SURFACE, ON RIB 3 UPPER AND LOWER CHORDS WITH SEVERAL MIGRATED SHIMS FROM L6 TO FRONT SPAR.(

FUEL TANK LEFT WING, INTERNAL SURFA - [SDR UIEA2024072400740](https://openairdocs.org/sdr/UIEA2024072400740), Jul 28, 2024: POSITION UNIT. WORN. WORN ON FITTING OF TRUCK POSITIONER, LEFT MAIN LANDING GEAR(

LH MLG SUPORT OF TRUCK POSITIONER WAS REPLACED IAW AMM 32-32-18-404-027 REV. 142 DATE 22 APR 24. - [SDR UIEA2024072400741](https://openairdocs.org/sdr/UIEA2024072400741), Jul 28, 2024: FUEL TANK. LEAKING. RH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK(

RH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK. THE FUEL LEAK WAS EVALUATED, SEALANT REM - [SDR UIEA2024072400742](https://openairdocs.org/sdr/UIEA2024072400742), Jul 28, 2024: TORQUE BOX. DELAMINATED. VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN BETWEEN FSS 183.3 AND FSS 230.91.(

VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, PANEL SK - [SDR UIEA2024072500746](https://openairdocs.org/sdr/UIEA2024072500746), Jul 28, 2024: HYDRAULIC LINE. CHAFED. CHAFING IN HYDRAULICS LINES RH LANDING GEAR, IN THE MIDDLE OF THE BACK(

RH LANDING GEAR, IN THE MIDDLE OF THE BACK. HYDRAULICS LINES WAS REPLACED IAW AMM 20-1 - [SDR UIEA2024072500747](https://openairdocs.org/sdr/UIEA2024072500747), Jul 28, 2024: INDICATOR. MALFUNCTIONED. LH WING, INNER ACCESS PANEL 521QB, RH FUEL QUANTITY INDICATION IN 888.8(

RH FUEL QUANTITY INDICATOR WAS REPLACED IAW AMM 28-21-13-404-016 REV. 142 DATE 22 APR - [SDR UIEA2024072500748](https://openairdocs.org/sdr/UIEA2024072500748), Jul 28, 2024: INDICATOR. MALFUNCTIONED. LH WING, INNER ACCESS PANEL 521QB, CENTER FUEL QUANTITY INDICATION, FLASHING INDICATION(

CENTER FUEL QUANTITY INDICATION WAS REPLACED IAW AMM 28-21-13-404-016 - [SDR UIEA2024072500749](https://openairdocs.org/sdr/UIEA2024072500749), Jul 28, 2024: VALVE. FAILED. FWD TRIM VALVE FAIL.(

FWD TRIM VALVE WAS REPLACED IAW AMM 21-61-07-404-011-003 REV. 142 DATE 22 APR 24. TORQUE APPLIED 45 LB-IN S/N 0823900243 DATE 15 NOV 24. - [SDR UIEA2024072500750](https://openairdocs.org/sdr/UIEA2024072500750), Jul 28, 2024: RELAY. FAULTED. AUTO SPEEDBRAKE DEPLOY INOPERATIVE WHEN T/R PULLED(

SYSTEM AUTO SPEED BRAKE. ACTUATOR WAS REPLACED IAW AMM 27-62-04-422-023 REV- 142 DATE 22 APR 24. TORQUE AP - [SDR UIEA2024061200514](https://openairdocs.org/sdr/UIEA2024061200514), Jun 11, 2024: LAMP. INOPERATIVE. EMERGENCY LIGHTS "UNARMED" LIGHT HALF BURNT OUT(

RELAMPED EMERGENCY LIGHTS "UNARMED" LIGHT IAW AMM 33-11-00. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024022100098](https://openairdocs.org/sdr/UIEA2024022100098), Feb 20, 2024: TAPE. BROKEN. TAPE ON ELT BROKEN/TORN(

TRANSFERRED TO MDDR # 203295 PER MEL 25-63-10-01, CAT D.  DUE DATE 19JUN24. PLACARDS INSTALLED.

/

PART ON HAND NOT CORREC - [SDR UIEA2024013100056](https://openairdocs.org/sdr/UIEA2024013100056), Jan 31, 2024: FMC. FAULTED. WHILE TAXIING ON GROUND IN MHT, A TURN SHOWED 26 KTS, WHICH I BELIEVE TO BE INCORRECT ON GROUND IN MHT. DURING CRUISE, ATC ADVISED WE WERE OFF COURSE AND LNAV S - [SDR UIEA2023100300862](https://openairdocs.org/sdr/UIEA2023100300862), Oct 3, 2023: TRIM SWITCH. UNKNOWN. UPON ROLL AT THRUST SET TO MASTER WARNING/CAUTION SIREN, EICAS MSG CONFIG / STABLIZER LOW SPEED REJECT(

T./S PER FIM TASK 31-51 FAULT TREE 807. R/R CONTORL "S - [SDR UIEA2024031500152](https://openairdocs.org/sdr/UIEA2024031500152), Sep 15, 2023: ALTIMETER. FAILED. CAPT ALTIMETER FAILED AND DISPLAYED OFF FLAG AT CRUISE. ACCOMPLISED QRH. NO CHANGE(

CAPTAIN ALTIMETER REMOVED AND REPLACED PER AMM 34-13-01/404. PERFOMRED OPS - [SDR UIEA2023091400830](https://openairdocs.org/sdr/UIEA2023091400830), Sep 15, 2023: FITTING. UNKNOWN. #1 PYLON FAN COWL SUPPORT BEAM FITTING CRACKED.(

R/R #1 ENG PYLON FAN COWL SUPPORT STRUCTURE AFT FITTING P/N 311T2114-7 PO 4842022 AS PER B767 SRM 51-40-02 &A - [SDR UIEA2023091400831](https://openairdocs.org/sdr/UIEA2023091400831), Sep 15, 2023: FITTING. UNKNOWN. #2Â PYLON FAN COWL SUPPORT FITTING CRACKED(

R/R #2 ENG PYLON FAN COWL SUPPORT STRUCTURE AFT FITTING P/N 311T2114-7 PO #4743771 AS PER BOEING DWG #311T2110 AND - [SDR UIEA2023091400832](https://openairdocs.org/sdr/UIEA2023091400832), Sep 15, 2023: ANGLE. UNKNOWN. #1 PYLON FAN COWL SUPPORT BEAM ANGLE P/N: 311U2510-113 IS CRACKED(

R/R CRACKED ANGLE R/N 311U2510-113. FABRICATED NEW ANGLE AND INSTALLED AS PER BOEING 767 SR - [SDR UIEA2023062000654](https://openairdocs.org/sdr/UIEA2023062000654), Jun 13, 2023: MEDICAL KIT. UNKNOWN. FIRST AID KIT ON OVHD BIN HAS SAFETY SEAL BROKEN(

REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-04-01. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2023011200017](https://openairdocs.org/sdr/UIEA2023011200017), Jan 8, 2023: PANEL. MISINSTALLED. EMERGENCY EGRESS WINDOW CAPT SIDE WILL NOT OPEN. REMOVED CAPTS WINDOW EMERGENCY EGRESS PANEL AND REINSTALLED / ADJUSTED PANEL IAW B767 AMM 20-11-00. NO DEFECTS - [SDR UIEA2022120301204](https://openairdocs.org/sdr/UIEA2022120301204), Dec 3, 2022: FSEU. FAULTED. CLIMBING THROUGH 10,000FT FLAPS UP & IN VNAV, NOTICED THE AIRPLANE SPEED BUG WAS AT 250KTS & THAT THE OVERSPEED TAPE WAS DOWN TO 250KTS. GIVEN A CLIMB TO FL230, - [SDR UIEA2022051500480](https://openairdocs.org/sdr/UIEA2022051500480), May 15, 2022: SWITCH. FAILED. BARBER POLE WOULD NOT ADVANCE AFTER PASSING 10,000FT. INVESTIGATED AND FOUND VMO SWITCH TO BE IN THE ALT POSITION. SWITCHED VMO LIMITING SWITCH TO NORM POSITION All 445: https://openairdocs.org/aircraft/N1361A/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 N1361A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1361A before. - [Cancelled 1973-06-05](https://openairdocs.org/deregistered/N1361A-1973-06-05): Piper PA-18S, S/N 18-1187. Owner: [The Oliver Stores](https://openairdocs.org/faa-owner/THE%20OLIVER%20STORES) ## Related - Other Boeing 767-31B aircraft: https://openairdocs.org/model/boeing-767-31b/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.