# N664GT: 1994 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: 26259 - Year built: 1994 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 13, 2021 - Certificate issued: March 31, 2021 - Expires: March 31, 2028 - Mode S code: A8C3BD - Registered owner: [Titan Aviation Leasing Ltd Americas Inc](https://openairdocs.org/faa-owner/TITAN%20AVIATION%20LEASING%20LTD%20AMERICAS%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=664GT - Page: https://openairdocs.org/aircraft/N664GT 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/N664GT/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 (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA23WA124](https://openairdocs.org/ntsb/DCA23WA124), Jan 5, 2023: Boeing 767-31B (N664GT), Hahn, Germany, incident, no damage ## FAA accident and incident reports None matched to N664GT. ## Service difficulty reports (130, 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 UIEA2026101300984](https://openairdocs.org/sdr/UIEA2026101300984), Oct 13, 2026: PUMP. FAILED. LEFT CENTER FUEL PUMP CB POPPED IN FLIGHT WITH FUEL IN CENTER TANK. R & R FUEL OVRD/JETT BOOST PUMP HARNESS (LH) PER WDM 28-22-12 SB 767-28A0104; OPS CHECKS GOO - [SDR UIEA2026101500988](https://openairdocs.org/sdr/UIEA2026101500988), Oct 13, 2026: LAMP. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHT NR 2 INOP. RELAMPED LT OVERWING EMERGENCY LIGHT IAW AMM 33-51-16. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026091200874](https://openairdocs.org/sdr/UIEA2026091200874), Sep 13, 2026: DUCT. LEAKING. SEAT 42-43 LEFT-HAND SIDE AREA, PNEUMATIC LOUD LEAK SOUND, BLOWING HOT AIR INTO CABIN. LASTED 30 SECONDS TO 1 MINUTE AT 3-MINUTE INCREMENTS. REPLACED AFT CARGO - [SDR UIEA2026090800859](https://openairdocs.org/sdr/UIEA2026090800859), Sep 8, 2026: BATTERY. INOPERATIVE. AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00-212-001. OPS CHKD OK. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026081400760](https://openairdocs.org/sdr/UIEA2026081400760), Aug 14, 2026: WIRE. DAMAGED. CENTER SECTION ROW 26 AND AFT DID NOT DEPLOY O2 MASKS, REPAIRED WIRE W0720-01-14 BTWN PANEL P19 AND CONNECTOR D6000. OPS CHECKED GOOD IAW SWPM 20-10-11, WDM 35- - [SDR UIEA2026080800686](https://openairdocs.org/sdr/UIEA2026080800686), Aug 10, 2026: POWER SUPPLY. INOPERATIVE. R4 DOOR HAS 2 EACH EMERGENCY SIGNS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY M1210 IAW AMM 33-51-09-002-006 AND AMM 33-51-07-402-010. OPS CHECKS GOOD. POWE - [SDR UIEA2026080800687](https://openairdocs.org/sdr/UIEA2026080800687), Aug 10, 2026: POWER SUPPLY. INOPERATIVE. LEFT EXTERIOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED POWER SUPPLY M736 AND M738 IAW AMM 33-51-07-002-006. OPS CHECK GOOD. - [SDR UIEA2026081000725](https://openairdocs.org/sdr/UIEA2026081000725), Aug 10, 2026: SLIDE. FAULTED. DURING CONNECTION OF LT OVERWING EXIT DOOR BATTERY CONNECTOR, SLIDE DOOR DEPLOYED CAUSING SLIDE LANYARD TO DISENGAGE FROM SLIDE BAR. DURING TROUBLESHOOTING, FOU - [SDR UIEA2026081000727](https://openairdocs.org/sdr/UIEA2026081000727), Aug 10, 2026: POWER SUPPLY. INOPERATIVE. L/H EXTERIOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED POWER SUPPLY M736 AND M738 IAW AMM 33-51-07-002-006. OPS CHKD GOOD. - [SDR UIEA2026081000729](https://openairdocs.org/sdr/UIEA2026081000729), Aug 10, 2026: BEARING. LOOSE. RIGHT PYLON SIDE LINK FITTING, ATTACHED ON RIGHT WING WS 400 FORWARD SPAR LOWER PANEL HAS 1EA LOOSE BEARING. REMOVED AND REPLACED FITTING ASSEMBLY ON RT WING FO - [SDR UIEA2026081000730](https://openairdocs.org/sdr/UIEA2026081000730), Aug 10, 2026: SKIN. CORRODED. CORROSION ON LOWER FUSELAGE SKIN AROUND DRAIN VALVE BETWEEN STA.1540 - 1562 AND BETWEEN S-39L AND S-39R. REMOVED CORROSION L = 5.290" X W = 2.215" AND ACCOMPLIS - [SDR UIEA2026081000731](https://openairdocs.org/sdr/UIEA2026081000731), Aug 10, 2026: SKIN. DENTED. DENT ON FUSELAGE SKIN AT STA 364 BETWEEN S-38L AND S-39L. ACCOMPLISHED PERMANENT CATEGORY B EXTERNAL REPAIR ON FUSELAGE SKIN ON ZONE-A AT STA 364 BETWEEN S-38L - [SDR UIEA2026060300425](https://openairdocs.org/sdr/UIEA2026060300425), Jun 3, 2026: DRIVE ASSY. FAULTED. AIR TURN BACK - AFTER LEVELING IN CRUISE FLIGHT, THE FLAP INDICATOR NEEDLES INDICATED FLAPS 1 ON BOTH NEEDLES. ALSO, RECEIVED FLAP/SLAT ELEC, HI FLOW INHIBIT ST - [SDR UIEA2025112101318](https://openairdocs.org/sdr/UIEA2025112101318), Nov 21, 2025: LAMP. INOPERATIVE. LEFT AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED SLIDE AND OVERWING ESCAPE LIGHT LAMPS IAW AMM 33-51-06-902-082, REV 146, 22 AUG 2025. OPERA - [SDR UIEA2025110301291](https://openairdocs.org/sdr/UIEA2025110301291), Oct 31, 2025: OVEN. SMOKE. OVEN NR 2 RIGHT GIVES A LOT OF SMOKE. OVEN OPS CHK OK IAW AMM 25-32-00

) - [SDR UIEA2025092501244](https://openairdocs.org/sdr/UIEA2025092501244), Sep 25, 2025: SLIDE. INOPERATIVE. FA OPENED ARMED L4 DOOR SLIDE DID NOT INFLATE. R & R L4 SLIDE IAW AMM 25-66-01. OPS CHECK NORMAL. THIS CLOSES MDDR 238866. PLACARD REMOVED. - [SDR UIEA2025082801147](https://openairdocs.org/sdr/UIEA2025082801147), Aug 28, 2025: WINDOW SHADE. MALFUNCTIONED. LEFT OVERWING EMERGENCY EXIT (SEAT 23) WINDOW SHADE DOES NOT STOW PROPERLY(

R/R SEAT 23 LH WINDOW SHADE IAW AMM 25-27-01. OPS CHK OK. DMI 237098 CLOSED.  - [SDR UIEA2025082001128](https://openairdocs.org/sdr/UIEA2025082001128), Aug 18, 2025: PUMP. FAULTED. LH AFT FUEL PUMP EICAS MSG RAN QRH WHICH SAID TURN PUMP OFF, PUMP WENT OUT AT 12000. MX FOUND C/B POPPED. R & R LT AFT FUEL PUMP IAW AMM 28-22-03-404-074. OPS C - [SDR UIEA2025081101120](https://openairdocs.org/sdr/UIEA2025081101120), Aug 11, 2025: PIN. DISLODGED. COCKPIT FIRE EXTINGUISHER PIN FELL OUT. REINSTALLED PULL TIGHT SEAL PER AMM 26-26-02. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025062300794](https://openairdocs.org/sdr/UIEA2025062300794), Jun 21, 2025: MODULE. UNSECURE. L1 FLIGHT ATTENDANT, EMERGENCY O2 MODULE ASSY NOT SECURED. RESECURED O2 MODULE AT L1 ATTENDANT SEAT REF AMM 35-21-12/201. OPS CHECK GOOD. - [SDR UIEA2025052900707](https://openairdocs.org/sdr/UIEA2025052900707), May 29, 2025: FUEL FILTER. CONTAMINATED. R ENG FUEL FILT EICAS MESSAGE ILLUMINATED BRIEFLY TWICE ON CLIMB OUT.(

ITEM 1: FOUND CONTAMINATION. REMOVED AND REPLACED RH FUEL FILTER & LK CHECK OK REF - [SDR UIEA2025052100648](https://openairdocs.org/sdr/UIEA2025052100648), May 21, 2025: SATCOM. FAULTED. SATCOM DATALINK INOP (SATELLITE COMMUNICATION ) SATCOM SYSTEMS.(

MDDR 230661 CONTINUE, OPEN TEST ACTION PLAN AP -31160. AFTER CALLING SATCOM TEAM, ACTIVATED N - [SDR UIEA2025052100649](https://openairdocs.org/sdr/UIEA2025052100649), May 21, 2025: FILTER. NOT REPORTED. L/H ENGINE FUEL FILTERS REQUIRE REPLACEMENT AT OR BEFORE 450 FLIGHT HOURS(

REMOVED L/H FUEL FILTER REF 767 M/M 73-11-02-002-003-G00, OK TO INSTALL NEW FILTER. - [SDR UIEA2025052100650](https://openairdocs.org/sdr/UIEA2025052100650), May 21, 2025: OXYGEN BOX. FAULTED. RIGHT OBSERVER OXYGEN REGULATOR STOWAGE BOX DOES NOT CLOSE.(

RESTOWED OBSERVER O2 MASK REGULATOR IN STOWAGE BOX IAW B767 AMM 35-11-51, OPS TEST NORMAL. NO FAU - [SDR UIEA2025052100651](https://openairdocs.org/sdr/UIEA2025052100651), May 21, 2025: LATCH. FAULTED. #2 ENGINE NACELLE STRUT, TWO LATCHES CHECK FOR OPERATION ON WALL ARROUND, FOUND BOTH PARTIAL OPEN.(

REMOVED AND REPLACED 2EA DEFECTIVE LATCHES AT #2 ENG NACEL - [SDR UIEA2025052100652](https://openairdocs.org/sdr/UIEA2025052100652), May 21, 2025: BRACKET. CRACKED. #1 ENGINE PYLON I/B DOOR OPEN ROD DAMAGE & BRACKET CRACKED.(

LOCATED, DRILLED, AND INSTALLED NEW HOLD OPEN ROD SUPPORT BRACKET IAW B767 SRM 51-40-02 & - [SDR UIEA2025052100653](https://openairdocs.org/sdr/UIEA2025052100653), May 21, 2025: ANTENNA. DAMAGED. CENTER VHF COMM ANTENNA DAMAGE.(

REPLACED CENTER VHF COMM ANTENNA LOWER FUSELAGE. PERFORM OPS TEST, TEST OK IAW AMM 23-12-03 & AIPC 23-12-03-02B.

) - [SDR UIEA2025052100654](https://openairdocs.org/sdr/UIEA2025052100654), May 21, 2025: ANTENNA. DAMAGED. LEFT DME ANTENNA DAMAGE.(

REPLACED LEFT DME ANTENNA LOWER FUSELAGE & PERFORMED OPERATIONAL TEST, TEST OK IAW B767 AMM 34-55-02.

) - [SDR UIEA2025052100655](https://openairdocs.org/sdr/UIEA2025052100655), May 21, 2025: ANTENNA. DAMAGED. RIGHT DME ANTENNA DAMAGED.(

REPLACED RIGHT DME ANTENNA LOWER FUSELAGE & PERFORMED OPS TEST, TEST OK IAW B767 AMM 34-55-02.

) - [SDR UIEA2025052100656](https://openairdocs.org/sdr/UIEA2025052100656), May 21, 2025: ROD. DAMAGED. #1 ENGINE INBOARD, HOLD OPEN ROD, CORE COWL LH DAMAGE WON'T LOCK.(

REMOVED AND REPLACED #1 ENG INBOARD HOLD OPEN ROD COWL LH AS REQUIRED IAW B767 AMM 71-11-11 - [SDR UIEA2025052100657](https://openairdocs.org/sdr/UIEA2025052100657), May 21, 2025: FILTER. WARNING MESSAGE. ON CLIMB OUT, RH ENG FUEL FILTER EICAS MESSAGE APPEARED THEN DISAPPEARED TWICE. C/W WITH QRH.(

REMOVED AND REPLACED FUEL FILTER AT RH ENG AS PER B767-300 AMM - [SDR UIEA2025052100658](https://openairdocs.org/sdr/UIEA2025052100658), May 21, 2025: LATCH. WORN. #2 ENG PYLON STRUT TWO LATCH WORN OUT. NEED TO BE REPLACED R/H ACCESS PANEL.(

REMOVED DAMAGED LATCHED AT LHS ACCESS PANEL AT #2 ENGINE PYLON STRUT, LOCATED, C - [SDR UIEA2025052100659](https://openairdocs.org/sdr/UIEA2025052100659), May 21, 2025: EXHAUST CONE. DAMAGED. #1 ENG OFF EXHAUST PLUG REQUIRE SHEET METAL SUPPORT TO REMOVE HARDWARE.(

REMOVED HARDWARE AT #1 ENG EXHAUST PLUG ON OFF UNIT IAW B767 SRM 51-40-02. NO FURTHER - [SDR UIEA2025052100660](https://openairdocs.org/sdr/UIEA2025052100660), May 21, 2025: BRACKET. DAMAGED. MAIN PASSENGER CABIN FWD STORAGE CLOSET MEGAPHONE BRACKET DAMAGED.(

REMOVED AND REPLACED MEGAPHONE BRACKET AT MAIN DECK FWD STORAGE CLOSET IAW B767 SRM 51-40- - [SDR UIEA2025052100661](https://openairdocs.org/sdr/UIEA2025052100661), May 21, 2025: LIGHT. INOPERATIVE. CABIN READING LIGHTS AT 4D INOP.(

TRANSFER TO DMI 231105 PER MEL 25-20-01 CAT E DUE DATE 17SEP2025.

) - [SDR UIEA2025052100662](https://openairdocs.org/sdr/UIEA2025052100662), May 21, 2025: FUEL FILTER. NOT REPORTED. R/H ENGINE REQUIRES REPLACEMENT OF FUEL FILTER AT OR BEFORE 450 FLIGHT HOURS PER AMM 28-11-00-582-342.
(

REMOVED AND REPLACED FUEL FILTER AT R/H ENG AS PER - [SDR UIEA2025052100663](https://openairdocs.org/sdr/UIEA2025052100663), May 21, 2025: FUEL FILTER. NOT REPORTED. APU REQUIRES REPLACEMENT OF FUEL FILTER AT OR BEFORE 450 FLIGHT HOURS PER AMM 28-11-00-582-342. REMOVED FILTER IAW 767 AMM 49-31-04-004-001. FILTER GOOD TO INST - [SDR UIEA2025052200672](https://openairdocs.org/sdr/UIEA2025052200672), May 21, 2025: ROLLER. DAMAGED. FWD CARGO PDU UNIT R/H STA 580 HAS DAMAGE ROLLER.(

REMOVED AND REPLACED FWD CARGO PDU UNIT R/H STA 580 IAW B767-300 AMM 25-53-01. OPERATION CHECK OK GOOD.

- [SDR UIEA2025032500384](https://openairdocs.org/sdr/UIEA2025032500384), Mar 24, 2025: PRESSURE SWITCH. MALFUNCTIONED. DURING CLIMB OUT AT 7 MINS AFTER DEPARTURE, WHILE BOTH ENGINES ARE AT 14.0 FF MOMENTARY. RH ENG FUEL FILTER EICAS MSG AND RH ENG FUEL FILTER REMAINS.(

REMOVED - [SDR UIEA2025031500350](https://openairdocs.org/sdr/UIEA2025031500350), Mar 15, 2025: FUEL FILTER. CLOGGED. DURING CLIMBOUT EICAS MESSAGE "L ENG FUEL FILTER" SHOWED. DUE TO ETOPS RESTRICTION RETURNED TO OKO. LP1691828: ENG RUN DUE PER COMPANY REQUEST.(

REMOVED AND R - [SDR UIEA2025012200102](https://openairdocs.org/sdr/UIEA2025012200102), Jan 22, 2025: FUEL FILTER. WARNING MESSAGE. "L" ENG FUEL FILTER EICAS MSG FOLLOWED BY STATUS MSG. COMPLIED WITH QRH, ENGINE OPS NORMAL.(

INSPECTION & REPLACEMENT OF LEFT ENG FILTER IN WORK (OPEN DIS - [SDR UIEA2025011400058](https://openairdocs.org/sdr/UIEA2025011400058), Jan 14, 2025: FLOORBEAM. CORRODED. BULK CARGO COMPARTMENT CEILING AREA FLOOR BEAM STA 1502 BETWEEN LBL88.5 AND RBL 88.5 LOWER CHORD SOME EXFOLATION L=1.625" W=0.812"(

CORROSION WAS REPAIRED CORROSION WAS REPAIRED I - [SDR UIEA2025011400055](https://openairdocs.org/sdr/UIEA2025011400055), Jan 14, 2025: RIB. CRACKED. RH WINGLET, CRACK ON RIB INNER FACE WBL 929.1227. CRACK ON RH WINGLET STRUCTURE UPPER FLANGE OF RIB 1, AFT WAS REPAIRED IAW TRE6757273 ISSUED DATE: 21 DEC24 AND - [SDR UIEA2025011300051](https://openairdocs.org/sdr/UIEA2025011300051), Jan 14, 2025: SKIN. DENTED. RH WING, AFT FLAP LOWER SKIN OUTER PLIES WITH DENT BETWEEN IFS 230 AND IFS 280.(

DENT WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 4 PAGE 1-5. NO FURTHER - [SDR UIEA2025011300050](https://openairdocs.org/sdr/UIEA2025011300050), Jan 14, 2025: SOCKET. NO TEST. DURING CHECK, AFT CARGO HEAT INHIBIT AFTER AFT ARMED SWITCH ACTIVATION, FUNCTIONAL TEST WAS NOT SATISFACTORY, IN REF TASK CARD A-26-010-00-01.(

SOCKETS WERE R - [SDR UIEA2025011300049](https://openairdocs.org/sdr/UIEA2025011300049), Jan 14, 2025: FITTING. LEAKING. RIGHT CENTER TANK, REAR SPAR BULKHEAD TERMINAL FITTING, LOWER SURFACE, STA 955 AND RBL92 WITH FUEL LEAK.(

FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV - [SDR UIEA2025011300048](https://openairdocs.org/sdr/UIEA2025011300048), Jan 14, 2025: FITTING. LEAKING. RIGHT CENTER TANK, REAR SPAR BULKHEAD TERMINAL FITTING, UPPER SURFACE, STA 955 AND RBL87 WITH FUEL LEAK.(

FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV - [SDR UIEA2025011300047](https://openairdocs.org/sdr/UIEA2025011300047), Jan 14, 2025: FUEL TANK. LEAKING. RIGHT CENTER TANK, LOWER SKIN, STRG L-17 AND RBL 62 WITH FUEL LEAK.(

RIGHT CENTER TANK, LOWER SKIN, STRG L-17 AND RBL 62 FUEL LEAK WAS REPAIRED IAW AMM 28-11- - [SDR UIEA2025011300046](https://openairdocs.org/sdr/UIEA2025011300046), Jan 14, 2025: FRAME. CORRODED. DURING THE REMOVAL OF THE FWD ACOUSTIC PANEL, CORROSION WAS FOUND ON THE FAN FRAME, ENGINE 2, BETWEEN 8:00 AND 10:00 O'CLOCK POSITION.(

ON THE FAN FRAME, ENGI All 130: https://openairdocs.org/aircraft/N664GT/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 ## 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.