# N641GT: 1992 Boeing 767-38E - Status: Valid registration - Airframe: [Boeing 767-38E](https://openairdocs.org/model/boeing-767-38e) (registry code 1385154, 290 seats) - Engine: [GE CF6-80C2B6F](https://openairdocs.org/engine/ge-cf6-80c2b6f) (registry code 30109) - Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs) - Serial number: 25132 - Year built: 1992 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 28, 2011 - Certificate issued: June 30, 2011 - Expires: June 30, 2027 - Mode S code: A8699A - 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=641GT - Page: https://openairdocs.org/aircraft/N641GT 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): 34 in force ### Matched by airframe (Boeing 767-38E) None in force. ### Matched by engine (GE CF6-80C2B6F) - [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 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 - [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991 - [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991 - [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 1991 ### 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 - [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 ## Information bulletins (advisory) (4 in force) - [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023 - [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 DCA18CA252](https://openairdocs.org/ntsb/DCA18CA252), Jul 27, 2018: Boeing 767 (N641GT), Portsmouth, NH, substantial damage. Probable cause: an improper landing flare technique and the lack of the appropriate bounced landing recovery procedure. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20180727017409A](https://openairdocs.org/incident/20180727017409A), Jul 27, 2018: Boeing 767-38E (N641GT), Portsmouth, NH, Substantial damage. During landing and derotation, the nose of the aircraft was rapidly lowered, causing the nose gear to contact the runway with increased force. The impact… ## Service difficulty reports (1,007, 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 UIEA2026091200875](https://openairdocs.org/sdr/UIEA2026091200875), Sep 10, 2026: PROBE. FAULTED. DURING CRUISE FLIGHT WITH CENTER TANK PUMPS OPERATIONS, RIGHT MAIN TANK AND LEFT TANK FUEL IMBALANCE INCREASED TO 8000 LBS. PERFORMED FUEL QTY CHECK PER AMM 28- - [SDR UIEA2026083000823](https://openairdocs.org/sdr/UIEA2026083000823), Aug 30, 2026: DOOR. BROKEN. RIGHT LAV MID, HAD THE O2 DOOR BROKEN, WILL NOT HOLD IN O2 MASK. TRANSFER TO DMI 258393 PER MEL 35-21-01-01A CAT B. SECURED THE O2 MASK DOOR IAW AMM 35-21-34. O - [SDR UIEA2026061900531](https://openairdocs.org/sdr/UIEA2026061900531), Jun 19, 2026: RELEASE MECH. STUCK. L1 SLIDE RELEASE BUTTON NOT COME OUT. PERFORMED HANDLE MECHANISM ADJUSTMENT IAW AMM 52-11-25/201 & AMM 52-11-00/501. L1 DOOR OPS CHECKED GOOD. - [SDR UIEA2026042100230](https://openairdocs.org/sdr/UIEA2026042100230), Apr 21, 2026: LAMP. INOPERATIVE. RIGHT AFT EXTERNAL EMERGENCY SLIDE LIGHT FWD OF AFT LWR CARGO DOOR INOP(

RELAMPED IAW B767 33-51-06. OPS CHECK GOOD. OK FOR SERVICE

) - [SDR UIEA2026032300104](https://openairdocs.org/sdr/UIEA2026032300104), Mar 20, 2026: OXYGEN MASK. INOPERATIVE. 1ST OBS O2 MASK INOP CAUSING FEEDBACK(

R/R 1ST OBSERVER'S O2 MASK IAW AMM 35-11-51. OPS CHECKS GOOD

) - [SDR UIEA2026011200012](https://openairdocs.org/sdr/UIEA2026011200012), Jan 10, 2026: ELT. NOT REPORTED. ELT REQ REPLACEMENT. REMOVED AND REPLACED FIXED ELT REF AMM 23-24-01, OPS CHECK GOOD. PER MCC REQ, R/R FIXED ELT CRADLE BOX PER AMM 23-24-01. & IPC SMM CEIS MOD - [SDR UIEA2026011000007](https://openairdocs.org/sdr/UIEA2026011000007), Jan 10, 2026: INDICATION SYS. MALFUNCTIONED. ALL AFT LAVS FIRE EXTINGUISHER TRASH CANS DO NOT HAVE WAX. FOUND ALL HEAT AND FIRE INDICATORS STRIPE WITH NO FIRE OR HEAT INDICATING IAW AMM 26-24-00/001. NO FU - [SDR UIEA2025102301277](https://openairdocs.org/sdr/UIEA2025102301277), Oct 23, 2025: SLIDE. ACTIVATED. R4 ENTRY DOOR SLIDE ACTIVATED DUE TO FLT ATTENDANT INADVERTENT OPENING, DOOR ARMED. R & R DOOR SLIDE PER AMM 25-66-01. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025100801262](https://openairdocs.org/sdr/UIEA2025100801262), Oct 8, 2025: BATTERY. INOPERATIVE. L4 JUMPSEAT FLASHLIGHT OR BATTERY NOT CHARGING. REMOVED AND REPLACED FLASHLIGHT BATTERY REF AMM 25-64-00. OPS CHECK GOOD. - [SDR UIEA2025090301152](https://openairdocs.org/sdr/UIEA2025090301152), Sep 3, 2025: SLIDE. LOW PRESSURE. R1 DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED ESCAPE SLIDE PER AMM 25-66-01. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025041800549](https://openairdocs.org/sdr/UIEA2025041800549), Apr 18, 2025: LIGHT. DISCONNECTED. R1 LOWER EMERGENCY EXIT SIGN WILL NOT ILLUMINATE.(

FOUND R1 EMERGENCY EXIT SIGN LIGHT PLATE DISCONNECTED IAW WDM 33-51-14. RESECURED CONNECTOR AND LIGHT OPS C - [SDR UIEA2025011900088](https://openairdocs.org/sdr/UIEA2025011900088), Jan 19, 2025: PBE. MISSING. PBE AT R4 DOOR MISSING TAMPER SEAL.(

R/R PBE IAW AMM 25-64-00-01. NO FURTHER DEFECTS NOTED. DMI 224468 CLOSED. REF IPC 25-64-54-19. OSD: 1/23/2025 - [SDR UIEA2025011700079](https://openairdocs.org/sdr/UIEA2025011700079), Jan 17, 2025: ACTUATOR. FAULTED. LH OVERWING EXIT INOP (MAIN ENTRY DOORS/SLIDES/EMERGENCY).(

R/R LEFT WING SPOILER BLOW DOWN ACTUATOR PER AMM 25-65-20. OPS CHECK GOOD. DMI 224324 CLOSED

) - [SDR UIEA2025011900087](https://openairdocs.org/sdr/UIEA2025011900087), Jan 17, 2025: GIRT BAR. OUT OF ADJUST. R1 RIGHT FORWARD ENTRY DOOR SLIDE WILL NOT ARM. INSTALLED SHIM ON GIRT BAR FITTING AND BEARING ASSY IAW AMM 52-11-00/501 AND IPC 52-11-41-01. OPS CHECK GOOD. DO - [SDR UIEA2024120101139](https://openairdocs.org/sdr/UIEA2024120101139), Jan 15, 2025: ANTENNA. CORRODED. CORROSION ON BASE ANTENNA TCAS UPPER FUSELAGE(

TCAS ANTENNA WAS REPLACED WITH SATISFACTORY TEST IAW AMM 34-45-02-344-158. TORQUE APPLIED 20-LB-IN S/N 92440113 - [SDR UIEA2025011000011](https://openairdocs.org/sdr/UIEA2025011000011), Jan 15, 2025: SKIN. CORRODED. LEFT HORIZONTAL STABILIZER TIP UPPER SURFACE WITH LIGHT CORROSION AT 4.5'' FROM TRAILING EDGE.(

STABILIZER TIP UPPER SURFACE AT 4.5'' FROM TRAILING EDGE BASE - [SDR UIEA2025011000012](https://openairdocs.org/sdr/UIEA2025011000012), Jan 15, 2025: CONNECTOR. CORRODED. UPPER HALF OF FUSELAGE, TOP TCAS ANTENNA, FOUR CONNECTORS, WITH CORROSION.(

CONNECTORS WERE CLEANED AS CLIENT REQUIREMENT, CORROSION INHIBITING COMPOUND AV25 - [SDR UIEA2025011000013](https://openairdocs.org/sdr/UIEA2025011000013), Jan 15, 2025: INLET. CORRODED. CORROSION AT ENG 1 INLET COWL, INBD SIDE (INSIDE ACCESS PANEL) AT 8:00 O'CLOCK.(

ENG 1 INLET COWL WAS REPLACED IAW AMM 71-11-01-004-002-H00. NO FURTHER DEFECT - [SDR UIEA2025011000014](https://openairdocs.org/sdr/UIEA2025011000014), Jan 15, 2025: INLET. CORRODED. ENG 1, INLET COWL, ZONE 411, WITH POINTS OF CORROSION INNER ACCESS 412, AT INNER BARREL SKIN SURFACE, AT 12 HRS POSITION.(

 ENG 1, INLET COWL WAS REPLACE - [SDR UIEA2025011000015](https://openairdocs.org/sdr/UIEA2025011000015), Jan 15, 2025: SKIN. CRACKED. FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP.(

FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP, CRACK WAS R - [SDR UIEA2025011000016](https://openairdocs.org/sdr/UIEA2025011000016), Jan 15, 2025: SKIN. CRACKED. SERVICE DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP.(

SERVICE DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP, CRACK WAS REPAIRED IAW - [SDR UIEA2025011000017](https://openairdocs.org/sdr/UIEA2025011000017), Jan 15, 2025: WEDGE. BUCKLED. LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE WITH BUCKLING AT 28'' FROM INBD EDGE AND 11'' FROM TE.(

LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SU - [SDR UIEA2025011000018](https://openairdocs.org/sdr/UIEA2025011000018), Jan 15, 2025: WEDGE. BUCKLED. LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE WITH BUCKLING AT 45'' FROM INBD EDGE AND 11'' FROM TE.(

LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SU - [SDR UIEA2025011000019](https://openairdocs.org/sdr/UIEA2025011000019), Jan 15, 2025: SKIN. DELAMINATED. LEFT WING, INBOARD FLAP LOWER AREA BTW WS 314 AND WS404 WITH DELAMINATION.(

LEFT WING INBOARD FLAP LOWER AREA WAS REPAIRED IAW SRM 57-53-01-2R-1. NO FURTHER D - [SDR UIEA2025011000020](https://openairdocs.org/sdr/UIEA2025011000020), Jan 15, 2025: SKIN. MECHANIC ERROR. MISDRILLED ON LH FUSELAGE SKIN AND BODY RIB CHORD BETWEEN BSTA 933 TO BSTA 938.5 AND WL185.2 AT BBL 97.42.(

MISDRILLED ON LH FUSELAGE SKIN AND BODY RIB CHORD - [SDR UIEA2025011000021](https://openairdocs.org/sdr/UIEA2025011000021), Jan 15, 2025: BULB. NO TEST. EMERGENCY LIGHTS TEST, EMERGENCY LIGHT OF CEILING PANELS ROWS 16 LH AND 19 RH INOP(

EMERGENCY LIGHTS OF CEILING PANELS ROWS 16 LH AND 19 RH BULBS WERE REPLACE - [SDR UIEA2025011000022](https://openairdocs.org/sdr/UIEA2025011000022), Jan 15, 2025: FIRE SEAL. DAMAGED. ENGINE 2 LH CORE COWL (427AL), ZONE CC5, FIRE SHIELD WITH SEALANT DAMAGE.(

ENGINE 2 LH CORE COWL (427AL), ZONE CC5, FIRE SHIELD SEALANT WAS RESTORED IAW AMM 7 - [SDR UIEA2025011000023](https://openairdocs.org/sdr/UIEA2025011000023), Jan 15, 2025: LINER. BROKEN. BROKEN LINING DOOR COVER AT RH AFT EMERGENCY EXIT DOOR.(

LINING DOOR COVER AT RH AFT EMERGENCY EXIT DOOR. WAS REPAIRED IAW AMM 25-00-00-308-166. NO FURTHER DE - [SDR UIEA2025011000024](https://openairdocs.org/sdr/UIEA2025011000024), Jan 15, 2025: FIRE SEAL. WORN. ENGINE #1 NACELLE STRUT FIRE SEAL ON NAC STA 256 INBOARD AND OUTBOARD SIDE WITH WEAR.(

ENGINE #1 NACELLE STRUT FIRE SEAL ON NAC STA 256 INBOARD AND OUTBOARD S - [SDR UIEA2025011000025](https://openairdocs.org/sdr/UIEA2025011000025), Jan 15, 2025: PCA. LEAKING. RUDDER, LOWER PCA WITH HYDRAULIC LEAK.(

RUDDER, LOWER PCA WAS ADJUSTED PER AMM 27-21-02-422-038. LEAK CHK GOOD. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025011000026](https://openairdocs.org/sdr/UIEA2025011000026), Jan 15, 2025: BOLT. LOOSE. REMOVAL AND INSTALATION OF SLIDE ON LEFT WING FOR ACCESS LOOSE BOLT(

THE LOOSE BOLT OF SLIDE ON LEFT WING WAS INSTALLED CORRECTLY IAW AMM 20-11-00-910-802. NO - [SDR UIEA2025011400059](https://openairdocs.org/sdr/UIEA2025011400059), Jan 15, 2025: SKIN. CORRODED. LH WING, UPPER SURFACE, BETWEEN REAR SPAR AND STGR L-10, WBL 97.9566 WITH CORROSION(

THE CORROSION AREA WAS REPAIRED BY INSTALLING 2 REPAIR DOUBLERS, 1 SKIN F - [SDR UIEA2025011400060](https://openairdocs.org/sdr/UIEA2025011400060), Jan 15, 2025: FUEL TANK. LEAKING. RIGHT WING, DRY BAY WITH FUEL LEAK ON LOWER AFT PART BETWEEN RIB 7 AND RIB9(

FUEL LEAK ON LOWER AFT PART BETWEEN RIB 7 AND RIB9 RIGHT WING, RIGHT WING, DRY BA - [SDR UIEA2025011400061](https://openairdocs.org/sdr/UIEA2025011400061), Jan 15, 2025: FITTING. LEAKING. FUEL LEAK ON LH WING LOWER SURFACE WBL310.0 AT WING DIAGONAL BRACE WING FITTING.(

FUEL LEAK ON LH WING LOWER SURFACE WBL310.0 AT WING DIAGONAL BRACE WING FITT - [SDR UIEA2025011600065](https://openairdocs.org/sdr/UIEA2025011600065), Jan 15, 2025: PUMP. CORRODED. RH WING, OUTBOARD HOUSING UNIT OF BOOST PUMP WITH CORROSION(

RH WING, OUTBOARD HOUSING UNIT OF BOOST PUMP WITH CORROSION WAS REPLACED PER AMM 28-22-03-004-001 - [SDR UIEA2024101400987](https://openairdocs.org/sdr/UIEA2024101400987), Oct 8, 2024: ESCAPE HATCH. OUT OF ALIGNMENT. RIGHT OVERWING ESCAPE STEP MISALIGNED(

REMOVED RIGHT AFT EMERGENCY ESCAPE HATCH. REALIGNED ESCAPE STEP, REINSTALLED RIGHT AFT EMERGENCY HATCH PER AMM 52 - [SDR UIEA2024082900859](https://openairdocs.org/sdr/UIEA2024082900859), Aug 29, 2024: LAMP. INOPERATIVE. 1 EA OVERHEAD EMER LT INOP NEAR 30AC(

RELAMPED 1 EA EMER LT 30AC & OPS CHK OK IAW AMM 33-51-07

) - [SDR UIEA2024071300658](https://openairdocs.org/sdr/UIEA2024071300658), Jul 15, 2024: BRACKET. DAMAGED. AFT MEGAPHONE BRACKET DAMAGE LH AFT CLOSET(

REMOVED DAMAGED BRACKET ASSY AT AFT MEGAPHONE BY LH AFT CLOSET, MD. LOCATED, CLEARED, PREPARED, SECURED AND INSTAL - [SDR UIEA2024071300659](https://openairdocs.org/sdr/UIEA2024071300659), Jul 15, 2024: LATCH. LOOSE. ENG #2 NACELLE STRUT INBOARD DOOR WITH LATCH LOOSE(

LOCATED, CLEANED, PREPARED & REMOVED ADJUSTABLE BOLT & SAFETY WIRE, PROCEED TO PERFORM ADJUSTMENT, - [SDR UIEA2024071300660](https://openairdocs.org/sdr/UIEA2024071300660), Jul 15, 2024: OXYGEN BOTTLE. DAMAGED. FWD CLOSET PORTABLE OXYGEN BOTTLE MFG LABEL DAMAGE P/N 9700C1A-BF23A(

REMOVED AND REPLACED PORTABLE OXYGEN CYLINDER LOCATED IN CABIN FWD CLOSET AS REQUIRED IA - [SDR UIEA2024071400668](https://openairdocs.org/sdr/UIEA2024071400668), Jul 15, 2024: CAP. UNKNOWN. ENGINE #2 INB T/R VALVE TO OPEN AND CLOSE C/DUCT INOP.(

REMOVED AND REPLACED OPENING VALVE AT #2 REVERSER INBOARD HALF IAW AMM 78-31-03. INSTALLED REVERSER CO - [SDR UIEA2024071400669](https://openairdocs.org/sdr/UIEA2024071400669), Jul 15, 2024: BOLT. LOOSE. ENGINE # 1 AFT NACELLE O/B ACCESS DOOR REAR HINGE FITTING WITH BOLT LOOSE(

REMOVED DAMAGE ANGLE AT ENG 1, AFT NACCELLE O/B ACCESS DOOR REAR HINGE FITTING AREA - [SDR UIEA2024070300572](https://openairdocs.org/sdr/UIEA2024070300572), Jul 2, 2024: FIRE BOTTLE. LEAKING. FIRE BOTTLE LEAKED(

REMOVED AND REPLACED FIRE BOTTLE IAW EO 6725A252. OK FOR SERVICE

) - [SDR UIEA2025042100551](https://openairdocs.org/sdr/UIEA2025042100551), Apr 18, 2024: SIGN. DISCONNECTED. R1 LOWER EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. FOUND R1 EMERGENCY EXIT SIGN PLATE DISCONNECTED. RECONNECTED PER WDM 33-51-14. OPS CHECK GOOD PER AMM 33-51-09 - [SDR UIEA2024031300144](https://openairdocs.org/sdr/UIEA2024031300144), Mar 16, 2024: BATTERY. INOPERATIVE. DURING OPERATIONAL TEST EXTERIOR EMERGENCY LIGHTS, THREE RIGHT REAR LIGHTS DO NOT OPERATE IN STA 1197, STA 1219, AND 1562.(

THE M733 POWER SUPPLY BATTERY PACK - [SDR UIEA2024031600153](https://openairdocs.org/sdr/UIEA2024031600153), Mar 16, 2024: SWITCH. FAULTED. DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS ATTENDANT´S SWITCH WAS FOUND WITH FAIL(

EMERGENCY LIGHTS ATTENDANT´S SWITCH WAS REPLACED PER AMM 33-51-00. NO F - [SDR UIEA2024022200111](https://openairdocs.org/sdr/UIEA2024022200111), Feb 18, 2024: SIGN. LOOSE. LEFT OVERWING EMERGENCY EXIT SIGN FOUND LOOSE(

RE-SECURED LEFT WING EMERGENCY EXIT SIGN. SECURED IAW AMM 33-51-01

) - [SDR UIEA2023092700854](https://openairdocs.org/sdr/UIEA2023092700854), Sep 27, 2023: UNKNOWN. UNKNOWN. LI-ION EXTINGUSHING AGENT P/N LKFD IN RH SIDE LAST OVERHEAD BIN FOUND LEAKING NEEDS REPLACMENT(

REMOVED AND REPLACED LI-ION EXTINGUISHING AGENT REFERENCE ATLA - [SDR UIEA2023081100775](https://openairdocs.org/sdr/UIEA2023081100775), Aug 11, 2023: PBE. UNKNOWN. L1 PBE INDICATOR STRIP SHOWS RED(

REMOVED AND REPLACED PBE AT L1 DOOR IAW AMM 25-64-00

) - [SDR UIEA2023071900758](https://openairdocs.org/sdr/UIEA2023071900758), Jul 16, 2023: UNKNOWN. UNKNOWN. CAPT & F/O EVAS INOP(

INSTALLED NEW EVAS SECURITY SEAL STICKERS IAW EO6725A222. NO FURTHER DEFECTS NOTED

) All 1,007: https://openairdocs.org/aircraft/N641GT/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 CF6-80C2B6F) - [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 - [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 ## Related - Other Boeing 767-38E aircraft: https://openairdocs.org/model/boeing-767-38e/aircraft.md - The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.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.