# N298FE: 2012 Boeing 767-32LF

- Status: Valid registration
- Airframe: [Boeing 767-32LF](https://openairdocs.org/model/boeing-767-32lf) (registry code 138528K, 292 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: 41069
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 30, 2015
- Certificate issued: February 10, 2015
- Expires: February 29, 2028
- Mode S code: A313B4
- Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=298FE
- Page: https://openairdocs.org/aircraft/N298FE

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 767-32LF)

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

None matched to N298FE.

## FAA accident and incident reports

None matched to N298FE.

## Service difficulty reports (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 FDEA202607110902](https://openairdocs.org/sdr/FDEA202607110902), Jul 11, 2026: SUPPORT BEAM. CRACKED. CRACK ON UPPER PANEL SUPPORT BEAM, WS 1054 INNER ACCESS PANEL 561QB, LH WING UPPER PANEL SUPPORT BEAM, WS1054 INNER ACCESS PANEL 561QB, LH WING WAS REPLACED AND
- [SDR FDEA202607100885](https://openairdocs.org/sdr/FDEA202607100885), Jul 10, 2026: FLOOR PANEL. PUNCTURED. TWO PUNCTURES ON FLOOR PANEL 231QFF AT MDCC FLOOR PANEL 231QFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV.94 DEC 15/ 2025
- [SDR FDEA202607090876](https://openairdocs.org/sdr/FDEA202607090876), Jul 9, 2026: FLOOR PANEL. PUNCTURED. FIVE PUNCTURES ON FLOOR PANEL 231AFF AT MDCC. THE FLOOR PANEL 231AFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2, PAR 4.B, FIG 201, SHEET 2, REV 94. DEC 15/2025.
- [SDR FDEA202607090874](https://openairdocs.org/sdr/FDEA202607090874), Jul 9, 2026: FLOOR PANEL. PUNCTURED. THREE PUNCTURES ON FLOOR PANEL 232NFF AT MDCC FLOOR PANEL 232 NFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R, PAR. 4-B, FIG. 201, SHEET 2, REV 94 DEC 15/2025
- [SDR FDEA202607090873](https://openairdocs.org/sdr/FDEA202607090873), Jul 9, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 231LFF AT MDCC FLOOR PANEL 231 LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202607090872](https://openairdocs.org/sdr/FDEA202607090872), Jul 9, 2026: FLOOR PANEL. DENTED. DENT WITH DELAMINATION ON FLOOR PANEL 242CFF AT MDCC FLOOR PANEL 242CFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201, SHEET 2, REV 94, DEC 15/2025.
- [SDR FDEA202607090871](https://openairdocs.org/sdr/FDEA202607090871), Jul 9, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 231KFF AT MDCC FLOOR PANEL 231KFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 94 DEC 15/2025
- [SDR FDEA202607090870](https://openairdocs.org/sdr/FDEA202607090870), Jul 9, 2026: FLOOR PANEL. DENTED. DENT WITH DELAMINATION ON FLOOR PANEL 231LFF AT MDCC FLOOR PANEL 231LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV. 94 DEC 15/20
- [SDR FDEA202607070861](https://openairdocs.org/sdr/FDEA202607070861), Jul 7, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 231EFF AT MDCC FLOOR PANEL 231 EFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG.201 SHEET 2 REV.94 DEC 15/2025
- [SDR FDEA202607070860](https://openairdocs.org/sdr/FDEA202607070860), Jul 7, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 231CFF AT MDCC FLOOR PANEL 231CFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4-B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202607070859](https://openairdocs.org/sdr/FDEA202607070859), Jul 7, 2026: FLOOR PANEL. DAMAGED. TWO PUNCTURES ON FLOOR PANEL 231DFF AT MDCC FLOOR PANEL 231DFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV.94 DEC 15/2025
- [SDR FDEA202607070858](https://openairdocs.org/sdr/FDEA202607070858), Jul 7, 2026: FLOOR PANEL. DENTED. DENT WITH DELAMINATION ON FLOOR PANEL 251KFF AT MDCC FLOOR PANEL 251KFF AT MDCC WAS REPAIRED IAW B767 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202607070856](https://openairdocs.org/sdr/FDEA202607070856), Jul 7, 2026: FLOOR PANEL. DAMAGED. 2 PUNCTURE ON FLOOR PANEL 251KFF AT MDCC FLOOR PANEL 251KFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC 15/2025
- [SDR FDEA202607070855](https://openairdocs.org/sdr/FDEA202607070855), Jul 7, 2026: FLOOR PANEL. DENTED. THREE DENTS WITH DELAMINATION ON FLOOR PANEL 241AFF AT MDCC, THE FLOOR PANEL 241AFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2 REV 
- [SDR FDEA202607070853](https://openairdocs.org/sdr/FDEA202607070853), Jul 7, 2026: FLOOR PANEL. DAMAGED. PUNTURE ON FLOOR PANEL 241KFF AT MDCC FLOOR PANEL 241KFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 94 DEC 15/2025
- [SDR FDEA202607070850](https://openairdocs.org/sdr/FDEA202607070850), Jul 7, 2026: FLOOR PANEL. DAMAGED. TWO PUNCTURES ON FLOOR PANEL 251PFF AT MDCC FLOOR PANEL 251PFF AT MDCC. REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2, REV. 94 DEC 15/2025
- [SDR FDEA202607070849](https://openairdocs.org/sdr/FDEA202607070849), Jul 7, 2026: FLOOR PANEL. DAMAGED. PUNCTURED FLOOR PANEL 232HFF AT MDCC FLOOR PANEL 232HFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV. 94 DEC 15/2025
- [SDR FDEA202607060843](https://openairdocs.org/sdr/FDEA202607060843), Jul 6, 2026: FLOOR PANEL. CRACKED. 2 PUNCTURES ON FLOOR PANEL 231 RFF AT MDCC. FLOOR PANEL 231 RFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201 SHEET 2 REV. 94 DEC 15/2025.
- [SDR FDEA202607060842](https://openairdocs.org/sdr/FDEA202607060842), Jul 6, 2026: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 241WFF AT MDCC. FLOOR PANEL 241 WFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 94 DEC 15/2025.
- [SDR FDEA202607060841](https://openairdocs.org/sdr/FDEA202607060841), Jul 6, 2026: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL, 242SFF AT MDCC. FLOOR PANEL 242 SFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC 15/2025.
- [SDR FDEA202607030839](https://openairdocs.org/sdr/FDEA202607030839), Jul 3, 2026: SKIN. PUNCTURED. PUNCTURE AT AFT FLAP LOWER SURFACE BTW 32" FROM INBOARD EDGE AND 2.5" FROM LOWER EDGE. LH WING PUNCTURE AT AFT FLAP LOWER SURFACE BTW 32" FROM INBOARD EDGE AND 
- [SDR FDEA202607030838](https://openairdocs.org/sdr/FDEA202607030838), Jul 3, 2026: FLOOR PANEL. DENTED. DENT WITH DELAMINATION ON FLOOR PANEL 251FFF AT MDCC FLOOR PANEL 251FFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202607030837](https://openairdocs.org/sdr/FDEA202607030837), Jul 3, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 252DFF AT MDCC FLOOR PANEL 252DFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202607030836](https://openairdocs.org/sdr/FDEA202607030836), Jul 3, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 251EFF AT MDCC FLOOR PANEL 251EFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202607030835](https://openairdocs.org/sdr/FDEA202607030835), Jul 3, 2026: FLOOR PANEL. CRACKED. 4 PUNCTURES ON FLOOR PANEL 251VFF AT MDCC FLOOR PANEL 251VFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC15/2025
- [SDR FDEA202607030834](https://openairdocs.org/sdr/FDEA202607030834), Jul 3, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 252MFF AT MDCC FLOOR PANEL 252MFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202607030833](https://openairdocs.org/sdr/FDEA202607030833), Jul 3, 2026: FLOOR PANEL. CRACKED. THREE DENTS WITH DELAMINATION ON FLOOR PANEL 252HFF AT MDCC FLOOR PANEL 252HFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 
- [SDR FDEA202607030832](https://openairdocs.org/sdr/FDEA202607030832), Jul 3, 2026: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 251LFF AT MDCC FLOOR PANEL 251LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202407141000](https://openairdocs.org/sdr/FDEA202407141000), Jul 14, 2024: FLOOR SUPPORT. CRACKED. STA. 266, APROX RT BL 20 FLOOR SUPPORT "V" BRACKET CRACKED. REMOVED AND REPLACED SUPPORT V BRACKET 141T5602-8 REF BOEING DRAWING 141T5601 REV C & B767 SRM 51-40
- [SDR FDEA202209242364](https://openairdocs.org/sdr/FDEA202209242364), Sep 24, 2022: SWITCH. FAILED. EMERGENCY EXIT UNARMED PUSH BUTTON LIGHT FELL APART DURNG RELAMPING ON PREFLIGHT. REPLACED ANNUNCIATOR I/A W M/M 33-16-02-2 OPS CHECKS GOOD REF M/M 33-51-08-4
- [SDR FDEA202204030857](https://openairdocs.org/sdr/FDEA202204030857), Apr 3, 2022: NONE. NONE. LH WING LE AT STA OSS441 RIVETS LOOSE AND FORMER CRACKED P/N 114T2170-5. INSTALLED NEW FORMER REF: E.A. H-5720-T0367810. SEQ:146. W/O:82588.
- [SDR FDEA202204030856](https://openairdocs.org/sdr/FDEA202204030856), Apr 3, 2022: NONE. NONE. L/H WING L/E #5 SLAT GOUGED STA 499. 0000452710 : ROSNER, DANIEL D - 05-APR-2022 02:00 SEQ 152.. TH-5750-T0367838 P1 N/R 23 L/H WING L/E #5 SLAT GOUGED STA 499.
- [SDR FDEA202204030855](https://openairdocs.org/sdr/FDEA202204030855), Apr 3, 2022: NONE. NONE. L/H WING L/E #5 SLAT GOUGED STA 441. 0000452710 : ROSNER, DANIEL D - 05-APR-2022 02:02 SEQ 151.. TH-5750-T0367837 P1 N/R 22 L/H WING L/E #5 SLAT GOUGED STA 441.
- [SDR FDEA202106301624](https://openairdocs.org/sdr/FDEA202106301624), Jun 30, 2021: CONTROLLER. MALFUNCTIONED. CABIN ALTITUDE EICAS WARNING CLIMBING THROUGH 10,000 FEET OUT OF KGSO. LEVELED THE AIRCRAFT AT 10,000, RAN QRH, CONSULTED GOC AND GSO MAINTENANCE. TRIED BOTH AU
- [SDR FDEA2020091412173](https://openairdocs.org/sdr/FDEA2020091412173), Sep 11, 2020: CABIN PRESSURE. MALFUNCTIONED. PDIS 298 21-30 4361 1SEP20 MEM. NO PRESSURIZATION ON TAKEOFF MODE SELECTORS 1 OR 2 WOULD NOT WORK, USED MANUAL MODE REMAINDER OF FLIGHT, STAYED 20,000 AND BELOW
- [SDR FDEA2020090982145](https://openairdocs.org/sdr/FDEA2020090982145), Sep 8, 2020: SKIN. CHAFED. RT WING NR 8 SLAT T/E LOWER SURFACE CHAFED AT INBOARD AUX TRACK. REPAIRED RT WING NR 8 SLAT T/E LOWER SURFACE, IAW B767 SRM 57-43-02-2R REPAIR 1, 51-70-10-2R FI
- [SDR FDEA2020090962136](https://openairdocs.org/sdr/FDEA2020090962136), Sep 6, 2020: SKIN. DENTED. LT WING INBOARD AFT FLAP LOWER SURFACE IS DENTED 10.5 INCHES AFT OF THE LEADING EDGE AND 31.5 INCHES FROM INBOARD SIDE. REPAIRED LT WING INBOARD AFT FLAP LOWER 
- [SDR FDEA2020090962135](https://openairdocs.org/sdr/FDEA2020090962135), Sep 6, 2020: SKIN. DENTED. LT WING INBOARD AFT FLAP LOWER SURFACE IS DENTED AT TRAILING EDGE AND 64 INCHES FROM INBOARD SIDE. REPAIRED LT WING INBOARD AFT FLAP LOWER SURFACE, IAW B767-300
- [SDR FDEA202009032088](https://openairdocs.org/sdr/FDEA202009032088), Sep 3, 2020: SKIN. CHAFED. LEFT WING #5 SLAT WING STATION OSS 441 IS CHAFFED ON LOWER SURFACE DUE TO WORKING RIVETS REPAIRED LEFT WING #5 SLAT IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REP
- [SDR FDEA202009032087](https://openairdocs.org/sdr/FDEA202009032087), Sep 3, 2020: SKIN. CHAFED. LEFT WING #5 SLAT AT WING STATION OSS 499 IS CHAFFED ON LOWER SURFACE DUE TO WORKING RIVETS REPAIRED LEFT WING #5 SLAT IAW B767 SRM 57-43-02-2R AND 51-70-10-2R 
- [SDR FDEA2020021080290](https://openairdocs.org/sdr/FDEA2020021080290), Feb 8, 2020: STICK SHAKER. INOPERATIVE. "WARN ELEX" ON STATUS PAGE DURING PREFLIGHT TROUBLESHOOTING PER B767 FIM 27-32 FT803, WITH IRU'S ALIGNED THE WARN ELEX MSG CLEARS BUT PER BLK 2 WHEN THE LEFT ST
- [SDR FDEA201905261163](https://openairdocs.org/sdr/FDEA201905261163), May 26, 2019: UNKNOWN. MALFUNCTIONED. SPOILER DID NOT DEPLOY AT TOUCHDOWN AUTOMATICALLY. HAD TO MANUALLY DEPLOY. FACT 28MAY19 01:56 TPA PERFORMED AUTO SPEEDBRAKE OPERATIONAL TEST AND ALL FUNCTIONS P
- [SDR FDEA2019022870507](https://openairdocs.org/sdr/FDEA2019022870507), Feb 27, 2019: CONTROLLER. FAILED. PDIS 298 21-30 2907 26FEB19 LAX FACT U LOGPAGES:3042464 ON CLIMBOUT RECEIVED " CABIN ALTITUDE " WARNING LEVELED OFF ALERT WENT AWAY , AIRCRAFT PRESSURIZED TO BE
- [SDR FDEA201812273612](https://openairdocs.org/sdr/FDEA201812273612), Dec 27, 2018: PROXIMITY SENSOR. FAILED. AT CRUISE, FL 380 GOT MAIN CARGO DOOR MESSAGE. RAN QRH, SET LANDING ALT TO 9500'. THE AIRPLANE HELD PRESSURE ALL THROUGH DESCENT. DESCENDING THROUGH FL 185, LIG
- [SDR FDEA2018120653439](https://openairdocs.org/sdr/FDEA2018120653439), Dec 5, 2018: SENSOR. FAILED. PDIS 298 21-30 2688 05DEC18 MEM OPEN U LOGPAGES:2932480 AT FL 340, CABIN PRESSURE ALTITUDE WARNING. WENT ON CREW DONNED O2 MASK. DID RED TAB CABIN ALTITUDE LOSS
- [SDR FDEA2018082322150](https://openairdocs.org/sdr/FDEA2018082322150), Aug 22, 2018: SKIN. DENTED. RIGHT INBD FLAP TOP SURFACE WAS DENTED APPROX 39 INCHES FROM INBD EDGE, AND 6 INCHES FROM AFT EDGE. ACCOMPLISHED A REPAIR ON THE RTFLAP TOP SURFACE IAW SRM 57-5
- [SDR FDEA201709292797](https://openairdocs.org/sdr/FDEA201709292797), Sep 29, 2017: CONTROL VALVE. FAILED. ALTERNATE SLAT INBD POWER CIRCUIT BREAKER FOUND TRIPPED, DURING FLIGHT DECK INSPECTION. REPLACED CONTROL VALVE MODULE ASSY IAW AMM 27-81-12-4 3.
- [SDR FDEA201709132534](https://openairdocs.org/sdr/FDEA201709132534), Sep 13, 2017: SMOKE DETECTOR. FALSE ACTIVATION. DURING PUSH BACK, AND ENGINE START, THE LAVATOPRY SMOKE DETECTOR STARTED GOING OFF. THE LED SHOWED RED AS ALARM SOUNDED. ALARM STOPPED AFTER ABOUT THREE MINUTES
- [SDR FDEA201704211300](https://openairdocs.org/sdr/FDEA201704211300), Apr 21, 2017: CONNECTOR. DEFECTIVE. ON DEPARTURE CLIMBING THROUGH APPROXIMATE 2000 FT EICAS MESSAGE "FWD CARGO DOOR" DECLARED EMERGENCY. ACCOMPLISH QRH. RETURNED TO KEWR LANDED UNEVENTFULLY. REPLA
- [SDR FDEA201607072308](https://openairdocs.org/sdr/FDEA201607072308), Jul 7, 2016: LIGHT. BROKEN. DURING APPROCH, FLT TO IND THE RIGHT MAIN GEAR INDICATOR LIGHT FAILED TO ILLUMINATE GREEN WHEN THE GEAR WAS EXTENDED. QRH PROCEDURES WERE FOLLOWED, ALTERNATE GE

## 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 767-32LF aircraft: https://openairdocs.org/model/boeing-767-32lf/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.