# N126FE: 2015 Boeing 767-3S2F

- Status: Valid registration
- Airframe: [Boeing 767-3S2F](https://openairdocs.org/model/boeing-767-3s2f) (registry code 138513F, 6 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: 42718
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 16, 2015
- Certificate issued: October 6, 2015
- Expires: October 31, 2028
- Mode S code: A06A7E
- 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=126FE
- Page: https://openairdocs.org/aircraft/N126FE

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 767-3S2F)

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 N126FE.

## NTSB investigations on N126FE not matched to an aircraft (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 ATL86IA197](https://openairdocs.org/ntsb/ATL86IA197), Jul 16, 1986: Boeing 727-25C (N126FE), Erlanger, KY, incident, no damage

## FAA accident and incident reports

None matched to N126FE.

## Reports on N126FE not matched to an aircraft (1)

They name N126FE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19860716052469I](https://openairdocs.org/incident/19860716052469I), Jul 16, 1986: Boeing 72725C (N126FE), Huntington, WV. Unscheduled landing after smoke emitted from package containing hazardous materials.

## Service difficulty reports (49)

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 FDEA202507241313](https://openairdocs.org/sdr/FDEA202507241313), Jul 24, 2025: FLOOR PANEL. CRACKED. CRACK ON FLOOR PANEL 251EFF AT MDC SEC 46 FLOOR PANEL 251EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507231305](https://openairdocs.org/sdr/FDEA202507231305), Jul 23, 2025: FLOOR PANEL. CRACKED. CRACK ON PREVIOUS REPAIR OF FLOOR PANEL 251CFF AT MDC SEC 46 FLOOR PANEL 251CFF MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 
- [SDR FDEA202507231303](https://openairdocs.org/sdr/FDEA202507231303), Jul 23, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 251DFF AT MDC SEC 46. FLOOR PANEL 251DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507231301](https://openairdocs.org/sdr/FDEA202507231301), Jul 23, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 232DFF AT MDC SECTION 43 FLOOR PANEL 232DFF MDC SECTION 43 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2
- [SDR FDEA202507231300](https://openairdocs.org/sdr/FDEA202507231300), Jul 23, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 251KFF AT MDC SEC 46. FLOOR PANEL 251KFF MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507231299](https://openairdocs.org/sdr/FDEA202507231299), Jul 23, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 251PFF AT MDC SEC 46. FLOOR PANEL 251PFF MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507221292](https://openairdocs.org/sdr/FDEA202507221292), Jul 22, 2025: FLOOR PANEL. CRACKED. PUNCTURES ON ACCESS PANEL 221EFF SECTION 41 OF MDC FLOOR PANEL 221EFF MDC SECTION 41 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 92 APR 15
- [SDR FDEA202507211285](https://openairdocs.org/sdr/FDEA202507211285), Jul 21, 2025: FLOOR PANEL. CRACKED. CRACK ON FLOOR PANEL 241DFF AT MDC SEC 45 FLOOR PANEL 241DFF MDC SEC 45 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025.
- [SDR FDEA202507211284](https://openairdocs.org/sdr/FDEA202507211284), Jul 21, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 241KFF AT MDC SEC 45 FLOOR PANEL 241KFF MDC SEC 45 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025
- [SDR FDEA202507211283](https://openairdocs.org/sdr/FDEA202507211283), Jul 21, 2025: FLOOR PANEL. CRACKED. DENT WITH CRACK ON FLOOR PANEL 252DFF AT MDC SEC 46 FLOOR PANEL 252DFF MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2
- [SDR FDEA202507211282](https://openairdocs.org/sdr/FDEA202507211282), Jul 21, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 241ZFF AT MDC SEC 45 FLOOR PANEL 241ZFF MDC SEC 45 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025
- [SDR FDEA202507171230](https://openairdocs.org/sdr/FDEA202507171230), Jul 17, 2025: SKIN. DENTED. ONE DENT IN SURFACE INNERSIDE LOWER SKIN INSIDE CORNER OF INBOARD AFT FLAP OF INBOARD FLAP RIGHT WING. RT WING, INBD T/E FLAP LOWER SURFACE, DENT WAS REPAIRED I
- [SDR FDEA202505120751](https://openairdocs.org/sdr/FDEA202505120751), May 12, 2025: PITOT HEAD. OBSTRUCTED. DURING CLIMB AT ABOUT 20K, JUST AFTER PASSING THRU SOME CLOUDS, RECEIVED ALT DISAGREE ADVISORY EICAS. CONSULTED QRH AND DETERMINED FO ALTIMETER WAS THE ISSUE AT
- [SDR FDEA202408051083](https://openairdocs.org/sdr/FDEA202408051083), Aug 5, 2024: FLOORBOARD. DELAMINATED. NR #7 READ "FLOORBOARD DAMAGED BETWEEN STATIONS 1100-1197". INSPECTED NOT ACCEPTED. MAIN DECK FLOORBOARD REPAIR MISCLASSIFIED AS MINOR REPAIR. RII BUYBACK FOR M
- [SDR FDEA202408051082](https://openairdocs.org/sdr/FDEA202408051082), Aug 5, 2024: SEAT TRACK. DAMAGED. SEAT TRACK LOBE DAMAGED AT APPROXIMATELY STA.500 RBL 11. REMOVED AND INSTALLED SEAT TRACK, REPAIR ANGLES (2EACH) AND REPAIR STRAP (1EACH) PER FDX E.A. H-5310-T0
- [SDR FDEA202403210330](https://openairdocs.org/sdr/FDEA202403210330), Mar 21, 2024: OUTLET. INOPERATIVE. EFB POWER OUTLET ON THE FO SIDE WAS NOT PROVIDING 110V AC POWER. WHEN THE F/O PLUGGED INTO THE 110V AC POWER OUTLET WE SMELLED ELECTRICAL SMOKE, SO HE UNPLUGGED
- [SDR FDEA202311231887](https://openairdocs.org/sdr/FDEA202311231887), Nov 23, 2023: ORIFICE. FAILED. THE DOOR TO THE CRM IS EXTREMELY HARD TO OPEN - THE CRM IS HOLDING TOO MUCH PRESSURE. DID NOTICE THE EYEBALL VENT DOES NOT EMIT MUCH AIR - SUSPECT MAYBE THE CRM
- [SDR FDEA202307271320](https://openairdocs.org/sdr/FDEA202307271320), Jul 27, 2023: SLAT. GOUGED. RW #8 SLAT LOWER T/E SURFACE AFT OF I/B AUX TRACK GUIDE ARM IS GOUGED REPAIRED RW #8 SLAT LOWER T/E SURFACE AFT OF I/B AUX TRACK GUIDE ARM IAW B767 SRM 57- 43-0
- [SDR FDEA202307271319](https://openairdocs.org/sdr/FDEA202307271319), Jul 27, 2023: AILERON. DAMAGED. LEFT WING I/B AILERON I/B L/E ATTACH FAIRING HAS EXPOSED COMPOSITE MATERIAL COMPLETED PERMANENT REPAIR TO L/H WING AILERON I/B L/E ATTACH FAIRING IAW B767 SRM 5
- [SDR FDEA202307271318](https://openairdocs.org/sdr/FDEA202307271318), Jul 27, 2023: BRACKET. CRACKED. LW INBD L/E AT LES 289 SLAT TORQUE TUBE GUIDE BRACKET IS CRACKED IN SEVERAL PLACES REMOVED AND REPLACED GUIDE BRACKET IAW BOEING DRAWING 114T1240, SHEET 6, REV 
- [SDR FDEA202307251291](https://openairdocs.org/sdr/FDEA202307251291), Jul 25, 2023: BEAM. CRACKED. #2 PYLON, O/B WING DOOR ATTACH ANGLE IS CRACKED REPARED #2 PYLON, OUTBOARD LATCHBEAM IAW EA# H-5450-T0375415-P1, RELEASED AUG 01, 2023,
- [SDR FDEA202307241331](https://openairdocs.org/sdr/FDEA202307241331), Jul 24, 2023: UNKNOWN. UNKNOWN. RUDDER TIP HAS WEAR ON UPPER LEADING EDGE. PERFORMED PERMANENT REPAIR OF RUDDER TIP UPPER LEADING EDGE IAW FDX B767-300 SRM 55-40-30-2R, FDX B767-300 SRM 55-40-
- [SDR FDEA202307201255](https://openairdocs.org/sdr/FDEA202307201255), Jul 20, 2023: BRACKET. CRACKED. R/H WING I/B FIXED L/E SLAT TORQUES TUBE GUIDE BRACKET CRACKED AT THE FASTENER HOLES APPROX LES 285. REMOVED AND REPLACED TORQUE TUBE GUIDE BRACKET IAW BAC DWG 
- [SDR FDEA202302210329](https://openairdocs.org/sdr/FDEA202302210329), Feb 21, 2023: CONTROL LEVER. FAILED. WHEN LANDING GEAR LEVER PLACE TO OFF DURING AFTER TAKE OFF CHECK FROM MMMY THE RIGHT MAIN AND NOSE GEAR EXTENDED WITH GREEN LIGHTS ON. LEFT MAIN STAYED UP. DOOR
- [SDR FDEA202210292694](https://openairdocs.org/sdr/FDEA202210292694), Oct 29, 2022: IDG. FAULTED. BEGINNING T/O ROLL ON RWY 18L AT MEM, RECEIVED R GEN DRIVE EICAS T/O REJECTED AT 7 KTS GROUND SPEED. EXITED RUNWAY. RAN QRH, DIRECTED RIGHT GEN DRIVE DISCONNECT
- [SDR FDEA202209252369](https://openairdocs.org/sdr/FDEA202209252369), Sep 25, 2022: FORMER. CRACKED. CRACK ON NOSE FORMER OSS 441.596 L/H SIDE. REPLACED L/H LEADING EDGE FORMER AT STA OSS441 IAW E.A. H-5720-T0370796 PART1
- [SDR FDEA202209252368](https://openairdocs.org/sdr/FDEA202209252368), Sep 25, 2022: FORMER. CRACKED. R/H LEADING EDGE FORMER CRACKED AT OSS 441 REPLACED R/H LEADING EDGE FORMER AT STA OSS-441 IAW E.A. H-5720-T0370795 PART1
- [SDR FDEA202204120941](https://openairdocs.org/sdr/FDEA202204120941), Apr 12, 2022: FORMER. CRACKED. R/H WING L/E AT STA OSS-441 HAS LOOSE RIVETS AND A CRACKED FORMER P/N 114T2170-6 0000452710 : ROSNER, DANIEL D - 13-APR-2022 02:58 COMPLIED WITH E.A WORK CARD T
- [SDR FDEA202204120940](https://openairdocs.org/sdr/FDEA202204120940), Apr 12, 2022: FORMER. CRACKED. L/H WING L/E AT STA OSS565 HAS LOOSE RIVETS AND A CRACKED FORMER P/N 114T2512-13 0000355851 : MITROVICH, DAVID T - 13-APR-2022 02:39 C/W EA T H-5720-T0367965 P1
- [SDR FDEA202204120938](https://openairdocs.org/sdr/FDEA202204120938), Apr 12, 2022: FORMER. CRACKED. L/H WING L/E AT STA OSS441 HAS LOOSE RIVETS AND A CRACKED FORMER P/N 114T2170-5 0000553921 : DAVIES, ANDREW M - 13-APR-2022 00:38 REPLACED LOOSE FASTENERS AND R
- [SDR FDEA202204120937](https://openairdocs.org/sdr/FDEA202204120937), Apr 12, 2022: RIVET. LOOSE. R/H WING L/E AT STA OSS-565 HAS LOOSE RIVETS 0000301922 : VERNON, JAMES L - 12-APR-2022 22:36 REPLACED FASTENERS REF E.A. TH-5729-T0367962 , PAGE 3 OF 3 , W/O 8
- [SDR FDEA202204120936](https://openairdocs.org/sdr/FDEA202204120936), Apr 12, 2022: RIVET. LOOSE. R/H WING L/E AT STA OSS-499 HAS LOOSE RIVETS 0000301922 : VERNON, JAMES L - 12-APR-2022 22:33 REPLACED FASTENERS REF E.A. TH-5720-T0367962 P2 , PAGE 3 OF 3 , SE
- [SDR FDEA202204120935](https://openairdocs.org/sdr/FDEA202204120935), Apr 12, 2022: RIVET. LOOSE. L/H WING L/E AT STA OSS499 HAS LOOSE RIVETS. REPLACED LOOSE RIVETS WITH SCREWS. REF. E.A. H-5720-T0367962 P1.
- [SDR FDEA202204120934](https://openairdocs.org/sdr/FDEA202204120934), Apr 12, 2022: RIVET. LOOSE. R/H WING L/E AT STA OSS-437 HAS LOOSE RIVETS 0000301922 : VERNON, JAMES L - 12-APR-2022 22:27 REPLACED FASTENERS REF E.A. TH-5720-T0367962 P2 , PAGE 3 OF 3 , SE
- [SDR FDEA202202210933](https://openairdocs.org/sdr/FDEA202202210933), Feb 21, 2022: RIVET. LOOSE. LOOSE RIVETS INSTALLED SCREWS
- [SDR FDEA202012143155](https://openairdocs.org/sdr/FDEA202012143155), Dec 14, 2020: SWITCH. OUT OF TOLERANCE. AT FL380 EICAS MAIN CARGO DOOR ILLUMINATED FOLLOWED QRH PROCEDURES & LANDED. LIGHT EXTINGUISHED PASSING 16,000 IN DECENT. NO CABIN DEPRESSURIZATION OR NOISE FRO
- [SDR FDEA2020072311601](https://openairdocs.org/sdr/FDEA2020072311601), Jul 21, 2020: SKIN. DENTED. LEFT WING INBOARD FLAP DENTED OUTBOARD END. REPAIRED THE LT WING INBD FLAP IAW EA H-5750-T0355223-P1.
- [SDR FDEA2020072301592](https://openairdocs.org/sdr/FDEA2020072301592), Jul 20, 2020: FLOORBOARD. DELAMINATED. MAIN CABIN FLOORBOARD 241TFF WAS DELAMINATED ON BOTTOM FLOOR PANEL SKIN. FABRICATED NEW FLOORBOARD IAW SRZ 25-005
- [SDR FDEA2020072301591](https://openairdocs.org/sdr/FDEA2020072301591), Jul 20, 2020: FLOORBOARD. DELAMINATED. MAIN CABIN FLOOR PANEL 242QFF HAS DELAM ON BOTTOM FLOOR SKIN. FAB'D NEW FLOORBOARD 242QFF IAW FED EX SRZ-25-005
- [SDR FDEA2020072301589](https://openairdocs.org/sdr/FDEA2020072301589), Jul 20, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 242UFF HAD BROKEN INSERTS. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005, REV R.
- [SDR FDEA202004230774](https://openairdocs.org/sdr/FDEA202004230774), Apr 23, 2020: SWITCH. OUT OF ADJUST. ON CLIMBOUT APPROACHING LEVEL OFF ALTITUDE (PASSING FL 330) EICAS MAIN CARGO DOOR DISPLAYED. PRESSURIZATION WAS NORMAL, DIFFERENTIAL PRESSURE WAS SHOWING APPROX
- [SDR FDEA201904100780](https://openairdocs.org/sdr/FDEA201904100780), Apr 10, 2019: TIRE. FAILED. PDIS 126 32-41 3425 09APR19 MEM SUSPECT NOSE TIRE FAILURE DURING TAXI OUT AT NORMAL TAXI SPEED ON STRAIGHT AWAY. FACT 09APR19 19:13 MEM AMM: 32-45-02-4 - FOUND 
- [SDR FDEA201811243366](https://openairdocs.org/sdr/FDEA201811243366), Nov 24, 2018: LATCH. OUT OF POSITION. CAPT'S SIDE ESCAPE ROPE COVER WILL NOT STAY LATCHED CLOSED. REPOSITIONED LATCH 10C80-2 ON PANEL ASSY TO ENSURE ESCAPE ROPE COVER DOOR WILL LATCH CLOSED. REF DRA
- [SDR FDEA201810032774](https://openairdocs.org/sdr/FDEA201810032774), Oct 3, 2018: BUSHING. WORN. NR 2 ENGINE INBOARD AFT FAIRING STRUT SKIRT BEAM AFT HINGE BUSHING AND LUG WORN. INSTALLED REPAIR BUSHINGS AT WORN HINGE LOCATION ON NR 2 ENGINE INBD AFT FAIRIN
- [SDR FDEA2018091082422](https://openairdocs.org/sdr/FDEA2018091082422), Sep 8, 2018: ADAPTER. LEAKING. RIGHT GEN DRIVE EICAS CAME ON RESULTED IN A REJECTED TAKE OFF AT 40 KTS. INSPECTED THE RIGHT IDG AND OIL SYSTEM, NO LEAKAGE WAS FOUND. DRAINED AND SERVICED THE 
- [SDR FDEA201711203282](https://openairdocs.org/sdr/FDEA201711203282), Nov 20, 2017: UNKNOWN. ODOR. BURNED RUBBER ODOR IN THE COCKPIT DURING TAXI. ODOR WENT AWAY AND CAME BACK ON POWER RUN UP FOR TAKEOFF. RAN BOTH ENGINES UP TO HIGH POWER AND APU IAW JRH. RAN 
- [SDR FDEA201704171226](https://openairdocs.org/sdr/FDEA201704171226), Apr 17, 2017: UNKNOWN. ODOR. DURING DESCENT, WITH THROTTLES AT IDLE PASSING 16,000', CREW NOTICED FAINT ODOR OF BURNING TIRES. NO VISIBLE SMOKE OBSERVED BY CREW DURING FLIGHT. ODOR LESSENED
- [SDR FDEA201601200212](https://openairdocs.org/sdr/FDEA201601200212), Jan 20, 2016: VALVE. DISCONNECTED. AT APPROX 4000' WE HEARD AN ABNORMAL NOISE FOLLOWED BY A RUMBLE OF AIRFLOW FROM LOWER EQUIP COMPARTMENT. RECEIVED A FWD EQUIPMENT VALVE, EICAS. RAN ALL QRH PROL
- [SDR FDEA201601190205](https://openairdocs.org/sdr/FDEA201601190205), Jan 19, 2016: CONNECTOR. DISCONNECTED. AT APPROX 4000' WE HEARD AN ABNORMAL NOISE FOLLOWED BY A RUMBLE OF AIRFLOW FROM LOWER EQUIP COMPARTMENT. WE THEN GOT A, FWD EQPT VAL, EICAS. RAN ALL QRH PROLS. 

## 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 767-3S2F aircraft: https://openairdocs.org/model/boeing-767-3s2f/aircraft.md
- The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.md

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