# N122FE: 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: 42715
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 12, 2015
- Certificate issued: July 7, 2015
- Expires: July 31, 2028
- Mode S code: A05BA2
- 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=122FE
- Page: https://openairdocs.org/aircraft/N122FE

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 N122FE.

## FAA accident and incident reports

None matched to N122FE.

## Service difficulty reports (37)

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 FDEA202610031487](https://openairdocs.org/sdr/FDEA202610031487), Oct 3, 2026: SEAT TRACK. BROKEN. DURING UNLOADING, RAMP CREW REPORTED THE MDC LOCK (ID: H503) FLOOR SEAT TRACK IS BROKEN. COMPLIED WITH EA H-5310-T0388991 REPAIRED THE BROKEN MAIN DECK FLOOR CA
- [SDR FDEA202506180987](https://openairdocs.org/sdr/FDEA202506180987), Jun 18, 2025: WARNING LIGHT. FALSE ACTIVATION. ON A 10 MILE FINAL WITH THE GEAR DOWN, WE SELECTED FLAPS 25 AND GOT A MASTER CAUTION, LE SLAT DISAGREE LIGHT. WE ELECTED TO DO A GO AROUND AND SELECTED FLAPS 20
- [SDR FDEA202504200622](https://openairdocs.org/sdr/FDEA202504200622), Apr 20, 2025: STRINGER SPLICE. NOT REPORTED. COMPLY WITH FEDEX EO:H-5310-E0365800 A P2 FOR INSTALL THE SPLICE FITTINGS ON S-20R AT STA 1506, STA 1530, STA 1552. COMPLIED WITH FEDEX EO: H-5310-E0365800 A P2
- [SDR FDEA202504200621](https://openairdocs.org/sdr/FDEA202504200621), Apr 20, 2025: STRINGER SPLICE. NOT REPORTED. COMPLY WITH FEDEX EO:H-5310-E0365800 A P1 FOR INSTALL THE SPLICE FITTINGS ON S-20L AT STA 1506, STA 1530, STA 1552. COMPLIED WITH FEDEX EO: H-5310-E0365800 A P1
- [SDR FDEA202305300973](https://openairdocs.org/sdr/FDEA202305300973), May 30, 2023: DOOR. GOUGED. #1 ENGINE I/B T/R LOWER FWD PANEL INNER SURFACE HAS 2EA GOUGES AS MARKED REPAIRED #1 ENGINE, INBOARD TR, FWD BLOWOUT DOOR IAW FEDEX EA# H-7830-T0374581-P1, TITL
- [SDR FDEA202305260951](https://openairdocs.org/sdr/FDEA202305260951), May 26, 2023: FRAME. CRACKED. #1 PYLON, HYDRAULIC BAY, OUTBOARD MID SPAR FITTING IS CRACKED REPAIRED #1 PYLON, AFT FAIRING ASSY, NAC STA 329 MID SPAR FRAME IAW B767 SRM 54-52-71- 2R, REPAIR 
- [SDR FDEA202305260947](https://openairdocs.org/sdr/FDEA202305260947), May 26, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-8, WO# 8558
- [SDR FDEA202305260946](https://openairdocs.org/sdr/FDEA202305260946), May 26, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-6, WO# 8558
- [SDR FDEA202305260945](https://openairdocs.org/sdr/FDEA202305260945), May 26, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-5, WO# 8558
- [SDR FDEA202305260944](https://openairdocs.org/sdr/FDEA202305260944), May 26, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-7, WO# 8558
- [SDR FDEA202305240935](https://openairdocs.org/sdr/FDEA202305240935), May 24, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-6, WO# 8558
- [SDR FDEA202305240934](https://openairdocs.org/sdr/FDEA202305240934), May 24, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-8, WO# 8558
- [SDR FDEA202305240933](https://openairdocs.org/sdr/FDEA202305240933), May 24, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-5, WO# 8558
- [SDR FDEA202305240932](https://openairdocs.org/sdr/FDEA202305240932), May 24, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-7, WO# 8558
- [SDR FDEA202305220914](https://openairdocs.org/sdr/FDEA202305220914), May 22, 2023: SLAT. CHAFED. #5 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OF OBRD MAIN TRACK. REPAIRED #5 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OUTBOARD MAIN TRACK WITH PERMANEN
- [SDR FDEA202305220913](https://openairdocs.org/sdr/FDEA202305220913), May 22, 2023: FLAP. DAMAGED. LW INBOARD MAIN FLAP, UPPER SKIN HAS DAMAGE ON OB EDGE. REPAIRED LW INBOARD MAIN FLAP, UPPER SURFACE SKIN IAW FED EX EA H-5750-T0374477-P1- WING-FLIGHT SURFACES
- [SDR FDEA202305220912](https://openairdocs.org/sdr/FDEA202305220912), May 22, 2023: FLAP. DAMAGED. RH WING INBD MAIN FLAP UPPER SURFACE HAS EDGE DAMAGE ON OUTBD END. REPAIRED RH WING INBD MAIN FLAP UPPER SURFACE ON OUTBD END IAW FED EX EA H-5750- T0374487-P1-
- [SDR FDEA202305200911](https://openairdocs.org/sdr/FDEA202305200911), May 20, 2023: SLAT. GOUGED. RIGHT WING #8 SLAT TRAILING EDGE LOWER SKIN HAS 2 GOUGES. REPAIRED RIGHT WING #8 SLAT LOWER SKIN IAW B767 SRM 57-43-02-1A AND 51-70-10-2R.
- [SDR FDEA202305190910](https://openairdocs.org/sdr/FDEA202305190910), May 19, 2023: FLAP. CHAFED. RIGHT WING INBOARD FLAP LOWER SURFACE HAS CHAFFING WEAR MARKS ON EACH SIDE OF #6 FLAP FAIRING REPAIRED RIGHT WING INBOARD FLAP LOWER SKIN IAW B767 SRM 57-53-01-
- [SDR FDEA202305190909](https://openairdocs.org/sdr/FDEA202305190909), May 19, 2023: FLAP. GOUGED. RIGHT WING INBOARD AFT FLAP HAS EDGE DAMAGE ON TRAILING EDGE UPPER SURFACE. REPAIRED RIGHT WING INBOARD AFT FLAP IAW B767 SRM 57-53-01-2R AND 51-70-10-2R.
- [SDR FDEA202305190908](https://openairdocs.org/sdr/FDEA202305190908), May 19, 2023: FLAP. GOUGED. RIGHT WING INBOARD AFT FLAP HAS EDGE DAMAGE ON TRAILING EDGE UPPER SURFACE. REPAIRED RIGHT WING INBOARD AFT FLAP IAW B767 SRM 57-53-01-2R AND 51-70-10-2R.
- [SDR FDEA202305190907](https://openairdocs.org/sdr/FDEA202305190907), May 19, 2023: SLAT. CHAFED. #5 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OF INBOARD AUX. TRACK. REPAIRED #5 SLAT WEDGE LOWER SKIN IAW B767 SRM 57-43-02-2R AND 51-70-10-2R.
- [SDR FDEA202305190906](https://openairdocs.org/sdr/FDEA202305190906), May 19, 2023: SLAT. CHAFED. #4 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OF INBOARD ACTUATOR CONTROL ROD. REPAIRED #4 SLAT WEDGE LOWER SKIN IAW B767 SRM 57-43-02-2R AND 51-70-10-2R.
- [SDR FDEA202209012133](https://openairdocs.org/sdr/FDEA202209012133), Sep 1, 2022: NONE. NONE. AT CRUISE FL380 RECEIVED FUEL CONFIG EICAS AND FUEL CONFIG AMBER LIGHT ON FUEL PANEL. FUEL LEVEL WAS ABOUT 4K LOWER IN RIGHT MAIN THAN LEFT MAIN, RAN QRH PROCED
- [SDR FDEA202209012134](https://openairdocs.org/sdr/FDEA202209012134), Sep 1, 2022: WARNING MESSAGE. ACTIVATED. AT CRUISE FL380 RECEIVED FUEL CONFIG EICAS AND FUEL CONFIG AMBER LIGHT ON FUEL PANEL. FUEL LEVEL WAS ABOUT 4K LOWER IN RIGHT MAIN THAN LEFT MAIN, RAN QRH PROCED
- [SDR FDEA202207311834](https://openairdocs.org/sdr/FDEA202207311834), Jul 31, 2022: BEAM. CHAFED. #1 ENG INBD PANEL 436CR HAS A LOOSE NUTPLATE THAT HAS WORN INTO THE STRUT FAIRING BEAM. REPAIRED #1 ENGINE INBD SKIRT BEAM AT FOWARD END REF 767 SRM 54-52-71-2R
- [SDR FDEA202207301849](https://openairdocs.org/sdr/FDEA202207301849), Jul 30, 2022: BEAM. CHAFED. #1 ENGINE, PYLON PANEL 437BR HAS WORN HINGES. MWT 0000481208 : MEYER, LONNY W - 03-AUG-2022 10:53 SKIRT PANEL WAS REMOVED AND BUSHINGS REPLACED REF 767 SRM 51-4
- [SDR FDEA202112042990](https://openairdocs.org/sdr/FDEA202112042990), Dec 4, 2021: NONE. NONE. LIGHTNING STRIKE APPROX. STA 532, STR 39L. MWT 0000530614 : TURCOTTE, GARRETT S - 05-DEC-2021 15:18 INSTALLED REPAIR DOUBLER REF 767 SRM 53-00-01-2R REPAIR 1 AT
- [SDR FDEA201911012813](https://openairdocs.org/sdr/FDEA201911012813), Nov 1, 2019: FSEU. MALFUNCTIONED. LE SLAT DISAGREE ON FINAL. AFTER GO AROUND AND QRH, EICAS WENT AWAY FOR NORMAL CONFIGURATION AT LANDING. NO STATUS MESSAGE. FSEU SHOWED INTERMITTENT FAULTS WITH
- [SDR FDEA2018122433597](https://openairdocs.org/sdr/FDEA2018122433597), Dec 23, 2018: LAMP. INOPERATIVE. L1 DOOR SLIDE EMERGENCY EXIT LIGHT INOP. RE-LAMPED, GRND CKS NORMAL.
- [SDR FDEA201709262724](https://openairdocs.org/sdr/FDEA201709262724), Sep 26, 2017: FLOOR PANEL. DELAMINATED. FLOOR PANEL 141T5856-107 HAS DELAM. FABRICATED NEW FLOOR PANEL 141T5856-107 ON T17/1297035, PER SRZ 25-005, REV M. MAJOR REPAIR.
- [SDR FDEA201703170946](https://openairdocs.org/sdr/FDEA201703170946), Mar 17, 2017: SWITCH. STUCK. DURING GEAR DOWN LIGHT CHECK PRESSED LIGHTS TEST SWITCH AND ALL LIGHT STUCK IN THE TEST MODE. UNABLE TO CHANGE RADIO FRQ'S ETC. AFTER LANDING, WE COULD CYCLE TH
- [SDR FDEA201608283101](https://openairdocs.org/sdr/FDEA201608283101), Aug 28, 2016: FITTING. OUT OF POSITION. FOUND HAZCAN FIRE EXTINGUISHER FITTINGS IN THE WRONG POSITION IAW DWG B67-26-001, SHEET 4. MOVED HAZCAN FIRE EXTINGUISHER FITTINGS TO THE CORRECT POSITION IAW D
- [SDR FDEA201608263102](https://openairdocs.org/sdr/FDEA201608263102), Aug 26, 2016: FITTING. OUT OF POSITION. FOUND HAZCAN FIRE EXTINGUISHER FITTINGS IN THE WRONG POSITION IAW DWG B67-26-001, SHEET 4. MOVED HAZCAN FIRE EXTINGUISHER FITTINGS TO THE CORRECT POSITION IAW D
- [SDR FDEA201511083518](https://openairdocs.org/sdr/FDEA201511083518), Nov 8, 2015: SUPPORT ANGLE. CRACKED. WHILE REPAIRING LOWER AFT CARGO DOOR UPPER SEAL RETAINER, REF WRI 52-30/0336, FOUND FORM ANGLE CRACK, PICTURES ATTACHED. CUT OUT DAMAGED AREA OF SUPPORT ANGLE &
- [SDR FDEA201511033455](https://openairdocs.org/sdr/FDEA201511033455), Nov 3, 2015: PROBE. DAMAGED. ABORTED TAKEOFF ROLL AT 85 KTS. CAPTAINS AIRSPEED INDICATOR REMAINED AT 30 KTS, NEVER INCREASED FROM STATIC. FIRST OFFICERS AIRSPEED INDICATOR READ 85 KTS AT RE
- [SDR FDEA201510013035](https://openairdocs.org/sdr/FDEA201510013035), Oct 1, 2015: OXYGEN MASK. FAILED. DURING IN FLIGHT USE OF FIRST OFFICERS O2 MASK, NOTICED THERE WAS RESTRICTION TO AIRFLOW DRAW & A PULSED DELIVERY. CONSTANT EMER FLOW WOULD NOT WORK. SWAPPED WI

## 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

## Earlier aircraft with N122FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N122FE before.

- [Cancelled 1994-02-25](https://openairdocs.org/deregistered/N122FE-1994-02-25): Boeing 727-25C, S/N 19358. Exported to Canada. Owner: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)

## 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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