# N118FE: 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: 42714
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 8, 2015
- Certificate issued: April 22, 2015
- Expires: April 30, 2028
- Mode S code: A04A6D
- 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=118FE
- Page: https://openairdocs.org/aircraft/N118FE

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 N118FE.

## FAA accident and incident reports

None matched to N118FE.

## Service difficulty reports (55, 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 FDEA202607170939](https://openairdocs.org/sdr/FDEA202607170939), Jul 17, 2026: SEAT TRACK. DAMAGED. DURING UNLOADING, RAMP CREW REPORTED THE MDC LOCK (ID: H373) FLOOR SEAT TRACK IS BROKEN. CAN NO RESTRICTION REF EA H-5321-T0387977 MDC LOCK ID H373 BS 500 FLOOR
- [SDR FDEA202511182189](https://openairdocs.org/sdr/FDEA202511182189), Nov 18, 2025: STRUCTURE. NO DISCREPANCY. WE HEARD A LOUD BANG IN FLIGHT AT THE TOP OF DESCENT. THE SAME NOISE OCCURRED SEVERAL MORE TIMES AT THE BEGINNING OF EACH DESCENT. UPON INSPECTION AFTER LANDING
- [SDR FDEA202404180467](https://openairdocs.org/sdr/FDEA202404180467), Apr 18, 2024: VALVE. FAILED. WHILE WE WERE AWAITING TAKEOFF CLEARANCE WITH THE PARKING BRAKE SET, RECEIVED A MASTER CAUTION WITH A R HYD QTY EICAS MESSAGE FOLLOWED BY A R HYD PRIM PUMP EICA
- [SDR FDEA202401260114](https://openairdocs.org/sdr/FDEA202401260114), Jan 26, 2024: CIRCUIT CARD. INOPERATIVE. SPEED BRAKES SEGMENT LIGHT & SPREED BRAKES EXT EICAS MESSAGE ILLUMINATED AFTER TAKEOFF BELOW 1000FT. AFTER ARRIVAL, ACFT CAUTION MSG EICAS & SPEED BRAKES ANNUNC
- [SDR FDEA202311251896](https://openairdocs.org/sdr/FDEA202311251896), Nov 25, 2023: ACCESS DOOR. CRACKED. LOWER HALF OF FUSELAGE, ACCESS DOOR 113AL WITH A BIRD STRIKE ON EXTERNAL SURFACE. THE DAMAGE AT EXTERNAL SURFACE IN ACCESS DOOR 113AL WAS REPAIRED. I.A.W. DRAWI
- [SDR FDEA202311241891](https://openairdocs.org/sdr/FDEA202311241891), Nov 24, 2023: SKIN. DENTED. LOWER HALF OF FUSELAGE, BETWEEN STA 135.5 AND STA 148.5, AND BETWEEN STGR 21R AND STGR 30R, BIRD STRIKE. DAMAGE AT LOWER HALF OF FUSELAGE, BETWEEN STA 135.5 AND
- [SDR FDEA202311241890](https://openairdocs.org/sdr/FDEA202311241890), Nov 24, 2023: SKIN. CRACKED. UPPER HALF OF FUSELAGE, BETWEEN STA 132.5 AND STA 143.5, AND BETWEEN STGR 14-L AND STGR 18-L, BIRD STRIKE. DAMAGE AT UPPER HALF OF FUSELAGE, BETWEEN STA 132.5 A
- [SDR FDEA202311241889](https://openairdocs.org/sdr/FDEA202311241889), Nov 24, 2023: SKIN. DAMAGED. LOWER HALF OF FUSELAGE, BETWEEN STA 132.5 AND 143.5, AND BETWEEN STGR 30-L AND STGR 31-L, BIRD STRIKE. DAMAGE AT LOWER HALF OF FUSELAGE, BETWEEN STA 132.5 AND B
- [SDR FDEA202308021344](https://openairdocs.org/sdr/FDEA202308021344), Aug 2, 2023: UNKNOWN. UNKNOWN. ESCAPE ROPE FOR CREW ENTRY DOOR IS PARTIALLY OUT OF ITS POCKET JAMMING THE DOOR. REINSTALLED EMERGENCY ECSAPE ROPE AS REQUIRED IAW MM 25-61-04-2-1. OK FOR SERVI
- [SDR FDEA202304150655](https://openairdocs.org/sdr/FDEA202304150655), Apr 15, 2023: FLAP. UNKNOWN. FOUND DENT ON RH INBOARD TRAILING EDGE FLAP TOPSIDE. REPAIRED RT WING- INBOARD FLAP UPPER SKIN TOP SURFACE TRAILING EDGE DENT AT LOCATION INBD FLAP TRAILING EDG
- [SDR FDEA202206061384](https://openairdocs.org/sdr/FDEA202206061384), Jun 6, 2022: SLAT. DENTED. RH WING SLAT # 8 WITH 11 DENTS IN UPPER WEDGE AREA RH WING SLAT # 8 WITH 14 DENTS WERE EVALUATED AND FOUND WITHIN LIMITS IAW SRM MAXIMIM DIMENSION L= 1.600" W=0
- [SDR FDEA202206041375](https://openairdocs.org/sdr/FDEA202206041375), Jun 4, 2022: FLAP. DELAMINATED. RIGHT WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION WBL: 414. RIGHT WING OUTBOARD FLAP LEADING EDGE WBL 414 WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 PAG
- [SDR FDEA202206041374](https://openairdocs.org/sdr/FDEA202206041374), Jun 4, 2022: SLAT. DENTED. LEFT WING SLAT NO 5 DENT IN UPPER WEDGE AREA WS. 433.1 LEFT WING SLAT NO 5 DENT IN UPPER WEDGE AREA WS 433.1 THAT WAS REPAIRED I.A.W. SRM 57- 43-02-2R FIG. 201 
- [SDR FDEA202204160978](https://openairdocs.org/sdr/FDEA202204160978), Apr 16, 2022: FORMER. CRACKED. CRACKED FORMER ON LS PN: 114T2170-5/WITH ANGLE 114T 2171-4; LOOSE/DAMAGED FASTENERS LOCATED AT LS FLE OSS 441 ALSO. 0000452710 : ROSNER, DANIEL D - 17-APR-2022 
- [SDR FDEA202103290794](https://openairdocs.org/sdr/FDEA202103290794), Mar 29, 2021: SLAT. GOUGED. RIGHT WING #8 SLAT, UPPER TRAILING EDGE, LOWER FACE IS GOUGED AT OUTBOARD AUX TRACK. REPAIRED RIGHT WING #8 SLAT UPPER TRAILING EDGE LOWER FACE GOUGED AT OUTBOA
- [SDR FDEA202103230756](https://openairdocs.org/sdr/FDEA202103230756), Mar 23, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 242SFF IS PUNCTURED & HAS EDGE DAMAGE REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R
- [SDR FDEA202103230755](https://openairdocs.org/sdr/FDEA202103230755), Mar 23, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241KFF IS PUNCTURED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R
- [SDR FDEA202103230754](https://openairdocs.org/sdr/FDEA202103230754), Mar 23, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241YFA IS PUNCTURED & HAS EDGE DAMAGE REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R
- [SDR FDEA202103230753](https://openairdocs.org/sdr/FDEA202103230753), Mar 23, 2021: FLOOR PANEL. DELAMINATED. MAIN DECK FLOOR PANEL 242UFF IS DELAMINATED ON FWD END REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R
- [SDR FDEA202103230752](https://openairdocs.org/sdr/FDEA202103230752), Mar 23, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241FFF DENTED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R
- [SDR FDEA202103230751](https://openairdocs.org/sdr/FDEA202103230751), Mar 23, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241BFF HAS DAMAGED INSERT REMOVED & REPLACED INSERT IAW B767 SRM 53-00-50-2R & FEDEX DRAWING SRZ-25-005, REV R
- [SDR FDEA202103210735](https://openairdocs.org/sdr/FDEA202103210735), Mar 21, 2021: STRAP. CRACKED. LEFT WING LEADING EDGE SPLIC STRAP IS CRACKED REMOVED & REPLACED STRAP IAW BAC DWG 114T2800 REV C
- [SDR FDEA202103210734](https://openairdocs.org/sdr/FDEA202103210734), Mar 21, 2021: STRAP. CRACKED. RH WING LEADING EDGE SPLICE STRAP IS CRACKED REMOVED & REPLACED STRAP IAW BAC DWG 114T2800 SHT 6 REV C
- [SDR FDEA202103210736](https://openairdocs.org/sdr/FDEA202103210736), Mar 21, 2021: SHEAR TIE. CRACKED. #2 PYLON, INBD SHEAR TIE @ NAC STA 303 IS CRACKED REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310 REV -
- [SDR FDEA202103200711](https://openairdocs.org/sdr/FDEA202103200711), Mar 20, 2021: HEAT SHIELD. CRACKED. TAIL SECTION , INTERNAL , APU BLEED AIR DUCT HEAT SHIELD IS CRACKED AT THE UPPER AFT ATTACH FASTENER HOLE IN THE L/H STABILIZER TORSION BOX AREA BELOW THE THS J
- [SDR FDEA202103190710](https://openairdocs.org/sdr/FDEA202103190710), Mar 19, 2021: FLOOR SUPPORT. CRACKED. L/H NOSE TUNNEL MAIN CABIN FLOOR SUPPORT STRUCTURAL VERTICAL ANGLE IS CRACKED AT STA 246 APROX LBL50 REMOVED AND REPLACED ANGLE IAW BAC DRAWING 141T5146, REV B
- [SDR FDEA202103190709](https://openairdocs.org/sdr/FDEA202103190709), Mar 19, 2021: ATTACH ANGLE. CRACKED. AFT PIT, FWD OF PIT STA 1087 LBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH ANGLE UPPER SIDE IS CRACKED REMOVED AND REPLACED AFT PIT , FWD OF AFT PIT STA 1087 LB
- [SDR FDEA202103190708](https://openairdocs.org/sdr/FDEA202103190708), Mar 19, 2021: FLOOR SUPPORT. CRACKED. AFT PIT , FWD OF AFT COMP. STA 1087 RBL20 FLOOR SUPPORT STRUCTURE VERTICAL ATTACH CLIP UPPER SIDE IS CRACKED REMOVED AND REPLACED AFT PIT , FWD OF AFT COMPT. ST
- [SDR FDEA202103190704](https://openairdocs.org/sdr/FDEA202103190704), Mar 19, 2021: TUBE. CRACKED. BULK DOOR COMPARTMENT DOOR COUNTER BALANCE SPRING TUBE IS CRACKED REMOVED AND REPLACED BULK DOOR COUNTER BALANCE SPRING TUBE PER B767 AMM 52-36- 02-5
- [SDR FDEA202103180698](https://openairdocs.org/sdr/FDEA202103180698), Mar 18, 2021: SHEAR TIE. CRACKED. NO.1 PYLON, INBD SIDE, NAC STA 303 SHEAR TIE IS CRACKED REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310
- [SDR FDEA202103180699](https://openairdocs.org/sdr/FDEA202103180699), Mar 18, 2021: SHEAR TIE. CRACKED. NO.1 PYLON, INBD SIDE, NAC STA 303 HAS CRACKED SHEAR TIE REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310
- [SDR FDEA202103180690](https://openairdocs.org/sdr/FDEA202103180690), Mar 18, 2021: PANEL. CRACKED. LEFT WING, LEADING EDGE , FUELING PANEL 521 QB , WEB IS CRACKED REPAIRED WEB BEHIND 521 QB IAW B767 SRM 57-41-13-2R , B767 SRM 51-20-01 AND B767 AMM 52-49- 04-4
- [SDR FDEA202103170682](https://openairdocs.org/sdr/FDEA202103170682), Mar 17, 2021: FORMER. CRACKED. LEFT WING NOSE FORMER & ANGLE CRACKED @ OSS 441 REMOVED & REPLACED FORMER & ANGLE ASSY IAW BAC DWG 114T2241REV - & FEDEX EA H- 5720-T0360399-P1
- [SDR FDEA202103140647](https://openairdocs.org/sdr/FDEA202103140647), Mar 14, 2021: FORMER. CRACKED. LH WING LEADING EDGE NOSE FORMER IS CRACKED @ OSS 499 REMOVED & REPLACED FORMER IAW BAC DWG 114T2161 REV - & FEDEX EA H-5720-T0360398-P1
- [SDR FDEA202103140646](https://openairdocs.org/sdr/FDEA202103140646), Mar 14, 2021: BRACKET. CRACKED. RIGHT WING FUELING STATION DOOR LIGHT HOUSING BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW B767 AMM 52-49-04
- [SDR FDEA202103140645](https://openairdocs.org/sdr/FDEA202103140645), Mar 14, 2021: FRAME ANGLE. CRACKED. #1 PYLON, NAC STA 377, OUTBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F
- [SDR FDEA202103140644](https://openairdocs.org/sdr/FDEA202103140644), Mar 14, 2021: FRAME ANGLE. CRACKED. #1 PYLON, NAC STA 377, INBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F
- [SDR FDEA202103140643](https://openairdocs.org/sdr/FDEA202103140643), Mar 14, 2021: FRAME ANGLE. CRACKED. #2 PYLON, NAC STA 377, OUTBD FRAME CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F
- [SDR FDEA202103140642](https://openairdocs.org/sdr/FDEA202103140642), Mar 14, 2021: FRAME ANGLE. CRACKED. #2 PYLON, NAC STA 377, INBD SIDE, FRAME CLIP CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV F
- [SDR FDEA202103120625](https://openairdocs.org/sdr/FDEA202103120625), Mar 12, 2021: BRACKET. CRACKED. RH WING TORQUE TUBE GUIDE BRACKET CRACKED @ LES 285 REMOVED & REPLACED BRACKET IAW BAC DWG 114T1240 REV -
- [SDR FDEA202103120624](https://openairdocs.org/sdr/FDEA202103120624), Mar 12, 2021: BRACKET. CRACKED. LH WING TORQUE TUBE GUIDE BRACKET CRACKED LES 285 REMOVED & REPLACED BRACK IAW BAC DWG 114T1240 REV -
- [SDR FDEA2020082521988](https://openairdocs.org/sdr/FDEA2020082521988), Aug 22, 2020: ROD. DAMAGED. DURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND #6 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT DISASSEMBLED AND R
- [SDR FDEA2020082521987](https://openairdocs.org/sdr/FDEA2020082521987), Aug 22, 2020: ROD. DAMAGED. DURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND #5 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT DISASSEMBLED AND R
- [SDR FDEA2020082521986](https://openairdocs.org/sdr/FDEA2020082521986), Aug 22, 2020: ROD. DAMAGED. DURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND #2 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT DISASSEMBLED AND R
- [SDR FDEA2020082521985](https://openairdocs.org/sdr/FDEA2020082521985), Aug 22, 2020: ROD. DAMAGED. DURING ACCOMPLISHMENT OF FEA H-3243-F0356064, FOUND NR 4 MLG BRAKE ROD NEED TO BE DISASSEMBLE AND PROPERLY REASSEMBLE TO BRAKE ATTACHMENT JOINT. DISASSEMBLED AN
- [SDR FDEA202002070279](https://openairdocs.org/sdr/FDEA202002070279), Feb 7, 2020: PUMP. MALFUNCTIONED. 20 MINUTES INTO FLIGHT GOT FUEL CONFIG ALERT. RETURNED TO KMEM. FUEL NOT FEEDING FROM LEFT TANK. REMOVED AND REPLACED THE L/H AFT BOOST PUMP IN REF. TO B767 AMM
- [SDR FDEA202002040260](https://openairdocs.org/sdr/FDEA202002040260), Feb 4, 2020: PUMP. MALFUNCTIONED. 20 MINUTES INTO FLIGHT GOT FUEL CONFIG ALERT. RETURNED TO KMEM. FUEL NOT FEEDING FROM LEFT TANK. CHANGED LEFT AND RIGHT BOOST PUMPS MPN 5006003D. REMOVED AND RE
- [SDR FDEA201912240001](https://openairdocs.org/sdr/FDEA201912240001), Dec 24, 2019: SKIN. DAMAGED. FUSELAGE HAS IMPACT DAMAGE AT STA 1109 AT STR 4L REPAIRED FUSELAGE SKIN PER E.A. H-5330-T0351626 PART 1.
- [SDR FDEA201909132268](https://openairdocs.org/sdr/FDEA201909132268), Sep 13, 2019: PUMP. LEAKING. APPROX 2HRS INTO FLT, EICAS ALERT 'L HYD QTY', LT HYD QTY SLOWLY DECREASED FROM ABOVE 0.9 TO 0.01 WITH 'RF' INDICATED. EICAS ALERT 'HYD PRIM PUMP' DISPLAYED SHO
- [SDR FDEA2019080871812](https://openairdocs.org/sdr/FDEA2019080871812), Aug 7, 2019: WEDGE. GOUGED. LEFT WING #5 SLAT TRAILING EDGE WEDGE GOUGED REPAIRED DAMAGED IAW EA# H-2780-T0348663 - P1 FLIGHT CONTROL- L/E SLATS-#5 SLAT, TRAILING EDGE SKIN- GOUGE GOUGE-RS

All 55: https://openairdocs.org/aircraft/N118FE/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

## Earlier aircraft with N118FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N118FE before.

- [Cancelled 2002-10-31](https://openairdocs.org/deregistered/N118FE-2002-10-31): Boeing 727-25C, S/N 19300, built 1966. Triennial form not returned. 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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