# N115FE: 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: 42713
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 5, 2015
- Certificate issued: March 23, 2015
- Expires: March 31, 2028
- Mode S code: A03F48
- 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=115FE
- Page: https://openairdocs.org/aircraft/N115FE

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 N115FE.

## FAA accident and incident reports

None matched to N115FE.

## Service difficulty reports (40)

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 FDEA202609141334](https://openairdocs.org/sdr/FDEA202609141334), Sep 14, 2026: SKIN. DAMAGED. NR 10 SLAT HAS MINOR DAMAGE ON LOWER SURFACE APPROXIMATELY 31.5" FROM INBD EDGE. REPAIRED RT WING NR 10 SLAT T/E WEDGE AT OSS 713 .5 IAW SRM 57-43-02-2R AND SRM
- [SDR FDEA202601230081](https://openairdocs.org/sdr/FDEA202601230081), Jan 23, 2026: WINDOW. HAZE. L3, R1, R3 WINDOWS DELAMINATING OBSCURING CRITICAL VISIBILITY AREA AND CREATING A FLIGHT SAFETY HAZARD. AMM: 56-11-00-6-0 REF WRI 56-10/1646, R1 (F/O WONDSHIELD
- [SDR FDEA202512142251](https://openairdocs.org/sdr/FDEA202512142251), Dec 14, 2025: SKIN. DENTED. LEFT WING NR 5 SLAT HAS A DENT IN UPPER TRAILING WEDGE SKIN 34 INCHES FROM INBD EDGE. REPAIRED LT WING NR 5 SLAT UPPER T/E WEDGE SKIN IAW SRM 57-43-02-0I, PG 1-
- [SDR FDEA202512142250](https://openairdocs.org/sdr/FDEA202512142250), Dec 14, 2025: SKIN. DENTED. LEFT WING NR 1 SLAT HAS DENT IN UPPER TRAILING WEDGE SKIN 16" FROM I/B EDGE. REPAIRED LEFT WING NR 1 SLAT UPPER T/E WEDGE SKIN SURFACE 16" FROM I/B EDGE IAW SRM
- [SDR FDEA202511272214](https://openairdocs.org/sdr/FDEA202511272214), Nov 27, 2025: IDG. FAILED. R GEN DRIVE EICAS IN-FLIGHT. ACCOMPANIED BY ILLUMINATED R GEN DRIVE SWITCH LIGHT. COMPLIED WITH QRH. EMERGENCY DECLARED. PERFORMED RT ENG RUN TEST BER AMM 71-00
- [SDR FDEA202511112158](https://openairdocs.org/sdr/FDEA202511112158), Nov 11, 2025: FLAP SYSTEM. FAULTED. AT APPROX 80 KTS ON TAKEOFF GOT EICAS FLAPS AND CONIF. REJECTED THE TAKEOFF RUNWAY 02R AT BKK AT 303 TOGW AND 31C TEMP. RAN CHECKLISTS, RETURNED TO THE GATE LEA
- [SDR FDEA202409051247](https://openairdocs.org/sdr/FDEA202409051247), Sep 5, 2024: BATTERY. NO TEST. MDIS 115 33-50 0178 05SEP24 02:24 TPE FACT DURING SERVICE CHECK, FOUND EMERGENCY LIGHT DIDN'T ILLUMANATE. FACT 05SEP24 02:30 TPE FIM: 33-51-00-815-802 AMM: 33-5
- [SDR FDEA202403080261](https://openairdocs.org/sdr/FDEA202403080261), Mar 8, 2024: SLIDING WINDOW. CRACKED. FO NOTICE IN FLIGHT CRACKING ON PERIMETER OF WINDOWS. RAN CHECKLIST FOR CRACKED WINDOW IN FLIGHT. AS PER CREW DEBRIEF F/O SLIDING WINDOW CRACKED ALONG THE EDGE.
- [SDR FDEA202203310790](https://openairdocs.org/sdr/FDEA202203310790), Mar 31, 2022: NONE. NONE. ON APPROACH INTO SKBO (BOG) AT APPROXIMATELY 10700 MSL, AFTER PUTTING THE LANDING GEAR DOWN, WE ONLY GOT GREEN NOSE GEAR AND A GREEN RIGHT MAIN GEAR LIGHTS. WE 
- [SDR FDEA202203010383](https://openairdocs.org/sdr/FDEA202203010383), Mar 1, 2022: NONE. NONE. RECEIVED MAIN CARGO DOOR ALERT AT FL 390. QRH WAS FOLLOWED AND DIVERTED TO KJAX. NO PRESSURIZATION ISSUES WERE NOTED AT ANY TIME. ALERT WENT AWAY ON DESCENT PAS
- [SDR FDEA202202110749](https://openairdocs.org/sdr/FDEA202202110749), Feb 11, 2022: NONE. NONE. MDIS 115 33-50 6883 11FEB22 BOG DURING POSFLIGHT CHECK FOUND DOOR EMERGENCY LIGHT TOO DIM. FOUND WRONG LAMP INSTALLED. RELAMPED DOOR EMERGENCY LIGHT IAW AMM33-5
- [SDR FDEA202201140069](https://openairdocs.org/sdr/FDEA202201140069), Jan 14, 2022: NONE. SHEARED. REFER TO HUB STRIKE DAMAGE TO LH SLAT UPON INSPECTION OF UNDERLYING STRUCTURE AFTER REMOVAL OF BONDED PANEL ASSY 521ZB, DISCOVERED HOLE IN LEFT WING FIXED LEADI
- [SDR FDEA202104210962](https://openairdocs.org/sdr/FDEA202104210962), Apr 21, 2021: TRANSMITTER. OUT OF ADJUST. LE SLAT DISAGREE ADJUSTED FLAP HANDLE POS. TRANSMITTERS ON TSI 27-80/6190. PERFORMED FLAP AND SLAT PRIMARY DRIVES AND POSITION INDICATING SYSTEM - TEST REF AMM 
- [SDR FDEA202102170386](https://openairdocs.org/sdr/FDEA202102170386), Feb 17, 2021: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241DFF HAS DAMAGE TO SKIN REPAIRED FLOOR PANEL 241DFF PER B767 SRM 53-00-50-2R PARA 4.E
- [SDR FDEA202102170385](https://openairdocs.org/sdr/FDEA202102170385), Feb 17, 2021: SKIN. CRACKED. LH WING, FIXED LEADING EDGE SKIN IS CRACKED @ FASTENER HOLE @ OSS 665 REPAIRED LEADING EDGE SKIN IAW B767 SRM 57-41-01-2R, FIGURE 201
- [SDR FDEA202102160375](https://openairdocs.org/sdr/FDEA202102160375), Feb 16, 2021: SHEAR TIE. CRACKED. #2 PYLON @ DOOR 447BL, FWD SKIRT BEAM SHEAR TIE IS CRACKED REMOVED AND REPLACED SHEAR TIE PER BAC DWG 313T2310REV -
- [SDR FDEA202102160374](https://openairdocs.org/sdr/FDEA202102160374), Feb 16, 2021: BEAM. CRACKED. LEFT WING NOSE BEAM IS CRACKED @ OSS 679 REPAIRED NOSE BEAM WEB IAW B767 SRM 57-41-13-2R, RPEIAR 3
- [SDR FDEA202102120343](https://openairdocs.org/sdr/FDEA202102120343), Feb 12, 2021: SUPPORT ANGLE. CRACKED. AS SEEN FROM BULK PIT AREA, SEAT TRACK SUPPORT ANGLE @ STA 1576, INSIDE R/H SIDEWALL AREA IS CRACKED REMOVED AND REPLACED SEAT TRACK SUPPORT ANGLE PER BAC DWG14
- [SDR FDEA202102120342](https://openairdocs.org/sdr/FDEA202102120342), Feb 12, 2021: SUPPORT. CRACKED. SEAT TRACK SUPPORT ANGLE @ STA 1576, INSIDE L/H SIDEWALL AREA SEAT TRACK SUPPORT ANGLE IS CRACKED REMOVED AND REPLACED SUPPORT ANGLE PER BAC DWG 146T5650 REV C.
- [SDR FDEA202102120338](https://openairdocs.org/sdr/FDEA202102120338), Feb 12, 2021: BEAM. CRACKED. R/W L/E LOWER NOSE WEB IS CRACKED.(FWD OF FUEL/DEFUEL PANEL 621QB.) REMOVED DAMAGED WEB SECTION AND REPAIRED IAW B767 SRM 57-41-13-2R. TREATED REPAIR AREA IAW B
- [SDR FDEA202102110336](https://openairdocs.org/sdr/FDEA202102110336), Feb 11, 2021: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241WFF HAS FIBER DAMAGE. FABRICATED FLOOR PANEL 241KFF PER SRZ-25-005 REV R.
- [SDR FDEA202102110335](https://openairdocs.org/sdr/FDEA202102110335), Feb 11, 2021: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241KFF HAS FIBER DAMAGE FABRICATED NEW FLOOR PANEL PER SRZ-25-005 REV R.
- [SDR FDEA202102100320](https://openairdocs.org/sdr/FDEA202102100320), Feb 10, 2021: SEAL. CRACKED. LEFT WING FIXED L/E INNER STRAP CRACKED AT L.E.S 555. REMOVED AND REPLACED STRAP AT L.E.S 555 IAW B767 SRM 51-40-02, 51-40-05 AND BAC DWG 114T2800 REV.C
- [SDR FDEA202102090317](https://openairdocs.org/sdr/FDEA202102090317), Feb 9, 2021: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT FLOOR SUPPORT STRINGER IS CRACKED AT RBL 36.91 AT STA.1480. REMOVED AND REPLACED FLOOR STRINGER SECTION AT RBL 36.91 IAW B767 SRM 51-40-0
- [SDR FDEA202102070305](https://openairdocs.org/sdr/FDEA202102070305), Feb 7, 2021: ATTACH ANGLE. CRACKED. R/H WING L/E FORMER ATTACH ANGLE CRACKED @ OSS 441 REMOVED CRACKED FORMER ATTACH ANGLE/INSTALLED NEW L/E FORMER ATTACH ANGLE IAW IAW BAC DWG 114T2241 REV-
- [SDR FDEA202102070301](https://openairdocs.org/sdr/FDEA202102070301), Feb 7, 2021: FORMER. CRACKED. LEFT WING L/E FORMER CRACKED @OSS 441 RRMOVED CRACKED FORMER/INSTALLED NEW FORMERIAW BAC DWG114T2241 REV-
- [SDR FDEA202102070307](https://openairdocs.org/sdr/FDEA202102070307), Feb 7, 2021: FORMER. CRACKED. R/H WING L/E FORMER CRACKED @ OSS499 REMOVED CRACKED R/H L/E FORMER/INSTALLED NEW R/H L/E FORMER @ OSS 499
- [SDR FDEA202102070306](https://openairdocs.org/sdr/FDEA202102070306), Feb 7, 2021: FORMER. CRACKED. R/H WING L/E FORMER CRACKED @ OSS 565 REMOVED CRACKED R/H L/E FORMER/INSTALLED NEW R/H L/E FORMER IAW BAC DWG 114T2512 114T2512 REV D
- [SDR FDEA202102070304](https://openairdocs.org/sdr/FDEA202102070304), Feb 7, 2021: FORMER. CRACKED. R/H WING L/E FORMER CRACKED @ OSS 441 REMOVED CRACKED FORMER/INSTALLED NEW FORMER IAW BAC DWG 114T2241 REV-
- [SDR FDEA202102070303](https://openairdocs.org/sdr/FDEA202102070303), Feb 7, 2021: FORMER. CRACKED. L/H WING L/E FORMER CRACKED @ OSS 565 REMOVED CRACKED FORMER/INSTALLED NEW FORMER IAW BAC DWG 114T2162 REV-
- [SDR FDEA202102070302](https://openairdocs.org/sdr/FDEA202102070302), Feb 7, 2021: ATTACH ANGLE. CRACKED. L/H WING L/E FORMER ATTACH ANGLE CRACKED @ OSS 437 REMOVED CRACKED FORMER ATTACH ANGLE/INSTALLED NEW FORMER ATTACH ANGLE IAW BAC DWG 114T2240 REV-
- [SDR FDEA202102070300](https://openairdocs.org/sdr/FDEA202102070300), Feb 7, 2021: ATTACH ANGLE. CRACKED. L/H WING FORMER ATTACH ANGLE CRACKED @OSS441 REMOVED CRACKED FORMER ATTACH ANGLE/INSTALLED NEW ANGLE IAW BAC DWG114T2241,REV-
- [SDR FDEA202102010262](https://openairdocs.org/sdr/FDEA202102010262), Feb 1, 2021: FLANGE. CRACKED. AFT LOWER CARGO PIT STA. 1087 VERTICAL FLANGE BELOW FLOOR LINE AT LBL25 UPPER END IS CRACKED. REMOVED AND REPLACED AFT LOWER CARGO PIT STA.1087 VERTICAL FLANGE 
- [SDR FDEA2019122313277](https://openairdocs.org/sdr/FDEA2019122313277), Dec 21, 2019: ECU. MALFUNCTIONED. CRUISE FL370 SCANNING OVERHEAD PRIOR TO DESCENT. OBSERVED RT EEC ALTN IN MODE SWITCH. NO ACCOMPANY EICAS. REFERENCED QRH, DECIDED TO PUT BOTH EEC IN SAME MODE "
- [SDR FDEA2018080311862](https://openairdocs.org/sdr/FDEA2018080311862), Jul 31, 2018: LIGHT. INOPERATIVE. UPON LOWERING GEAR HAD NOSE & LEFT GEAR INDICATION BUT NO RIGHT GEAR INDICATION. RAN CHECKLIST FOR GEAR DISAGREE. JUMPSEATER WAS ABLE TO GET US A BULB TO REPLAC
- [SDR FDEA201803070639](https://openairdocs.org/sdr/FDEA201803070639), Mar 7, 2018: MODULE. MALFUNCTIONED. CAPT ALTIMETER INDICATING 300' LOW DURING CLIMB AFTER 18,000' AT FL340 AND AFTER DESCENT TO FL280. ERROR WENT AWAY AFTER 15-20 MINUTES F/O & STBY ALT INDICATED 
- [SDR FDEA201710263047](https://openairdocs.org/sdr/FDEA201710263047), Oct 26, 2017: SWITCH. FAILED. AFTER FLYING THIS AIRPLANE FOR A COUPLE DAYS IN A ROW, THE SOURSE OF BURNING RUBBER SMELL IS FROM THE RIGHT "RUNWAY TURNOFF" LIGHT. EACH TIME WE TURNED IT ON, W
- [SDR FDEA201708172244](https://openairdocs.org/sdr/FDEA201708172244), Aug 17, 2017: INDICATOR. INOPERATIVE. ALTERNATE GEAR EXTEND WAS USED DUE TO THE RIGHT MLG GEAR INDICATION INOPERATIVE. COMPLIED WITH CHECK OF NOSE AND MLG LOAD LIMITER CLEARANCES, ALL WITHIN LIMITS 
- [SDR FDEA201708162241](https://openairdocs.org/sdr/FDEA201708162241), Aug 16, 2017: LAMP. INOPERATIVE. RIGHT MAIN GEAR LIGHTS DID NOT WORK ON GEAR EXTENSION. COMPLIED WITH RED TABS. REPLACED THE LAMPS IN THE RIGHT MAIN GEAR DOWN INDICATION IAW 20-84-18. OK TO CON
- [SDR FDEA201507202282](https://openairdocs.org/sdr/FDEA201507202282), Jul 20, 2015: LIGHT. INOPERATIVE. EXTERNAL EMER LIGHT IS INOPERATIVE, RIGHT BELOW DOOR. RELAMPED EXTERIOR EMER LIGHT IAW AMM33-51-16-2. OPERATIONS CHECKED GOOD.

## 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 N115FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N115FE before.

- [Cancelled 2004-06-07](https://openairdocs.org/deregistered/N115FE-2004-06-07): Boeing 727-116C, S/N 19814. Owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [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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