# N114FE: 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: 42712
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 17, 2015
- Certificate issued: February 26, 2015
- Expires: February 29, 2028
- Mode S code: A03B91
- 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=114FE
- Page: https://openairdocs.org/aircraft/N114FE

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 N114FE.

## FAA accident and incident reports

None matched to N114FE.

## Service difficulty reports (60, 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 FDEA202501240135](https://openairdocs.org/sdr/FDEA202501240135), Jan 24, 2025: SKIN. DELAMINATED. RIGHT WING, INBOARD MAIN FLAP LEADING EDGE WITH DELAMINATION AT 10" FROM OUTBOARD EDGE RIGHT WING, INBOARD MAIN FLAP LEADING EDGE WAS REPAIRED I.A.W. B767 S.R.M
- [SDR FDEA202501230122](https://openairdocs.org/sdr/FDEA202501230122), Jan 23, 2025: ACCESS PANEL. CRACKED. WING RH ACCESS PANEL 666 MT, PERFORATED WING RH ACCESS PANEL 666 MT WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG 201 SHEET 3 AND B767 SRM 51-70-10-2R REPA
- [SDR FDEA202501210112](https://openairdocs.org/sdr/FDEA202501210112), Jan 21, 2025: SKIN. WORN. RIGHT WING, SLAT NO.8 INTERNAL SURFACE UPPER EDGE WITH WEAR MARK AT 41.5" FROM INBOARD EDGE RIGHT WING, SLAT N. 8 INTERNAL SURFACE UPPER EDGE AT 41.5" FROM INBO
- [SDR FDEA202501170102](https://openairdocs.org/sdr/FDEA202501170102), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURED FLOOR PANEL 251BFF ON MDC MAIN DECK CARGO FLOOR PANEL 251 BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024.
- [SDR FDEA202501170101](https://openairdocs.org/sdr/FDEA202501170101), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 251JFF OF MDC MAIN DECK CARGO FLOOR PANEL 251 JFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV: 90 AUG 15/2024
- [SDR FDEA202501170100](https://openairdocs.org/sdr/FDEA202501170100), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 251FFF OF MDC MAIN DECK CARGO FLOOR PANEL 251 FFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV: 90 AUG 15/2024
- [SDR FDEA202501170099](https://openairdocs.org/sdr/FDEA202501170099), Jan 17, 2025: FLOAT VALVE. CRACKED. PUNCTURED FLOOR PANEL 241AGF ON MDC MAIN DECK CARGO FLOOR PANEL 241 AGF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202501170098](https://openairdocs.org/sdr/FDEA202501170098), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 241KFF OF MDC MDC FLOOR PANEL 241 KFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV: 90 AUG 15/2024
- [SDR FDEA202501170097](https://openairdocs.org/sdr/FDEA202501170097), Jan 17, 2025: FLOAT VALVE. CRACKED. PUNCTURED FLOOR PANEL 242VFF ON MDC MAIN DECK CARGO FLOOR PANEL 242 VFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024.
- [SDR FDEA202501170096](https://openairdocs.org/sdr/FDEA202501170096), Jan 17, 2025: FLOAT VALVE. CRACKED. PUNCTURE ON FLOOR PANEL 231TFF OF MDC FLOOR PANEL 231 TFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024.
- [SDR FDEA202501170095](https://openairdocs.org/sdr/FDEA202501170095), Jan 17, 2025: FLOOR MAT. CRACKED. PUNCTURE ON FLOOR PANEL 232KFF OF MDC. MAIN DECK CARGO FLOOR PANEL 232 KFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV: 90 AUG 15/202
- [SDR FDEA202501170094](https://openairdocs.org/sdr/FDEA202501170094), Jan 17, 2025: FLOOR MAT. CRACKED. PUNCTURE ON FLOOR PANEL 231LFF OF MDC FLOOR PANEL 231 LFF OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024.
- [SDR FDEA202501170093](https://openairdocs.org/sdr/FDEA202501170093), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 231QFF OF MDC FLOOR PANEL 231 QFF OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024.
- [SDR FDEA202501170092](https://openairdocs.org/sdr/FDEA202501170092), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 231VFF OF MDC FLOOR PANEL 231 VFF OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024.
- [SDR FDEA202501170091](https://openairdocs.org/sdr/FDEA202501170091), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 232PFF OF MDC FLOOR PANEL 232 PFF OF MDC WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV: 90 AUG 15/2024
- [SDR FDEA202501170090](https://openairdocs.org/sdr/FDEA202501170090), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 232NFF OF MDC FLOOR PANEL 232 NFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024.
- [SDR FDEA202501170089](https://openairdocs.org/sdr/FDEA202501170089), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURED FLOOR PANEL 251EFF ON MDC MAIN DECK CARGO FLOOR PANEL 251 EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024.
- [SDR FDEA202501170088](https://openairdocs.org/sdr/FDEA202501170088), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURED FLOOR PANEL 241ZFF ON MDC MAIN DECK CARGO FLOOR PANEL 241ZFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202501170087](https://openairdocs.org/sdr/FDEA202501170087), Jan 17, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 232MFF OF MDC FLOOR PANEL 232 MFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV 90 AUG 15/2024.
- [SDR FDEA202301230158](https://openairdocs.org/sdr/FDEA202301230158), Jan 23, 2023: SKIN. DENTED. SLAT 5 WITH DENT AT UPPER SKIN, TRAILING EDGE WEDGE. LH WING SLAT #5 TRAILING EDGE WEDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R PAG. 1-2 FIG. 201 AND B767 SRM 51
- [SDR FDEA2023012320155](https://openairdocs.org/sdr/FDEA2023012320155), Jan 22, 2023: SKIN. WORN. RH WING, OUTBOARD SLAT (8), TRAILING EDGE, LOWER SURFACE WITH WEAR (TWO POINTS) RH WING, OUTBOARD SLAT 8 TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW SRM 57-43
- [SDR FDEA202102120341](https://openairdocs.org/sdr/FDEA202102120341), Feb 12, 2021: FLOOR PANEL. DELAMINATED. MAIN DECK FLOOR PANEL 251PFF IS DAMAGED REPAIRED FLOOR PANEL 251PFF IAW B767 SRM 53-00-50-2R, FIGURE 201, PARAGRAPH 4.E
- [SDR FDEA202102090318](https://openairdocs.org/sdr/FDEA202102090318), Feb 9, 2021: FLOOR PANEL. DELAMINATED. MAIN DECK FLOOR PANEL 242SFF IS DAMAGED THROUGHOUT FABRICATED NEW FLOOR PANEL IAW FEDEX DRAWING SRX-25-005, REV R
- [SDR FDEA202102080315](https://openairdocs.org/sdr/FDEA202102080315), Feb 8, 2021: FLOOR SUPPORT. CRACKED. MAIN DECK FLOOR SUPPORT STRUCTURE HAS CRACKED SPLICE ANGLE @ STA 1570 RBL80 REMOVED & REPLACED ANGLE IAW BAC DWG 146T5650
- [SDR FDEA202102080314](https://openairdocs.org/sdr/FDEA202102080314), Feb 8, 2021: FLOOR SUPPORT. CRACKED. MAIN DECK FLOOR SUPPORT STUCTURE HAS CRACKED SPLICE ANGLE @ STATION 1570, LBL 80 REMOVED & REPLACED ANGLE IAW BAC DWG 146T5650
- [SDR FDEA202102080313](https://openairdocs.org/sdr/FDEA202102080313), Feb 8, 2021: BEAM. CRACKED. #1 PYLON / STRUT, OUTBD LOWER LATCH BEAM ASSY IS CRACKED REPAIRED #1 PYLON, OUTBD LOWER LATCH BEAM IAW B767 SRM 54-52-71-2R, FIGURE 201, REPAIR 3, & FEDEX EA H-
- [SDR FDEA202102080312](https://openairdocs.org/sdr/FDEA202102080312), Feb 8, 2021: FORMER. CRACKED. RH WING, OSS 499, LEADING EDGE NOSE FORMER CRACKED REMOVED & REPLACED FORMER IAW BAC DWG 114T2161 REV - & FEDEX EA H-5720-T0359274-P1 P1
- [SDR FDEA202102050295](https://openairdocs.org/sdr/FDEA202102050295), Feb 5, 2021: FRAME. CRACKED. NO.1 PYLON, MID-SPAR FRAME @ NACELLE STA 329, CRACKED AT INBD UPPER CORNER REPAIRED MID-SPAR FRAME, INBD, UPPER CORNER IAW B767 SRM 54-52-71-2R, FIGURE 201, REP
- [SDR FDEA202102040290](https://openairdocs.org/sdr/FDEA202102040290), Feb 4, 2021: BRACKET. CRACKED. RH WING, INBD LEADING EDGE CAVITY, SLAT TORQUE TUBE GUIDE BRACKET IS CRACKED REMOVED & REPLACE BRACKET IAW BAC DWG 114T1240 REV E
- [SDR FDEA202102040289](https://openairdocs.org/sdr/FDEA202102040289), Feb 4, 2021: BEAM. CRACKED. RH WING NOSE BEAM WEB IS CRACKED @ OSS 679.82 REPAIRED RH WING NOSE BEAM WEB IAW B767 SRM 57-41-13-2R, FIG 201, REPAIR 3
- [SDR FDEA202102040288](https://openairdocs.org/sdr/FDEA202102040288), Feb 4, 2021: BEAM. CRACKED. LH WING, NOSE BEAM WEB CRACKED @ OSS 679.82 REPAIRED LH WING NOSE BEAM WEB @ OSS 679-82 IAW B767 SRM 57-41-13-2R, FIG 201, REPAIR 3
- [SDR FDEA202102040286](https://openairdocs.org/sdr/FDEA202102040286), Feb 4, 2021: ANGLE. CRACKED. MAIN EQUIPMENT CENTER, LEFT TUNNEL STATION 246 LBL 50 UPPER FLOOR ANGLE CRACKED. REMOVED AND REPLACED FLOOR ANGLE CLIP 141T5146-16 IAW BAC DWG 141T5600 REV.B.
- [SDR FDEA202102030277](https://openairdocs.org/sdr/FDEA202102030277), Feb 3, 2021: SUPPORT. CRACKED. AFT PIT DOOR CUT-OUT FWD CEILING SUPPORT ANGLE CRACKED REMOVED AND REPLACED CEILING SUPPORT ANGLE IAW BAC DWG 146T8501 REV: B
- [SDR FDEA202102020273](https://openairdocs.org/sdr/FDEA202102020273), Feb 2, 2021: SUPPORT. CRACKED. FWD PIT DOOR CUT-OUT AFT CEILING SUPPORT ANGLE CRACKED REMOVED AND REPLACED CEILING SUPPORT ANGLE 453T1654-18 PO # 991529.1 IAW BAC DWG 143T8514 REV: A
- [SDR FDEA202102020272](https://openairdocs.org/sdr/FDEA202102020272), Feb 2, 2021: SUPPORT. CRACKED. AFT PIT DOOR CUTOUT AFT CEILING SUPPORT ANGLE CRACKED. REMOVED AND REPLACED NEW ANGLE SUPPORT TAW FED EX EA H-5320-T0359501-P1 AND BAC DWG 146T8501 REV.B.
- [SDR FDEA202102020270](https://openairdocs.org/sdr/FDEA202102020270), Feb 2, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241AGF IS DAMAGED REPAIRED FLOOR PANEL 241AGF IAW B767 SRM 53-00-50-2R, FIG 201, PARA, 4.D
- [SDR FDEA202102020269](https://openairdocs.org/sdr/FDEA202102020269), Feb 2, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241PFF IS DAMAGED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R, FIG 201, PARA 4.G.3
- [SDR FDEA202102020268](https://openairdocs.org/sdr/FDEA202102020268), Feb 2, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241JFF IS DAMAGED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R, FIG 201, PARA 4.C & 4.D
- [SDR FDEA202102020267](https://openairdocs.org/sdr/FDEA202102020267), Feb 2, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 242GFF DAMAGED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R, FIG 201, PARAGRAPH 4.D
- [SDR FDEA202102020266](https://openairdocs.org/sdr/FDEA202102020266), Feb 2, 2021: ATTACH ANGLE. CRACKED. RIGHT WING OSS 441, NOSE FORMER & ATTACH ANGLE CRACKED REMOVED & REPLACED NOSE FORMER (114T2170-3( & ANGLE ( 114T2171-4) IAW BAC DWG 114T2241 REV - & FEDEX EA# 
- [SDR FDEA202102020265](https://openairdocs.org/sdr/FDEA202102020265), Feb 2, 2021: ATTACH ANGLE. CRACKED. LEFT WING OSS 441, NOSE FORMER & ATTACH ANGLE CRACKED REMOVED & REPLACED NOSE FORMER (114T2170-5) & ANGLE (114T2171-3) ASSY IAW BAC DWG 114T2241 REV - & FEDEX E
- [SDR FDEA202101310257](https://openairdocs.org/sdr/FDEA202101310257), Jan 31, 2021: FORMER. CRACKED. LEFT WING LEADING EDGE FORMER @ OSS 441 CRACKED. REMOVED & REPLACED FORMER IAW BAC DWG 114T2241 REV.
- [SDR FDEA202101310256](https://openairdocs.org/sdr/FDEA202101310256), Jan 31, 2021: BRACKET. CRACKED. NUMBER 2 PYLON, OTBD HYDRAULIC BAY, HYDRAULIC LINE SUPPORT BRACKET CRACKED. REMOVED & REPLACED BRACKET IAW BAC DWG 272T0037 REV D.
- [SDR FDEA202101310254](https://openairdocs.org/sdr/FDEA202101310254), Jan 31, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241HFF HAS DAMAGED EDGE FILL. REPAIRED EDGE FILL IAW B767 SRM 53-00-50-2R, PARAGRAPH 4.G.2.
- [SDR FDEA202101310253](https://openairdocs.org/sdr/FDEA202101310253), Jan 31, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241AFF HAS DAMAGED EDGE FILL. REPAIRED EDGE FILL IAW B767 SRM 53-00-50-2R, PARAGRAPH 4.G.2.
- [SDR FDEA202101310252](https://openairdocs.org/sdr/FDEA202101310252), Jan 31, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 242LFA HAS DAMAGED EDGE FILL. REPAIRED FLOOR PANEL EDGE FILL IAW B767 SRM 53-00-50-2R, PARAGRAPH 4.G.2.
- [SDR FDEA202101290232](https://openairdocs.org/sdr/FDEA202101290232), Jan 29, 2021: SKIN. DAMAGED. EXTERIOR FUSELAGE @ STA 518, STRINGER 12R HAS STATIC DISCHARGE REPAIRED EXTERNAL FUSELAGE SKIN WITH EXTERNAL DOUBLER IAW B767 SRM 53-00-01-2R, FIGURE 201, REPAI
- [SDR FDEA202101290231](https://openairdocs.org/sdr/FDEA202101290231), Jan 29, 2021: SHEAR TIE. CRACKED. LT STRUT, AFT, INBOARD, JUST FWD OF HYDRAULIC BAY DOOR, INTERNAL BRACKET CRACKED. REMOVED & REPLACED SHEAR TIE, IAW BAC DWG 313T3310, REV.
- [SDR FDEA202101260194](https://openairdocs.org/sdr/FDEA202101260194), Jan 26, 2021: FORMER. CRACKED. LOWER OUTBOARD FORMER CRACKED AT NR 5 SLAT OUTBOARD AUX TRACK REMOVED AND REPLACED CRACKED FORMER AT NR 5 SLAT OTBD AUX TRACK WITH NEW P/N 114T2511U13, IAW SRM 
- [SDR FDEA202009262331](https://openairdocs.org/sdr/FDEA202009262331), Sep 26, 2020: SLIDE. UNWANTED DEPLOY. FUELING REPORTED TROUBLE WITH MAIN ENTRY DOOR. ARRIVED AT AIRCRAFT AND FOUND ESCAPE DEPLOYED. ESCAPE ROPE COVER BOTTOM FORWARD SNAP RIPPED THROUGH. FACT 26SEP20

All 60: https://openairdocs.org/aircraft/N114FE/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 N114FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N114FE before.

- [Cancelled 2004-08-26](https://openairdocs.org/deregistered/N114FE-2004-08-26): Boeing 727-24C, S/N 19527, built 1967. 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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