# N129FE: 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: 43548
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 20, 2015
- Certificate issued: December 16, 2015
- Expires: December 31, 2028
- Mode S code: A075A3
- 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=129FE
- Page: https://openairdocs.org/aircraft/N129FE

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 N129FE.

## FAA accident and incident reports

None matched to N129FE.

## 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 FDEA202512012216](https://openairdocs.org/sdr/FDEA202512012216), Dec 1, 2025: POWER SUPPLY. FAILED. EMERGENCY LIGHTS INOP ON WALK AROUND. IAW AMM 33-51-07-2 REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW 33-51-07-2-0, CHECKED GOOD FOR SECURITY AND OPS I
- [SDR FDEA202509051632](https://openairdocs.org/sdr/FDEA202509051632), Sep 5, 2025: SKIN. DENTED. A DENT ON EXTERNAL SKIN OF VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR AT FSS 28 AND B. STA 1643 APROX (LH SIDE). VERTICAL STABILIZER AUXILIARY SPAR TO FRO
- [SDR FDEA202509041619](https://openairdocs.org/sdr/FDEA202509041619), Sep 4, 2025: FLOOR PANEL. CRACKED. FLOOR PANEL HAS A SMALL GOUGE IN TOP OF FLOOR PANEL FLOOR PANEL 222CFF LOCATED AT STATION 347.00 WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B, FIG 201, SHEET 2, REV.
- [SDR FDEA202509041618](https://openairdocs.org/sdr/FDEA202509041618), Sep 4, 2025: FLOOR PANEL. CRACKED. BROKEN PANEL 241ZFF, UPPER CARGO COMPT FLOOR PANEL 241ZFF UPPER CARGO COMPARTMENT WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PARAGRAPH 4G (2) REV 92 APR 15, 2025
- [SDR FDEA202509041617](https://openairdocs.org/sdr/FDEA202509041617), Sep 4, 2025: FLOOR PANEL. CRACKED. BROKEN FLOOR PANEL 241MFF, UPPER CARGO COMPT FLOOR PANEL 241MFF UPPER CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PARAGRAPH 4G (2) REV 92 APR 15, 20
- [SDR FDEA202509021611](https://openairdocs.org/sdr/FDEA202509021611), Sep 2, 2025: FLOOR PANEL. DAMAGED. BROKEN PANEL 241LFF, UPPER CARGO COMPT. FLOOR PANEL 241LFF, UPPER CARGO COMPT. WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 92 APR. 15, 2025.
- [SDR FDEA202509011598](https://openairdocs.org/sdr/FDEA202509011598), Sep 1, 2025: FLOOR PANEL. DELAMINATED. DISBONDED CORNER AT FLOOR PANEL 242SFF, MDCC. FLOOR PANEL 242SFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 DETAIL I REV. 92 APR. 15, 2025.
- [SDR FDEA202509011597](https://openairdocs.org/sdr/FDEA202509011597), Sep 1, 2025: FLOOR PANEL. DAMAGED. BROKEN COMPOSITE LAYER AT FWD CORNER OF FLOOR PANEL 242UFF, 2" X 2.5" APROX. FLOOR PANEL 242UFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 DETAIL I
- [SDR FDEA202509011596](https://openairdocs.org/sdr/FDEA202509011596), Sep 1, 2025: FLOOR PANEL. DELAMINATED. DISBONDED CORNER AT FLOOR PANEL 242UFF, MDCC. FLOOR PANEL 242UFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 DETAIL I REV. 92 APR. 15, 2025.
- [SDR FDEA202509011595](https://openairdocs.org/sdr/FDEA202509011595), Sep 1, 2025: FLOOR PANEL. DAMAGED. BROKEN UPPER COMPOSITE LAYERS. FLOOR PANEL 241QFF. UPPER COMPOSITE LAYERS OF FLOOR PANEL 241QFF WERE REPAIRED IAW B767 SRM 53-00-50- 2R PAR. 4.B FIG. 201 SHEET 
- [SDR FDEA202509011593](https://openairdocs.org/sdr/FDEA202509011593), Sep 1, 2025: FLOOR PANEL. DENTED. SEVERAL DENTS ON FLOOR PANEL 212CFF OF CONTROL CABIN. FLOOR PANEL 212CFF OF CONTROL CABIN WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 92 APR
- [SDR FDEA202509011591](https://openairdocs.org/sdr/FDEA202509011591), Sep 1, 2025: FLOOR PANEL. DELAMINATED. DISBONDED CORNER AT FLOOR PANEL 242JFF, MDCC. FLOOR PANEL 242JFF, MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4.B FIG. 201 SHEET 2 REV. 92 APR 15, 2025
- [SDR FDEA202509011588](https://openairdocs.org/sdr/FDEA202509011588), Sep 1, 2025: FLOOR PANEL. DAMAGED. SEVERAL PUNCTURES ON FLOOR PANEL 242UFF LOWER SURFACE, MDCC. FLOOR PANEL 242UFF LOWER SURFACE AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG 201 SHE
- [SDR FDEA202509011587](https://openairdocs.org/sdr/FDEA202509011587), Sep 1, 2025: FLOOR PANEL. DENTED. SEVERAL DENTS AT EDGES OF LOWER SURFACE OF FLOOR PANEL 241YFA. EDGES OF LOWER SURFACE OF FLOOR PANEL 241YFA WERE REPAIRED IAW B767 SRM 53-00-50- 2R PAR. 4.B FIG
- [SDR FDEA202508291578](https://openairdocs.org/sdr/FDEA202508291578), Aug 29, 2025: SKIN. DENTED. DENT INNER PART OF INBOARD FLAP WING RH INBOARD FLAP, INNER PART, WING RH WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1, FIG. 201, SHEET 1-6, TABLE I REV.92 AP
- [SDR FDEA202508291577](https://openairdocs.org/sdr/FDEA202508291577), Aug 29, 2025: FLOOR PANEL. DAMAGED. EXPOSED FIBERS ON FLOOR PANEL 242KFF, MDCC. EXPOSED FIBERS ON FLOOR PANEL 242KFF WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 92 APR 15,2025
- [SDR FDEA202508291576](https://openairdocs.org/sdr/FDEA202508291576), Aug 29, 2025: FLOOR PANEL. CRACKED. SEVERAL PUNCTURES AT FLOOR PANEL 241AGF SEVERAL PUNCTURES AT FLOOR PANEL 241AGF WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV.92 APR 15,2025
- [SDR FDEA202508291575](https://openairdocs.org/sdr/FDEA202508291575), Aug 29, 2025: FLOOR PANEL. BROKEN. BROKEN PANEL 241PFF, UPPER CARGO COMPT BROKEN PANEL 241PFF, UPPER CARGO COMPT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 REV. 92 APR 15,2025
- [SDR FDEA202508291574](https://openairdocs.org/sdr/FDEA202508291574), Aug 29, 2025: FLOOR PANEL. DENTED. DENT ON FLOOR PANEL 242VFF UPPER SURFACE MDCC DENT ON FLOOR PANEL 242VFF UPPER SURFACE, MDCC WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4-B FIG 201 SHEET 2 REV.
- [SDR FDEA202508291573](https://openairdocs.org/sdr/FDEA202508291573), Aug 29, 2025: FLOOR PANEL. DENTED. SEVERAL DENTS ON FLOOR PANEL 222CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 222CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IA
- [SDR FDEA202508291572](https://openairdocs.org/sdr/FDEA202508291572), Aug 29, 2025: FLOOR PANEL. DENTED. SEVERAL DENTS ON FLOOR PANEL 221 CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 221CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED I
- [SDR FDEA202508291571](https://openairdocs.org/sdr/FDEA202508291571), Aug 29, 2025: FLOOR PANEL. DENTED. SEVERAL DENTS ON FLOOR PANEL 221 CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 221CFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED I
- [SDR FDEA202508291570](https://openairdocs.org/sdr/FDEA202508291570), Aug 29, 2025: FLOOR PANEL. DENTED. SEVERAL DENTS ON FLOOR PANEL 221DFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 221DFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IA
- [SDR FDEA202508291569](https://openairdocs.org/sdr/FDEA202508291569), Aug 29, 2025: FLOOR PANEL. DENTED. SEVERAL DENTS ON FLOOR PANEL 222AFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 222AFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IA
- [SDR FDEA202508291568](https://openairdocs.org/sdr/FDEA202508291568), Aug 29, 2025: FLOOR PANEL. DENTED. SEVERAL DENTS ON FLOOR PANEL 222BFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT FLOOR PANEL 222BFF OF SECTION 41 AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IA
- [SDR FDEA202508281560](https://openairdocs.org/sdr/FDEA202508281560), Aug 28, 2025: SKIN. DENTED. DENT ON LOWER SURFACE OF OUTBOARD FLAP, AT 70" FROM OUTBOARD EDGE AND 8" FROM TRAILING EDGE, LH WING. LOWER SURFACE OF OUTBOARD FLAP, AT 70" FROM OUTBOARD EDGE 
- [SDR FDEA202310201780](https://openairdocs.org/sdr/FDEA202310201780), Oct 20, 2023: FLAP. DENTED. R/H WING INBD FLAP TRAILING EDGE LOWER SURFACE DENTS REMOVED , REPAIRED AND REINSTALLED R/H WING INBD FLAP IAW FEDEX EA# : H-5750-T0376594
- [SDR FDEA202310171771](https://openairdocs.org/sdr/FDEA202310171771), Oct 17, 2023: ANGLE. CRACKED. AREA AFT OF THE BULK CARGO COMPARTMENT R/H SIDE MAIN CABIN FLOOR SUPPORT STRUCTURE HAS 2EA SPLICE ANGLES CRACKED BETWEEN STA 1562 & 1582, RBL 70 REMOVED AND REP
- [SDR FDEA202310171770](https://openairdocs.org/sdr/FDEA202310171770), Oct 17, 2023: ANGLE. CRACKED. AREA AFT OF THE BULK CARGO COMPARTMENT L/H SIDE MAIN CABIN FLOOR SUPPORT STRUCTURE HAS 2EA SPLICE ANGLES CRACKED BETWEEN STA 1562 & 1582, LBL 70 REMOVED AND REP
- [SDR FDEA202310161768](https://openairdocs.org/sdr/FDEA202310161768), Oct 16, 2023: FRAME. CRACKED. #1 PYLON: NACELLE STA 329, MID-SPAR FRAME IS CRACKED AT THE INBOARD, UPPER CORNER REPAIRED #1 PYLON, NAC STA 329 FRAME IAW FEDEX EA # H-5450-T0376579-P1, RELEAS
- [SDR FDEA202310061748](https://openairdocs.org/sdr/FDEA202310061748), Oct 6, 2023: SKIN. CRACKED. RH ELEVATOR CTR PCA CUTOUT HAS A SMALL CRACK AND DELAMINATION REPAIRED RH ELEVATOR CENTER PCA CUTOUT CRACK AND DELAMINATION IAW FED EX EA H- 5520-T0376560-P1-ST
- [SDR FDEA202010172546](https://openairdocs.org/sdr/FDEA202010172546), Oct 17, 2020: BRACKET. CRACKED. NR 1 PYLON OUTBOARD FWD END OF PANEL 437BL BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON THE NR 1 PYLON FWD END OF PANEL 437BL, PER B DWG 313T3310.
- [SDR FDEA202010172545](https://openairdocs.org/sdr/FDEA202010172545), Oct 17, 2020: BRACKET. CRACKED. HYDRAULIC DRAIN TUBE BRACKET IS CRACKED ON NR 1 OUTBOARD PYLON. REMOVED AND REPLACED DRAIN TUBE BRACKET, PER B767 SRM 51-40-02 AND BOEING DWG 313T2380 REV E.
- [SDR FDEA202010172543](https://openairdocs.org/sdr/FDEA202010172543), Oct 17, 2020: FORMER. CRACKED. LEFT WING LEADING EDGE, NR 5 SLAT OUTBOARD ACTUATOR ROD APPROXIMATELY LES 489 HAS CRACKED FORMER. REMOVED AND REPLPACED FORMER AT NR 5 SLAT OUTBOARD ACTUATOR RO
- [SDR FDEA202010172542](https://openairdocs.org/sdr/FDEA202010172542), Oct 17, 2020: ANGLE. CRACKED. LEFT WING LEADING EDGE, NR 5 SLAT OUTBOARD ACTUATOR ROD APPROXIMATELY LES 489 HAS CRACKED ANGLE. REMOVED AND REPLACED ANGLE AT APPROXIMATELY LES 489, PER EA H-5
- [SDR FDEA202010172541](https://openairdocs.org/sdr/FDEA202010172541), Oct 17, 2020: ANGLE. CRACKED. RIGHT WING NR 8 SLAT, INBOARD GUIDE ARM, FORMER CRACKED. REMOVED AND REPLACED FORMER AT NR 8 SLAT INBOARD GUIDE ARM CUTOUT, PER B DWG 114T2241, EA4-5720-T035742
- [SDR FDEA202010172540](https://openairdocs.org/sdr/FDEA202010172540), Oct 17, 2020: SKIN. CHAFED. LEFT WING, INBOARD FLAP, LOWER SURFACE, ABOVE NR 6 TIRE, PREVIOUS REPAIR GOUGED, CIRCLED. REMOVED DAMAGED ROCKSHIELD. REPAIRED IAW EA H-2750-T0357370, B767 SRM 
- [SDR FDEA202010152522](https://openairdocs.org/sdr/FDEA202010152522), Oct 15, 2020: LATCH. CHAFED. NR 2 ENGINE T/R HINGE LATCH PANEL FWD EDGE GOUGED AND HAS BARE METAL. REPAIRED NR 2 FWD LATCH PANEL, IAW STEA CMM 78-32-09 REPAIR 5.
- [SDR FDEA202010152521](https://openairdocs.org/sdr/FDEA202010152521), Oct 15, 2020: LATCH. CHAFED. NR 1 INBOARD FWD T/R LATCH PANEL, FWD LIP WORN AND CHAFED 2 PLACES. REPAIRED NR 1 FWD LATCH PANEL, IAW STEA CMM 78-32-09 REPAIR 5.
- [SDR FDEA202010152520](https://openairdocs.org/sdr/FDEA202010152520), Oct 15, 2020: FORMER. CRACKED. RIGHT WING, NR 8 SLAT, OUTBOARD ROTARY ACTUATOR ARM CUTOUT, FORMER IS CRACKED. REMOVED AND REPLACED NOSE FORMER, IAW BOEING DWG 114T2161 REV E AND FEDEX EA H-57
- [SDR FDEA202010152519](https://openairdocs.org/sdr/FDEA202010152519), Oct 15, 2020: SKIN. GOUGED. NR 2 ENGINE CORE COWLING LT LOWER SURFACE IS GOUGED. ACCOMPLISHED REPAIR OF NR 2 ENGINE CORE COWLING LT, IAW ROHR SRM 54-40-00 REPAIR 2.
- [SDR FDEA202010132479](https://openairdocs.org/sdr/FDEA202010132479), Oct 13, 2020: ANGLE. CRACKED. LEFT WING FUEL PANEL 521QB HINGE ANGLE CRACKED IN CENTER AREA. REPAIRED LEADING EDGE AT FUEL PANEL 521QB HINGE, IAW B767 SRM 57-41-13-2R REPAIR 3.
- [SDR FDEA202010132478](https://openairdocs.org/sdr/FDEA202010132478), Oct 13, 2020: SKIN. GOUGED. RIGHT HORIZONTAL STABILIZER FIXED LOWER SKIN GOUGED. REPAIRED DAMAGE, IAW B767 SRM 55-10-01-2R FIG 201 AND SRM 51-70-10-2R REPAIR 4 FIG 201.
- [SDR FDEA202010122465](https://openairdocs.org/sdr/FDEA202010122465), Oct 12, 2020: BRACKET. CRACKED. LT WING INBOARD LEADING EDGE AREA TORQUE TUBE GUIDE BRACKET IS CRACKED AT THE LOWER AFT FASTENER HOLE. REMOVED AND REPLACED TORQUE TUBE GUIDE BRACKET, IAW B767 
- [SDR FDEA202010122464](https://openairdocs.org/sdr/FDEA202010122464), Oct 12, 2020: SEAL. CRACKED. LEFT WING APPROXIMATELY LES 506, STRAP IS CRACKEDAT FASTENER HOLE. REMOVED AND REPLACED LT WING APPROXIMATELY LES 506 STRAP, IAW BAC DWG 114T2800.
- [SDR FDEA202010102458](https://openairdocs.org/sdr/FDEA202010102458), Oct 10, 2020: ANGLE. CRACKED. NR 1 PYLON AFT OUTBOARD ANGLE CLIP CRACKED. REMOVED AND REPLACED ANGLE CLIP, PER B767 SRM 51-40-02 AND BOEING DWG 313T3380 REV N.
- [SDR FDEA202010102457](https://openairdocs.org/sdr/FDEA202010102457), Oct 10, 2020: ANGLE. CRACKED. NR 2 ENG PYLON AFT A-FRAME IN BOARD CLIP CRACKED. REMOVED AND REPLACED CLIP, IAW B767 SRM 51-40-02 AND BOEING DWG 313T3380 REV N.
- [SDR FDEA2020072301436](https://openairdocs.org/sdr/FDEA2020072301436), Jul 3, 2020: WARNING MESSAGE. FALSE ACTIVATION. AT LEVEL 360 MAIN CARGO DOOR EICAS MESSAGE , NO VIBRATION, NO PRESSURIZATION ISSUES. MESSAGE EXTINGUISHED DESCENDING THRU 16000FT. OPENED DOOR PANEL EXPOSING S8
- [SDR FDEA2020070631436](https://openairdocs.org/sdr/FDEA2020070631436), Jul 3, 2020: WARNING SYSTEM. FALSE ACTIVATION. LEVEL 360 MAIN CARGO DOOE EICAS MESSAGE, NO VIBRATION, NO PRESSURIZATION ISSUES. MESSAGE EXTINGUISHED DESCENDING THRU 16000.
- [SDR FDEA2018122193545](https://openairdocs.org/sdr/FDEA2018122193545), Dec 19, 2018: SWITCH. BROKEN. PDIS 129 33-40 2768 19DEC18 IND OPEN U LOGPAGES:3055686 AN ACRID ODOR WAS SENSED THREE TIMES. WE BELIEVE THE ODOR COICIDES WITH TURNING ON THE RUNWAY TURNOFF LI

All 55: https://openairdocs.org/aircraft/N129FE/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

## 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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