# N135FE: 2016 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: 42722
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 10, 2016
- Certificate issued: July 27, 2016
- Expires: July 31, 2029
- Mode S code: A08E46
- 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=135FE
- Page: https://openairdocs.org/aircraft/N135FE

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 N135FE.

## FAA accident and incident reports

None matched to N135FE.

## Service difficulty reports (31)

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 FDEA202608181141](https://openairdocs.org/sdr/FDEA202608181141), Aug 18, 2026: SKIN PANEL. DENTED. DENT ON RH LWR HORIZONTAL IB FWD SKIN APPLIED PERMANENT REPAIR AT RH LWR HORIZONTAL I/B FWD SKIN IAW B757 SRM 51-70-10-2R REP 4
- [SDR FDEA202602260282](https://openairdocs.org/sdr/FDEA202602260282), Feb 26, 2026: SKIN. DENTED. HAIL STRIKE (12 EA'S) ON OUTBOARD FLAP TOP SKIN BETWEEN OTEF STA 25 & OTEF STA 222.5, LH WING. OUTBOARD FLAP TOP SKIN BETWEEN OTEF 25 & OTEF STA 222.5 LH WING W
- [SDR FDEA202602240274](https://openairdocs.org/sdr/FDEA202602240274), Feb 24, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON 251PFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 251PFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 93 AUG 15-2025
- [SDR FDEA202602240273](https://openairdocs.org/sdr/FDEA202602240273), Feb 24, 2026: SKIN. DELAMINATED. DELAMINATION IN LEADING EDGE AT 69" INNER END ON OUTBOARD FLAP, RH WING LEADING EDGE AT 69 " INNER END ON OUTBOARD FLAP, RH WING WAS REPAIRED IAW B767 SRM 57-53
- [SDR FDEA202602240272](https://openairdocs.org/sdr/FDEA202602240272), Feb 24, 2026: SKIN. DELAMINATED. DELAMINATION IN LEADING EDGE AT 50" OF INBOARD FLAP SUPPORT FAIRING ON OUTBOARD FLAP, RH WING LEADING EDGE AT 50" OF INBOARD FLAP SUPPORT FAIRING ON OUTBOARD FL
- [SDR FDEA202602240271](https://openairdocs.org/sdr/FDEA202602240271), Feb 24, 2026: SKIN. DELAMINATED. DELAMINATION ON LEADING EDGE OF THE OUTBOARD FLAP AT 63" FROM INBOARD EDGE, LEFT WING LEADING EDGE OF THE OUTBOARD FLAP AT 63" FROM INBOARD EDGE LEFT WING WAS R
- [SDR FDEA202602230266](https://openairdocs.org/sdr/FDEA202602230266), Feb 23, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON 231EFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 231 EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4-B FIG. 201 SHEET 2 REV.93 AUG 15-2025
- [SDR FDEA202602230265](https://openairdocs.org/sdr/FDEA202602230265), Feb 23, 2026: FLOOR PANEL. PUNCTURED. SEVERAL PUNCTURES ON 241 AGF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 241AGF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV 93 AUG 1
- [SDR FDEA202602230264](https://openairdocs.org/sdr/FDEA202602230264), Feb 23, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON 241KFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 241KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15-2025
- [SDR FDEA202602230263](https://openairdocs.org/sdr/FDEA202602230263), Feb 23, 2026: FLOOR PANEL. BROKEN. BROKEN 241DFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 241DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV 93 AUG 15/2025
- [SDR FDEA202602230262](https://openairdocs.org/sdr/FDEA202602230262), Feb 23, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON 241AFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 241AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV.93 AUG 15/2025
- [SDR FDEA202602230261](https://openairdocs.org/sdr/FDEA202602230261), Feb 23, 2026: FLOOR PANEL. DAMAGED. PUNCTURE ON 232GFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 232GFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV 93 AUG 15/2025
- [SDR FDEA202602230260](https://openairdocs.org/sdr/FDEA202602230260), Feb 23, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON 241CFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 241CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV 93 AUG 15/2025
- [SDR FDEA202602220256](https://openairdocs.org/sdr/FDEA202602220256), Feb 22, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON 231AFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 231 AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 REV 93 AUG 15/2025
- [SDR FDEA202602220255](https://openairdocs.org/sdr/FDEA202602220255), Feb 22, 2026: FLOOR PANEL. PUNCTURED. SEVERAL PUNCTURE & DENTS ON 222CFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 222 CFF WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV 93.
- [SDR FDEA202602220254](https://openairdocs.org/sdr/FDEA202602220254), Feb 22, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON 221EFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 221EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV 93 AUG 15/2025
- [SDR FDEA202602190242](https://openairdocs.org/sdr/FDEA202602190242), Feb 19, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON 242VFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 242VFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4-B FIG.201 SHEET2 REV.93 AUG 15/2025
- [SDR FDEA202602190241](https://openairdocs.org/sdr/FDEA202602190241), Feb 19, 2026: FLOOR PANEL. BROKEN. BROKEN 242UFF FLOOR PANEL OF MAIN CARGO COMPARTMENT. FLOOR PANEL 242UFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 93 AUG 15/2025
- [SDR FDEA202602190240](https://openairdocs.org/sdr/FDEA202602190240), Feb 19, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON 251JFF FLOOR PANEL OF MAIN CARGO COMPARTMENT. FLOOR PANEL 251JFF WAS REPAIRED IAW 767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 93 AUG 15/2025
- [SDR FDEA202602190239](https://openairdocs.org/sdr/FDEA202602190239), Feb 19, 2026: FLOOR PANEL. CRACKED. PUNCTURE ON 251LFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 251LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV.93 AUG15/2025
- [SDR FDEA202602190238](https://openairdocs.org/sdr/FDEA202602190238), Feb 19, 2026: FLOOR PANEL. CRACKED. PUNCTURE ON 252EFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 252EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 93 AUG 15/2025
- [SDR FDEA202403280397](https://openairdocs.org/sdr/FDEA202403280397), Mar 28, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT, STA 317, (221CFF) FLOOR PANEL WITH DENTS. MDC, FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B REV. 88 DEC 15/202
- [SDR FDEA202403280396](https://openairdocs.org/sdr/FDEA202403280396), Mar 28, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT, STA 317, (222AFF) FLOOR PANEL WITH DENTS. MDC, FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B REV. 88 DEC 15/2023
- [SDR FDEA202403280395](https://openairdocs.org/sdr/FDEA202403280395), Mar 28, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT, STA 317, (221DFF) FLOOR PANEL WITH DENTS. MDC, FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B REV. 88 DEC 15/2023
- [SDR FDEA202403280393](https://openairdocs.org/sdr/FDEA202403280393), Mar 28, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT, STA 317, (222CFF) FLOOR PANEL WITH DENTS. MDC, FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B REV. 88 DEC 15/202
- [SDR FDEA202403280392](https://openairdocs.org/sdr/FDEA202403280392), Mar 28, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT, STA 317, (222BFF) FLOOR PANEL WITH DENTS. MDC. FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B REV. 88 DEC 15/202
- [SDR FDEA2020041310733](https://openairdocs.org/sdr/FDEA2020041310733), Apr 11, 2020: SKIN. GOUGED. RIGHT WING #8 SLAT TRAILING EDGE LOWER SURFACE GOUGED REPAIRED DAMAGE PER B767 SRM 57-43-02-2R
- [SDR FDEA2018061201438](https://openairdocs.org/sdr/FDEA2018061201438), Jun 9, 2018: SKIN. DENTED. LEFT WING NR 5 SLAT UPPER SURFACE DENTED. REPAIRED THE DENT IAW SRM 57-43-02-2R, AND SRM 51-70-10 4. MAJOR REPAIR.
- [SDR FDEA201712093353](https://openairdocs.org/sdr/FDEA201712093353), Dec 9, 2017: WIRE. BROKEN. RECEIVED "MAIN CARGO DOOR" EICAS ALERT AT CRUISE. OCCURED AT FL 370. REMOVED AND MOUNTED S892 REF B767 AMM 52-71-09-2, REQUIRES AVIONICS TO TERMINATE CONNECTION
- [SDR FDEA201709012441](https://openairdocs.org/sdr/FDEA201709012441), Sep 1, 2017: ACM. MALFUNCTIONED. DURING TAXI IN SMELLED BURNT AIR THEN GOT "LEFT PACK TEMP EICAS" SHUT DOWN PACK AND PARKED JET. COMPLIED WITH SMOKE OR FUMES IN THE CABIN PER AMM 05-51-56-2, TA
- [SDR FDEA201607022223](https://openairdocs.org/sdr/FDEA201607022223), Jul 2, 2016: ESCAPE ROPE. OUT OF POSITION. CREW ENTRANCE DOOR ESCAPE ROPE CAUGHT IN DOOR ROLLER. REINSTALLED THE L1 DOOR EMERGENCY ESCAPE ROPE IAW AMM 25-10-00-2 & 25-61-04-2.

## 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 N135FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N135FE before.

- [Cancelled 2004-08-26](https://openairdocs.org/deregistered/N135FE-2004-08-26): Boeing 727-25C, S/N 19853, built 1968. Triennial form not returned. 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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