# N133FE: 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: 43549
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 17, 2016
- Certificate issued: January 9, 2017
- Expires: January 31, 2030
- Mode S code: A086D8
- 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=133FE
- Page: https://openairdocs.org/aircraft/N133FE

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 N133FE.

## FAA accident and incident reports

None matched to N133FE.

## Service difficulty reports (34)

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 FDEA202609071268](https://openairdocs.org/sdr/FDEA202609071268), Sep 7, 2026: FLOORBOARD. PUNCTURED. PUNCTURE HOLE IN FLOORBOARD 231NFF AT CARGO STATION 4L. FABRICATED MAINDECK CARGO FLOOR PANEL 231NFF, BS 654 22 - 654 22, LBL 33 - LBL 54.75. IAW DWG 143T5876-1
- [SDR FDEA202609051264](https://openairdocs.org/sdr/FDEA202609051264), Sep 5, 2026: SKIN. DENTED. INBOARD SLAT NR 6 (LEFT) UPPER SURFACE APROX 4' IB MULTIPLE DENTS. REPAIRED THE LT WING NR 6 INBD SLAT AT ISS 204 TOP SKIN SURFACE IAW SRM 57-43-02-2R & SRM 51-
- [SDR FDEA202609011255](https://openairdocs.org/sdr/FDEA202609011255), Sep 1, 2026: SKIN. DELAMINATED. RIGHT WING, NR 9 SLAT UPPER SURFACE T/E WEDGE DENTED AND DELAMINATED AT INBD EDGE. REPAIRED THE NR 9 SLAT UPPER SURFACE T/E WEDGE INBD EDGE AT STA OSS 531 IAW S
- [SDR FDEA202609011254](https://openairdocs.org/sdr/FDEA202609011254), Sep 1, 2026: SKIN. DELAMINATED. RIGHT WING, NR 9 SLAT UPPER SURFACE T/E WEDGE DELAMINATED AT OTBD EDGE. REPAIRED RT WING, NR 9 SLAT, UPPER SURFACE T/E WEDGE, OTBD EDGE AT STA OSS 682 IAW SRM 5
- [SDR FDEA202508281557](https://openairdocs.org/sdr/FDEA202508281557), Aug 28, 2025: WEDGE. DENTED. LH WING O/B FLAP (MPN: 113T3100-1078) TRAILING EDGE WEDGE LWR SURFACE A (7.7-INCH X 6.7- INCH) DENT AT WS. 672. REPAIRED LH WING O/B FLAP TRAILING EDGE WEDGE LW
- [SDR FDEA202409121315](https://openairdocs.org/sdr/FDEA202409121315), Sep 12, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO, SECTION 41, (221DFF) FLOOR PANEL WITH SEVERAL DENTS. MAIN DECK CARGO, SECTION 41, (221DFF) FLOOR PANEL WAS REPAIRED IAW B767 SRM 53-00-50- 2R P
- [SDR FDEA202409111313](https://openairdocs.org/sdr/FDEA202409111313), Sep 11, 2024: FLOOR PANEL. WORN. MAIN CARGO FLOOR PANEL242LFA WITH FRAYED. MAIN CARGO FLOOR PANEL 242LFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV. 90 AUG 15/2024.
- [SDR FDEA202409111312](https://openairdocs.org/sdr/FDEA202409111312), Sep 11, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO, SECTION 41, (231AFF) FLOOR PANEL WITH SEVERAL DENTS MDC, SECTION 41 231 AFF FLOOR PANEL, WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG. 201
- [SDR FDEA202409111311](https://openairdocs.org/sdr/FDEA202409111311), Sep 11, 2024: SKIN. WORN. LH WING, INBOARD AILERON LEADING EDGE INBOARD/ OUTBOARD SIDE EXPOSED FIBERS. LH WING, INBOARD AILERON LEADING EDGE INBOARD/OUTBOARD SIDE WAS REPAIRED IAW B767 S
- [SDR FDEA202409111310](https://openairdocs.org/sdr/FDEA202409111310), Sep 11, 2024: SKIN. DENTED. RH WING, SLAT NO. 8, TWO DENTS AT UPPER SURFACE OF WEDGE, AT 17" FROM OUTBOARD EDGE AND 2" FROM TRAILING EDGE. RH WING SLAT NO. 8 T/E WEDGE UPPER SURFACE , AT 1
- [SDR FDEA202409111308](https://openairdocs.org/sdr/FDEA202409111308), Sep 11, 2024: FLOORBOARD. DENTED. MAIN DECK CARGO, SECTION 43, (231LFF) FLOOR PANEL WITH DENTS MAIN DECK CARGO, SECTION 43, (231LFF) FLOOR PANEL WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4.B FI
- [SDR FDEA202409111307](https://openairdocs.org/sdr/FDEA202409111307), Sep 11, 2024: FLOORBOARD. CRACKED. MAIN CARGO FLOOR PANEL 242UFF WITH PUNCTURE MAIN CARGO FLOOR PANEL 242UFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202409111306](https://openairdocs.org/sdr/FDEA202409111306), Sep 11, 2024: FLOORBOARD. CRACKED. MAIN DECK CARGO, SECTION 45, (251LFF) FLOOR PANEL WITH PUNCTURES MAIN DECK CARGO, SECTION 45, (251LFF) FLOOR PANEL WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4.
- [SDR FDEA202409111305](https://openairdocs.org/sdr/FDEA202409111305), Sep 11, 2024: FLOORBOARD. DENTED. MAIN DECK CARGO, SECTION 45, (231QFF) FLOOR PANEL WITH SEVERAL DENTS MAIN DECK CARGO, SECTION 45, (231 QFF) FLOOR PANEL WAS REPAIRED IAW B767 SRM 53-00-50- 2R P
- [SDR FDEA202409111304](https://openairdocs.org/sdr/FDEA202409111304), Sep 11, 2024: FLOORBOARD. DENTED. MAIN DECK CARGO, SECTION 45, (251FFF) FLOOR PANEL WITH DENTS MAIN DECK CARGO, SECTION 45, (251FFF) FLOOR PANEL WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4.B FI
- [SDR FDEA202409101277](https://openairdocs.org/sdr/FDEA202409101277), Sep 10, 2024: FLOOR PANEL. DELAMINATED. MAIN CARGO FLOOR PANEL 241WFF DELAMINATED MDC, FLOOR PANEL 241WFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202409101276](https://openairdocs.org/sdr/FDEA202409101276), Sep 10, 2024: FLOOR PANEL. CRACKED. MAIN DECK CARGO, SECTION 45, (241AFF) FLOOR PANEL WITH PUNCTURE MAIN DECK CARGO, SECTION 45, FLOOR PANEL 241AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FI
- [SDR FDEA202409101275](https://openairdocs.org/sdr/FDEA202409101275), Sep 10, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO, SECTION 43, (232LFF) FLOOR PANEL WITH DENTS MAIN DECK CARGO, SECTION 43, (232LFF) FLOOR PANEL WAS REPAIRED IAW B767 SRM 53-00-50- 2R PAR 4.B FI
- [SDR FDEA202409101274](https://openairdocs.org/sdr/FDEA202409101274), Sep 10, 2024: FLOOR PANEL. CRACKED. MAIN DECK CARGO, SECTION 41, (221FFF) FLOOR PANEL WITH PUNCTURE MAIN DECK CARGO, SECTION 41, FLOOR PANEL 221FFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FI
- [SDR FDEA202409101273](https://openairdocs.org/sdr/FDEA202409101273), Sep 10, 2024: FLOOR PANEL. CRACKED. MAIN DECK CARGO, SECTION 43, (231AFF) FLOOR PANEL WITH PUNCTURE MAIN DECK CARGO, SECTION 43, FLOOR PANEL 231AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FI
- [SDR FDEA202409101272](https://openairdocs.org/sdr/FDEA202409101272), Sep 10, 2024: FLOOR PANEL. CRACKED. MAIN DECK CARGO, SECTION 43, (231RFF) FLOOR PANEL WITH PUNCTURES MAIN DECK CARGO, SECTION 43, FLOOR PANEL 231RFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B F
- [SDR FDEA202409101271](https://openairdocs.org/sdr/FDEA202409101271), Sep 10, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO, SECTION 41, (222AFF) FLOOR PANEL WITH SEVERAL DENTS MAIN DECK CARGO, SECTION 41, FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4
- [SDR FDEA202409101270](https://openairdocs.org/sdr/FDEA202409101270), Sep 10, 2024: SKIN. DENTED. LH WING, SLAT (N 5), DENTS ON UPPER WEDGE AREA BTW OSS 492.95 TO 531.75. LH WING, SLAT NO.5 ON UPPER WEDGE AREA BTW OSS 492.95 TO 531.75 WAS REPAIRED IAW B767 S
- [SDR FDEA202404230273](https://openairdocs.org/sdr/FDEA202404230273), Apr 23, 2024: SKIN. CRACKED. THE R/H WING FIXED LEADING EDGE IS CRACKED O/B OF THE #2 ENG. PYLON. REPAIRED THE R/H WING FIXED LEADING EDGE REF. B767 SRM 57-41-01
- [SDR FDEA202403070255](https://openairdocs.org/sdr/FDEA202403070255), Mar 7, 2024: HMU. FAILED. COMPRESSOR STALL AT 370 ON LEFT ENGINE. ENGINE WOULD NOT PRODUCE REQUESTED THRUST. RAN QRH AND ELECTED TO KEEP THE ENGINE AT IDLE THRUST FOR THE REMAINING DURAT
- [SDR FDEA202301150114](https://openairdocs.org/sdr/FDEA202301150114), Jan 15, 2023: PUMP. MISINSTALLED. CREW REPORT ON DEBRIEF THAT C HYD PRIM 2 MESSAGE MOMENTALLY CAME ON WITH GEAR OPERATION. REMOVEDAND REPLACED CENTER HYD PRIM NR 2 PUMP IAW AMM 29-11-02-4. LEAK 
- [SDR FDEA202108202045](https://openairdocs.org/sdr/FDEA202108202045), Aug 20, 2021: ENGINE. LEAKING. ON DEPARTURE HAD FAIRLY STRONG DIRTY SOCK SMELL. DISSIPATED AT CRUISE AND THEN RETURNED ON DESCENT PASSING APPROXIMATELY FL240. REMAINED THROUGHOUT LANDING. FUM
- [SDR FDEA202010052417](https://openairdocs.org/sdr/FDEA202010052417), Oct 5, 2020: STIFFENER. CRACKED. LT NOSE TUNNEL MAIN CABIN FLOOR BEAM STA 246 APPROX LBL 43 1 EA VERTICAL STIFFENER ANGLE CRACKED. REMOVED AND FABRICATED NEW STIFFENER P/N 141T5146-16, IAW BAC 
- [SDR FDEA202010012391](https://openairdocs.org/sdr/FDEA202010012391), Oct 1, 2020: SUPPORT ANGLE. CRACKED. AFT CARGO COMPARTMENT ZONE 152 ANGLE JUST BELOW THE FLOOR LEVEL IS CRACKED IN THE RADIUS APPROX RBL 25 AT STA 1087. REMOVED AND REPLACED ANGLE P/N 146T8250-6, I
- [SDR FDEA202009302364](https://openairdocs.org/sdr/FDEA202009302364), Sep 30, 2020: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT FLOOR PANEL 241ZFF IS PUNCTURED. REPAIRED MAIN CARGO COMPARTMENT FLOOR PANEL 241ZFF PUNCTURES, IAW B767-SRM 53-00-50-2R PARA 4C.
- [SDR FDEA202009302363](https://openairdocs.org/sdr/FDEA202009302363), Sep 30, 2020: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241BFF REQUIRES REPAIR. FABRICATED REPLACEMENT FLOOR PANEL TO REPLACE INCOMING DAMAGE ON MAIN DECK FLOOR PANEL 241BFF, IAW SRZ-25-005 REV 
- [SDR FDEA202009292355](https://openairdocs.org/sdr/FDEA202009292355), Sep 29, 2020: SKIN. DENTED. LT WING TRAILING EDGE INBOARD AFT FLAP, LOWER SURFACE DENTED. REPAIRED LT WING TRAILING EDGE INBOARD AFT FLAP LOWER SURFACE, IAW B767 SM 57-53-01-2R REPAIR 1 FI
- [SDR FDEA202009292354](https://openairdocs.org/sdr/FDEA202009292354), Sep 29, 2020: SKIN. DENTED. LT WING TRAILING EDGE INBOARD AFT LAP, UPPER SURFACE DENTED INBOARD. REPAIRED DENT ON UPPER SURFACE L/W T/E INBOARD AFT FLAP WITH BONDED DOUBLER REPAIR, IAW B76
- [SDR FDEA201805161243](https://openairdocs.org/sdr/FDEA201805161243), May 16, 2018: WARNING MESSAGE. ILLUMINATED. DURING CLIMB, LEVELING AT FL 360. AN EICAS MESSAGE FOR THE MAIN CARGO DOOR DISPLAYED. ON THE CARGO DOOR PANEL VISIBLE FROM THE CAPTAIN'S SEAT, NO LIGHTS WERE IL

## 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 N133FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N133FE before.

- [Cancelled 2004-08-26](https://openairdocs.org/deregistered/N133FE-2004-08-26): Boeing 727-25C, S/N 19851, 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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.