# N131FE: 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: 61205
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 29, 2016
- Certificate issued: October 31, 2016
- Expires: October 31, 2029
- Mode S code: A07F6A
- 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=131FE
- Page: https://openairdocs.org/aircraft/N131FE

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 N131FE.

## FAA accident and incident reports

None matched to N131FE.

## Service difficulty reports (58, 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 FDEA202606100691](https://openairdocs.org/sdr/FDEA202606100691), Jun 10, 2026: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPARTMENT SECTION 46, FLOOR PANEL 252DFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 252DFF, MPN: 146T5869-2, RBL 77.50 - RBL 86.50, STATI
- [SDR FDEA202606080681](https://openairdocs.org/sdr/FDEA202606080681), Jun 8, 2026: SKIN. WORN. RIGHT WING IB AILERON FWD EDGE HAS HEAVY WEAR MARKS. REPAIRED RT INBD AILERON LOWER L/E PANEL 656AB (MPN: 113T6109-92G) AT WS 445 IAW SRM 57-60-01-2R AND SRM 51
- [SDR FDEA202606080680](https://openairdocs.org/sdr/FDEA202606080680), Jun 8, 2026: SKIN. WORN. LEFT WING, INBD AILERON, LOWER SURFACE, INBD FWD CORNER HAS AREA OF WEAR DOWN TO WIRE MESH APPROX 7.5" LONG. REPAIRED LT INBD AILERON LOWER SURFACE PANEL 556AB 
- [SDR FDEA202601310110](https://openairdocs.org/sdr/FDEA202601310110), Jan 31, 2026: COMPUTER. FAILED. ISSUE WITH FMS, AUTOPILOT & FLT DIRECTOR. CLIMBING OUT OF SCL, IN VNAV/LNAV, RECEIVED A CLIMB VIA CLEARANCE FROM ATC. ACFT LEVELED OFF AT 9000 AT SEKSE, IAW DON
- [SDR FDEA202601060006](https://openairdocs.org/sdr/FDEA202601060006), Jan 6, 2026: VALVE. LEAKING. DURING POST FLIGHT WALK AROUND FOUND FUEL LEAKING FROM LEFT WING AFT SPAR FWD OF LMLG, SHUT DOWN THE APU AND FUEL STOPPED LEAKING. VERIFIED FUEL LEAK AT APU FUE
- [SDR FDEA202509031612](https://openairdocs.org/sdr/FDEA202509031612), Sep 3, 2025: DOOR. OPEN. DURING POST FLIGHT INSPECTION FOUND CREW REST UPPER PSU DOOR OPEN. COULD NOT REST PSU DOOR. REPAIRED DOOR ASSY. OPS CHK GOOD. OK FOR SERVICE.
- [SDR FDEA202406240858](https://openairdocs.org/sdr/FDEA202406240858), Jun 24, 2024: SKIN. DENTED. LEFT WING, SLAT NO.6 INTERNAL SURFACE WITH DENT AT 6" FROM UPPER EDGE AND 14.5" FROM OUTBOARD EDGE. LH WING, SLAT NO.6 INTERNAL SURFACE WITH DENT AT 6" FROM UPP
- [SDR FDEA202406240857](https://openairdocs.org/sdr/FDEA202406240857), Jun 24, 2024: SKIN. DENTED. LEFT WING, SLAT NO.6 INTERNAL SURFACE WITH DENT AT 6" FROM UPPER EDGE AND 14.5" FROM OUTBOARD EDGE. LH WING, SLAT NO.6 INTERNAL SURFACE WITH DENT AT 6" FROM UPP
- [SDR FDEA202406240856](https://openairdocs.org/sdr/FDEA202406240856), Jun 24, 2024: SKIN. DENTED. LEFT WING, SLAT NR 6 INTERNAL SURFACE WITH DENT AT 7.5" FROM UPPER EDGE AND 28" FROM OUTBOARD EDGE. LH WING, SLAT NR 6 INTERNAL SURFACE WITH DENT AT 7.5" FROM U
- [SDR FDEA202406230854](https://openairdocs.org/sdr/FDEA202406230854), Jun 23, 2024: SKIN. DAMAGED. LOWER HALF OF FUSELAGE, BTW STA 1417 AND STA 1439, BTW STRG 33L AND 38L, WITH SCRATCH. LOWER FUSELAGE SKIN BTWN STA 1417/1439 AND STGR 33L/37R WAS REPAIRED IAW 
- [SDR FDEA202406210833](https://openairdocs.org/sdr/FDEA202406210833), Jun 21, 2024: SKIN. WORN. RH WING, INBOARD AILERON, LEADING EDGE, RH SIDE, WITH WEAR. RH WING, INBOARD AILERON, LEADING EDGE, ACCESS PANEL 656AB WAS REPAIRED IAW B767 SRM 57-60-01-2R REP
- [SDR FDEA202406210832](https://openairdocs.org/sdr/FDEA202406210832), Jun 21, 2024: SKIN. DAMAGED. LEFT WING, INBOARD AILERON LEADING EDGE INBOARD LOWER SECTION WITH WEAR. LEFT WING, INBOARD AILERON LEADING EDGE, ACCESS PANEL 556AB WAS REPAIRED IAW B767 SRM 5
- [SDR FDEA202406210831](https://openairdocs.org/sdr/FDEA202406210831), Jun 21, 2024: FLOOR PANEL. DENTED. MAIN CARGO COMPARTMENT, FLOOR PANEL 231AFF, SKIN WITH DENTS. MDC, FLOOR PANEL 231AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15
- [SDR FDEA202406210830](https://openairdocs.org/sdr/FDEA202406210830), Jun 21, 2024: FLOOR PANEL. DENTED. MAIN CARGO COMPARTMENT, FLOOR PANEL 221CFF, SKIN WITH SEVERAL DENTS. MDC, FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 8
- [SDR FDEA202309231641](https://openairdocs.org/sdr/FDEA202309231641), Sep 23, 2023: SHEAR TIE. CRACKED. MOD TYPE T MOD NO. H-5400-T0376310 REV NO. PS P1 NACELLES/PYLON - NACELLE/PYLON GEN - #1 PYLON SHEAR TIE, NAC STA 308 INBD, ALTE COMPLY WITH E..A. H-5400-T03763
- [SDR FDEA202206221508](https://openairdocs.org/sdr/FDEA202206221508), Jun 22, 2022: FORMER. CRACKED. L/H WING L/E NOSE FORMER IS CRACKED AT APPROX OFSS 434 REPLACED FORMER IAW FEDEX EA # H-5720-T0368847-P1.
- [SDR FDEA202206221507](https://openairdocs.org/sdr/FDEA202206221507), Jun 22, 2022: FORMER. CRACKED. L/H WING L/E NOSE FORMER IS CRACKED AT APPROX OSS 437 (JUST INBD OF THE #5 SLAT INBD AUX TRACK) REPLACEDFORMER IAW EA # H-5720-T0368847-P1.
- [SDR FDEA202206221506](https://openairdocs.org/sdr/FDEA202206221506), Jun 22, 2022: FORMER. CRACKED. RW FIXED L/E OTBD NOSE FORMER CRACKED AT THE #8 SLAT INBD AUX TRACK REPLACED FORMER IAW FEDEX EA # H-5720-T0368847-P1.
- [SDR FDEA202206221505](https://openairdocs.org/sdr/FDEA202206221505), Jun 22, 2022: FORMER. CRACKED. RW FIXED L/E NOSE FORMER CRACKED AT THE #8 SLAT INBD AUX TRACK REPLACED FORMER IAW EA # H-5720-T0368847-P.
- [SDR FDEA202206221504](https://openairdocs.org/sdr/FDEA202206221504), Jun 22, 2022: FORMER. CRACKED. L/H WING LE SUBSTRUCTURE NOSE FORMER IS CRACKED JUST INBD OF THE #4 SLAT INBD ROTARY ACUTATOR OSS 565 REPLACED FORMER IAW EA # H-5720-T0368847-P1.
- [SDR FDEA202206221503](https://openairdocs.org/sdr/FDEA202206221503), Jun 22, 2022: FORMER. CRACKED. L/H WING LE SUBSTRUCTURE NOSE FORMER IS CRACKED JUST OTBD OF THE #5 SLAY OTBD ROTARY ACTUATOR AT OSS 499 REPLACED FORMER IAW FEDEX EA # H-5720-T0368847-P1, RELE
- [SDR FDEA202206211490](https://openairdocs.org/sdr/FDEA202206211490), Jun 21, 2022: BRACKET. CRACKED. R.WING I/B L/E @ LES 285 SLAT TORQUE TUBE GUIDE BRACKET IS CRACKED. REMOVED CRACKED BRACKET, LOCATED AND DRILLED NEW BRACKET AND REINSTALLED BRACKET PER B767 SR
- [SDR FDEA202206211489](https://openairdocs.org/sdr/FDEA202206211489), Jun 21, 2022: SHEAR TIE. CRACKED. #2 PYLON UNDER PANEL #447BL FWD UPPER BRACKET CRACK AT NAC STA 296 REMOVED & REPLACED SHEAR TIE IAW B767 SRM 51-40-02 & BAC DWG 313T2310, SHEET 95, REVISION -
- [SDR FDEA202206211488](https://openairdocs.org/sdr/FDEA202206211488), Jun 21, 2022: ANGLE. CRACKED. AREA AFT OF BULK CARGO COMPARTMENT L/H SIDE JUST BELOW MAIN CABIN FLOOR LEVEL, FLOOR SUPPORT STRUVTURE HAS 1EA INBD FACING SPLICE CRACKED REMOVED & REPLACED ANG
- [SDR FDEA202206211487](https://openairdocs.org/sdr/FDEA202206211487), Jun 21, 2022: ANGLE. CRACKED. AREA AFT OF THE BULK CARGO COMPARTMENT L/H SIDE JUST BELOW THE MAIN CABIN FLOOR LEVEL, FLOOR SUPPORT STRUCTURE HAS 1EA OTBD FACING SPLICE CRACKED REMOVED & REPL
- [SDR FDEA202206211486](https://openairdocs.org/sdr/FDEA202206211486), Jun 21, 2022: ANGLE. CRACKED. AREA AFT OF THE BULK CARGO COMPARTMENT R/H SIDE JUST BELOW THE MAIN CABIN FLOOR LEVEL, FLOOR SUPPORT STRUCTURE HAS 1EA INBD FACING SPLICE CRACKED REMOVED & REPL
- [SDR FDEA202206171456](https://openairdocs.org/sdr/FDEA202206171456), Jun 17, 2022: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241AGF HAS A LARGE CRACKED/DENTED DAMAGE AREA, STA 1011-1019, LBL 84-90 REPAIRED DAMAGE ON FLOOR PANEL 241AGF STA 1011-1019, LBL 84-90 IA
- [SDR FDEA202206171455](https://openairdocs.org/sdr/FDEA202206171455), Jun 17, 2022: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241ZFF IS CRACKED / DENTED IN 2 PLACES, STA 1085-1110, LBL 71 REPAIRED DAMAGE ON FLOOR PANEL 241ZFF STA 1085-1110, LBL 71 IAW B767 SRM 53
- [SDR FDEA202206171454](https://openairdocs.org/sdr/FDEA202206171454), Jun 17, 2022: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241WFF IS CRACKED/DENTED AT STA 984 AND LBL2 REPAIRED DAMAGE ON FLOOR PANEL 241WFF STA 984, LBL 2 IAW B767 SRM 53-00-50-2R, PARA 4.D.
- [SDR FDEA202206171453](https://openairdocs.org/sdr/FDEA202206171453), Jun 17, 2022: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241AFF IS CRACKED / DENTED AT BS 757, RBL 7 REPAIRED DAMAGE ON FLOOR PANEL 241AFF STA 757, RBL 7 IAW SRM 53-00-50-2R, PARA 4.C.
- [SDR FDEA202206171452](https://openairdocs.org/sdr/FDEA202206171452), Jun 17, 2022: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241JFF IS CRACKED / DENTED AT STA 883, LBL 74 REPAIRED DAMAGE ON FLOOR PANEL 241JFF STA 882, LBL 74 IAW B767 SRM 53-00-50-2R, PARA 4.C.
- [SDR FDEA202206171451](https://openairdocs.org/sdr/FDEA202206171451), Jun 17, 2022: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 242SFF HAS THREE AREAS CRACKED, STA 1024-1063, RBL 24-30 REPAIRED 3EA DAMAGE LOCATION ON FLOOR PANEL 242SFF, STA 1024-1063, RBL 24-30 IAW
- [SDR FDEA202206171450](https://openairdocs.org/sdr/FDEA202206171450), Jun 17, 2022: FLOOR PANEL. DAMAGED. **PARTS RACK AREA** MAIN CABIN FLOOR PANEL 241KFF HAS SEVERAL DAMAGE AREAS, STA 886-900 AND LBL 80-90 FABRICATED NEW FLOOR PANEL 241KFF IAW FEDEX DWG SRZ-25-005
- [SDR FDEA202206171459](https://openairdocs.org/sdr/FDEA202206171459), Jun 17, 2022: WEB. CRACKED. L/H WING L/E AREA BULLNOSE WEB IS CRACKED IN THE LOWER RADIUS AT APPROX OFSS 675 UNDER THE LE FUEL SVC ACCESS DOOR 521QB REPAIRED LEFT WING LEADING EDGE NOSE BE
- [SDR FDEA202206171449](https://openairdocs.org/sdr/FDEA202206171449), Jun 17, 2022: FRAME. CRACKED. #2 PYLON DOOR 447BR LOWER BULKHEAD CRACKED AT NAC STA 329.50 REPAIRED #2 PYLON MID-SPAR FRAME IAW B767 SRM 54-52-71-2R, REPAIR 4
- [SDR FDEA202206171448](https://openairdocs.org/sdr/FDEA202206171448), Jun 17, 2022: FRAME. CRACKED. #1 PYLON AFT FAIRING UNDER PANEL 437BR LOWER I/B SIDE SUPPORT CRACKED @ STA 326 REPAIRED #1 PYLON MID-SPAR FRAME IAW B767 SRM 54-52-71-2R, REPAIR 4 & FEDEX EA H
- [SDR FDEA202206161446](https://openairdocs.org/sdr/FDEA202206161446), Jun 16, 2022: SKIN. GOUGED. RW #8 SLAT OTBD LWR T/E SURFACE GOUGED. REPAIRED R/W #8 SLAT OUTBOARD LWE T/E SURFACE WITH A PERMANENT REPAIR IAW B767 SRM 57-42-02-2R AND 51-70-10-2R REPAIR 4.
- [SDR FDEA202206161445](https://openairdocs.org/sdr/FDEA202206161445), Jun 16, 2022: WEDGE. GOUGED. RH WING #8 SLAT TRAILING EDGE WEDGE LOWER SURFACE IS GOUGED ON INBD SIDE AT APPROX WS 435. REPAIRED RW #8 SLAT T/E WEDGE LOWER SURFACE ON I/B SIDE APPROX WS 435
- [SDR FDEA202206161444](https://openairdocs.org/sdr/FDEA202206161444), Jun 16, 2022: WEDGE. GOUGED. L/H WING #5 SLAT T/E WEDGE LOWER SURFACE IS GOUGED JUST OTBD OF THE INBD UX TRACK. ACCOMPLISHED PERMANENT REPAIR L/H WING #5 SLAT T/E WEDGE LOWER SURFACE GOUGE 
- [SDR FDEA202206161442](https://openairdocs.org/sdr/FDEA202206161442), Jun 16, 2022: WEDGE. GOUGED. LH #5 SLAT T/E WEDGE LOWER SURFACE IS GOUGED APPROX OTBD OF THE OTBD ROTARY ACTUATOR. ACCOMPLISHED PERMANENT REPAIR OF L/H WING #5 SLAT T/E WEDGE LOWER SURFACE 
- [SDR FDEA202206151430](https://openairdocs.org/sdr/FDEA202206151430), Jun 15, 2022: SKIN. WORN. LEFT WING, INBOARD AILERON, INBOARD LEADING EDGE, LOWER SURFACE PANEL IA WORN WITH EXPOSED COMPOSITE MATERIAL. REPAIRED WORN SKIN AREA ON L/W I/B AILERON LOWER 
- [SDR FDEA202206151429](https://openairdocs.org/sdr/FDEA202206151429), Jun 15, 2022: SKIN. WORN. RH WING AILERON LOWER LEADING EDGE SKIN PANEL IS WORN ON INBD SIDE. REPAIRED WORN SKIN AREA ON R/W I/B AILERON LOWER L/E PANEL WITH 250 DEGREE FIBERGLASS DOUBLE
- [SDR FDEA202109252405](https://openairdocs.org/sdr/FDEA202109252405), Sep 25, 2021: UNKNOWN. ODOR. WHEN INCREASING THRUST TO CROSS RUNWAY, RECEIVED A VERY STRONG ODOR OF BURNING. POWER WAS APPROXIMATELY 30 - 40 %. ODOR WAS SIMILAR TO BURNING RUBBER. RETURNED 
- [SDR FDEA202102020271](https://openairdocs.org/sdr/FDEA202102020271), Feb 2, 2021: CHANNEL. DAMAGED. EMERGENCY ESCAPE ROPE STOWAGE CHANNEL DAMAGED STOWED ESCAPE ROPE I/A/W B767 M.M. CH. 25-61-04-2-1 AND REPLACED COVER ASSY (REF IPC 25-61-02-02, ITEM 70 DUE TO M
- [SDR FDEA2020082652033](https://openairdocs.org/sdr/FDEA2020082652033), Aug 25, 2020: SLAT SYSTEM. OUT OF RIG. APPROACHING THE FIELD (IND) WHEN SELECTING FLAPS 1 DEG, RECEIVED "LE SLAT ASYM". RAN CHECKLIST, LANDED FLAPS 20 USING ALT TE FLAPS. IND U FOUND A SPLIT BETWEEN 
- [SDR FDEA202006261370](https://openairdocs.org/sdr/FDEA202006261370), Jun 26, 2020: FLOOR PANEL. DELAMINATED. FWD CARGO FLOOR PANEL 121AF IS DAMAGED. REPAIRED FWD CARGO PANEL 121AF IAW SRM 53-30-53-1A AND SRM 53-00-50-2R.
- [SDR FDEA2020062541337](https://openairdocs.org/sdr/FDEA2020062541337), Jun 24, 2020: FLOORBOARD. DELAMINATED. MAIN DECK FLOOR PANEL 241NFF HAS DAMAGED CORNER. REPAIRED DAMAGED CORNER ON MAIN DECK FLOOR PANEL 241NFF IAW SRM 53-00-50-2R PAR 4.G.3. MAJOR REPAIR.
- [SDR FDEA2020062541336](https://openairdocs.org/sdr/FDEA2020062541336), Jun 24, 2020: FLOORBOARD. DENTED. MAIN DECK FLOORBOARD 221DFF HAS MULTIPLE DENTS. REPAIRED MAIN DECK FLOORBOARD 221DFF IAW SRM 53-00-50-2R. MAJOR REPAIR.
- [SDR FDEA2020062541335](https://openairdocs.org/sdr/FDEA2020062541335), Jun 24, 2020: FLOORBOARD. DENTED. MAIN DECK FLOORBOARD 221BFF HAS MULTIPLE DENTS. REPAIRED MAIN DECK FLOORBOARD 221BFF IAW SRM 53-00-50-2R. MAJOR REPAIR.
- [SDR FDEA2020062541334](https://openairdocs.org/sdr/FDEA2020062541334), Jun 24, 2020: FLOORBOARD. DENTED. MAIN DECK FLOORBOARD 221AFF HAS MULTIPLE DENTS. REPAIRED MAIN DECK FLOORBOARD 221AFF IAW SRM 53-00-50-2R.

All 58: https://openairdocs.org/aircraft/N131FE/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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