# N124FE: 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: 43546
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 29, 2015
- Certificate issued: July 23, 2015
- Expires: July 31, 2028
- Mode S code: A06310
- 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=124FE
- Page: https://openairdocs.org/aircraft/N124FE

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 N124FE.

## FAA accident and incident reports

None matched to N124FE.

## 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 FDEA202609241437](https://openairdocs.org/sdr/FDEA202609241437), Sep 24, 2026: ENGINE. BIRD INGESTION. CLIMBING THRU APPROXIMATELY 500-600FT AGL DEPARTING VCP WE STRUCK A LARGE BLACK BIRD ON THE NOSE CONE OF THE LEFT ENGINE. A LOUD BANG WAS HEARD ALONG WITH A PUT
- [SDR FDEA202505290824](https://openairdocs.org/sdr/FDEA202505290824), May 29, 2025: SKIN. DENTED. LH WING, INBOARD FLAP WITH SEVERAL DENTS LH WING, INBOARD FLAP WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R FIG. 201 (SHEET 2) DETAIL I,SRM 51-70-10-2R REPAIR 2 FIG
- [SDR FDEA202505290823](https://openairdocs.org/sdr/FDEA202505290823), May 29, 2025: SKIN. DENTED. LH WING, INBOARD TRAILING FLAP WITH SEVERAL DENTS LH WING, INBOARD TRAILING FLAP WAS REPAIRED I.A.W. B767 57-53-01-2R FIG. 201 (SHEET 4) NOTE "A" AND SRM 51-70-
- [SDR FDEA202505290822](https://openairdocs.org/sdr/FDEA202505290822), May 29, 2025: SKIN. DENTED. LH WING, INBOARD FLAP WITH SEVERAL DENTS LH WING, INBOARD FLAP WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R FIG. 201 (SHEET 2) DETAIL I,SRM 51-70-10-2R REPAIR 2 FIG
- [SDR FDEA202505260802](https://openairdocs.org/sdr/FDEA202505260802), May 26, 2025: FLOOR PANEL. PUNCTURED. SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231DFA SECTION 43 OF MDC FLOOR PANEL 231DFA SECTION 43 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAE 4 B FIG 201 SH
- [SDR FDEA202505260801](https://openairdocs.org/sdr/FDEA202505260801), May 26, 2025: FLOOR PANEL. PUNCTURED. SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231CFF SECTION 43 OF MDC FLOOR PANEL 231CFF SECTION 43 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SH
- [SDR FDEA202505260800](https://openairdocs.org/sdr/FDEA202505260800), May 26, 2025: FLOOR PANEL. PUNCTURED. SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231EFF SECTION 43 OF MDC FLOOR PANEL 231EFF SECTION 43 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SH
- [SDR FDEA202505220791](https://openairdocs.org/sdr/FDEA202505220791), May 22, 2025: FLOOR PANEL. CRACKED. SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231AFF SECTION 43 OF MDC FLOOR PANEL 231AFF SECTION 43 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET
- [SDR FDEA202505220790](https://openairdocs.org/sdr/FDEA202505220790), May 22, 2025: FLOOR PANEL. CRACKED. SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231UFF SECTION 43 OF MDC FLOOR PANEL 231UFF SECTION 43 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET
- [SDR FDEA202505220789](https://openairdocs.org/sdr/FDEA202505220789), May 22, 2025: FLOOR PANEL. CRACKED. SECONDARY FINDING PUNCTURE ON FLOOR PANEL 241LFF ON SECTION 45 OF MDC. FLOOR PANEL 241LFF SECTION 45 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 S
- [SDR FDEA202505220788](https://openairdocs.org/sdr/FDEA202505220788), May 22, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 251QFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 251QFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 SHEET 2 PAR 4 B REV 90 AUG 1
- [SDR FDEA202505220787](https://openairdocs.org/sdr/FDEA202505220787), May 22, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 251PFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 251PFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 1
- [SDR FDEA202505220786](https://openairdocs.org/sdr/FDEA202505220786), May 22, 2025: FLOOR PANEL. CRACKED. MAIN DECK FLOOR PANEL (252DFF) WITH PUNCTION MAIN DECK CARGO COMPARTMENT MAIN DECK FLOOR PANEL 252DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEE
- [SDR FDEA202505220785](https://openairdocs.org/sdr/FDEA202505220785), May 22, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242LFA WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 242LFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 1
- [SDR FDEA202505220784](https://openairdocs.org/sdr/FDEA202505220784), May 22, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 251YFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 251YFF WAS REPAIRED IAW SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 15/202
- [SDR FDEA202505220783](https://openairdocs.org/sdr/FDEA202505220783), May 22, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 251VFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 251VFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 1
- [SDR FDEA202505220782](https://openairdocs.org/sdr/FDEA202505220782), May 22, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242GFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 242GFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 1
- [SDR FDEA202405180687](https://openairdocs.org/sdr/FDEA202405180687), May 18, 2024: SUPPORT ANGLE. CRACKED. MEC, LT TUNNEL, AFT SIDE OF STA 246 BEAM HAS 1 EACH CRACKED "L" BRACKET. (PN: 141T5146- 16) REMOVED AND REPLACED SUPPORT ANGLE 147T5146-16 AT STA 246 PER DWG 14
- [SDR FDEA202405180684](https://openairdocs.org/sdr/FDEA202405180684), May 18, 2024: STIFFENER. CRACKED. MEC, LT TUNNEL, FWD SIDE OF STA 246 BEAM HAS 1 EACH CRACKED "L" BRACKET (PN: 141T5814- 136) REMOVED AND INSTALLED NEW STIFFENER PN: 141T5814-136. REF SRM 51-40-
- [SDR FDEA202306151044](https://openairdocs.org/sdr/FDEA202306151044), Jun 15, 2023: SKIN. DELAMINATED. RUDDER , R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE ON THE AFT EDGE. REPAIRED RUDDER , R/H EXTERNAL SURFACE APPROX 8FT UP FROM THE FUSE
- [SDR FDEA202306151043](https://openairdocs.org/sdr/FDEA202306151043), Jun 15, 2023: SKIN. DELAMINATED. RUDDER , R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE APPROX 10" FWD OF THE AFT EDGE REPAIRED R/H EXTERNAL SURFACE OF RUDDER APPROX 8FT U
- [SDR FDEA202306151042](https://openairdocs.org/sdr/FDEA202306151042), Jun 15, 2023: SKIN. DELAMINATED. RUDDER , R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE APPROX 27" FWD OF THE AFT EDGE REPAIRED RUDDER , R/H EXTERNAL SURFACE , APPROX 8FT 
- [SDR FDEA202306141036](https://openairdocs.org/sdr/FDEA202306141036), Jun 14, 2023: BEAM. CRACKED. L/H WING T/E SUPPORT STRUCTURE IS CRACKED AT APPROX WS 1030 REMOVED & REPLACED LEFT WING TRAILING EDGE PANEL SUPPORT BEAM IAW BAC DWG 113T1913, REVISION A
- [SDR FDEA202306131030](https://openairdocs.org/sdr/FDEA202306131030), Jun 13, 2023: ANGLE. CRACKED. MAIN CABIN FLOORBEAM AT STA 1575 RBL 65-68, ATTACH ANGLE IS CRACKED FABRICATED AND REPLACED CRACKED ATTACH ANGLE AT STA 1575, RBL 65-68, PER BOEING DWG 146T5650
- [SDR FDEA202306131029](https://openairdocs.org/sdr/FDEA202306131029), Jun 13, 2023: ANGLE. CRACKED. MAIN CABIN FLOORBEAM AT STA 1575 LBL 65, ATTACH ANGLE IS CRACKED FABRICATED AND REPLACED CRACKED ATTACH ANGLE AT STA 1575, LBL 65, PER BOEING DWG 146T5650, SHT 
- [SDR FDEA202306131028](https://openairdocs.org/sdr/FDEA202306131028), Jun 13, 2023: SLAT. GOUGED. LW #5 SLAT LWR TE HAS 2 GOUGES . CLEANED SANDED REMOVED DAMAGE AND REPAIRED LW #5 SLAT LWR TE 2 GOUGES WITH PERMANENT REPAIR IAW B767 SRM 57-43-02 AND 51-70-10-
- [SDR FDEA202306111023](https://openairdocs.org/sdr/FDEA202306111023), Jun 11, 2023: SLAT. DENTED. #8 SLAT LOCATED JUST OB OF OB TRACK, SLAT TE HAS A DENT . CLEANED SANDED AND REMOVED DAMAGE ON RIGHT WING #8 SLAT AND REPAIRED IAW B767 SRM 57-43-02-2R AND 51-7
- [SDR FDEA202306050995](https://openairdocs.org/sdr/FDEA202306050995), Jun 5, 2023: BRACKET. CRACKED. RW INBD L/E AT STA LES 285 TORQUE TUBE GUIDE BRACKET IS CRACKED REMOVED AND REPLACED RIGHT WING, INBOARD LEADING EDGE, TORQUE TUBE GUIDE BRACKET IAW B767 SRM 51
- [SDR FDEA202211052733](https://openairdocs.org/sdr/FDEA202211052733), Nov 5, 2022: FORMER. CRACKED. FORMER CRACKED AT R/W FLE OSS 441, (PN INSTALLED 114T2170-6, WITH 114T2171-3) REPLACED PART WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS F
- [SDR FDEA202205281324](https://openairdocs.org/sdr/FDEA202205281324), May 28, 2022: FORMER. CRACKED. ON LS FLE OSS 499 CRACKED FORMER 114T2511-13 W/ANGLE 114T2511-11 28-MAY-2022 22:54 REPLACED L/W L/E FORMER STA. OSS499 REF E.A. H-5720-TO368711 P1 , SEQ. 165
- [SDR FDEA202104301077](https://openairdocs.org/sdr/FDEA202104301077), Apr 30, 2021: EVAS UNIT. NO TEST. CAPT'S EVAS HAS AN UNSATISFACTORY OPS CKS PER WRI 25-60/5316 AND E.O. H-2560-E0324416 REV NO. G POS. P2. REMOVED AND REPLACE CAPT'S EVAS
- [SDR FDEA201911243085](https://openairdocs.org/sdr/FDEA201911243085), Nov 24, 2019: SKIN. DENTED. INCOMING ITEM : LOWER LH FUSELAGE AT STA 1225, BETWEENSTRINGERS 32L-33L HAS A DENT COMPLIED WITH EA H-5310-T0350997 A. TITLED "FUSELAGE-MAINFRAME-FUSELAGE SKIN,
- [SDR FDEA201802130383](https://openairdocs.org/sdr/FDEA201802130383), Feb 13, 2018: WARNING SYSTEM. OUT OF ADJUST. WHILE PERFORMING THE CABIN ALTITUDE WARNING TEST DURING CRM INSTALLATION - FITMENT TESTING. DISCOVERED THE CABIN ALTITUDE WARNING SYSTEM WAS INOPERATIVE. ADJUST
- [SDR FDEA201709062461](https://openairdocs.org/sdr/FDEA201709062461), Sep 6, 2017: FIRE BOTTLE. INOPERATIVE. APU FIRE EXTINGUISHER SYSTEM INOP. INSPECTED APU COMPT FOR ANY SIGNS OF FIRE OR LEAKS, NONE FOUND LOOKS PRISTINE. REMOVED AND REPLACED THE APU FIRE BOTTLE AND O

## 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 N124FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N124FE before.

- [Cancelled 2004-08-26](https://openairdocs.org/deregistered/N124FE-2004-08-26): Boeing 727-25C, S/N 19360, built 1967. 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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