# N123FE: 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: 42716
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 28, 2015
- Certificate issued: August 17, 2015
- Expires: August 31, 2028
- Mode S code: A05F59
- 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=123FE
- Page: https://openairdocs.org/aircraft/N123FE

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 N123FE.

## FAA accident and incident reports

None matched to N123FE.

## Reports on N123FE not matched to an aircraft (1)

They name N123FE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19890805049129I](https://openairdocs.org/incident/19890805049129I), Aug 5, 1989: Boeing 72725C (N123FE), Omaha, NE. A system hydraulic failure on descent. Landed safely. Replaced hydraulic quantity transmitter.

## Service difficulty reports (44)

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 FDEA202510292103](https://openairdocs.org/sdr/FDEA202510292103), Oct 29, 2025: WINDSHIELD. FAILED. IN FLIGHT AT FL 340 OFFICERS FRONT WINDSHIELD SHATTERED. EMERGENCY DECLARED. REMOVED AND INSTALLED FO #1 WINDOW UP TO AND INCLUDING 3.G.(31). AND STEPS 3.G(34)-
- [SDR FDEA202507081142](https://openairdocs.org/sdr/FDEA202507081142), Jul 8, 2025: SKIN. DENTED. DENT ON RH WING, INBD TE FLAP, AFT FLAP LOWER SURFACE, AT 60" FROM INBD EDGE AND 2" FROM TE DENT ON RH WING, INBD TE FLAP, AFT FLAP LOWER SURFACE WAS REPAIRED I
- [SDR FDEA202507071131](https://openairdocs.org/sdr/FDEA202507071131), Jul 7, 2025: SKIN. DENTED. DENT ON OUTBOARD FLAP LOWER SKIN, BETWEEN WS 746 AND 772 LH WING OUTBOARD FLAP LOWER SKIN BETWEEN WS 746 AND 772 LH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R T
- [SDR FDEA202507071130](https://openairdocs.org/sdr/FDEA202507071130), Jul 7, 2025: SKIN. CORRODED. EVIDENCE OF CORROSION ON RH WING, INBD TE FLAP, AFT FLAP UPPER SURFACE, 5'' FROM OUTBD EDGE AND 7'' FROM TE RH WING, INBD TE FLAP, AFT FLAP UPPER SURFACE, 5'' F
- [SDR FDEA202507041120](https://openairdocs.org/sdr/FDEA202507041120), Jul 4, 2025: SKIN. DAMAGED. DENT ON OUTBOARD FLAP LOWER SKIN, BETWEEN WS 746 AND 772 LH WING. OUTBOARD FLAP LOWER SKIN, BETWEEN WS 746 ON 772 LH WING WAS REPAIRED IAW B767 SRM 57-53-012R T
- [SDR FDEA202507031110](https://openairdocs.org/sdr/FDEA202507031110), Jul 3, 2025: SKIN. DENTED. TWO DENTS ON RH WING, INBD TE FLAP, AFT FLAP UPPER SURFACE, AT 20" FROM OUTBD EDGE AND 12" AND 2" FROM TE RH WING, INBD FLAP, AFT FLAP UPPER SURFACE, TWO DENTS 
- [SDR FDEA202507031109](https://openairdocs.org/sdr/FDEA202507031109), Jul 3, 2025: FLOOR PANEL. PUNCTURED. MDC FLOOR PANEL 251DFF WITH PUNCTURES MDC FLOOR PANEL 251DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 REV 92 APR 15,2025
- [SDR FDEA202507031108](https://openairdocs.org/sdr/FDEA202507031108), Jul 3, 2025: FLOOR PANEL. PUNCTURED. MDC FLOOR PANEL 251QFF WITH PUNCTURES MDC FLOOR PANEL 251QFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 PAR 15/2025
- [SDR FDEA202507031107](https://openairdocs.org/sdr/FDEA202507031107), Jul 3, 2025: FLOOR PANEL. PUNCTURED. MDC FLOOR PANEL 252DFF WITH PUNCTURES MDC FLOOR PANEL 252DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507031106](https://openairdocs.org/sdr/FDEA202507031106), Jul 3, 2025: FLOOR PANEL. PUNCTURED. MDC FLOOR PANEL 251EFF WITH PUNCTURES MDC FLOOR PANEL 251EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507031105](https://openairdocs.org/sdr/FDEA202507031105), Jul 3, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 241KFF WIYH PUNCTURES MDC FLOOR PANEL 241KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 PAR 4B SHEET 2, REV 92. APR 15/2025.
- [SDR FDEA202507031104](https://openairdocs.org/sdr/FDEA202507031104), Jul 3, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 242HFF WITH CRACK MDC FLOOR PANEL 242HFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507031103](https://openairdocs.org/sdr/FDEA202507031103), Jul 3, 2025: SKIN. DENTED. DENT ON OUTBOARD LOWER SKIN, BETWEEN WS 720 AND 746 LH WING LH WING, OUTBOARD FLAP LOWER SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 SHEET 3 DETAIL II AN
- [SDR FDEA202507011092](https://openairdocs.org/sdr/FDEA202507011092), Jul 1, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 252JFF WITH PUNTURES MDC FLOOR PANEL 252JFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025
- [SDR FDEA202507011091](https://openairdocs.org/sdr/FDEA202507011091), Jul 1, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 251AFF WITH PUNCTURES MDC FLOOR PANEL 251AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202507011090](https://openairdocs.org/sdr/FDEA202507011090), Jul 1, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 252SFF WITH PUNCTURES MDC FLOOR PANEL 252SFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202507011089](https://openairdocs.org/sdr/FDEA202507011089), Jul 1, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 252HFF WITH PUNCTURES MDC FLOOR PANEL 252HFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025
- [SDR FDEA202507011088](https://openairdocs.org/sdr/FDEA202507011088), Jul 1, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 251KFF WITH PUNCTURES MDC FLOOR PANEL 251KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202506301085](https://openairdocs.org/sdr/FDEA202506301085), Jun 30, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 251LFF WITH PUNCTURES MDC FLOOR PANEL 251LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202506301084](https://openairdocs.org/sdr/FDEA202506301084), Jun 30, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 251PFF WITH CRACK MDC FLOOR PANEL 251PFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202506301083](https://openairdocs.org/sdr/FDEA202506301083), Jun 30, 2025: FLOOR PANEL. CRACKED. MDC FLOOR PANEL 252NFF WITH PUNCTURES MDC FLOOR PANEL 252NFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202410061440](https://openairdocs.org/sdr/FDEA202410061440), Oct 6, 2024: ESCAPE REEL. FAILED. MDIS 123 25-60 8503 06OCT24 08:56 MEM FACT #2 EMERGENCY DESCENT DEVICE FOUND EXPIRED. R/I 06OCT24 16:01 MEM REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN
- [SDR FDEA202406060775](https://openairdocs.org/sdr/FDEA202406060775), Jun 6, 2024: FLOORBEAM. CRACKED. [MEC, LT TUNNEL, STA 246 (LBL 26.06) FLOOR BEAM, FWD SIDE, "L" BRACKET CRACKED. (PN 141T5814-136) INSTALLED NEW FABRICARTED SUPPORT (PN 141T5814-136) USING DRW 
- [SDR FDEA202406050772](https://openairdocs.org/sdr/FDEA202406050772), Jun 5, 2024: TEE ANGLE. CRACKED. MEC, LT TUNNEL, STA 246, APROX BL 20 LT, "T" BRACKET CRACKED. INSTALLED NEW FABERCATED T-CLIP 141T5603-6 IAW DRAWING #141T5601 & 141T5600, SRM 51-40-02-0G.
- [SDR FDEA202406050771](https://openairdocs.org/sdr/FDEA202406050771), Jun 5, 2024: TEE ANGLE. DAMAGED. T CLIP CRACKED AT APPROX. STA 266 BL 0. INSTALLED NEW FABERCATED T-CLIP 141T5603-7 IAW DRAWING #141T5601, SRM 51-40-02-0G.
- [SDR FDEA202307181239](https://openairdocs.org/sdr/FDEA202307181239), Jul 18, 2023: RUDDER. DAMAGED. VERT STAB, RUDDER, L/H SIDE, TRAILING EDGE HAS EDGE DAMAGE AT APPROX RUDDER STA 305 REPAIRED RUDDER TRAILING EDGE IAW FEDEX EA# H-5540-T0375223-P1, RELEASED JUL
- [SDR FDEA202307181238](https://openairdocs.org/sdr/FDEA202307181238), Jul 18, 2023: SKIN. DAMAGED. L/H HOR. STAB, UPPER SKIN IS DENTED AND GOUGED AT APPROX 75" O/B OF STAB ROOT JUST AFT OF L/E PANEL 332BL REPAIRED L/H HOR STAB, UPPER SKIN DENT AND GOUGE APPRO
- [SDR FDEA202307181237](https://openairdocs.org/sdr/FDEA202307181237), Jul 18, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR SUPPORT IS CRACKED AT APPROX STA 1575, LBL 68 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C
- [SDR FDEA202307181236](https://openairdocs.org/sdr/FDEA202307181236), Jul 18, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX STA 1575, LBL 65 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C
- [SDR FDEA202307181235](https://openairdocs.org/sdr/FDEA202307181235), Jul 18, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT APPROX STA 1575, RBL 68 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C.
- [SDR FDEA202307181234](https://openairdocs.org/sdr/FDEA202307181234), Jul 18, 2023: ANGLE. CRACKED. MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX STA 1575, RBL 65 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C
- [SDR FDEA202307141216](https://openairdocs.org/sdr/FDEA202307141216), Jul 14, 2023: SHEAR TIE. CRACKED. 1EA ATTACH CLIP IS CRACKED AT #2 PYLON AFT BULKHEAD ON INBD SIDE AT APPROX NAC STA 295, JUST BELOW INBD MID-SPAR FITTING REMOVED AND REPLACED #2 PYLON, INBOARD 
- [SDR FDEA202307121203](https://openairdocs.org/sdr/FDEA202307121203), Jul 12, 2023: BRACKET. CRACKED. #1 PYLON/NACELLE, I/B SIDE, ACCESSED BY PANEL 437BR, HYD. RESERVOIR BAY FWD BULKHEAD UPPER CORNER ATTACH BRACKET CRACKED REMOVED AND REPLACED ATTACH BRACKET LOC
- [SDR FDEA202307101195](https://openairdocs.org/sdr/FDEA202307101195), Jul 10, 2023: FITTING. CRACKED. #1 PYLON AFT FAIRING, INBD SIDE FRAME, NAC STA 380, MID ATTACH CLIP, IS CRACKED. REMOVED AND REPLACED ATTACH CLIP (BRACKET) LOCATED ON #1 PYLON AFT FAIRING, INB
- [SDR FDEA202307101194](https://openairdocs.org/sdr/FDEA202307101194), Jul 10, 2023: FITTING. CRACKED. #2 PYLON AFT FAIRING, OTBD SIDE, FRAME ATTACH CLIP, AT APPROX. NAC STA 380, IS CRACKED REMOVED AND REPLACED ATTACH CLIP LOCATED ON #2 PYLON AFT FAIRING, OTBD SI
- [SDR FDEA202307071169](https://openairdocs.org/sdr/FDEA202307071169), Jul 7, 2023: BRACKET. CRACKED. RIGHT WING FUELING STATION PANEL HOLD OPEN SUPPORT BRACKET CRACKED REMOVED AND REPLACED SUPPORT BRACKET ON RIGHT WING FUELING STATION PANEL PER BOEING DWG 114T2
- [SDR FDEA202307071168](https://openairdocs.org/sdr/FDEA202307071168), Jul 7, 2023: BRACKET. CRACKED. RIGHT WING FUELING STATION PANEL LIGHT SUPPORT BRACKET CRACKED REMOVED AND REPLACED LIGHT SUPPORT BRACKET ON RIGHT WING FUELING STATION PANEL PER BOEING DWG 284
- [SDR FDEA202307061217](https://openairdocs.org/sdr/FDEA202307061217), Jul 6, 2023: SKIN. GOUGED. LH HORIZONTAL STAB. UPPER SKIN IS DENTED AND GOUGED AT APPROX 75" OB OF STAB. ROOT, JUST AFT OF LE PANEL 332BL. REPAIRED LH HORIZONTAL STABILIZER UPPER SKIN DEN
- [SDR FDEA202203290798](https://openairdocs.org/sdr/FDEA202203290798), Mar 29, 2022: FORMER. CRACKED. RH WING LE AT STA OSS-441 HAS LOOSE RIVETS AND A BROKEN FORMER P/N 114T2170-6. 0000301922 : VERNON, JAMES L - 30-MAR-2022 01:18 REPLACED R/W L/E FORMER AT WS 44
- [SDR FDEA202203290797](https://openairdocs.org/sdr/FDEA202203290797), Mar 29, 2022: FORMER. CRACKED. LH WING LE AT STA OSS499 HAS LOOSE RIVETS AND BROKEN FORMER P/N 114T2511-13 0000452710 : ROSNER, DANIEL D - 30-MAR-2022 01:37 COMPLIED WITH EA TH-5720-T0367715P
- [SDR FDEA202203290796](https://openairdocs.org/sdr/FDEA202203290796), Mar 29, 2022: FORMER. NONE. LH WING LE AT STA OSS441 HAS LOOSE RIVETS AND A BROKEN FORMER P/N 114T2170-5 0000493008 : CRAIL, ROGER L - 30-MAR-2022 01:41 REPLACED LOOSE RIVETS AND BROKEN BR
- [SDR FDEA202107141773](https://openairdocs.org/sdr/FDEA202107141773), Jul 14, 2021: SKIN. WORN. RH WING #7 SLAT T/E WORN BTW ISS160.41 - ISS180.56 PERFORMED THE REPAIR ON RH WING #7 SLAT T/E WEDGE PER B767 SRM 57-43-02-2R REPAIR 1 AND SRM 51-70-10-2R REPAI
- [SDR FDEA201807081648](https://openairdocs.org/sdr/FDEA201807081648), Jul 8, 2018: SKIN. DENTED. COMPLY WITH EA H-5330-T0340792-P1, FUSELAGE SKIN REPAIR AT STA 1430. REPAIRED FUSELAGE SKIN AT STA 1430 ABOVE STR 35L AND BELOW STR 39L IAW EA NR H-5330-T034079
- [SDR FDEA201803310827](https://openairdocs.org/sdr/FDEA201803310827), Mar 31, 2018: BATTERY. FAILED. TRIED TO START THE APU TWICE, NO START. APU FAULT EICAS. OPENED PANEL ON THE E-6 RACK AND NOTICED APU BATTERY COMPARTMENT WAS FULL OF SMOKE AND SMELLED STRONG. 

## 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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