# N110FE: 2014 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: 43542
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 4, 2014
- Certificate issued: December 30, 2014
- Expires: December 31, 2027
- Mode S code: A02CB5
- 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=110FE
- Page: https://openairdocs.org/aircraft/N110FE

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA24WA180](https://openairdocs.org/ntsb/DCA24WA180), May 8, 2024: Boeing 767-3S2F (N110FE), Istanbul, Türkiye, incident, minor damage

## FAA accident and incident reports

None matched to N110FE.

## Reports on N110FE not matched to an aircraft (1)

They name N110FE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19810123010009I](https://openairdocs.org/incident/19810123010009I), Jan 23, 1981: Boeing 72722C (N110FE), Middletown, PA. No 2 engine fire warning system came on during climb out. Maintenace found a bad cowl and saddle duct.

## 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 FDEA202604300525](https://openairdocs.org/sdr/FDEA202604300525), Apr 30, 2026: LENS. MISSING. L1 DOOR INTERIOR EXIT LIGHT LENS MISSING EMERGENCY EXIT SIGN LENS LOCATED IN FLT DECK, REFITTED PER AMM 33-51-01-2. CHECKS OK.
- [SDR FDEA202410151511](https://openairdocs.org/sdr/FDEA202410151511), Oct 15, 2024: SKIN. PUNCTURED. RH WING NO.7 SLAT MID SECTION LOW SURFACE FOUND PUNCTURE, AS MARKED REPAIRED THE RH WING NO.7 SLAT MID SECTION LOW SURFACE PER B767 SRM57-43-02-2R REPAIR 1 & SR
- [SDR FDEA202410151510](https://openairdocs.org/sdr/FDEA202410151510), Oct 15, 2024: STRINGER. DAMAGED. FUSELAGE FRAME STA1502 - STRINGER CLIP AND S-20L STRINGER 1EA FASTENER HOLE ENLARGED REPAIRED THE DISCREPANT(ENLARGED) HOLE AT FUSELAGE FRAME STA1502 - STRINGER
- [SDR FDEA202405150673](https://openairdocs.org/sdr/FDEA202405150673), May 15, 2024: SKIN. DAMAGED. E&E BAY DOOR AND SURROUNDING STRUCTURE DAMAGED. E&E BAY DOOR REPLACE AND SURROUNDING STUCTURES REPAIRED UNDER FED-RE-2403203 REM 97-2.
- [SDR FDEA202405150672](https://openairdocs.org/sdr/FDEA202405150672), May 15, 2024: SKIN. DAMAGED. LOWER FUSELAGE SKIN DAMAGED AT APPROX. STATION 157. FUSELAGE SKIN REPAIRED IAW FED-RE-2403203
- [SDR FDEA202405130657](https://openairdocs.org/sdr/FDEA202405130657), May 13, 2024: ACTUATOR. FAILED. NLG FAILED TO EXTEND, UPON LANDING ACFT REMAINED ON CENTERLINE OF RUNWAY SURFACE. REF E.A H-5310-T0380090 P1 WORKED IN CONJUSCTION WITH 53-10/0463 COMPLETED INS
- [SDR FDEA202401130076](https://openairdocs.org/sdr/FDEA202401130076), Jan 13, 2024: UNKNOWN. UNKNOWN. WEIGHT CHECK DUE FOR THE FLIGHT DECK PORTABLE FIRE EXTINGUISHER MOUNTED IN FRONT OF RAFT STOWAGE. GMM: 9-4-404 AMM: 26-26-02-4-1 COMPLETED WEIGHT CHECK PROCEDUR
- [SDR FDEA202311061831](https://openairdocs.org/sdr/FDEA202311061831), Nov 6, 2023: FLAP. DAMAGED. LH WING, INBOARD AFT FLAP LOWER SURFACE RH SIDE WITH PUNCTURE LH WING INBOARD AFT FLAP LOWER SURFACE, RH SIDE WAS REPAIRED IAW B767 SRM 57-53-01- 2R FIG 201 TAB
- [SDR FDEA202305260966](https://openairdocs.org/sdr/FDEA202305260966), May 26, 2023: ELT. UNKNOWN. ELT HAS BEEN DETECTED EMITTING DURING FLIGHT. FOR INFO: IST STATION LOCAL TOWER WARNED US FOR ELT SIGNAL. RELEASED FOR SERVICE PER MEL : 25-63-10-02-A ON ARRIVA
- [SDR FDEA202210082517](https://openairdocs.org/sdr/FDEA202210082517), Oct 8, 2022: SKIN. DENTED. LEFT WING OUT BOARD TRAILING EDGE FLAP WITH DENT (LOWER SURFACE) LEFT WING OUTBOARD FLAP T/E, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG. 1-7 AND B
- [SDR FDEA202210052471](https://openairdocs.org/sdr/FDEA202210052471), Oct 5, 2022: WEDGE. DENTED. LEFT WING SLAT NO. 6 TRAILING EDGE WEDGE WITH DENT. RH WING SLAT #6 TRAILING EDGE WEDGE UPPER SURFACE AT POSITION ISS 231-236 SKIN WAS REPAIRED IAW SRM 51-70-10
- [SDR FDEA202208161984](https://openairdocs.org/sdr/FDEA202208161984), Aug 16, 2022: FIRE BOTTLE. FAILED. MDIS 110 26-11 8313 16AUG22 MXP OPEN U APU FIRE EXT. BOTTLE DISCHARGE LIGHT ILLUMINATED. MEL 16AUG22 15:22 MXP U RELEASED FOR SERVICE PER MEL : 26-22-01-B CATEG
- [SDR FDEA202205141205](https://openairdocs.org/sdr/FDEA202205141205), May 14, 2022: INSERT. FAILED. FOUND RH MLG FWD DOOR STOP FASTENERS TO BE LOOSE AND SHIM FASTENER HOLES TO BE ELONGATED. REMOVED INSERTS FROM RH MLG FWD DOOR STOP AND REPLACED FASTENERS REF E
- [SDR FDEA202205141204](https://openairdocs.org/sdr/FDEA202205141204), May 14, 2022: INSERT. FAILED. FOUND LH MLG FWD DOOR STOP FASTENERS TO BE LOOSE AND SHIMS TO HAVE MIGRATED. REMOVED INSERTS FROM LH MLG FWD DOOR STOP AND REPLACED FASTENERS REF E.A. TH- 3212-
- [SDR FDEA202111242929](https://openairdocs.org/sdr/FDEA202111242929), Nov 24, 2021: NONE. NONE. MDIS 110 33-50 7324 24NOV21 CDG FACT U EMERGENCY LIGHT GUARD IS BROKEN . FACT 24NOV21 03:19 CDG U R&R'D EMERGENCY LIGHT GUARD PER MM:33-51-08-4 , OPS CHK OK .
- [SDR FDEA202104271048](https://openairdocs.org/sdr/FDEA202104271048), Apr 27, 2021: ENGINE. OVERTEMP. STARTED DESCENT FROM FL 310, THE OIL TEMP SPIKED UP TO 165 ON THE LT ENGINE. THROTTLE WAS PULLED TO IDLE, & CHECKLIST RUN FOR HIGH OIL TEMP, LT ENGINE. OIL QUAN
- [SDR FDEA202012153166](https://openairdocs.org/sdr/FDEA202012153166), Dec 15, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241YFA MISSING EDGE FILLER AT LBL 54. FABRICATED NEW FLOOR PANEL 241YFA, IAW FEDEX DWG SRZ-25-005 REV C.
- [SDR FDEA202012153167](https://openairdocs.org/sdr/FDEA202012153167), Dec 15, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 242SFF HAS SEVERAL AREAS OF DELAMINATION AND CRUSH DAMAGE AROUND FLOOR FITTING CUTOUTS. FABRICATED NEW FLOOR PANEL 241SFF, IAW FEDEX DWG 
- [SDR FDEA202012153165](https://openairdocs.org/sdr/FDEA202012153165), Dec 15, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 242TFA IS PUNCTURED TWO PLACES. FABRICATED NEW FLOOR PANEL 242TFA, IAW FEDEX DWG SRZ-25-005, REV R.
- [SDR FDEA202012153164](https://openairdocs.org/sdr/FDEA202012153164), Dec 15, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241ZFF HAS CRUSH AND DELAM DAMAGE, SEVERAL AREAS ALONG THE ENTIRE LENGTH. FABRICATED NEW FLOOR PANEL 241ZFF, IAW FEDEX DWG SRZ-25-005, RE
- [SDR FDEA202012153163](https://openairdocs.org/sdr/FDEA202012153163), Dec 15, 2020: FLOOR SUPPORT. CRACKED. RT AFT FUSELAGE, AFT CARGO BS 1576 RBL 78, MAIN CARGO DECK FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE RIGHT AFT FUSELAGE MAIN CARGO DECK FLOOR SUPPORT SPLI
- [SDR FDEA202012153162](https://openairdocs.org/sdr/FDEA202012153162), Dec 15, 2020: FLOOR SUPPORT. CRACKED. LT AFT FUSELAGE, AFT CARGO BS 1576 LBL 78, MAIN CARGO DECK FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE LEFT AFT FUSELAGE MAIN CARGO DECK FLOOR SUPPORT SPLIC
- [SDR FDEA202012093082](https://openairdocs.org/sdr/FDEA202012093082), Dec 9, 2020: SKIN. CHAFED. RIGHT WING NR 9 SLAT LOWER TRAILING EDGE WEDGE SKIN CHAFED. REPAIRED NR 9 SLAT RIGHT WING LOWER TRAILING EDGE WEDGE 33.75" FROM INBOARD END BY BONDING FILLER SK
- [SDR FDEA202012083072](https://openairdocs.org/sdr/FDEA202012083072), Dec 8, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241NFF HAS BROKEN INSERTS AND DELAMINATION DAMAGE ALONG THE FORWARD EDGE. FABRICATED NEW MAIN CABIN FLOOR PANEL 241NFF, IAW FEDEX DWG SRZ
- [SDR FDEA202012083071](https://openairdocs.org/sdr/FDEA202012083071), Dec 8, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241JFF HAS CRUSH AND DELAMINATION DAMAGE ALONG THE LBL 55 SIDE, ENTIRE LENGTH. FABRICATED NEW MAIN CABIN FLOOR PANEL 241JFF, IAW FEDEX DW
- [SDR FDEA202012083070](https://openairdocs.org/sdr/FDEA202012083070), Dec 8, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241WFF HAS THREE SEPARATE AREAS OF DAMAGE. REPAIRED 3 EA DAMAGE AREAS ON FLOOR PANEL 241WFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202012073171](https://openairdocs.org/sdr/FDEA202012073171), Dec 7, 2020: BEAM. DAMAGED. NR 2 PYLON INBOARD SKIRT BEAM FWD FLANGE HAS ELONGATED HOLES. REPAIRED ELONGATED HOLES ON NR 2 PYLON INBOARD SKIRT BEAM FWD FLANGE, IAW FEDEX EA H-5450-T0358609
- [SDR FDEA202012073056](https://openairdocs.org/sdr/FDEA202012073056), Dec 7, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241HFF HAS MISSING EDGE FILLER SEVERAL AREAS. REPAIRED EDGE FILLER ON FLOOR PANEL 241HFF, IAW B767 SRM 53-00-50-2R PARA 4G (2).
- [SDR FDEA202012063051](https://openairdocs.org/sdr/FDEA202012063051), Dec 6, 2020: ANGLE. CRACKED. FWD LT FRAME STA 246 LBL 50 BELOW FLOOR INTERCOSTAL ANGLE CRACKED. REMOVED AND REPLACED ANGLE P/N 141T5146-16, IAW B767 SRM 51-40-02 AND BAC DWG 141T5600 REV-.
- [SDR FDEA202012053039](https://openairdocs.org/sdr/FDEA202012053039), Dec 5, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 242BFA IS PUNCTURED TWO PLACES. REPAIRED DAMAGES TO FLOOR PANEL 242BFA, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202012053038](https://openairdocs.org/sdr/FDEA202012053038), Dec 5, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241LFF PUNCTURED TWO PLACES AND HAS MISSING EDGE FILLER. REPAIRED DAMAGES TO FLOOR PANEL 241LFF, IAW B767 SRM 53-00-50-2R, PARA 4C AND 4G
- [SDR FDEA202012053037](https://openairdocs.org/sdr/FDEA202012053037), Dec 5, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241FFF PUNCTURED THREE PLACES. REPAIRED DAMAGES TO FLOOR PANEL 241FFF, IAW B767 SRM 53-00-50-2R, PARA 4D AND 4E.
- [SDR FDEA202012053036](https://openairdocs.org/sdr/FDEA202012053036), Dec 5, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 242VFF HAS A PUNCTURE. REPAIRED FLOOR PANEL 242VFF, IAW B767 SRM 53-00-50-2R, PARA 4D.
- [SDR FDEA202012053035](https://openairdocs.org/sdr/FDEA202012053035), Dec 5, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 242HFF IS PUNCTURED, MARKED. REPAIRED FLOOR PANEL 242HFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202012053033](https://openairdocs.org/sdr/FDEA202012053033), Dec 5, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241KFF IS DAMAGED AT 3 SEPARATE AREAS, MARKED. REPAIRED 3 EA DAMAGES ON FLOOR PANEL 241KFF, IAW B767 SRM 53-00-50-2R, PARA 4C AND 4D.
- [SDR FDEA202012053032](https://openairdocs.org/sdr/FDEA202012053032), Dec 5, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241QFF HAS PUNCTURE DAMAGE, MARKED. REPAIRED FLOOR PANEL 241QFF, IAW B767 SRM 53-00-50-2R, PARA 4D.
- [SDR FDEA2020080751775](https://openairdocs.org/sdr/FDEA2020080751775), Aug 5, 2020: DRIVE UNIT. MALFUNCTIONED. WX FAIL ON EITHER SELECTED ON LT OR RT CTR CONTROL PANEL ON CENTER PEDESTAL. WINDSHEAR SYS EICAS LT WAS ALSO PRESENT DURING ENROUTE PHASE OF FLIGHT. R & R THE W
- [SDR FDEA201804281143](https://openairdocs.org/sdr/FDEA201804281143), Apr 28, 2018: LAMP. INOPERATIVE. DURING APPROACH, THE LEFT LANDING GEAR LIGHT DID NOT ILLUMINATE. ACCOMPLISHED GO AROUND, QRH AND MOCC/GOC. GEAR CYCLED, DID NOT HELP. NO SECONDARY OR TERTIARY W
- [SDR FDEA201710052868](https://openairdocs.org/sdr/FDEA201710052868), Oct 5, 2017: FLOOR PANEL. DAMAGED. INCOMING DISCREPANCY WRI 53-21/2521, AFT PIT FLOOR PANEL STA 1197 DAMAGED. REMOVED AND REPLACED FLOOR BOARD ON WORK ORDER 00069928 SEQ 000807.
- [SDR FDEA201710042851](https://openairdocs.org/sdr/FDEA201710042851), Oct 4, 2017: FLOORBOARD. GOUGED. IN LOWER AFT CARGO FOUND DAMAGE ON CARGO FLOOR BOARD AT STATION 1197 70 MEASURING 3 1/2" LONG X 3/4" WIDE. REMOVED DAMAGED AFT PIT FLOORBOARD PER SRM 51-40-02-0
- [SDR FDEA201710032847](https://openairdocs.org/sdr/FDEA201710032847), Oct 3, 2017: FLOOR PANEL. GOUGED. LOAD CREW REPORTS A GOUGE IN THE FIBERGLASS FLOOR PANEL OF THE AFT PIT AT STA 1197, ON THE OUTBOARD EDGE OF THE RIGHT SIDE PANEL. GOUGE IS APPROX 1 INCH LONG AN
- [SDR FDEA201710032845](https://openairdocs.org/sdr/FDEA201710032845), Oct 3, 2017: FLOORBOARD. CRACKED. FLOORBOARD 145T5876-94 CRACKED EDGES. FABRICATED FLOORBOARD 242FF 145T5876-94 ON T17/1299306 PER SRZ-25-005 REV M MAJOR REPAIR CAT A.
- [SDR FDEA201606232114](https://openairdocs.org/sdr/FDEA201606232114), Jun 23, 2016: LATCH. DAMAGED. ON PREFLIGHT, FOUND LATCH HANDLE ON EMERGENCY RAFT LOCKER JAMMED, PREVENTING ACCESS. COMPLIED WITH EA H-2560-T0326232 REV NO A POS P3, R&R THE LATCH ON THE LIFE
- [SDR FDEA201511183705](https://openairdocs.org/sdr/FDEA201511183705), Nov 18, 2015: LIGHT. INOPERATIVE. FUSELAGE MOUNTED EMER EXIT LIGHT INOPERATIVE. RELAMPED FUSELAGE MOUNTED EMER EXIT LIGHT. OPERATIONS CHECKED OK.

## 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

---
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.