# N297FE: 2012 Boeing 767-32LF

- Status: Valid registration
- Airframe: [Boeing 767-32LF](https://openairdocs.org/model/boeing-767-32lf) (registry code 138528K, 292 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: 41068
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 4, 2015
- Certificate issued: February 10, 2015
- Expires: February 29, 2028
- Mode S code: A30FFD
- 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=297FE
- Page: https://openairdocs.org/aircraft/N297FE

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 767-32LF)

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 DCA23FA149](https://openairdocs.org/ntsb/DCA23FA149), Feb 4, 2023: Boeing 767-32LF (N297FE), Austin, TX, incident, no damage. Probable cause: the local controller’s incorrect assumption that the Southwest Airlines (SWA) airplane would depart from the runway before the Federal Express airplane arrived on the same runway, which resulted in a…

## FAA accident and incident reports

None matched to N297FE.

## Service difficulty reports (47)

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 FDEA202607160937](https://openairdocs.org/sdr/FDEA202607160937), Jul 16, 2026: TRANSMITTER. FAILED. ON APPROACH INTO LAS, SELECTED FLAPS 25 & CAPTAIN NOTICED FLAPS BECAME ASYMMETRICAL LEAVING 20. NEVER RECEIVED ANY INDICATION ON ICAS. VERIFIED DETENT OF 25. EL
- [SDR FDEA202602090148](https://openairdocs.org/sdr/FDEA202602090148), Feb 9, 2026: SKIN. WORN. RH WING, T/E MAIN FLAP, OTBD EDGE UPPER SURFACE HAS AREA THAT IS WORN INTO COMPOSITE. REPAIRED RT WING INBD MAIN FLAP OTBD EDGE UPPER SURFACE 23 INCHES FROM T/E
- [SDR FDEA202602080146](https://openairdocs.org/sdr/FDEA202602080146), Feb 8, 2026: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252HFF DENTED. FABRCATED FLOORPANEL (252HFF) IAW DRAWING SR67-53-009 AND DRAWING 146T5869-10, RBL 77.50-12.85 BS 1197-12
- [SDR FDEA202602070145](https://openairdocs.org/sdr/FDEA202602070145), Feb 7, 2026: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 252GFF IS DENTED IN TWO LOCATIONS. FABRICATED NEW FLOOR PANEL 252GFF, RBL 54.75- RBL 77.5, STA 1197 22-1197 132 IAW DWG
- [SDR FDEA202602060139](https://openairdocs.org/sdr/FDEA202602060139), Feb 6, 2026: FLOOR PANEL. DELAMINATED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222AFF HAS AREA OF DELAMINATION FABRICATED NEW FLOOR PANEL 222AFF, MPN 141T5856-107, RBL11 - RBL 33, STATION 285 - 412 
- [SDR FDEA202602050134](https://openairdocs.org/sdr/FDEA202602050134), Feb 5, 2026: FLOORBOARD. DENTED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222BFF DENTED. FABRICATED NEW FLOOR PANEL MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222BFF DENTED 222BFF, MPN 141T5856- 
- [SDR FDEA202602050133](https://openairdocs.org/sdr/FDEA202602050133), Feb 5, 2026: FLOOR PANEL. DENTED. MIAN DECK CARGO COMPARTMENT, FLOOR PANEL 251LFF DENTED. JM40 FABRICATED NEW FLOOR PANEL 251LFF, MPN: 146T5869-127, LBL 11- RBL 11, STA 1208-1351 IN REF. TO BOEI
- [SDR FDEA202602050131](https://openairdocs.org/sdr/FDEA202602050131), Feb 5, 2026: FLOORBOARD. DELAMINATED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232MFF HAS AREA OF DELAMINATION. FABRICATED NEW FLOOR PANEL 232MFF, MPN: 148T5875-19 RBL 54.75- RB L 77.5, STA 654-784.
- [SDR FDEA202602050130](https://openairdocs.org/sdr/FDEA202602050130), Feb 5, 2026: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251KFF HAS PUNCTURE DAMAGE. JM39. (INCORRECT REF. AND REWORK PROCEDURE USED FOR DAMAGED AREAS.) FABRICATED NEW FLOOR PA
- [SDR FDEA202602040126](https://openairdocs.org/sdr/FDEA202602040126), Feb 4, 2026: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241WFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 241WFF, MPN: 145T5876-51, RBL 11- LBL 11, STA 1114.82-984.95 IN 
- [SDR FDEA202602040124](https://openairdocs.org/sdr/FDEA202602040124), Feb 4, 2026: FLOORBOARD. DAMAGED. FLOORBOARD 241AGF IS DAMAGED. FABRICATED NEW FLOOR PANEL 241AGF, MPN: 145T5874-31, RBL 77.50 - RBL 89.50, STA 984.95-1087 IN REF. TO BOEING DWG 145T5874-31, AND
- [SDR FDEA202602040123](https://openairdocs.org/sdr/FDEA202602040123), Feb 4, 2026: FLOOR PANEL. DAMAGED. FLOOR PANEL 242MFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 242MFF, RBL 74.25"- RBL 86.25", STA 933- 984.95 IN REF. TO BOEING DWG 145T5876-21. SEE JPF FOR ALL THE
- [SDR FDEA202602040122](https://openairdocs.org/sdr/FDEA202602040122), Feb 4, 2026: FLOORBOARD. DAMAGED. FLOORBOARD 241QFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 241QFF, LBL 77.50"- LBL 89.50", STA 933- 984.95 IN REF. TO BOEING DWG 145T5876-15. SEE JPF FOR ALL THE 
- [SDR FDEA202602040121](https://openairdocs.org/sdr/FDEA202602040121), Feb 4, 2026: FLOOR PANEL. DAMAGED. FLOORBOARD 242LFA IS DAMAGED. FABRICATED NEW FLOOR PANEL 242LFA, MPN: 145T5874-18, RBL 54.75- RBL 74.25, STA 930-972 IN REF. TO BOEING DWG 145T5874-18. SEE JPF 
- [SDR FDEA202602030115](https://openairdocs.org/sdr/FDEA202602030115), Feb 3, 2026: FLOOR PANEL. DAMAGED. FLOORBOARD 241XFF IS DAMAGED. FABRICATED FLOOR PANEL 241XFF (MPN: 145T5874-39) AT BS 9984.95- 1114.82, BETWEEN LBL11- LBL33 IN REF TO DRAWING 145T5874-39., AND 
- [SDR FDEA202601290098](https://openairdocs.org/sdr/FDEA202601290098), Jan 29, 2026: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242VFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 242VFF, MPN: 145T5874-32, RBL 84.25 - RBL 74.25, STA 984.95-1087
- [SDR FDEA202601280096](https://openairdocs.org/sdr/FDEA202601280096), Jan 28, 2026: FLOORBOARD. DENTED. FLOORBOARD 242VFF IS DAMAGED VFF SHOULD BE 242UFF. FABRICATED FLOOR PANEL 242UFF (MPN: 145T5874-34) AT STA 980.95 - STA1114.82, RBL 54.75 - RBL 74.25 IN REF TO 
- [SDR FDEA202404120457](https://openairdocs.org/sdr/FDEA202404120457), Apr 12, 2024: SKIN. DAMAGED. DURING HMV 1 AT INDY, A PRIOR LIGHTNING STRIKE WAS DISCOVERED AND ONE FASTENER LOCATION AT STA 452, ON STRINGER 30L WAS BLENDED TO 0.040 THICK FROM A 0.063 MATE
- [SDR FDEA202403290445](https://openairdocs.org/sdr/FDEA202403290445), Mar 29, 2024: SKIN. DENTED. RH OUTBD WING, #11 SLAT HAS SMALL DENT ON UPPER SURFACE. MARKED MK8 REPAIRED RH WING L/E # 11 SLAT TRAILING EDGE WEDGE TOP SURFACE AT WS OSS 856 IN REF TO 767 S
- [SDR FDEA202403290442](https://openairdocs.org/sdr/FDEA202403290442), Mar 29, 2024: FORMER. MISMANUFACTURED. R/H L/E NOSE FORMER ANGLE MALFORMED AND HAS MORE THAN .037" GAP TO LEADING EDGE SKIN. ENGINEERING CONTACTED PER SEQUENCE 708 AND RECOMMENDS REPLACEMENT.
- [SDR FDEA202403290440](https://openairdocs.org/sdr/FDEA202403290440), Mar 29, 2024: FORMER. MISALIGNED. R/H L/E NOSE FORMER ANGLE MALFORMED AND HAS MORE THAN .037" GAP TO LEADING EDGE SKIN. ENGINEERING CONTACTED PER SEQUENCE 708 AND RECOMMENDS REPLACEMENT. REF. SE
- [SDR FDEA202308241491](https://openairdocs.org/sdr/FDEA202308241491), Aug 24, 2023: SKIN. DELAMINATED. R/H I/B AILERON, LOWER SURFACE HAS SMALL AREA OF SKIN DELAMINATION NEAR I/B AFT CORNER. M.W.T. 0000553921 : DAVIES, ANDREW M - 24-AUG-2023 23:10 INSTALLED BONDE
- [SDR FDEA202108011918](https://openairdocs.org/sdr/FDEA202108011918), Aug 1, 2021: LINE. LEAKING. AFTER BLOCK IN, MX REPORTED A HYDRAULIC MIST/DRIP FROM LEFT MAIN WHEEL WELL. CRASH FIRE AND RESCUE WAS CALLED. TRACED HYDRAULIC LEAK TO BRAKE PRESSURE TUBE ASSY
- [SDR FDEA202105201320](https://openairdocs.org/sdr/FDEA202105201320), May 20, 2021: WARNING MESSAGE. FALSE ACTIVATION. FWD CARGO DOOR CAUTION ON CLIMB OUT. CHECKED FWD CARGO DOOR PROX SENSORS 150,151,152,153, AND 154 WITH BREAKOUT BOX, ALL SENSORS CHECK GOOD, READING 4.8 MH ON15
- [SDR FDEA202105201315](https://openairdocs.org/sdr/FDEA202105201315), May 20, 2021: WARNING LIGHT. FALSE ACTIVATION. FWD CARGO DOOR CAUTION ON CLIMB OUT. RAN QRH. DECLARED EMERGENCY. RELEASED FOR SERVICE PER MEL : 52-71-01-01-B CATEGORY C. INSPECTED FWD LOWER CARGO DOOR. IT WA
- [SDR FDEA202104130909](https://openairdocs.org/sdr/FDEA202104130909), Apr 13, 2021: ANGLE. CRACKED. MAIN DECK FLOOR SPLICE IS CRACKED REMOVED & REPLACED FLOOR SPLICE ANGLE IAW BAC DWG 146T5650
- [SDR FDEA202104130908](https://openairdocs.org/sdr/FDEA202104130908), Apr 13, 2021: ANGLE. CRACKED. MAIN DECK FLOOR SPLICE ANGLE IS CRACKED REMOVED & REPLACED ANGLE IAW BAC DWG 146T5650
- [SDR FDEA202104130907](https://openairdocs.org/sdr/FDEA202104130907), Apr 13, 2021: ANGLE. CRACKED. LH NOSE TUNNEL @ STA 246, LBL 50, FLOOR SUPPORT ANGLE IS CRACKED REMOVED & REPLACED ANGLE IAW BAC DWG 141T5600 SHEET 4 REV - & BAC DWG 141T5146 REV F
- [SDR FDEA202104110887](https://openairdocs.org/sdr/FDEA202104110887), Apr 11, 2021: ANGLE. CRACKED. AFT CARGO COMPARTMENT, FWD END-WALL, @ STA 1087 HAS CRACKED ATTACH ANGLE REMOVED & REPLACED ANGLE IAW BAC DWG 140T0130
- [SDR FDEA202007171555](https://openairdocs.org/sdr/FDEA202007171555), Jul 17, 2020: UNKNOWN. ODOR. DURING DECENT, BELOW 16000 FT, THERE WAS A STRONG CIGARETTE LIKE SMELL EMITTING FROM AN UNKNOWN SOURCE. NO SMOKE WAS VISIBLE. THE ODOR DISSIPATED AFTER TAXI-IN.
- [SDR FDEA2020021430335](https://openairdocs.org/sdr/FDEA2020021430335), Feb 13, 2020: BEARING. FAILED. BRAKE TEMP LT ILLUMINATED ON BLOCK IN BRAKE TEMPS WERE 23/44/22/54 FOUND THAT THE #7 BRAKE OUTER BEARING FAILED AND IMPACTING THE WHEEL/ TIRE, REPLACED THE #7 B
- [SDR FDEA202002080299](https://openairdocs.org/sdr/FDEA202002080299), Feb 8, 2020: FAULT MESSAGE. FALSE ACTIVATION. MDIS 297 34-61 3894 08FEB20 MEM FACT U. PER CREW VERBAL: DURING APPROACH A/C FULLY CONFIGURED FLAPS 30, VREF FOR THE LANDING WEIGHT OF 302.3 WAS COMPUTING 141 K
- [SDR FDEA2020021080299](https://openairdocs.org/sdr/FDEA2020021080299), Feb 8, 2020: INDICATOR. FALSE INDICATION. MDIS 297 34-61 3894 08FEB20 MEM FACT U PER CREW VERBAL: DURING APPROACH A/C FULLY CONFIGURED FLAPS 30, VREF FOR THE LANDING WEIGHT OF 302.3 WAS COMPUTING 141 KT
- [SDR FDEA201903090563](https://openairdocs.org/sdr/FDEA201903090563), Mar 9, 2019: WINDOW. ARCED. L SIDE NR 2 WINDOW OVERHEAT WITH ARCING DELAMINATION AND CRACKING. FACT 10MAR19 04:42 DEN REMOVED AND REPLACED LEFT WINDOW NR 2 REF AMM 56-11-02-4. WINDOW OPS C
- [SDR FDEA201901020008](https://openairdocs.org/sdr/FDEA201901020008), Jan 2, 2019: WHEEL. DAMAGED. NR 5 TIRE WORN. UPON REMOVAL FOUND INNER HALF OF WHEEL TO BE DAMAGED FROM CONTACTING BRAKE ASSEMBLY. REMOVED AND REPLACED NR 5 WHEEL AND TIRE ASSEMBLY. REFERENC
- [SDR FDEA2019010113625](https://openairdocs.org/sdr/FDEA2019010113625), Dec 31, 2018: BUSHING. WORN. NOTED NR 5 WHEEL INNER SURFACE APPEARS TO BE CONTACTING OUTER BRAKE SURFACE. UPON REMOVAL OF TIRE AND BRAKE ASSEMBLY, FOUND BRAKE AXLE BUSHING WORN ALLOWING CON
- [SDR FDEA201811093168](https://openairdocs.org/sdr/FDEA201811093168), Nov 9, 2018: PSEU. FAULTY. LE SLAT DISAGREE MSG RECEIVED AFTER MOVING FLAP HANDLE TO 1 ON APPROACH. COMPLIED WITH QRH PROCEDURES. REPLACED PSEU REF AMM 32-09-04-4, NO DEFECTS NOTED. PERFO
- [SDR FDEA201804070907](https://openairdocs.org/sdr/FDEA201804070907), Apr 7, 2018: SKIN. DAMAGED. RT WING INBD AFT FLAP LOWER EDGE COMPOSITE SKIN HAS MINOR DAMAGE, 51 INCHES AWAY FROM INBD END. REPAIRED THE RT WING AFT FLAP IAW SRM 51-70-10-2R, AND EA TH-575
- [SDR FDEA201803310814](https://openairdocs.org/sdr/FDEA201803310814), Mar 31, 2018: SKIN. DENTED. LEFT WING NR 4 SLAT DENTED ON THE TE WEDGE UPPER SKIN FROM OTBD BETWEEN 5 AND 8 INCHES. REPAIRED IAW SRM 51-70-10-2R, REP 2, SRM 57-43-02-02R, AND EA T-5750-T03
- [SDR FDEA201803300806](https://openairdocs.org/sdr/FDEA201803300806), Mar 30, 2018: SKIN. DENTED. LEFT WING L/E SLAT HAS DENT ON T/E WEDGE UPPER SKIN FROM INBD BETWEEN 57 & 60 INCHES. REPAIRED IAW SRM 51-70-10, REPAIR 2, SRM 57-43-02-2R, AND EA H-5750-T03391
- [SDR FDEA201803270789](https://openairdocs.org/sdr/FDEA201803270789), Mar 27, 2018: SKIN. DENTED. RIGHT WING L/E NR 10 SLAT HAS DENTS ON T/E WEDGE UPPER SKIN FROM INBD BETWEEN 62 INCHES & 71 INCHES. REPAIRED THE SLAT IAW SRM 51-70-10-2R, REPAIR 2, MAJOR REPA
- [SDR FDEA201702110524](https://openairdocs.org/sdr/FDEA201702110524), Feb 11, 2017: TIRE. OUT OF ROUND. DURING TAKEOFF ROLL, ENCOUNTERED VERY NOTICABLE SHUDDER OF UNKNOWN ORIGIN. ABORTED TAKEOFF AT 100 KTS. JACKED NOSE GEAR AND FOUND BOTH NOSE TIRES OUT OF ROUND. 
- [SDR FDEA201610013406](https://openairdocs.org/sdr/FDEA201610013406), Oct 1, 2016: SKIN. CHAFED. RT WING I/B FLAP O/B END UPPER SURFACE HAS DEEP CHAFING MARK JUST ABOVE UPPER SEAL. REPAIRED RT WING IB FLAP OB END UPPER SURFACE IAW SRM 57-53-01-2R FIG 201 AN
- [SDR FDEA201609263366](https://openairdocs.org/sdr/FDEA201609263366), Sep 26, 2016: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 1398 BETWEEN STRINGERS 34-35L. COMPLIED WITH EA H-5330-T0328464 P1. FABRICATED A REPAIR DOUBLER AND FILLER. INSTALLED REPAIR.
- [SDR FDEA201609013098](https://openairdocs.org/sdr/FDEA201609013098), Sep 1, 2016: DUCT. LOOSE. PASSING FL 220 AT 330 IAS IN CLIMB, A SUDDEN AND EXTREMELY LOUD HORN, SIREN OR WHISTLE CAME ON. LEVELED AT FL 260 AND SLOWED TO 300 KTS IAS. SOUNDS CONTINUED FO
- [SDR FDEA201608222948](https://openairdocs.org/sdr/FDEA201608222948), Aug 22, 2016: SKIN. DAMAGED. BIRD STRIKE DENTED THE LT FORWARD FUSELAGE AT STA 148.5, WL 215. DENT MEASURES 6.4" X 3.5" X 0.336". REPAIRED DAMAGE IAW SRM 53-00-01, FIG 201, TABLE 5 WHICH RE
- [SDR FDEA201608112880](https://openairdocs.org/sdr/FDEA201608112880), Aug 11, 2016: SKIN. DAMAGED. BIRD STRIKE IMPACT CAUSED DENT IN STRUCTURE APPROXIMATELY 17" AFT OF RADOME AND 8" BELOW THE LT TAT PROBE. INSPECTED IAW EA H-5310-T0327414A PERFORMED HFEC OF E

## 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 767-32LF aircraft: https://openairdocs.org/model/boeing-767-32lf/aircraft.md
- The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.md

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