# N130FE: 2016 Boeing 767-3S2F

- Status: Valid registration
- Airframe: [Boeing 767-3S2F](https://openairdocs.org/model/boeing-767-3s2f) (registry code 138513F, 6 seats)
- Engine: [GE CF6-80C2B6F](https://openairdocs.org/engine/ge-cf6-80c2b6f) (registry code 30109)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 42720
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 17, 2016
- Certificate issued: March 19, 2016
- Expires: March 31, 2029
- Mode S code: A07BB3
- 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=130FE
- Page: https://openairdocs.org/aircraft/N130FE

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 N130FE.

## FAA accident and incident reports

None matched to N130FE.

## Service difficulty reports (32)

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 FDEA202603060324](https://openairdocs.org/sdr/FDEA202603060324), Mar 6, 2026: SKIN. DENTED. DENT ON LOWER SURFACE OF LT OTBD FLAP, LOCATED AT 39.5" FROM INBOARD EDGE AND 2.5" FROM AFT EDGE. LT OTBD FLAP LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R, R
- [SDR FDEA202603010302](https://openairdocs.org/sdr/FDEA202603010302), Mar 1, 2026: WEDGE. WORN. WEAR IN WEDGE TRAILING EDGE LOWER SURFACE AT 33.75 INCHES OF INBD END ON SLAT NR 4, LT WING. WEAR IN WEDGE T/E LOWER SURFACE AT 33.75 INCHES OF INBD EDGE WAS RE
- [SDR FDEA202603010301](https://openairdocs.org/sdr/FDEA202603010301), Mar 1, 2026: WEDGE. WORN. WEAR IN WEDGE TRAILING EDGE LOWER SURFACE AT 30" OF INBD END ON SLAT NR 5, LT WING. LT WING, SLAT NR 5 TRAILING EDGE WEDGE LOWER SURFACE AT 30" OF INBD END EDGE
- [SDR FDEA202602240277](https://openairdocs.org/sdr/FDEA202602240277), Feb 24, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 231NFF MDC FLOOR PANEL 231NFF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.
- [SDR FDEA202602240276](https://openairdocs.org/sdr/FDEA202602240276), Feb 24, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 231QFF MDC FLOOR PANEL 231QFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.
- [SDR FDEA202602240275](https://openairdocs.org/sdr/FDEA202602240275), Feb 24, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 251QFF MDC FLOOR PANEL 251QFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.
- [SDR FDEA202602230270](https://openairdocs.org/sdr/FDEA202602230270), Feb 23, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 241LFF MDC FLOOR PANEL 241LFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15/2025
- [SDR FDEA202602230269](https://openairdocs.org/sdr/FDEA202602230269), Feb 23, 2026: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 251DFF MDC FLOOR PANEL 251DFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15/2025
- [SDR FDEA202506271070](https://openairdocs.org/sdr/FDEA202506271070), Jun 27, 2025: BULB. INOPERATIVE. UPON SELECTING GEAR DOWN HAD NO GREEN LIGHT FOR NOSE GEAR. RAN QRH & DETERMINED IT WAS BULB & REPLACED BULBS. NORMAL GEAR EXTENSION THEREAFTER. NORMAL INDICATIO
- [SDR FDEA202406170810](https://openairdocs.org/sdr/FDEA202406170810), Jun 17, 2024: BULB. FAILED. ON APPROACH, AT GEAR EXTENSION, THE RT MLG DID NOT INDICATE SAFE (NO GREEN LIGHTS). THERE WAS NO EICAS OR GEAR DISAGREE LIGHT. BULBS TESTED GOOD. AFTER RETRACTI
- [SDR FDEA202403080263](https://openairdocs.org/sdr/FDEA202403080263), Mar 8, 2024: SUPPORT ANGLE. CRACKED. [UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, LBL 78, "I" BEAM REINFOR
- [SDR FDEA202403050249](https://openairdocs.org/sdr/FDEA202403050249), Mar 5, 2024: ANGLE. CRACKED. MAIN CARGO DECK, AT STA. 1582 LBL 78, HAS ANGLE BRACKET (P/N 146T5651-5) CRACKED REMOVED AND REPLACE ANGLE BRACKET P/N 146T5651-5 PER BOEING DWG 146T5651 AND SR
- [SDR FDEA202402260266](https://openairdocs.org/sdr/FDEA202402260266), Feb 26, 2024: SUPPORT BEAM. CRACKED. UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORC
- [SDR FDEA202402260265](https://openairdocs.org/sdr/FDEA202402260265), Feb 26, 2024: SUPPORT BEAM. CRACKED. UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, LBL 78, "I" BEAM REINFORC
- [SDR FDEA202402260243](https://openairdocs.org/sdr/FDEA202402260243), Feb 26, 2024: SUPPORT ANGLE. CRACKED. UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORC
- [SDR FDEA202402250258](https://openairdocs.org/sdr/FDEA202402250258), Feb 25, 2024: BRACKET. CRACKED. LH WING L/E BRACKET CRACKED, VIEWED INSIDE LIGHTNING HOLE AT APPROX WING STATION 510 (BETWEEN #5 SLAT OUTBD SIDE AND #5 SLAT OUTBD AUX TRACK). MARKED WITH ORANG
- [SDR FDEA202402250257](https://openairdocs.org/sdr/FDEA202402250257), Feb 25, 2024: BRACKET. CRACKED. RH WING L/E BRACKET CRACKED, VIEWED INSIDE LIGHTNING HOLE AT APPROX WING STATION 510 (BETWEEN #8 SLAT OUTBD SIDE AND #8 SLAT OUTBD AUX TRACK). MARKED WITH ORANG
- [SDR FDEA202402250241](https://openairdocs.org/sdr/FDEA202402250241), Feb 25, 2024: SHEAR TIE. CRACKED. #2 PYLON AFT TORQUE BOX BULKHEAD INBOARD SHEAR TIE CRACKED. REMOVE AND REPLACED SHEAR TIE (313T3310-1155) USING 767 SRM REFERENCE 51-40-02-0G AND IPC 54-51-53-1
- [SDR FDEA202402220267](https://openairdocs.org/sdr/FDEA202402220267), Feb 22, 2024: SUPPORT BEAM. CRACKED. UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORC
- [SDR FDEA202402220264](https://openairdocs.org/sdr/FDEA202402220264), Feb 22, 2024: SUPPORT ANGLE. CRACKED. UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORC
- [SDR FDEA202308111397](https://openairdocs.org/sdr/FDEA202308111397), Aug 11, 2023: FORMER. FAILED. NOSE FORMER ANGLE AT OSS 499.6 ON THE LEFT WING FIXED LEADING EDGE IS CRACKED. REMOVED THE BROKEN NOSE FORMER ANGLE AT OSS 499.6 ON THE LEFT WING FIXED LEADING 
- [SDR FDEA202011132839](https://openairdocs.org/sdr/FDEA202011132839), Nov 13, 2020: SKIN. GOUGED. NR 2 ENGINE INBOARD CORE COWL INNER SIDE NR 2 FRAME FROM FWD END IS GOUGED. REPAIRED NR 2 ENGINE INBOARD CORE COWL NR 2 FRAME, IAW B767 SRM 54-45-01-2R REPAIR 3
- [SDR FDEA202011112827](https://openairdocs.org/sdr/FDEA202011112827), Nov 11, 2020: BEAM. DAMAGED. NR 2 PYLON INBOARD LATCH BEAM MISSING NUTPLATE. REMOVED NR 2 PYLON INBOARD LATCH BEAM, IAW B767 SRM 54-52-71-2R. REPAIRED LATCH BEAM, IAW B767-SRM 54-52-71-2R. 
- [SDR FDEA202011052783](https://openairdocs.org/sdr/FDEA202011052783), Nov 5, 2020: BRACKET. CRACKED. RIGHT WING NR 7 SLAT DRIVESHAFT LOOP BRACKET CRACKED, STREAMER ATTACHED. REMOVED AND REPLACED LOOP BRACKET, PER B767 SRM 51-40-02 AND BOEING DWG 114T1240 REV E.
- [SDR FDEA202011052782](https://openairdocs.org/sdr/FDEA202011052782), Nov 5, 2020: BRACKET. CRACKED. LEFT WING LES 284 SLAT DRIVESHAFT LOOP BRACKET CRACKED, STREAMER ATTACHED. REMOVED AND REPLACED LOOP BRACKET, PER B767 SRM 51-40-02 AND BOEING DWG 114T1240 REV 
- [SDR FDEA202007291700](https://openairdocs.org/sdr/FDEA202007291700), Jul 29, 2020: FLAP SYSTEM. MALFUNCTIONED. ON APPROACH, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MSG & TRAILING EDGE LIGHT. COMPLETED THE QRH, TE FLAP ASYMMETRY CHECK LIST & USED ALT
- [SDR FDEA2020080329699](https://openairdocs.org/sdr/FDEA2020080329699), Jul 29, 2020: WARNING MESSAGE. FALSE ACTIVATION. ON APPROACH, AT 7000 FT, 210KTS, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MESSAGE AND TRAILING EDGE LIGHT. COMPLETED THE QRH TRAILING EDGE 
- [SDR FDEA2020073091699](https://openairdocs.org/sdr/FDEA2020073091699), Jul 29, 2020: FLAP SYSTEM. MALFUNCTIONED. DURING APPROACH, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MESSAGE AND TRAILING EDGE LIGHT. COMPLETED THE QRH, T/E FLAP ASYMMETRY CHECK LIST
- [SDR FDEA2020060111104](https://openairdocs.org/sdr/FDEA2020060111104), May 31, 2020: MOTOR. FAILED. LEVEL AT FL340 GOT A CABIN ALT WARNING. CABIN ALTITUDE WAS JUST ABOVE 10,00 FT. STARTED AN EMERGENCY DESCENT. WHILE IN DESCENT GOT CABIN ALT AUTO 1 INOPERATIVE 
- [SDR FDEA2020042730778](https://openairdocs.org/sdr/FDEA2020042730778), Apr 23, 2020: WARNING SYSTEM. FALSE ACTIVATION. TE FLAP DISAGREE LANDING MOVING FROM 1 TO 5 OPERATED FLAPS IN ALTN, NO FAULTS NO DISAGREE. OPERATED FLAPS NORAMLLY WITH ALL CENTER PUMPS ON (WITH ACMP ON) NO FA
- [SDR FDEA201901120103](https://openairdocs.org/sdr/FDEA201901120103), Jan 12, 2019: EVA SYSTEM. INOPERATIVE. WHILE C\W EA H-2560-E0324416 FOUND PILOTS(L\H) EVAS LIGHTS INOP\UNSEEABLE. REMOVED AND REPLACED CAPT EVAS, OPS CHECK GOOD. NOMENCLATURE - EMERGENCY VISION ASSUR
- [SDR FDEA201901110093](https://openairdocs.org/sdr/FDEA201901110093), Jan 11, 2019: LIGHT. INOPERATIVE. PDIS 130 33-50 2856 11JAN19 BWI FACT U LOGPAGES:3045527 EMERG LIGHTS DISARM LIGHT ON OVERHEAD PANEL INOP. MEL 11JAN19 13:09 BWI U RELEASED FOR SERVICE PER MEL :

## Service difficulty reports on N130FE not matched to an aircraft (1)

They name N130FE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 96FDEA00710](https://openairdocs.org/sdr/96FDEA00710), Mar 19, 1996: SKIN LAP. CORROSION. UPPER LOBE, CORROSION IN SKIN LAP FS 420 TO 440 BETWEEN STR 5 TO 6L. CORROSION REMOVED PER SRM 51-10-6, REPAIR INSTALLED PER SRM 51-40-2 PAGES 1 TO 6.

## 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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