# N106FE: 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: 42709
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 3, 2014
- Certificate issued: September 18, 2014
- Expires: September 30, 2027
- Mode S code: A01B80
- 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=106FE
- Page: https://openairdocs.org/aircraft/N106FE

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 N106FE.

## FAA accident and incident reports

None matched to N106FE.

## Service difficulty reports (17)

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 FDEA202601190069](https://openairdocs.org/sdr/FDEA202601190069), Jan 19, 2026: WEB. DENTED. FLIGHT DECK, BS 246, LBL 26 DAMAGED ON WEB. REPAIRED FLOORBEAM WEB BS 246 REF EA H-5310-TO386201 ALONG WITH SRM 51-20- 01-0G, SRM 51-40-02-0G, SRM 51-70-13-0G, 
- [SDR FDEA202505050715](https://openairdocs.org/sdr/FDEA202505050715), May 5, 2025: COVER. DEFORMED. DURING POST FLIGHT CHECK FOUND L1 DOOR ESCAPE ROPE RETAINER COVER WAS DEFORMED. AMM 25-61-04-8 L1 DOOR ESCAPE ROPE RETAINER DEFORMED AMM: 25-61-04-8 ITEM IS TRA
- [SDR FDEA202505050714](https://openairdocs.org/sdr/FDEA202505050714), May 5, 2025: HOOK AND LOOP. WORN. ON ARRIVAL, CREW ENTRY DOOR UNABLE TO FULLY OPEN DUE TO ESCAPE ROPE DROP DOWN & ENTANGLE THE DOOR. AMM: 25-59-03-4 AMM: 25-61-04-402-014-001 NOTICED FEW VELCRO 
- [SDR FDEA202409121314](https://openairdocs.org/sdr/FDEA202409121314), Sep 12, 2024: RETAINER. DAMAGED. CREW REPORTED, L1 DOOR ESCAPE ROPE RETAINER DEFORMED AMM 25-61-04-8. L1 DOOR ESCAPE ROPE RETAINER DEFORMED AND SEALED WITH CARGO PIT TAPE. PERFORMED GVI ON THE 
- [SDR FDEA202312191948](https://openairdocs.org/sdr/FDEA202312191948), Dec 19, 2023: FSEU. FAILED. ON FINAL APPROACH INTO CAN WHEN SELECTING FLAPS 25 RECEIVED A LEADING EDGE, SLAT DISAGREE EICAS MESSAGE. EXECUTED MISSED APPROACH AND PERFORMED QRH PROCEDURE. U
- [SDR FDEA202304140647](https://openairdocs.org/sdr/FDEA202304140647), Apr 14, 2023: WHEEL. DAMAGED. ON TAKEOFF ROLL LOTS OF VIBRATION ABOVE 130. ON LANDING ROLL ABOVE 130 SAME VIBRATION. ON POSTFLIGHT MECHANIC SAID WE HAD #6 TIRE HAD BLOWN. NO STATUS MESSAGES 
- [SDR FDEA202304030546](https://openairdocs.org/sdr/FDEA202304030546), Apr 3, 2023: SEAT TRACK. DAMAGED. MEL 25-58-01-A MDC RESTRAINT ID503 INOP / SEAT TRACK DAMAGE. REPAIRED THE MAIN DECK CARGO DAMAGED SEAT TRACK PER B767 SRM53-00-52-2R REPAIR 9. THIS IS CATEGORY 
- [SDR FDEA202209032170](https://openairdocs.org/sdr/FDEA202209032170), Sep 3, 2022: RELAY. FAULTED. UPON SELECTION OF FLAPS 1 ON ARRIVAL INTO CAN . LEADING EDGE SLAT DISAGREE EICAS.COMPLETED QRH 9.1.11"LEADING EDGE SLAT DISAGREE"DECLARED EMGERGENCY ,LANDED NOR
- [SDR FDEA202203070435](https://openairdocs.org/sdr/FDEA202203070435), Mar 7, 2022: ENGINE. LEAKING. PDIS 106 79-01 8034 07MAR22 PEN OPEN U LOGPAGES:2996686 RT ENGINE SHUTDOWN ON CLIMB-OUT DUE TO HIGH OIL TEMPERATURE, AS DIRECTED BY THE QRH. THIS WAS ACCOMPANIE
- [SDR FDEA202203070434](https://openairdocs.org/sdr/FDEA202203070434), Mar 7, 2022: ENGINE. UNKNOWN. PDIS 106 79-01 8034 07MAR22 PEN OPEN U LOGPAGES:2996686 RT ENGINE SHUTDOWN ON CLIMB-OUT DUE TO HIGH OIL TEMPERATURE, AS DIRECTED BY THE QRH. THIS WAS ACCOMPANIE
- [SDR FDEA202104130915](https://openairdocs.org/sdr/FDEA202104130915), Apr 13, 2021: CONTROL PANEL. INOPERATIVE. MDIS 106 33-50 7029 13APR21 MEM FACT U EMERGENCY LIGHT PANEL "UNARMED" LIGHT IS INOP. FACT 13APR21 19:03 MEM U RELAMPED PER B767 AMM 33-16-02-2 , NO HELP, IF YO
- [SDR FDEA2018110213080](https://openairdocs.org/sdr/FDEA2018110213080), Nov 1, 2018: DISPLAY. MALFUNCTIONED. AFTER TAKEOFF, FO MCDU FROZE ON THE LEGS PAGE. MCDU FROZE ON THE T/O PAGE, COULD NOT MANIPULATE ANY FMS FUNCTIONS ON EITHER. NO CIRCUIT BREAKERS TRIPPED. NO EIC
- [SDR FDEA201810202959](https://openairdocs.org/sdr/FDEA201810202959), Oct 20, 2018: CARABINER. MISSING. FOUND RIGHT JUMP/SUPERNUMERARY SEAT MISSING CARABINER/D- RING 1 EA. REINSTALLED THE D RING OF THE ESCAPE HARNESSES AS PER AMM 22-61-03-2. CHECKED NORMAL.
- [SDR FDEA201705201467](https://openairdocs.org/sdr/FDEA201705201467), May 20, 2017: SEAL. FAILED. AT FL 350 FIRST OFFICER HEARD A POP, FOLLOWED BY A HISS OF AIRFLOW ON AFT SEAL OF THE R2 WINDOW . NO FLUCTUATIONS IN PRESSURIZATION OR RATE ON PRESSURIZATION PA
- [SDR FDEA201602040456](https://openairdocs.org/sdr/FDEA201602040456), Feb 4, 2016: SLAT. CRACKED. NUMBER 5 SLAT HAS CRACK ON LOWER TE AT THE TELESCOPE DUCT. REPAIRED CRACK IAW SRM 57-43-01-2R FIG 201 TABLE 1 AND SRM 51-70-17 PAR 4 AND FIG 5 PG 38. ADJUSTED T
- [SDR FDEA201602010420](https://openairdocs.org/sdr/FDEA201602010420), Feb 1, 2016: LINE. CHAFED. RIGHT WING LE FIRE SUPPRESSION LINE WS 321, FOUND CHAFED THROUGH FROM SLAT TORQUE TUBE COUPLING NOT SECURED, MISSING BOLTS TO SECURE THE COUPLING. REF N00060, N
- [SDR FDEA201602010412](https://openairdocs.org/sdr/FDEA201602010412), Feb 1, 2016: SKIN. DAMAGED. RIGHT WING INBD MAIN FLAP, OTBD END HAS COMPOSITE MATERIAL EXPOSED, COMPLIED WITH EA H 5750-T0323058. RT INBD MAIN FLAP - SKIN REPAIR - RSC. REPAIRED MAIN FLAP 

## STCs that may be installed (OpenAirDocs) (5)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (GE CF6-80C2B6F)

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic
- [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series
- [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc
- [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc. Lists CF6-80 Series

## Earlier aircraft with N106FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N106FE before.

- [Cancelled 2013-01-08](https://openairdocs.org/deregistered/N106FE-2013-01-08): Boeing 727-22C, S/N 19201, built 1967. Sale reported. Owner: [Everett, WA](https://openairdocs.org/faa-place/WA/Everett)

## 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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