# N120FE: 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: 44380
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 1, 2015
- Certificate issued: May 28, 2015
- Expires: May 31, 2028
- Mode S code: A05434
- Registered owner: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION)
- 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=120FE
- Page: https://openairdocs.org/aircraft/N120FE

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 N120FE.

## FAA accident and incident reports

None matched to N120FE.

## Service difficulty reports (18)

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 FDEA202601120024](https://openairdocs.org/sdr/FDEA202601120024), Jan 12, 2026: UNKNOWN. ODOR. AFTER LANDING IN HAN, ON TAXI IN THE COCKPIT FILLED WITH INTENSE BURNING CHEMICAL ODOR NOSE AND EYES FELT BURNING SENSATION WE DONNED OUR OXYGEN MASKS COMPLETED
- [SDR FDEA202307291333](https://openairdocs.org/sdr/FDEA202307291333), Jul 29, 2023: BEAM. WORN. #1 ENGINE INBD PYLON ACCESS PANEL (437BR) CENTER 2 HINGE FITTINGS WORN. C/W EA H-5451-T0375481 P1
- [SDR FDEA202307291332](https://openairdocs.org/sdr/FDEA202307291332), Jul 29, 2023: BEAM. WORN. #1 ENGINE OTBD PYLON ACCESS PANEL (437BL) AFT HINGE ARM WORN. BOLT IS PULLED ALMOST COMPLETELY THROUGH HINGE FITTING. REPAIRED #1 ENGINE OTBD PYLON ACCESS PANEL
- [SDR FDEA202208121973](https://openairdocs.org/sdr/FDEA202208121973), Aug 12, 2022: SKIN. WORN. LEFT WING SLAT 5 TRAILING EDGE / INNER SKIN WITH WEAR AT INBOARD AUX TRACK. LEFT WING SLAT 5 TRAILING EDGE INNER SKIN AT INBOARD AUX TRACK WAS REPAIRED IAW SRM 
- [SDR FDEA202208121972](https://openairdocs.org/sdr/FDEA202208121972), Aug 12, 2022: SKIN. DELAMINATED. LEFT WING OUTBOARD FLAP LOWER SKIN WITH DENT AT OTEF STA 333. LH WING OUTBOARD FLAP LOWER SKIN, DENT AT OTEF 333 WAS REPAIRED IAW SRM 57-53-01-2R PAG. 1 TO 9 FI
- [SDR FDEA202205021100](https://openairdocs.org/sdr/FDEA202205021100), May 2, 2022: NONE. NONE. AFTER LANDING RWY 15 PANC CLEARED RUNWAY AND COULD NOT STEER AIRCRAFT. STOPPED AIRCRAFT AND CALLED MX. MX CHECKED NOSE GEAR AND CLEARED US TO TAXI TO GATE. STEE
- [SDR FDEA202007301717](https://openairdocs.org/sdr/FDEA202007301717), Jul 30, 2020: PSEU. FAILED. LE SLAT ASYM EICAS FOLLOWING SELECTION OF FLAPS 25 FOR LANDING. COMPLIED WITH QRH AFTER GA. EMERGENCY DECLARED. TROUBLESHOT IAW FIM 27-81 FAULT TREE 809. FSEU B
- [SDR FDEA202007221623](https://openairdocs.org/sdr/FDEA202007221623), Jul 22, 2020: PSEU. FAILED. AT FL 360 GOT MC LIGHT AND AMBER EICAS ALERT "MAIN CARGO DOOR". DESCENDED TO 10,000' IAW QRH. ALERT EXTINGUISHED AFTER PRESSURE EQUALIZED DURING DESCENT. EMERGE
- [SDR FDEA2020072321623](https://openairdocs.org/sdr/FDEA2020072321623), Jul 22, 2020: WARNING LIGHT. FALSE ACTIVATION. AT FL 360 RECEIVED A MC LIGHT AND AMBER EICAS ALERT, MAIN CARGO DOOR. DESCENDED TO 10,000 FT IAW QRH. ALERT EXTINGUISHED AFTER PRESSURE EQUALIZED DURING DESCENT
- [SDR FDEA201909192287](https://openairdocs.org/sdr/FDEA201909192287), Sep 19, 2019: WEDGE. CHAFED. LEFT WING #5 SLAT T/E WEDGE LOWER SURFACE CHAFED. REPAIRED THE T/E OF THE #5 SLAT IAW 57-43-02-2R, 51-70-10 AND EA H-2780-T0349554-P1 FLIGHT CONTROL- L/E SLATS 
- [SDR FDEA201909172272](https://openairdocs.org/sdr/FDEA201909172272), Sep 17, 2019: SKIN. DENTED. RIGHT WING I/B MAIN FLAP LOWER SURFACE HAS A DENT. REPAIRED RW I/B MAIN FLAP LOWER SURFACE IAW SRM 57-53-01-1A AND 51-70-10-1R AND EA H- 2750-T0349512 FLIGHT CO
- [SDR FDEA201810042788](https://openairdocs.org/sdr/FDEA201810042788), Oct 4, 2018: BEAM. DAMAGED. DURING L/H ENGINE CHANGE, FOUND DAMAGE TO OUTBOARD LATCHBEAM AT FORWARD NUTPLATE. REPAIRED OTBD BEAM REF EA #: H-5450-T0342766 PT 1
- [SDR FDEA201810042787](https://openairdocs.org/sdr/FDEA201810042787), Oct 4, 2018: BEAM. DAMAGED. DURING LT ENG CHANGE, FOUND DAMAGE TO INBOARD LATCHBEAM AT FORWARD NUTPLATE. REPAIRED DAMAGE AT NOTED LOCATION IAW EA H-5450-T0342766 PART 2.
- [SDR FDEA2018100542788](https://openairdocs.org/sdr/FDEA2018100542788), Oct 4, 2018: BEAM. DAMAGED. MDIS 120 54-50 3684 04OCT18 MEM OPEN U DURING LT ENGINE CHANGE, FOUND DAMAGE TO OUTBOARD LATCH BEAM AT FORWARD NUTPLATE. PART 04OCT18 10:01 MEM U IDENTIFIED PAR
- [SDR FDEA201710142961](https://openairdocs.org/sdr/FDEA201710142961), Oct 14, 2017: SENSOR. OUT OF ADJUST. WHILE CRUISING AT FL360 MAIN CARGO DOOR EICAS ILLUMINATED, FOLLOWED QRH BEGAN DESCENT TO 10,000FT, AT 21,000 LIGHT EXTINGUISHED. REMOVED SHIMS FROM SENSOR S-891
- [SDR FDEA201607052278](https://openairdocs.org/sdr/FDEA201607052278), Jul 5, 2016: COMPUTER. MALFUNCTIONED. ON DEPARTURE AFTER RT AUTOPILOT WAS ENGAGED FOR A FEW SECONDS. ACFT MADE A RAPID ROLL TO THE RT AND A/P DISENGAGED. ATTEMPTED TO ENGAGED A/P SECOND TIME WITH SA
- [SDR FDEA201605211705](https://openairdocs.org/sdr/FDEA201605211705), May 21, 2016: SMOKE WARNING. FALSE ACTIVATION. DURING CLIMB TOILET SMOKE ALARM ACTIVATED TWICE FOR ABOUT 10 SECONDS EACH TIME. INSPECTED LAVATORY, NO TROUBLE FOUND. PERFORMED TEST OF LAVATORY DETECTION SYS I
- [SDR FDEA201510143212](https://openairdocs.org/sdr/FDEA201510143212), Oct 14, 2015: RELAY. MALFUNCTIONED. CAPTAINS LDS DISPLAY WENT BLACK ON 10 MILE FINAL, CAME BACK ON AFTER ONE MINUTE. AFTER REPLACEMENT OF RELAY & CB. PERFORMED OPERATIONAL CHECK & RTS OF CAPTAIN'S

## 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 N120FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N120FE before.

- [Cancelled 2003-01-15](https://openairdocs.org/deregistered/N120FE-2003-01-15): Boeing 727-25C, S/N 19356, built 1966. Second triennial mailing, no response. Owner: [Rfc N120fe/9 Inc](https://openairdocs.org/faa-owner/RFC%20N120FE%2F9%20INC), [Cheyenne, WY](https://openairdocs.org/faa-place/WY/Cheyenne)

## 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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