# N107FE: 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: 44377
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 24, 2014
- Certificate issued: October 9, 2014
- Expires: October 31, 2027
- Mode S code: A01F37
- 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=107FE
- Page: https://openairdocs.org/aircraft/N107FE

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 N107FE.

## FAA accident and incident reports

None matched to N107FE.

## Service difficulty reports (22)

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 FDEA202512152255](https://openairdocs.org/sdr/FDEA202512152255), Dec 15, 2025: CLOSEOUT PANEL. DAMAGED. LEFT WING NR 4 SLAT, SLAT TAB AT OTBD MAIN TRACK HAS MATERIAL MISSING AROUND FASTNER. REPAIRED THE LT WING NR 4 SLAT OTBD CLOSEOUT PANEL AT OSS 607.24 - 682.74 
- [SDR FDEA202512152254](https://openairdocs.org/sdr/FDEA202512152254), Dec 15, 2025: CLOSEOUT PANEL. DAMAGED. LEFT WING NR 4 SLAT, SLAT TAB AT INBD MAIN TRACK HAS MATERIAL MISSING AROUND FASTNER. REPAIRED THE LT WING NR 4 INBD SLAT CLOSE OUT PANEL AT OSS 531.75 - 607.24
- [SDR FDEA202512152253](https://openairdocs.org/sdr/FDEA202512152253), Dec 15, 2025: CLOSEOUT PANEL. DAMAGED. LEFT WING NR 3 SLAT, SLAT TAB AT INBD MAIN TRACK HAS MATERIAL MISSING AROUND FASTNER. REPAIRED THE LT WING NR 3 SLAT CLOSE OUT PANEL AT OSS 682.74 - 782.74 IAW 
- [SDR FDEA202512152252](https://openairdocs.org/sdr/FDEA202512152252), Dec 15, 2025: CLOSEOUT PANEL. DAMAGED. LEFT WING NR 2 SLAT, SLAT TAB AT OTBD MAIN TRACK HAS MATERIAL MISSING AROUND FASTNER. REPAIRED THE LT WING NR 2 SLAT OTBD CLOSEOUT PANEL AT OSS 909.23 - 984.73 
- [SDR FDEA202512132248](https://openairdocs.org/sdr/FDEA202512132248), Dec 13, 2025: SKIN. DELAMINATED. LH WING #2 SLAT, SLAT TAB AT I/B MAIN TRACK HAS MATERIAL MISSING AROUND FASTNER. REPAIRED L/H WING # 2 SLAT TAB ON I/B CLOSE OUT PANEL AT STA 906.2-934.2 IN REF
- [SDR FDEA202512112235](https://openairdocs.org/sdr/FDEA202512112235), Dec 11, 2025: FLOOR PANEL. DENTED. MAIN DECK CARGO BAY FLOOR PANEL 232SFF HAS SEVERAL DENTS. FABRICATED A FLOOR PANEL 232SFF, RBL 77.5 - 77.5, BS 687 - 764 IAW DWG 143T5876-28, AND SR67-53-009. M
- [SDR FDEA202512112233](https://openairdocs.org/sdr/FDEA202512112233), Dec 11, 2025: FLOORBOARD. DENTED. MAIN DECK CARGO BAY FLOOR PANEL 242UFF HAD SEVERAL DENTS. REPAIRED THE FLOOR PANEL 242UFF, RBL 74.25 - 54.75, BS 984.95 - 1114.82 IAW SRM 53-00-50-2R, FIG 201, 
- [SDR FDEA202512112232](https://openairdocs.org/sdr/FDEA202512112232), Dec 11, 2025: FLOORBOARD. DENTED. MAIN DECK CARGO COMPARTMENT, LEFT FLOOR PANEL 251DFF HAS SEVERAL DENTS. REPAIRED THE FLOOR PANEL 251DFF, LBL 77.50 - 54.75, BS 1114.82 - 1197 22. IAW SRM 53-00-
- [SDR FDEA202512112231](https://openairdocs.org/sdr/FDEA202512112231), Dec 11, 2025: FLOORBOARD. PUNCTURED. MAIN DECK CARGO BAY FLOOR PANEL 221DFF HAD PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 221DFF, LBL 11 - 33, BS 285 - 392 IAW DWG 141T5856-108 & SR67-53-009. MAJ
- [SDR FDEA202512102228](https://openairdocs.org/sdr/FDEA202512102228), Dec 10, 2025: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232NFF GOUGED. REPAIRED MAIN DECK FLOOR PANEL 232NFF RBL 77.5 - 77.5, BS 654 + 22 INCHES, IAW SRM 53-00-50-2R. MAJOR RE
- [SDR FDEA202512102227](https://openairdocs.org/sdr/FDEA202512102227), Dec 10, 2025: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT, LT FLOOR PANEL 231NFF HAS SEVERAL DENTS. REPAIRED MAINDECK FLOOR PANEL 231NFF LBL 33 - 54.75, BS 654, 22 INCHES IAW SRM 53-00-50-2R
- [SDR FDEA202512102226](https://openairdocs.org/sdr/FDEA202512102226), Dec 10, 2025: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT, LT FLOOR PANEL 231PFF HAS PUNCTURE DAMAGE. REPAIRED MAIN DECK FLOOR PANEL 231PFF AT BS 654 22, LBL 54.75 - 77.5 IAW SRM 53-00-50-2R
- [SDR FDEA202412091788](https://openairdocs.org/sdr/FDEA202412091788), Dec 9, 2024: AOA. FAILED. PASSING FL 200 THE ALT DISAGREE EICAS MESSAGE ALONG WITH THE AURAL ALERT ACTIVATED MOMENTARILY AND THE AGAIN PASSING FL 220. FOLLOWED QRH. EICAS MESSAGE EXTINGU
- [SDR FDEA202407151014](https://openairdocs.org/sdr/FDEA202407151014), Jul 15, 2024: CIRCUIT CARD. FAILED. FIRE WARNING BELL CAME ON AT ROTATION. NO OTHER INDICATIONS. BELL WILL NOT SILENCE EVEN AFTER BLOCK IN AND ENGINES SHUTDOWN. MDIS 31-50 1103. REF. FIM 31-51 TAS
- [SDR FDEA202206051377](https://openairdocs.org/sdr/FDEA202206051377), Jun 5, 2022: SEAT TRACK. DAMAGED. MAIN DECK FLOOR SEAT TRACK DAMAGED AT STA610 10, RBL11. REPAIRED THE MAIN DECK DAMAGED FLOOR SEAT TRACK PER B767 SRM53-00-52-2R REPAIR 9 & EA H-5310-T0368785 P1
- [SDR FDEA202009092157](https://openairdocs.org/sdr/FDEA202009092157), Sep 9, 2020: CONNECTOR. DIRTY. PDIS 107, 29-11, 6407, 09SEP20, PEN, FACT, U. WHEN LEVELING AT FL 240 C HYD SYS PRESS LIGHT ILLUMINATED, COMPLIED WITH QRH PROCEDURE. FACT 09SEP20 14:00 PEN U. 
- [SDR FDEA202008282050](https://openairdocs.org/sdr/FDEA202008282050), Aug 28, 2020: SKIN. GOUGED. FUSELAGE, FWD LOWER FUSELAGE SKIN AT STATION 773 STRINGER 36 LT FOUND WITH EXISTING BLEND OUT WITH GOUGE MARK. FWD LOWER FUSELAGE SKIN AT STATION 773 STRINGER 3
- [SDR FDEA202008262032](https://openairdocs.org/sdr/FDEA202008262032), Aug 26, 2020: SKIN. DAMAGED. FUSELAGE, FORWARD LOWER FUSELAGE SKIN AT STATION 478, STRINGER 35 LEFT FOUND WITH EXISTING BLEND OUT. FWD LOWER FUSELAGE SKIN AT STATION 478 STRINGER 35 LEFT EX
- [SDR FDEA202008262030](https://openairdocs.org/sdr/FDEA202008262030), Aug 26, 2020: SKIN. DAMAGED. FUSELAGE, FWD LOWER FUSELAGE AT STATION 325, STRINGER 34 LT FOUND WITH EXISTING BLENDOUT. FWD LOWER FUSELAGE SKIN AT STATION 325 STRINGER 34 LT EXISTING BLENDOU
- [SDR FDEA202008262027](https://openairdocs.org/sdr/FDEA202008262027), Aug 26, 2020: SKIN. DAMAGED. FUSELAGE - RIGHT HAND LOWER FUSELAGE AT STATION 390, BETWEEN STRINGER 29 RIGHT TO 30 RIGHT FOUND WITH EXISTING BLEND OUT. RIGHT HAND LOWER FUSELAGE SKIN AT STAT
- [SDR FDEA2019112203017](https://openairdocs.org/sdr/FDEA2019112203017), Nov 20, 2019: WARNING MESSAGE. FALSE ACTIVATION. PDIS 107 27-50 5327 20NOV19 CRK FACT U LOGPAGES:3138465 AFTER SELECTING FLAPS 30 TE FLAP ASSYM ON EICAS, COMPLIED WITH QRH. FACT 20NOV19 23:26 CRK U FOLLOW FIM 
- [SDR FDEA201811023088](https://openairdocs.org/sdr/FDEA201811023088), Nov 2, 2018: CARABINER. MISSING. ON SVC CHK FOUND RIGHT AND CENTER JUMP/SUPERNUMERARY SEAT MISSING CARABINERS 4 EA. A/C OK FOR SVC. JUMPSEAT ESCAPE HARNESS OBS MPN A657C30 CPN 2526711 QTY 4 CAR

## 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 N107FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N107FE before.

- [Cancelled 2006-08-10](https://openairdocs.org/deregistered/N107FE-2006-08-10): Boeing 727-22C, S/N 19202, built 1967. Triennial form not returned. Owner: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)

## 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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