# N101FE: 2013 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: 42706
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 30, 2013
- Certificate issued: September 30, 2013
- Expires: September 30, 2029
- Mode S code: A008ED
- 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=101FE
- Page: https://openairdocs.org/aircraft/N101FE

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 N101FE.

## FAA accident and incident reports

None matched to N101FE.

## Service difficulty reports (20)

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 FDEA202606250827](https://openairdocs.org/sdr/FDEA202606250827), Jun 25, 2026: ELEC CONNECTOR. DAMAGED. FSS DISPLAY SHOWS UNARMED STATUS WHILE INFLIGHT. AMM: 26-90-03-2 EA: H-2624-T0387831 C/W E.A. H-2624-T0387831 TO RE-PIN D2166D PIN G8 TO F8. REACTIVATED FSS SYS
- [SDR FDEA202411291753](https://openairdocs.org/sdr/FDEA202411291753), Nov 29, 2024: FITTING. GOUGED. #1 ENG WERE OB SHEAR TIE (FWD OF SKIRT BEAM) HAS CHAFFED INTO THE FWD BULKHEAD OF TORQUE BOX. DURING CURRENT HMV CHECK IN INDIANAPOLIS, IN (IND), MAINTENANCE DI
- [SDR FDEA202411291752](https://openairdocs.org/sdr/FDEA202411291752), Nov 29, 2024: FLOORBEAM. DAMAGED. FOUND 2ND FROM THE BOTTOM IN WEB, WHERE STIFFENER ATTACHES AT STA. 246 LBL 24 HOLE DAMAGED, DAMAGE REMOVAL AT LBL 24 HOLE IS CURRENTLY 0.359" IN WEB MADE OF 0.0
- [SDR FDEA202411271750](https://openairdocs.org/sdr/FDEA202411271750), Nov 27, 2024: DOOR. DELAMINATED. RH PYLON PNL# 447BL FOUND WITH MISSING TOP FIBERGLASS SKIN PLYS MISSING AND PAINTED OVER. REPAIRED TOP SKIN ON RH PYLON (PNL#447BL/MPN: 313T3341-9110) IN REF. T
- [SDR FDEA202411251731](https://openairdocs.org/sdr/FDEA202411251731), Nov 25, 2024: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT POSITION 12L APROX STA. 1383, FLOORBOARD ON LEFT SIDE HAS 1 PUNCTURE. MARKED WITH DOT #58. REPAIRED FLOORBOARD MAIN CARGO COMPARTMENT PAN
- [SDR FDEA202411251730](https://openairdocs.org/sdr/FDEA202411251730), Nov 25, 2024: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT, CENTER FLOORBOARD BETWEEN POSITION 6 AND 7 HAS 3 EA PUNCTURES. MARKED WITH DOT #'S 55, 56, AND 57. REPAIRED FLOORBOARD MAIN CARGO COMPAR
- [SDR FDEA202408061091](https://openairdocs.org/sdr/FDEA202408061091), Aug 6, 2024: WARNING LIGHT. ILLUMINATED. MAIN CARGO DOOR EICAS MESSAGE AND CARGO DOORS LIGHT ILLUMINATED AT CRUISE FL350 TIME 0051Z. ALSO HAD RISING CABIN PRESSURE. RAN QRH AND DESCENDED TO 10,000 FEET
- [SDR FDEA202305120861](https://openairdocs.org/sdr/FDEA202305120861), May 12, 2023: SKIN. BURNED. FUSELAGE SKIN EXTERNAL SURFACE FOUND 4EA LIGHTNING STRIKES AT STA544- STA566 STGR38L- STGR39R REPAIRED THE FUSELAGE SKIN EXTERNAL SURFACE 4EA LIGHTNING STRIKES 
- [SDR FDEA202210192611](https://openairdocs.org/sdr/FDEA202210192611), Oct 19, 2022: APU. INOPERATIVE. APU SHUTDOWN- FAULT LIGHT AFTER T.O. APPROXIMATELY 2000 FEET. APU IS REQUIRED PER MEL 24-00-01-01-B. ATTEMPT RESTART AS PER QRH. RESTART SUCCESSFUL. ON ARRIVAL 
- [SDR FDEA202106131521](https://openairdocs.org/sdr/FDEA202106131521), Jun 13, 2021: SKIN. CRACKED. .RH WING OUTBOARD TRAILING EDGE FLAP NOSE SKIN CRACKED , LOC:APPROX 120CM FROM INBD EDGE TO OUTBD EDGE. PERFORMED THE REPAIR ON RH WING OUTBOARD TRAILING EDGE F
- [SDR FDEA2020060191087](https://openairdocs.org/sdr/FDEA2020060191087), May 29, 2020: UNKNOWN. ODOR. VERY STRONG BURNING ODOR ON TAKEOFF ROLL. PERFORMED RTO AT 120 KNOTS. IAW TSI 72-00/7281 COMPLETED WITH BIRD STRIKE INSPECTION IAW FIM 71-05 FAULT TREE 872, COM
- [SDR FDEA201910012396](https://openairdocs.org/sdr/FDEA201910012396), Oct 1, 2019: CONTROL PANEL. BURNED. ELECTRICAL FIRE IN LOWER LEFT SIDE OF OVERHEAD LIGHTS CONTROL PANEL CREW SAW AN ELECTRICAL FIRE ON OVERHEAD PANEL. SMOKE AND BURNING ODOR DETECTED. TROUBLESHOOT
- [SDR FDEA201907181629](https://openairdocs.org/sdr/FDEA201907181629), Jul 18, 2019: LATCH. WORN. PDIS 101 25-60 6211 18JUL19 ICN OPEN U LOGPAGES:3139917 F/O EMER ESCAPE ROPE DOORS KEEPS DROPPING OPEN AND WOULD NOT REMAINED CLOSED. ITEM DEFERRED PER THE NEF 
- [SDR FDEA201812043424](https://openairdocs.org/sdr/FDEA201812043424), Dec 4, 2018: DOOR. MISSING. AT FL 340 HEARD LOW RUMBLING & LOW VIBRATION ON OUR FEET, NOISE & VIBRATION CEASED AT FL 160 ON DESCENT. ALL INDICATIONS NORMAL GOOD CABIN PRESSURE. AS A RESULT
- [SDR FDEA201803160701](https://openairdocs.org/sdr/FDEA201803160701), Mar 16, 2018: HOOK AND LOOP. LOOSE. THE HOOK AND LOOP STRIP FOR THE FIRST OFFIER`S EVAS WAS FOUND LOOSE. SECURED THE EVAS HOOK AND LOOP STRIP IAW AMM 25-99-99-6. ACFT OK FOR SERVICE.
- [SDR FDEA201707272055](https://openairdocs.org/sdr/FDEA201707272055), Jul 27, 2017: D-RING. MISSING. POST FLIGHT, NOTED ONE ESCAPE HARNESS D-RING MISSING BELOW THE RT SUPERNUMERARY SEAT. INSTALLED THE NEW ESCAPE HARNESS D-RING.
- [SDR FDEA201707081880](https://openairdocs.org/sdr/FDEA201707081880), Jul 8, 2017: CARABINER. MISSING. DURING POST FLIGHT, FOUND DEMO ESCAPE HARNESS CARABINER MISSING. THE ESCAPE HARNESS WAS REMOVED AND A NEW CARABINER WAS INSTALLED IAW AMM 25-61-03-2. ACFT OK FO
- [SDR FDEA201612134399](https://openairdocs.org/sdr/FDEA201612134399), Dec 13, 2016: CONVERTER. DIRTY. ACRID ODOR IN THE COCKPIT, IN BEGINNING DESCENT. NO SMOKE OR OBSCURATION. INTENSE ODOR FOR 15-20 SECONDS THEN RAPIDLY DISSIPATED . NO ENGINE OR WING ANTI-ICE. N
- [SDR FDEA201612124386](https://openairdocs.org/sdr/FDEA201612124386), Dec 12, 2016: UNKNOWN. ODOR. INTERMITTENT BURNING ODOR, DURING DESENT. CREW STATED DID NOT SEE ANY SMOKE, IT WAS A RUBBER ODOR AND NOT OVERPOWERING. PERFORMED SNIFF TEST OF THE AVIONICS IN 
- [SDR FDEA201403140504](https://openairdocs.org/sdr/FDEA201403140504), Mar 14, 2014: SENSOR. OUT OF ADJUST. ENTRY DOOR SHOWED OPEN UPON LANDING. ACFT BLOCKED IN BEFORE DOOR WAS OPENED. RELEASED FOR SERVICE IAW MEL 52-71-01-01 CAT C. CREW ENTRY DOOR INDICATION SYS INOP

## 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 N101FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N101FE before.

- [Cancelled 2003-01-23](https://openairdocs.org/deregistered/N101FE-2003-01-23): Boeing 727-22C, S/N 19197, built 1967. Owner: [First Union Commercial Corp](https://openairdocs.org/faa-owner/FIRST%20UNION%20COMMERCIAL%20CORP), [Winston Salem, NC](https://openairdocs.org/faa-place/NC/Winston%20Salem)

## 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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