# N371FE: 1972 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-01-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 29, 2024
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas MD-10-10F](https://openairdocs.org/model/mcdonnell-douglas-md-10-10f) (registry code 3022112)
- Engine: [GE CF6-6D](https://openairdocs.org/engine/ge-cf6-6d) (registry code 30076)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 46609
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 19, 2007
- Certificate issued: January 23, 1998
- Last registry action: August 4, 2023
- Mode S code: A43804
- Owner when cancelled: [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 was based
- The mark today: https://openairdocs.org/aircraft/N371FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=371FE
- Page: https://openairdocs.org/deregistered/N371FE-2024-01-29

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas MD-10-10F: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f.md

## Service difficulty reports (76, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR FDEA201503201032](https://openairdocs.org/sdr/FDEA201503201032), Mar 20, 2015: DOOR. STUCK. R1 DOOR WILL NOT OPEN. RELEASED FOR SERVICE IAW MEL 52-10-03 CATEGORY C. TROUBLESHOOTING REQUIRED FOR REPAIR.
- [SDR FDEA201503060699](https://openairdocs.org/sdr/FDEA201503060699), Mar 6, 2015: MECHANISM. LACK OF LUBE. RECEIVED A CABIN DOOR FWD RT, DURING FLIGHT HANDLE IS NOT UP, FLUSH LIKE ON LT SIDE BUT WON'T GO UP ANYMORE. WHILE TROUBLESHOOTING WRI 52-10-6839 FOUND R1 DOOR 
- [SDR FDEA201408292353](https://openairdocs.org/sdr/FDEA201408292353), Aug 29, 2014: LIGHT. WRONG PART. EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATING SYS IS INOPERATIVE. RELEASED FOR SERVICE IAW MEL. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIF
- [SDR FDEA201403200538](https://openairdocs.org/sdr/FDEA201403200538), Mar 20, 2014: WIRE HARNESS. DAMAGED. RTO AT 110KTS FOR, ENG 3 EXCEEDANCE, LVL 1 ALERT. NR 3 EGT SHOWED YELLOW, 1011, FOR EXCEEDANCE, ESTIMATE EXCEEDANCE WAS MOMENTARY. PULLED UP VIA NR 3 ENG EXCEED
- [SDR FDEA201403020430](https://openairdocs.org/sdr/FDEA201403020430), Mar 2, 2014: PUSH-PULL CABLE. MALFUNCTIONED. ON TOP OF DESCENT NR 2 THROTTLE FROZE AT 92% N1 FROM FL 370 TO 10,000 FT NO MOVEMENT, SHUTDOWN ENG. CREW REPORTED THAT AFTER ARRIVAL AT GATE & SHUTDOWN NR 2 THR
- [SDR FDEA201311052693](https://openairdocs.org/sdr/FDEA201311052693), Nov 5, 2013: DOUBLER. CRACKED. CENTER WHEEL WELL DOUBLER HAS AN APPROXIMATLEY 5 INCH VERTICAL CRACK AT BS 1381. REMOVED AND REPLACED DOUBLER IAW SRM 51-31-01, RIGGED GOOD IAW AMM 27-60-00-05.
- [SDR FDEA201304241003](https://openairdocs.org/sdr/FDEA201304241003), Apr 24, 2013: DOUBLER. CRACKED. WHEN REMOVING EXISTING REPAIR DOUBLER, FOUND ADDITIONAL CRACK IN AEA0161-11 DOUBLER. BS 1391 APPROX 4" DOWN FROM TOP. REPAIRED IAW EA 8-5310-157389, PART 1.
- [SDR FDEA201304241000](https://openairdocs.org/sdr/FDEA201304241000), Apr 24, 2013: BULKHEAD. CRACKED. LEFT BULKHEAD CRACKED 16 INCHES AFT OF FWD BULKHEAD AND 4 INCHES DOWN FROM UPPER BULKHEAD. CRACK END MARKED USING HFEC. REPAIRED IAW EA 8-5310-157389, PART 1.
- [SDR FDEA201208293198](https://openairdocs.org/sdr/FDEA201208293198), Aug 29, 2012: PROXIMITY SENSOR. OUT OF ADJUST. ON GEAR RETRACTION RECEIVED A RED LT MAIN GEAR LIGHT ON THE PRIMARY AND SECONDARY INDICATORS. PERFORMED QHR PROCEDURES AND HAD SAME INDICATIONS. DUMPED FUEL TO 
- [SDR FDEA201206012043](https://openairdocs.org/sdr/FDEA201206012043), Jun 1, 2012: FIRE WARNING. ILLUMINATED. A LEVEL 3 CARGO FIRE LOWER FWD ILLUMINATED. PUSHED FLASHING DISCHARGE SWITCH, LANDED & ROLLED OUT TO FULL STOP. FIRE DEPTARTMENT REPORTED SLIGHT HEAT SIGNATURE 
- [SDR FDEA201111134891](https://openairdocs.org/sdr/FDEA201111134891), Nov 13, 2011: DOOR FRAME. CORRODED. AFT CARGO DOOR LWR FWD FRAME CORRODED. REMOVED CORROSION FROM AFT CARGO DOOR LWR FWD INTERIOR JAMB REF SRM53-50-00, VOL 1 FIG 15 AND ER 11-04534. REPAIRED IAW R
- [SDR FDEA201111034740](https://openairdocs.org/sdr/FDEA201111034740), Nov 3, 2011: FITTING. CRACKED. MAIN CARGO DOOR NR6 LATCH SPOOL LOWER FITTING CRACKED FROM INBD FWD SPOOL MOUNT BOLT HOLE. R & R SPOOL FITTING NR 6 REF SRM 51-33-01, VOL II.
- [SDR FDEA201107212886](https://openairdocs.org/sdr/FDEA201107212886), Jul 21, 2011: PITOT LINE. DAMAGED. ON TAKEOFF AIRSPEED STAGNATED THEN BECAME ERRATIC. COMPLIED WITH QRH. RETURNED TO KIND. R & R 3EA PITOT TUBES IAW MM 34-11-02-2. OPS CHECK REQ'D. PERFORMED A LO
- [SDR FDEA201107212885](https://openairdocs.org/sdr/FDEA201107212885), Jul 21, 2011: PITOT LINE. DAMAGED. ON TAKEOFF, AIRSPEED STAGNATED THEN BECAME ERRATIC. COMPLIED WITH QRH. RETURNED TO FIELD. R & R 3 PITOT TUBES IAW MM 34-11-02-2. PERFORMED A LOW RANGE LEAK TEST
- [SDR FDEA201003100734](https://openairdocs.org/sdr/FDEA201003100734), Mar 10, 2010: RELIEF VALVE. FAILED. FUEL SYS AUTO, ON LONG APP WITH MEL 28-22-01-04A. ALL PUMPS WERE ON THAT WERE NOT DEFFERRED. FUEL QTY TANK NR 2 STARTED A SLOW INCREASE AS FUEL QTY TANK NR1 DRO
- [SDR FDEA200712115024](https://openairdocs.org/sdr/FDEA200712115024), Dec 11, 2007: FRAME. CRACKED. MAIN CABIN FOUND 1 CRACK ON FRAME STA 1741, STR 14, RT. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I AND EA NR 8-5310-111521, 8-5330-111563.
- [SDR 07FDEA05024](https://openairdocs.org/sdr/07FDEA05024), Dec 11, 2007: FRAME. CRACKED. MAIN CABIN FOUND 1 CRACK ON FRAME STA 1741 STR 14 RT REPAIRED IAW SRM 53-30-00 FIG 5 VOL I AND EA NR 8-5380-111563.
- [SDR 07FDEA04984](https://openairdocs.org/sdr/07FDEA04984), Dec 3, 2007: LUG. CRACKED. FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 2 VOL I.
- [SDR 07FDEA04983](https://openairdocs.org/sdr/07FDEA04983), Dec 3, 2007: STRINGER. CRACKED. FOUND LOWER CHORD LUGS CRACKED. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 2 VOL I.
- [SDR 07FDEA04965](https://openairdocs.org/sdr/07FDEA04965), Nov 29, 2007: ANGLE. CRACKED. LOWER FWD COMPT CRACK ON TEE ANGLE. REPAIRED TEE CAP IAW EA NR 8-5310-111463.
- [SDR 07FDEA04964](https://openairdocs.org/sdr/07FDEA04964), Nov 29, 2007: LUG. CRACKED. FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW EA NR 8-5710-111524A.
- [SDR 07FDEA04963](https://openairdocs.org/sdr/07FDEA04963), Nov 29, 2007: LUG. CRACKED. AT ACCESS 634 AT FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW EA NR 8-5710-111525A.
- [SDR 07FDEA04962](https://openairdocs.org/sdr/07FDEA04962), Nov 29, 2007: SKIN. CRACKED. RT WING DROOPED FOUND CRACK ON UPPER EXTERNAL SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 55 VOL I.
- [SDR FDEA200711204866](https://openairdocs.org/sdr/FDEA200711204866), Nov 20, 2007: SEAT TRACK. CRACKED. DURING PERFORMING OK TO CLOSE FLOOR PANELS WITH J/C MD10-53210290-1J FOUND SEAT TRACK CRACK ON MAIN CABIN. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.
- [SDR 07FDEA04868](https://openairdocs.org/sdr/07FDEA04868), Nov 20, 2007: SEAT TRACK. CRACKED. ENTRY WAY ZONE AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10-600C220-1JR FOUND CRACK ON SEAT TRACK LUG LT SIDE. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 SHT 1 A
- [SDR 07FDEA04867](https://openairdocs.org/sdr/07FDEA04867), Nov 20, 2007: CHANNEL. CORRODED. CTR CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON CHANNEL. REPAIRED CHANNEL IAW SRM 53-70-00 VOL I FIG 5 SHT 5.
- [SDR 07FDEA04866](https://openairdocs.org/sdr/07FDEA04866), Nov 20, 2007: SEAT TRACK. CRACKED. DURING PERFORMING OK TO CLOSE FLOOR PANELS WITH J/C MD10-53210290-1J FOUND SEAT TRACK CRACK ON MAIN CABIN.
- [SDR 07FDEA04862](https://openairdocs.org/sdr/07FDEA04862), Nov 19, 2007: STRINGER. CRACKED. AT ACCESS 534 AT FOUND CRACK, ACCOMPLISHED EA NR 8-5710-111526.
- [SDR 07FDEA04861](https://openairdocs.org/sdr/07FDEA04861), Nov 19, 2007: SKIN. CRACKED. DURING U/S INSP OF HORIZ STB, FOUND TWO PANEL WITH CRACK IN FLYABLE LIMITS. ACCOMPLISHED EA NR 8-5510-111533.
- [SDR 07FDEA04859](https://openairdocs.org/sdr/07FDEA04859), Nov 19, 2007: SKIN. LOOSE. LT WING I/B FLAP UPPER SKIN EXISTING REPAIR. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I.
- [SDR 07FDEA04858](https://openairdocs.org/sdr/07FDEA04858), Nov 19, 2007: BULKHEAD. CRACKED. CLG WW CENTER CRACKS ON VERTICAL RT BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 VOL I.
- [SDR 07FDEA04853](https://openairdocs.org/sdr/07FDEA04853), Nov 19, 2007: SKIN. CRACKED. LT WING DROOPED FOUND CRACK AND DEEP WEAR ON EXT SKIN OUTBOARD SIDE DROOPED. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 15 SHT 1.
- [SDR 07FDEA04851](https://openairdocs.org/sdr/07FDEA04851), Nov 19, 2007: SKIN. WORN. RT WING DROOPED FOUND DEEP WEAR ON LWR EXTERNAL SKIN. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 39.
- [SDR 07FDEA04753](https://openairdocs.org/sdr/07FDEA04753), Nov 8, 2007: STRINGER. CRACKED. FOUND 2" CRACK ON RT WING STRINGER NR 40 AT XORS 346. REPAIR PER SRM 57-20-00 VOL 1 FIG 36 CONF.
- [SDR FDEA200710244668](https://openairdocs.org/sdr/FDEA200710244668), Oct 24, 2007: HINGE. DAMAGED. HINGE ASSY ITEM 360 BROKEN, REF IPC 55-22-02-01. REPLACE HINGE IAW STD REWORK DWG SR10-55-501.
- [SDR FDEA200710244665](https://openairdocs.org/sdr/FDEA200710244665), Oct 24, 2007: SEAT TRACK. CRACKED. FOUND 1 CRACK 4 INCH ON SEAT TRACK AT STA 635 X= 67 CUT APPROX AT STA 666 AND 624 AND REPAIR IAW SRM 53-70-00 VOL 1 FIG 1 AND FIG 11.
- [SDR 07FDEA04669](https://openairdocs.org/sdr/07FDEA04669), Oct 24, 2007: SKIN. DAMAGED. LT WING L/E SKIN LOWER SLAT TRACK CUT OUT NR 8 AT STA XOS 549 EXISTING REPAIR. REPLACED REPAIR PER SRM 57-10-00 VOL.1 FIG 68.
- [SDR 07FDEA04668](https://openairdocs.org/sdr/07FDEA04668), Oct 24, 2007: HINGE. DAMAGED. HINGE ASSY ITEM 360 BROKEN (REF IPC 55-22-02-01). REPLACED LATCH IAW FEDEX STD REWORK DWG SR10-55-501.
- [SDR 07FDEA04667](https://openairdocs.org/sdr/07FDEA04667), Oct 24, 2007: ANGLE. CORRODED. CTR CARGO COMPT EXFOLIATION CORROSION ON CAP ANGLE AT STA 1541 L NR 52 REPAIR CAP IAW SRM 53-30-00 VOL 1 FIG 8 SHEET 1.
- [SDR 07FDEA04666](https://openairdocs.org/sdr/07FDEA04666), Oct 24, 2007: ANGLE. CORRODED. EXFOLIATION CORROSION ON CAP ANGLE AT STA 1561 L NR 52 REPAIR IAW SRM 53-30-00 VOL 1 FIG 8 SHEET 1.
- [SDR 07FDEA04665](https://openairdocs.org/sdr/07FDEA04665), Oct 24, 2007: SEAT TRACK. CRACKED. FOUND 1 CRACK 4" ON SEAT TRACK AT STA 635 X= 67 CUT APPROX AT STA 666 AND 624 AND REPAIR IAW SRM 53-70-00 VOL 1 FIG 1 AND FIG 11.
- [SDR 07FDEA04664](https://openairdocs.org/sdr/07FDEA04664), Oct 24, 2007: STRINGER. CRACKED. RT WING L/E INTERNAL STRUCTURE FOUND 1 CRACK 0,75" LONG ON FIXED TEE AT XOS 906 REPAIR WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1.
- [SDR 07FDEA04423](https://openairdocs.org/sdr/07FDEA04423), Oct 1, 2007: ANGLE. CRACKED. LOWER CTR CARGO DOOR CRACK ON FWD LWR CORNER. REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL I.
- [SDR 07FDEA04340](https://openairdocs.org/sdr/07FDEA04340), Sep 27, 2007: RIB. CRACKED. RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.
- [SDR 07FDEA04339](https://openairdocs.org/sdr/07FDEA04339), Sep 27, 2007: RIB. CRACKED. RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.
- [SDR 07FDEA04338](https://openairdocs.org/sdr/07FDEA04338), Sep 27, 2007: RIB. CRACKED. RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.
- [SDR 07FDEA04337](https://openairdocs.org/sdr/07FDEA04337), Sep 27, 2007: RIB. CRACKED. RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.
- [SDR 07FDEA03821](https://openairdocs.org/sdr/07FDEA03821), Sep 17, 2007: MEMBRANE. CORRODED. COCKPIT INT AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10-0600C210-1JR FOUND SEVERE CORROSION ON 2 HORIZ MEMBRANE: FROM STA 303 TO STA 330 FROM X= 7.50 TO X=17 LT
- [SDR 07FDEA03820](https://openairdocs.org/sdr/07FDEA03820), Sep 17, 2007: FRAME. CRACKED. MAIN CABIN STRUCTURE HAS CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIG 5 VOL I.
- [SDR 07FDEA03816](https://openairdocs.org/sdr/07FDEA03816), Sep 17, 2007: RIB. CRACKED. RT WING L/E INT STRUCTURE FOUND CRACK ON RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.

All 76: https://openairdocs.org/deregistered/N371FE-2024-01-29/reports.md

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