# N365FE: 1971 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: 46601
- Year built: 1971
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 22, 2006
- Certificate issued: January 16, 1998
- Last registry action: August 4, 2023
- Mode S code: A41F61
- 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/N365FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=365FE
- Page: https://openairdocs.org/deregistered/N365FE-2024-01-29

From the FAA registry file of October 31, 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 (267, newest 50)

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

- [SDR FDEA201901130127](https://openairdocs.org/sdr/FDEA201901130127), Jan 13, 2019: GIRT BAR. LOOSE. GIRT BAR DOOR 1L HAS COME LOOSE RESECURED L-1 DOOR GIRT BAR. OK FOR SERVICE.
- [SDR FDEA201812163525](https://openairdocs.org/sdr/FDEA201812163525), Dec 16, 2018: SLIDE. FAILED. L1 DOOR SLIDE LIGHT FOUND ON DURING PREFLIGHT. RELEASED FOR SERVICE PER MEL 52-10-03. PERFORMED RESISTANCE CHECK PER MEL 25-61-01 OF DOOR SLIDE ELECTRICAL JACK.
- [SDR FDEA201812153505](https://openairdocs.org/sdr/FDEA201812153505), Dec 15, 2018: SWITCH. MALFUNCTIONED. ON PREFLIGHT L1 DOOR SLIDE CIRCUITRY LIGHT REMAINS ILLUMINATED. WHILE TRYING TO COMPLY WITH MEL 25-61-01 FOR THE "PRESS-TO-TEST" INDICATION, METHOD "A", THE TES
- [SDR FDEA201802220478](https://openairdocs.org/sdr/FDEA201802220478), Feb 22, 2018: CABLE. DEFORMED. R1 DOOR CLUTCH RELEASE CABLE HAS DEFORMATION AND KINKING AT FWD CABLE END. REMOVED AND REPLACED THE R1 DOOR CLUTCH RELEASE CABLE IAW AMM 52-11-12.
- [SDR FDEA201801080037](https://openairdocs.org/sdr/FDEA201801080037), Jan 8, 2018: CABLE. BROKEN. L1 DOOR AFT CABLE IS BROKEN AND WRAPPED AROUND SPOOL. UNABLE TO OPEN OR CLOSE DOOR WITHOUT DAMAGING OTHER COMPONENTS. R & R THE CABLE IAW AMM 52-10-02-2.
- [SDR FDEA201701120139](https://openairdocs.org/sdr/FDEA201701120139), Jan 12, 2017: BULKHEAD WEB. CRACKED. BS 595 BULKHEAD WEB AT LONGERON 41L HAS A .800 IN CRACK AT THE UPPER FASTENERS HOLE COMMON TO THE TEE CAP. INSTALLED REPAIRED PER SRM 53-40-00
- [SDR FDEA201701030077](https://openairdocs.org/sdr/FDEA201701030077), Jan 3, 2017: FLOOR SUPPORT. CORRODED. MAIN DECK BS 1881, RBL 27 FLOOR SUPPORT IS CORRODED.. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG WSP0711.
- [SDR FDEA201612294573](https://openairdocs.org/sdr/FDEA201612294573), Dec 29, 2016: PANEL. DELAMINATED. #2 ENGINE INLET (PICKLE BARREL) PANEL AJC7068 IS DELAMINATED. REPAIRED IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201612214518](https://openairdocs.org/sdr/FDEA201612214518), Dec 21, 2016: SKIN. CORRODED. CAC BAY LWR SKIN, BETWEEN STA 1079 TO STA 1099 LONGERON 52 TO LONGERON 51R, HAS CORROSION AND SHEAR RIVET. REPAIRED PER DWG AGA3097 AND SRM 53-20-00.
- [SDR FDEA201612214513](https://openairdocs.org/sdr/FDEA201612214513), Dec 21, 2016: FITTING. CRACKED. LEFT BS 1156 SUGAR SCOOP FITTING HAS THREE CRACKS ON HORIZONTAL LEG BETWEEN LONGERONS 38 AND 39L. REMOVED AND REPLACED FITTING IAW DWG. AYB 7000-1.
- [SDR FDEA201612214516](https://openairdocs.org/sdr/FDEA201612214516), Dec 21, 2016: SHEAR TIE. CORRODED. CAC BAY LOWER SKIN, BETWEEW BS 1079 TO 1099 LONGERON 51TO 52R HAS CORROSION AND SHEAR RIVET. REPLACED CORRODED SHEAR TIE IAW DWG. ADA 0112.
- [SDR FDEA201612214515](https://openairdocs.org/sdr/FDEA201612214515), Dec 21, 2016: FITTING. CRACKED. CAC BAY LT CTR WING TO FUSELAGE HAIRPIN FITTING UPPER AFT FASTENER AREA HAS 0.500 CRACK. REPAIRED IAW SRM 53-30-00 FIG 7 VOL 1.
- [SDR FDEA201612154464](https://openairdocs.org/sdr/FDEA201612154464), Dec 15, 2016: BULKHEAD. CRACKED. FWD CARGO COMP STA 595 AT LONGERON 36L PRESSURE BULKHEAD SUSPECT CRACK. REPAIRED PER SRM 53-40-00 FIG 4.
- [SDR FDEA201612154463](https://openairdocs.org/sdr/FDEA201612154463), Dec 15, 2016: TEE FITTING. CRACKED. FWD CARGO BAY BS 595, LONGERON 36L CRACKED. REPAIRED PER EA. 8-5310-T0330353.
- [SDR FDEA201612154462](https://openairdocs.org/sdr/FDEA201612154462), Dec 15, 2016: TEE FITTING. CRACKED. FWD CARGO BAY PRESSURE BULKHEAD AT BS 595, LWR TEE CAP UPPER TANG CRACKED BETWEEN TWO FASTENERS AND PROPAGATING TO THE EDGE BETWEEN L39L AND L40L. REPAIRED IAW 
- [SDR FDEA201612154459](https://openairdocs.org/sdr/FDEA201612154459), Dec 15, 2016: CAP. CRACKED. FWD CARGO, COMPARTMENT STA 595 LONGERON 39R SUSPECT CRACK. AFTER EVALUATION , FOUND TEE CAP CRACKED. REPAIRED TEE CAP PER EA 8-5310-T0330385
- [SDR FDEA201612114568](https://openairdocs.org/sdr/FDEA201612114568), Dec 11, 2016: SKIN. CRACKED. RIGHT WING NR 7 SLAT TRACK CUTOUT O/B CORNER CRACKED. REPAIRED IAW SRM 57-10-00, FIG.104 A , VOL. I
- [SDR FDEA201612054326](https://openairdocs.org/sdr/FDEA201612054326), Dec 5, 2016: OXYGEN MASK. UNSERVICEABLE. COCKPIT PORTABLE OXYGEN MASK FOUND DRY-ROTTED. REMOVED AND REPLACED COCKPIT PORTABLE OXYGEN MASK IN REF TO AMM 35-30-01-4. ACFT OK FOR SERVICE.
- [SDR FDEA201607152451](https://openairdocs.org/sdr/FDEA201607152451), Jul 15, 2016: DOOR. CRACKED. ON T/O, HAD UNSAFE, RED LIGHT, GEAR UP. LEFT MAIN CYCLED GEAR. GEAR DOWN, 3 GREEN, CYCLE D UP, UNSAFE LT MAIN, ACFT DIVERTED. REPLACED LT MLG DOOR.
- [SDR FDEA201604181255](https://openairdocs.org/sdr/FDEA201604181255), Apr 18, 2016: CRANK ASSY. DEFECTIVE. CAPTAIN DURING POST FLIGHT DEBRIEF REPORTED, RT BRAKE PEDAL EXCESSIVE TRAVEL & SLOW TO ACTUATE. R & R CAPTAINS RT BRAKE FEATHERING CRANK IAW EA 8-2720-TO324787.
- [SDR FDEA201511103550](https://openairdocs.org/sdr/FDEA201511103550), Nov 10, 2015: CONTACT. UNSECURE. FOUND LI DOOR SLIDE PRESS TEST LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C EXPIRATION 20 NOV 15. EVAC SLIDE REMOTE PRESS INDICATOR INOPE
- [SDR FDEA201510173273](https://openairdocs.org/sdr/FDEA201510173273), Oct 17, 2015: WINDSHIELD. CRACKED. DURING DESCENT PASSING THROUGH 16000 FEET THE CAPTAINS WINDSHIELD STARTED CRACKING. NEITHER PILOT NOTICED ANY BIRD IMPACT OR OTHER EXTERIOR FORCE THAT COULD HAV
- [SDR FDEA201507102195](https://openairdocs.org/sdr/FDEA201507102195), Jul 10, 2015: INDICATOR. INOPERATIVE. R1 DOOR SLIDE REMOTE PRESSURE, PRESS TO TEST SWITCH INOPERATIVE. R & R RT REMOTE SLIDE PACK PRESS INDICATOR. OPERATIONS CHECKED NORMAL.
- [SDR FDEA201506231958](https://openairdocs.org/sdr/FDEA201506231958), Jun 23, 2015: POWER SUPPLY. DEFECTIVE. EMERGENCY LIGHT BATTERY 1 LO LVL 1 ALERT DURING EMER LIGHT TEST ON PREFLIGHT. REMOVED AND REPLACED EMERGENCY LIGHTS PWR SUPPLY PER AMM 33-51-01-4. OPS CHECKS GO
- [SDR FDEA201506091729](https://openairdocs.org/sdr/FDEA201506091729), Jun 9, 2015: WARNING MESSAGE. FALSE ACTIVATION. LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW, ILLUMINATED DURING PREFLIGHT. ARMED EMERGENCY LIGHTS AND THE MESSAGE DID NOT RETURN. EMERGENCY LIGHTS TESTED GOOD IAW AMM
- [SDR FDEA201505031378](https://openairdocs.org/sdr/FDEA201505031378), May 3, 2015: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT BATTERY 1 LOW, LEVEL 1 ALERT ON EAD DURING EMERGENCY LIGHT PREFLIGHT TEST.
- [SDR FDEA201503030638](https://openairdocs.org/sdr/FDEA201503030638), Mar 3, 2015: LIGHT. INOPERATIVE. MAIN ENTRY DOOR SLIDE 1L DOES NOT TEST. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01. VERIFY
- [SDR FDEA201501230374](https://openairdocs.org/sdr/FDEA201501230374), Jan 23, 2015: DOOR. OUT OF ADJUST. THE L1 DOOR WILL NOT CLOSE. WHEN ATTEMPTING TO CLOSE THE DOOR THE TOP OF THE DOOR POPS INWARD ABOUT 10 INCHES. COMPLETED ADJUSTMENT TEST OF L1 DOOR PER AMM 52-1
- [SDR FDEA201412174135](https://openairdocs.org/sdr/FDEA201412174135), Dec 17, 2014: SUPPORT. OUT OF POSITION. DURING RAISING GEAR AFTER TAKEOFF, RT MAIN GEAR DID NOT INDICATE UP, RED LIGHT IN BOTH CONFIG PAGE & INDICATOR ABOVE GEAR HANDLE, DID NOT FEEL ADVERSE YAW OR NO
- [SDR FDEA201412104101](https://openairdocs.org/sdr/FDEA201412104101), Dec 10, 2014: SPAR. DAMAGED. FOUND HOLE ON LT WING REAR LOWER SPAR TO BE DIFFERENT. COMPLY WITH EA 8-5710-T0313003 PT 1.
- [SDR FDEA201411173717](https://openairdocs.org/sdr/FDEA201411173717), Nov 17, 2014: SEAT TRACK. DAMAGED. UPPER CARGO COMPARTMENT STATION 1422, RBL8 SEAT TRACK IS DAMAGED .552 BEYOND LIMITS IAW SRM 53-70 VOL 1 PAGE 21. SEAT TRACK SECTION REPLACED IAW SRM 53-70-00 VO
- [SDR FDEA201411143700](https://openairdocs.org/sdr/FDEA201411143700), Nov 14, 2014: PANEL. GOUGED. LEFT WING LOWER WING HINGE PANEL 551DB HAS GOUGE ON INNER SECTION FROM FLAP VANE CONTACT. REPAIRED HINGE PANEL 551DB AS REQUIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411143679](https://openairdocs.org/sdr/FDEA201411143679), Nov 14, 2014: ACCESS PANEL. DELAMINATED. LEFT HORIZONTAL STAB TE ACCESS PANEL 334HB HAS DELAMINATION INNER OTBD SECTION OF PANEL. REPAIR PANEL 334HB IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-
- [SDR FDEA201411123663](https://openairdocs.org/sdr/FDEA201411123663), Nov 12, 2014: BULKHEAD WEB. CRACKED. NOSE WW LT SIDEWALL SKIN HAS A FOUR INCH CRACK AT BS 485. REPAIRED IAW SRM 53-30-00 FIG 6
- [SDR FDEA201411123665](https://openairdocs.org/sdr/FDEA201411123665), Nov 12, 2014: PANEL. DELAMINATED. RIGHT WING ROOT PANEL ARC0446-502 IS DELAMINATED. REPAIRED PANEL ARC0446-502 AS REQUIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411123655](https://openairdocs.org/sdr/FDEA201411123655), Nov 12, 2014: PANEL. DELAMINATED. PANEL 541AB AT LT WING ROOT HAS SEPARATED LAYERS. REPAIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411113643](https://openairdocs.org/sdr/FDEA201411113643), Nov 11, 2014: SKIN. DAMAGED. RIGHT INBD FLAP INBD LE HAS DAMAGE. REPAIRED IAW SRM 57-10-00 & DWG SG 10570001.
- [SDR FDEA201411083594](https://openairdocs.org/sdr/FDEA201411083594), Nov 8, 2014: PANEL. DELAMINATED. PANEL ARC0446-503 AT LT WING ROOT HAS SEPARATED LAYERS. REPAIRED PANEL ARC0446-503 AS REQUIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201411083580](https://openairdocs.org/sdr/FDEA201411083580), Nov 8, 2014: BRACKET. CRACKED. LEFT OTBD FLAP, INBD HINGE FWD ATTACH POINT FITTING, Z BRACKET CRACKED ON INBD SIDE. R & R CRACKED BRACKET IAW SRM 51-31-01.
- [SDR FDEA201411043471](https://openairdocs.org/sdr/FDEA201411043471), Nov 4, 2014: SEAT TRACK. DAMAGED. MAIN DECK STATION 750 LBL 47 SEAT TRACK DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL I.
- [SDR FDEA201411043470](https://openairdocs.org/sdr/FDEA201411043470), Nov 4, 2014: SEAT TRACK. DAMAGED. MAIN DECK STATION 1015 LBL 47 SEAT TRACK DAMAGED. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-7--00 VOL 1.
- [SDR FDEA201410303426](https://openairdocs.org/sdr/FDEA201410303426), Oct 30, 2014: DOUBLER. CRACKED. CENTER LANDING GEAR WW BAY BS 1381, X=31.50 DOUBLER IS CRACKED. REMOVED AND REPLACED DOUBLER.
- [SDR FDEA201407172078](https://openairdocs.org/sdr/FDEA201407172078), Jul 17, 2014: SKIN. CRACKED. FOUND CRACKS ON RT WING FIXED LE UPPER SURFACE ANTI-ICE TELESCOPING DUCT CUT OUT. COMPLIED WITH EA 8-5720-T0309797 COMPLYING WITH SRM 57-40-01.
- [SDR FDEA201312213026](https://openairdocs.org/sdr/FDEA201312213026), Dec 21, 2013: BATTERY. INOPERATIVE. L1 DOOR EVACUATION SLIDE RAFT PRESS. INDICATOR LIGHT INOPERATIVE. REPLACED BATTERIES FOR L1 DOOR EVACUATION SLIDE RAFT PRESS TEST LIGHT, OPERATIONS CHECKED NORM
- [SDR FDEA201304300889](https://openairdocs.org/sdr/FDEA201304300889), Apr 30, 2013: LAMP. INOPERATIVE. R1 DOOR SLIDE PRESSURE INDICATOR LIGHT INOPERATIVE. REPLACED LAMP IAW 26-61-03-2, OPS CHECKED GOOD.
- [SDR FDEA201303150580](https://openairdocs.org/sdr/FDEA201303150580), Mar 15, 2013: DOUBLER. CRACKED. CLG W/W COMPARTMENT LT SIDEWALL CUTOUT DOUBLER CRACKED. R & R CENTER LANDING GEAR W/W LT SIDEWALL CUTOUT DOUBLER PN AEA0526U1.
- [SDR FDEA201303150579](https://openairdocs.org/sdr/FDEA201303150579), Mar 15, 2013: DOUBLER. CRACKED. CLG W/W COMPARTMENT RT SIDEWALL CUTOUT DOUBLER CRACKED. REMOVED CRACKED DOUBLER, INSTALLED DOUBLER RT SIDE REF SRM 51-00-01, VOL 2 AND 51-33-01, VOL 2.
- [SDR FDEA201211154038](https://openairdocs.org/sdr/FDEA201211154038), Nov 15, 2012: SPAR. CRACKED. RT SIDE OF HORIZONTAL STAB REAR SPAR VERTICAL TANG HAS A CRACK EMANATING FROM FASTENER HOLE, UPPER ROW SECOND OTBD APPROX .375" LONG. (MKD) NEED TO COMPLY WITH 
- [SDR FDEA201210263753](https://openairdocs.org/sdr/FDEA201210263753), Oct 26, 2012: ATTACH ANGLE. CRACKED. NR 3 ACM COMPARTMENT STA 565-595 OTBD CEILING WEB TO SKIN ATTACHING ANGLE CRACKED, CRACK RUNS FWD TO AFT IN ANGLE RADIUS APPROX 30 INCHES LONG. INSTALLED CUSP R
- [SDR FDEA201210183662](https://openairdocs.org/sdr/FDEA201210183662), Oct 18, 2012: CONTROL PANEL. BURNED. ELECTRICAL ODOR, LIKE HOT EQUIPTMENT, NOTICABLE IN THE COCKPIT. STRONGER ON THE CAPTAIN'S SIDE AND THE STRONGEST ON GROUND. ODOR APPEARS TO BE COMING FROM THE E

All 267: https://openairdocs.org/deregistered/N365FE-2024-01-29/reports.md

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