# N364FE: 1971 Mcdonnell Douglas MD-10-10F, registration cancelled 2004-02-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 25, 2004 - 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 CF6-6 series](https://openairdocs.org/engine/ge-cf6-6-series) (registry code 30020) - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 46600 - Year built: 1971 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 7, 2001 - Certificate issued: August 12, 1998 - Last registry action: May 16, 2001 - Mode S code: A41BAA - Owners when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Attn Michael Wilson III](https://openairdocs.org/faa-owner/ATTN%20%20MICHAEL%20WILSON%20III) - 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/N364FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=364FE - Page: https://openairdocs.org/deregistered/N364FE-2004-02-25 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 (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 03FDEA02175](https://openairdocs.org/sdr/03FDEA02175), Dec 8, 2003: PRESSURE SWITCH. FAILED. RECEIVED NR 1 MANIFOLD FAIL ALERT AT FL350. COULD NOT MAINTAIN CABIN PRESSURE. RAN RED TABS AND DIVERTED TO DEN. FOUND LEFT WING PRESSURE SWITCH FAULT BALL NO L - [SDR 03FDEA00822](https://openairdocs.org/sdr/03FDEA00822), May 28, 2003: BULKHEAD. CRACKED. COMPLY WITH E.A.8-5310-70387. FUSELAGE-MAINFRAME-REPAIR OF STA 1987 BULKHEAD P/N AJC7066-1. CLOSING ACTION ON 05-27-03 ON N/R C00019. COMPLIED WITH E.A.8-5310-7 - [SDR 03FDEA00800](https://openairdocs.org/sdr/03FDEA00800), May 24, 2003: RIB. CRACKED. NR 855 NR 3 ENGINE RTCORE COWL FWD RIB CRACKED AT UPPER L/E RADIUS. CLOSING ACTION ON 05/24/03. REMOVED FASTENERS FOR ACCESS IAW SRM 51-31-01. WELLED CRACK ON M - [SDR 03FDEA00801](https://openairdocs.org/sdr/03FDEA00801), May 24, 2003: CONTROL VALVE. FAILED. N 860 #2 O/B T/R FAILS TO AUTO-RESTOW CHECK. CLOSING ACTION ON 05/24/03. REMOVED AND REPLACED DIRECTI0NAL CONTROL VALVE IAW M/M 78-31-11-2, LEAK TO BE ACCOMPLIS - [SDR 03FDEA00802](https://openairdocs.org/sdr/03FDEA00802), May 24, 2003: SKIN. CRACKED. NR S 17 COMPLY WITH E.A.8-5710-70392.WINGS-RT-FIXED LEADING EDGE BEADED DOUBLER REPAIR ACB 1242. CLOSING ACTION ON 05/23/03. COMPLIED WITH E.A.8-5710-70392. - [SDR 03FDEA00803](https://openairdocs.org/sdr/03FDEA00803), May 24, 2003: CLIP. DAMAGED. AFT FUSELAGE PENTHOUSE CANTED FRAME AT Y=2029.88. HAS REPAIRS, SHOULD BE REPLACED PER E.O.8-5310-7-5000.PT 1. CLOSING ACTION ON 02/22/03. REMOVED AND REPLACED C - [SDR 03FDEA00804](https://openairdocs.org/sdr/03FDEA00804), May 24, 2003: RUB STRIP. CRACKED. LT PATIO DOOR UPPER STAINLESS STRIP CRACKED AND CRUSHED. CLOSING ACTION ON 05/24/03. REMOVED CLOSEOUT STRIP IAW SRM 51-31-01.FAB NEW RUB STRIP ON TRAVLER T2/333 - [SDR 03FDEA00781](https://openairdocs.org/sdr/03FDEA00781), May 20, 2003: HINGE. CORRODED. S 16 COMPLY WITH E.A.8-5740-70384. WINGS INBD FLAP OUTBD HINGE SUPPORT FITTING TO WING ATTACH HOLES REWORK. CLOSING ACTION ON 05/19/03. COMPLIED WITH E.A.8-5740 - [SDR 03FDEA00760](https://openairdocs.org/sdr/03FDEA00760), May 19, 2003: HINGE. CORRODED. S 14 C/W E.A.8-5740-70390. WINGS-RT INBD FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION ON 05/17/03. COMPLIED WITH E.A.8-5740-70390.WINGS R/H INBD FLAP HINGE - [SDR 03FDEA00726](https://openairdocs.org/sdr/03FDEA00726), May 12, 2003: DOOR FRAME. CRACKED. NR 200 RT PATIO DOOR NR 10 FRAME CRACKED AS MARKED. STOPPED DRILL CRACK IAW MD-10 SRM 53-30-00. FAB ANGLE REPAIR IAW MAE TRAVLER T2/333232. LOCATED AND DRILLED - [SDR 03FDEA0163](https://openairdocs.org/sdr/03FDEA0163), Feb 21, 2003: PROXIMITY SWITCH. INOPERATIVE. WHEN GEARS WERE LOWERED, ALL 3 GEAR INDICATED UNSAFE ON MAIN GEAR INDICATORS AND CONFIGURATION PAGE. NO ABNORMAL YAW OR NOISE. RECYCLED GEAR AND GOT 3 GOOD DOWN - [SDR 02FDEA00210](https://openairdocs.org/sdr/02FDEA00210), Mar 19, 2002: DETECTOR. INOPERATIVE. ON CLIMBOUT NR 2 MANIFOLD FAIL ILLUM'D. NR 2 MANIFOLD FAIL DET LOOP INOP, DO NOT PRESS PNEU SYS NR 2 EXCEPT FOR ENG START. - [SDR 01FDEA00954](https://openairdocs.org/sdr/01FDEA00954), Nov 1, 2001: SKIN. CRACKED. LEFT HAND INBOARD FLAP OUTER SKIN HAS .5 INCH CRACK. REMOVED AND REPLACED SKIN PER SRM 57-00-01. - [SDR 01FDEA00953](https://openairdocs.org/sdr/01FDEA00953), Nov 1, 2001: VANE. GOUGED. LEFT HAND OUTBOARD FLAP VANE HAS GOUGE. REMOVED AND REPLACED FLAP PER SRM 51-71-00. - [SDR 01FDEA00887](https://openairdocs.org/sdr/01FDEA00887), Oct 11, 2001: ATTACH ANGLE. CRACKED. IN CTR CARGO AT BS 1521 BILGE AREA BETWEEN LONGERONS R44 & R46 CRACK IN BULKHEAD ATTACH ANGLE. REMOVED AND REPLACED TEE CHORD PER SRM & AEA0453-1 & SRM 51-39-01 - [SDR 01FDEA00884](https://openairdocs.org/sdr/01FDEA00884), Oct 11, 2001: SPLICE. CRACKED. CTR CARGO BILGE AREA LEFT LONGERON 46 BETWEEN BS 1744 & 1761 LONGERON SPLICE CRACKED. REMOVED AND REPLACED SPLICE PER SRM 51-21-01, 51-35-01. - [SDR 01FDEA00885](https://openairdocs.org/sdr/01FDEA00885), Oct 11, 2001: SPLICE. CRACKED. CTR CARGO BILGE AREA L47 BETWEEN BS 1741 & 1761 LONGERON SPLICE CRACKED. REMOVED AND REPLACED SPLICE PER SRM 51-23-01, 51-00-00. - [SDR 01FDEA00886](https://openairdocs.org/sdr/01FDEA00886), Oct 11, 2001: SPLICE. CRACKED. IN CTR CARGO BILGE AREA BETWEEN BS 1701 & 1721 CRACK ON LONGERON SPLICE 51L. REMOVED AND REPLACED LONGERON SPLICE PER SRM 51-23-01 & 51-00-00. - [SDR 01FDEA00871](https://openairdocs.org/sdr/01FDEA00871), Oct 8, 2001: AILERON. CORRODED. SIX SEPARATE AREAS ON RT OUTBOARD AILERON LWR CORRODED. REMOVED AND REPLACED AILERON PER IAW AMM 27-10-02-4. - [SDR 2000ZZZX652](https://openairdocs.org/sdr/2000ZZZX652), Feb 11, 2000: WEB. CRACKED. DURING MAINTENANCE, 3.0 INCH CRACK WAS FOUND ON RIGHT/CENTER WHEELWELL WEB. CRACK AFFECTED UPPER SPLICE WEB, P/N AEA0161-1, RT SIDE, AND AEA0501-1. (X) - [SDR 99FDEA00304](https://openairdocs.org/sdr/99FDEA00304), Mar 10, 1999: BOLT. CORRODED. N2764, DURING A/C P-F CONV AT AERONAVALI, A SUSPECTED BOLT FAILURE WAS FOUND AT STA Y=275 FOR ATTACH P/N ABA7003-2, ABA7023-1, NBA6044-15 AND ABA7171. REPAIR WA - [SDR 99FDEA00305](https://openairdocs.org/sdr/99FDEA00305), Oct 21, 1998: SPAR. CRACKED. N2420 - DURING A/C PF CONVERSION AT AERONAVALI AND ACCOMPLISHMENT OF DAC SB 55-17, R3, AD 88-03-08, A CRACK WAS FOUND ON THE HORIZONTAL STAB. REPAIR ATTEMPS TO - [SDR 99FDEA00307](https://openairdocs.org/sdr/99FDEA00307), Sep 4, 1998: WEB. CRACKED. N0527 - DURING AC P-F CONV AT AERONAVALI, A CRACK 0.87 IN LONG WAS FOUND ON WEB OF UPPER TORQUE BOX PLANE AT Y=2017 AND RBL = 20. SRM 53-00-01, FIG 4 SHEET 2 WE - [SDR 99FDEA00306](https://openairdocs.org/sdr/99FDEA00306), Aug 18, 1998: DOUBLER. CORRODED. N0235 - DURING A/C P-F CONV AT AERONAVALI, CORROSION WAS FOUND ON LT UPPER WING AND MLG DOUBLER, TYPICAL PER DC10 SRM 57-00-01, FIG 8. THE AMOUNT OF DAMAGE FOUN ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA04MA011](https://openairdocs.org/ntsb/DCA04MA011), Dec 18, 2003: McDonnell Douglas MD-10-10F (N364FE), Memphis, TN, destroyed. Probable cause: 1) the first officer's failure to properly apply crosswind landing techniques to align the airplane with the runway centerline and to properly arrest the airplane's descent rate (flare) before the… ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20031218037819A](https://openairdocs.org/incident/20031218037819A), Dec 18, 2003: Doug MD1010F (N364FE), Memphis, TN, Destroyed. (-23) The right main gear failed on landing. - [Incident 20000819029279I](https://openairdocs.org/incident/20000819029279I), Aug 19, 2000: Doug DC1010F (N364FE), Mobile, AL, Minor damage. (-23)All (4) tires on right main landing gear truck blew during take-off and landing. Aircraft damages due to rubber debris are: 1)the #3 engine fan section… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.