# N366FE: 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: 46602
- Year built: 1971
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 31, 2007
- Certificate issued: December 2, 1997
- Last registry action: July 18, 2023
- Mode S code: A42318
- 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/N366FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=366FE
- Page: https://openairdocs.org/deregistered/N366FE-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 (67, newest 50)

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

- [SDR FDEA201506051699](https://openairdocs.org/sdr/FDEA201506051699), Jun 5, 2015: DOOR. CRACKED. UPON ARRIVAL FOUND FWD LOWER CORNER OF FWD LOWER CARGO DOOR DAMAGED. FWD CARGO DOOR CORNER DAMAGED, OK FOR SERVICE IAW EA 8-5230-T0317891. COMPLIED WITH PART 1 
- [SDR FDEA201505241627](https://openairdocs.org/sdr/FDEA201505241627), May 24, 2015: PANEL. MISSING. ON WALK AROUND NOTICED FWD INBD PANEL MISSING ON NR 1 PYLON LE. REPLACED PANEL WITH SERVICEABLE PANEL.
- [SDR FDEA201504081169](https://openairdocs.org/sdr/FDEA201504081169), Apr 8, 2015: CONNECTOR. NOT SEATED. EMER PWR TEST FAIL, LEVEL ONE ALERT ON PREFLIGHT. RESET 3 FUEL LEVERS & PERFORMED SYS TEST ALSO RESEATED BATTERY CHARGER CONNECTORS ON CHARGER. PREFORMED SYSTEM
- [SDR FDEA201503271102](https://openairdocs.org/sdr/FDEA201503271102), Mar 27, 2015: UNKNOWN. FAILED. ON PREFLIGHT EMER POWER TEST FAILED. CALLED MX.
- [SDR FDEA201407261981](https://openairdocs.org/sdr/FDEA201407261981), Jul 26, 2014: POWER SUPPLY. FAILED. DURING EMERGENCY LIGHT TEST, RECEIVED LEVEL 1 ALERT; EMERGENCY LIGHT BATTERY ONE LOW. R & R EMERGENCY LIGHTS POWER SUPPLY. OPS CHECKED GOOD. ACFT OK FOR SERVICE
- [SDR FDEA201406011246](https://openairdocs.org/sdr/FDEA201406011246), Jun 1, 2014: SKIN. CRACKED. APPEARS TO BE A CRACK IN RADIUS ON LT INBD FUELING PNL. PERFORMED HFEC INSP ON NEW CUT OUT IAW NTM PT 6, NO CRACK INDICATION FOUND. FABRICATED REPAIR DOUBLER & 
- [SDR FDEA201310152511](https://openairdocs.org/sdr/FDEA201310152511), Oct 15, 2013: SPAR. CRACKED. LEFT HORIZONTAL STABILIZER REAR SPAR UPPER ANGLE VERTICAL TANG HAS TWO CRACKS AT THE UPPER ROW OF FASTENERS COMING OUT FROM UNDER WASHER , SECOND AND THIRD FAST
- [SDR FDEA201310042412](https://openairdocs.org/sdr/FDEA201310042412), Oct 4, 2013: SUPPORT FITTING. CRACKED. MCD LOWER FRAME 6 SUPPORT FITTING IS CRACKED AT "C" HOLE. VERIFIED WITH HFEC AND BORESCOPE. R & R NR 6 SUPPORT FITTING MCD SPOOL REF SRM 51-31-01, VOL II.
- [SDR FDEA201309252311](https://openairdocs.org/sdr/FDEA201309252311), Sep 25, 2013: SILL. CORRODED. AFT LOWER CARGO COMPARTMENT DOOR SILL LOWER WEB AT BS 1835, JUST AFT OF AFT LATCH SPOOL FITTING, DOOR SILL WEB IS CORRODED. REMOVED CORROSION IAW SRM 53-50-00. 
- [SDR FDEA201302040262](https://openairdocs.org/sdr/FDEA201302040262), Feb 4, 2013: SWITCH. FAILED. R1 EVACUATION SLIDE PRESSURE PRESS TO TEST INDICATING INOPERATIVE. R & R R1 DOOR ESCAPE SLIDE PRESSURE PRESS-TO-TEST SWITCH IAW MM 25-61-03-2, OPS CHECKED GOOD,
- [SDR FDEA201211284193](https://openairdocs.org/sdr/FDEA201211284193), Nov 28, 2012: BULKHEAD WEB. CRACKED. RIGHT BULKHEAD CRACKED 25 INCHES FWD OF BS 1521 AND 19 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED BULKHEAD IAW SRM 53-00 -01, FIG 10.
- [SDR FDEA201109163910](https://openairdocs.org/sdr/FDEA201109163910), Sep 16, 2011: SKIN. DENTED. LEFT INBD FLAP UPPER SURFACE, DENTED 86" FROM INBD AND 6.5" FROM T/E. FOUND OUT OF LIMITS IAW SRM 51-80-01, PG 1, PARA 2. REPAIRED SKIN IAW SRM 57-00-01, FIG 4.
- [SDR FDEA201109163909](https://openairdocs.org/sdr/FDEA201109163909), Sep 16, 2011: SKIN. CORRODED. RIGHT WING TE FLAP UPPER SKIN CORRODED OUT OF LIMITS. REPAIRED SKIN IAW SRM 57-10-00, FIG 86.
- [SDR FDEA201109133864](https://openairdocs.org/sdr/FDEA201109133864), Sep 13, 2011: CABLE. OUT OF LIMITS. R1 DOOR SEQUENCE CABLE FOR AIR BOTTLE IS BINDING FOUND CABLE ADJUSTMENT OUT OF LIMITS. CABLE MOVEMENT GOOD. ADJUSTED AIR BOTTLE CABLE IAW MM 52-11-00-5. OPS CHE
- [SDR FDEA201109133866](https://openairdocs.org/sdr/FDEA201109133866), Sep 13, 2011: MOTOR. BINDING. R1 DOOR SEQUENCE CABLE FOR DECLUTCH IS BINDING. REMOVED AND REPLACED AC MOTOR AND ADJUSTED DECLUTCH CABLE IAW MM 52-11-01-2 AND 52-11-00-5. OPS CHECKED GOOD IAW
- [SDR FDEA201109133865](https://openairdocs.org/sdr/FDEA201109133865), Sep 13, 2011: CABLE. BINDING. R1 DOOR SEQUENCE CABLE FOR UPLOCK IS BINDING REMOVED AND REPLACED UPLOCK/CLOSE CABLE IAW AMM 52-11-12-2. ADJUSTED IAW AMM 52-11-00-5. OPS CHECKED GOOD.
- [SDR FDEA201109093809](https://openairdocs.org/sdr/FDEA201109093809), Sep 9, 2011: ROLLER. GOUGED. LEFT INBOARD FLAP WELL LOWER FORWARD ROLLER FITTING ASSY GOUGED. R & R LEFT INBOARD LOWER DUAL BRACKET ASSY IAW SRM 51-31-01.
- [SDR FDEA201109083769](https://openairdocs.org/sdr/FDEA201109083769), Sep 8, 2011: SEAT TRACK. WORN. SEAT TRACK, FS 1251 LBL 75, HAS WORN LOBE. CHECKED DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG. 5. R & R SEAT TRACK IAW SRM 53-70-00 FIG 1 S
- [SDR FDEA201109083767](https://openairdocs.org/sdr/FDEA201109083767), Sep 8, 2011: SEAT TRACK. WORN. SEAT TRACK FS 1320 RBL 28 HAS WORN LOBE. FOUND OUT OF LIMITS IAW SRM 53-70-00 FIG 5. CUT OUT DAMAGED PART REPAIRED IAW SRM 53-70-00 FIG 1 AND SRM 51-31-01. MAJO
- [SDR FDEA201106032103](https://openairdocs.org/sdr/FDEA201106032103), Jun 3, 2011: BATTERY. FAILED. DURING PREFLIGHT FOUND EMERGENCY LIGHT TEST SHOWS "EMER LT BATT 1 FAIL". R & R EMERGENCY LIGHTING BATTERY IAW AMM 33-51-01-4, OK FOR SERVICE.
- [SDR FDEA201106032102](https://openairdocs.org/sdr/FDEA201106032102), Jun 3, 2011: LENS. DAMAGED. DURING PREFLIGHT CHECK FOUND L1 DOOR EMERGENCY LIGHT LENS DAMAGED ON FLOOR. RELEASED FOR SERVICE IAW MEL: 33-50-02. REPLACED L1 DOOR EMERGENCY LIGHT LENS COVER 
- [SDR FDEA201106032101](https://openairdocs.org/sdr/FDEA201106032101), Jun 3, 2011: LENS. DAMAGED. DURING PREFLIGHT CHECK FOUND L1 DOOR EMERGENCY LIGHT LENS DAMAGED ON FLOOR. RELEASED FOR SERVICE IAW MEL: 33-50-02.
- [SDR FDEA201103070903](https://openairdocs.org/sdr/FDEA201103070903), Mar 7, 2011: SWITCH. FAILED. FOUND NR 2 ENGINE FIRE AGENT 1 LOW LIGHT ILLUMINATED WHILE PREFORMING ENGINE RUN CHECK LIST FOR REQUAL. TROUBLESHOT PROBLEM TO A BAD AGENT 1 LOW SWITCH, L2-216,
- [SDR FDEA201102150566](https://openairdocs.org/sdr/FDEA201102150566), Feb 15, 2011: ENGINE. VIBRATION. SHUTDOWN ENG NR 1 INFLIGHT FOR UNUSUAL VIBRATIONS. VIBES START AT 91 PERCENT - AND VERY NOTICABLE ABOVE 94 PERCENT - LIGHT TO MEDIUM "SHUDDER" RAPTED VIBRATION.
- [SDR FDEA201010314199](https://openairdocs.org/sdr/FDEA201010314199), Oct 31, 2010: BATTERY. INOPERATIVE. DURING THE EMERGENCY LIGHT TEST RECEIVED EMERG BAT 1 LOW ALERT. R & R NR1 EMERGENCY LIGHT BATTERY REF33-51-01-4-0. OPS CHECKED GOOD ACFT OK TO CONTINUE.
- [SDR FDEA201001190178](https://openairdocs.org/sdr/FDEA201001190178), Jan 19, 2010: HANDLE. MALFUNCTIONED. ON FIRST LANDING ATTEMPT, GOT 3 RED ON PANEL AND CONFIG PAGE (TRIED PUSHING DOWN ON HANDLE, NO HELP). RAN CHECKLIST AND PUT GEAR HANDLE DOWN THE SECOND TIME WIT
- [SDR FDEA200909273392](https://openairdocs.org/sdr/FDEA200909273392), Sep 27, 2009: ENGINE. MALFUNCTIONED. ABORT TAKEOFF, 75 KNOTS, ENG 3 EXCEEDANCE ON N2 PEAK 101, .2 RED: 101.0 FOR 2.3 SECONDS NO RESTRICTION, REF: AMM 72-00-00-6, NR 3 ENGINE N2 EXCEEDANCE 101.2 WIL
- [SDR FDEA200902100498](https://openairdocs.org/sdr/FDEA200902100498), Feb 10, 2009: SKIN. CORRODED. LOWER FUSELAGE DISHED RIVET AT LONG 48L STA 1761. REPAIRED AREA REF SRM 53-20-00.
- [SDR FDEA200902100497](https://openairdocs.org/sdr/FDEA200902100497), Feb 10, 2009: SKIN. CORRODED. LOWER FUSELAGE DISHED RIVET AT LONG. 46L STA 1741. REPAIRED AREA REF SRM 53-20-00.
- [SDR FDEA200902100496](https://openairdocs.org/sdr/FDEA200902100496), Feb 10, 2009: SKIN. CORRODED. LOWER FUSELAGE DISHED RIVET AT LONG 441 STATION 1682. REPAIRED FUSELAGE SKIN IAW DC 10 SRM 53-20-00 FIG 6.
- [SDR FDEA200901150209](https://openairdocs.org/sdr/FDEA200901150209), Jan 15, 2009: LINK. DAMAGED. RIGHT MAIN GEAR INDICATED UNSAFE ON DEPARTURE COMPLIED WITH QRH AND DIVERTED TO LAX. FOUND RT CRANK ASSY UPPER BOLT NUT MISSING. LINK ASSY FOUND DAMAGED REMOVED
- [SDR FDEA200809093782](https://openairdocs.org/sdr/FDEA200809093782), Sep 9, 2008: PUMP. LEAKING. 35 MINUTES INTO FLT, ENG NR 2 OIL QTY DROPPED TO ZERO, TEMP 7 PRESSURE NORMAL. PRESSURE FLUCTUATED CONSTANTLY DECREASING TO APPROX (15 PSI) FLUCTUATING /- 5 PSI
- [SDR 08FDEA03782](https://openairdocs.org/sdr/08FDEA03782), Sep 9, 2008: OIL SYSTEM. LOW. 35 MINUTES INTO FLT ENG NR 2 OIL QTY DROPPED TO ZERO. TEMP 7 PRESSURE NORMAL. PRESSURE FLUCTUATED CONSTANTLY DECREASING TO APPROX (15 PSI) FLUCTUATING /- 5 PSI 
- [SDR 08FDEA02167](https://openairdocs.org/sdr/08FDEA02167), Jun 5, 2008: NONE. NONE. REJECTED TAKEOFF FOR WINDSHEAR AURAL ALERT 80 KTS,34 DEG C ,386K FACT 05 JUN08 21:47 AFW U CHECKED PER AMM 05-56-00 AND 05-57-00, ACFT OK FOR SERVICE CHECKED PE
- [SDR 07FDEA04880](https://openairdocs.org/sdr/07FDEA04880), Nov 20, 2007: FRAME. MISREPAIRED. DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 840 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR H
- [SDR 07FDEA04879](https://openairdocs.org/sdr/07FDEA04879), Nov 20, 2007: SKIN. MISREPAIRED. DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON LT DROOPED L/E SKIN WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW ON
- [SDR 07FDEA04878](https://openairdocs.org/sdr/07FDEA04878), Nov 20, 2007: DOUBLER. DAMAGED. DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON EXTERNAL SKIN AT FWD CARGO DOOR AFT JAMB WAS FOUND DAMAGED. REPAIR AS BEEN REPLACED WITH A NEW ONE IAW SR
- [SDR 07FDEA04877](https://openairdocs.org/sdr/07FDEA04877), Nov 20, 2007: FRAME. MISREPAIRED. DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 879 BETWEEN LONG NR 47R AND 47L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR H
- [SDR 07FDEA04876](https://openairdocs.org/sdr/07FDEA04876), Nov 20, 2007: FRAME. MISREPAIRED. DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 824 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR H
- [SDR 07FDEA04875](https://openairdocs.org/sdr/07FDEA04875), Nov 20, 2007: FRAME. MISREPAIRED. DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 859 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA REPAIR HA
- [SDR 07FDEA04860](https://openairdocs.org/sdr/07FDEA04860), Nov 19, 2007: FITTING. CRACKED. DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION LT SIDE BAY JAMB STRUCTURE FRAME TO STA 528 DEFORMED CORROSION AND CRACK LONG 
- [SDR 07FDEA04857](https://openairdocs.org/sdr/07FDEA04857), Nov 19, 2007: FRAME. DAMAGED. DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), AVIONIC COMPT AT STA 449 RT AND X= -10 FRAME WITH HOLE OVALIZED PERFORMED REPAIR FOR SRM 53-30-00
- [SDR 07FDEA04855](https://openairdocs.org/sdr/07FDEA04855), Nov 19, 2007: SKIN PANEL. CRACKED. DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), LT WING T/E ON UPPER SKIN OUTBOARD FLAP XOF 620 FOUND DENT 1" BY 1" AND A TEE ANGLE WITH CRACK 1 
- [SDR 07FDEA04852](https://openairdocs.org/sdr/07FDEA04852), Nov 19, 2007: FITTING. CORRODED. DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING THE HOLES OF THE BOLTS WITH CORROSION. PERFORMED CORRO
- [SDR 07FDEA04849](https://openairdocs.org/sdr/07FDEA04849), Nov 19, 2007: FITTING. CRACKED. DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), CTR SECTION BOX WHEEL WELL AREA STA 1370 LT SIDE XCW 31.500 KEEL FITTING APB7078-1 WITH CRACK 5" 
- [SDR 07FDEA04846](https://openairdocs.org/sdr/07FDEA04846), Nov 19, 2007: DOOR FRAME. DEFORMED. DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION COMPT LT SIDE BAY JAMB STRUCTURE FRAME AT STA 486 DEFORMED REPAIRED FOR SRM 53
- [SDR 07FDEA04845](https://openairdocs.org/sdr/07FDEA04845), Nov 19, 2007: FRAME. CRACKED. DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK) PYLON NR 3 FOUND INTERNAL SIDE FRAME BROKEN AND DEFORMED. REPLACED STRAP P/N AVB7123-3, ANGLE P/N 
- [SDR 07FDEA04844](https://openairdocs.org/sdr/07FDEA04844), Nov 19, 2007: STRINGER. CRACKED. DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION LT SIDE FROM STA 561 TO STA 587 STRINGER 48 WITH CRACK AND SEVERAL CORROSION R
- [SDR 07FDEA04843](https://openairdocs.org/sdr/07FDEA04843), Nov 19, 2007: CHANNEL. CORRODED. DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK) FOUND IN LOWER FWD CARGO LIGHT CORROSION ON CHANNEL FROM STA 759 TO STA 879 X= 59. REMOVED CORROSI
- [SDR 07FDEA04671](https://openairdocs.org/sdr/07FDEA04671), Oct 24, 2007: STIFFENER. CRACKED. VANE AIR CONDITION COMPARTIMENT LT PACK N°2 INTERNAL SIDE STA 475 TEE P/N NCA6048-105 WITH CRACK 4 INCH. REPAIRED STIFFENER FOR SRM 53-40-00 FIG 10 VOL I.

All 67: https://openairdocs.org/deregistered/N366FE-2024-01-29/reports.md

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