# N392FE: 1975 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 CF6-6 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: 46626
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 23, 2003
- Certificate issued: March 17, 1997
- Last registry action: September 22, 2023
- Mode S code: A48AB9
- 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/N392FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=392FE
- Page: https://openairdocs.org/deregistered/N392FE-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 (70, newest 50)

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

- [SDR FDEA201412114107](https://openairdocs.org/sdr/FDEA201412114107), Dec 11, 2014: BATTERY PACK. FAILED. DURING SERVICE CHECK, FOUND EMERGENCY LIGHT BATTERY NR 1 LOW ALERT. REPLACED THE BATTERY PACK. OPS CHECKED GOOD.
- [SDR FDEA201408052076](https://openairdocs.org/sdr/FDEA201408052076), Aug 5, 2014: SKIN. CRACKED. LEFT WING FIXED LE VI FOUND EVIDENCE OF CRACKS AT THE TAI. TELESCOPING DUCT CUT OUT TOP CORNERS COMPLIES WITH EA 8-5710-T0309830 P1 BY REPAIRING USING SRM 57-40
- [SDR FDEA201403270594](https://openairdocs.org/sdr/FDEA201403270594), Mar 27, 2014: LAMP. INOPERATIVE. R1 DOOR SLIDE LIGHT WILL NOT TEST CORRECTLY. REPLACED LAMP IAW SMP. OPS NORMAL.
- [SDR FDEA201403190533](https://openairdocs.org/sdr/FDEA201403190533), Mar 19, 2014: CONNECTOR. LOOSE. R1 DOOR LIGHT FOR SLIDE INOPERATIVE. SECURED ELECTRICAL CONNECTOR ON WIRE LEAD TO PRESS TO TEST SWITCH. PRESS TO TEST SYSTEM FOR BATTERY AND LIGHT FUNCTION NORM
- [SDR FDEA201311232855](https://openairdocs.org/sdr/FDEA201311232855), Nov 23, 2013: BOTTLE. LOW PRESSURE. RIGHT ENTRY DOOR PNEUMATIC BOTTLE PRESSURE 0. FOUND DOOR R1 HANDLE IN THE EMERGENCY POSITION. RESET DOOR HANDLE & SERVICED DOOR ASSIST BOTTLE IAW MD10-10 MM 52-
- [SDR FDEA201307101522](https://openairdocs.org/sdr/FDEA201307101522), Jul 10, 2013: FIRE DETECTOR. FALSE ACTIVATION. THIRTY MINUTES AFTER TAKEOFF, RECEIVED A LEVEL 3 ALERT, LOWER CARGO FWD FIRE. DISCHARGED FIRE AGENT IAW PHASE 1 PROCEDEURES, RAN RED TABS. DIVERTED, CRASHED. FI
- [SDR FDEA201303010480](https://openairdocs.org/sdr/FDEA201303010480), Mar 1, 2013: WINDSHIELD. FAILED. ON FINAL APPROACH, MODERATE RIM ICE ACCUMULATATED ON F/O WINDSHIELD, ALMOST NO ICE ON CAPT SIDE. WINDSHIELD A/I HAD BEEN ON FOR ABOUT 10 MIN ON LOW ON BOTH SIDE
- [SDR FDEA201301040012](https://openairdocs.org/sdr/FDEA201301040012), Jan 4, 2013: RELAY. INTERMITTENT. AIR MANIFOLD NR 3 FAILED LEVEL 3 ALERT WHEN ANTI-ICE SELECTED ON DURING DESCENT. PERFORMED TEST OF THE PNEUMATIC PRESSURE SW IAW EA 8-3622-114705, SWITCH OPS NO
- [SDR FDEA201301030011](https://openairdocs.org/sdr/FDEA201301030011), Jan 3, 2013: RELAY. FAILED. AIR MANIFOLD NR 3 FAILED LEVEL 3 ALERT WHEN ANTI-ICE SELECTED ON, DURING DESCENT. PERFORMED A GVI OF PNUEMATIC DUCTS AND VALVES IN WING AND PYLON AREA. PERFORME
- [SDR FDEA201107152714](https://openairdocs.org/sdr/FDEA201107152714), Jul 15, 2011: SHAFT. SHEARED. NR1 ACM PACK RUNS ALMOST FULL HOT REGARDLESS OF RAM AIR DOOR AND PACK VALVE TRANSMITTER POSITIONS. REMOVED NR 1 ACM PACK, FOUND A BROKEN TURNBINE SHAFT. R & R A
- [SDR FDEA201107072608](https://openairdocs.org/sdr/FDEA201107072608), Jul 7, 2011: SPAR CAP. CRACKED. RT WING REAR SPAR CAP HAS 2 HOLES WITH CRACK INDICATION. ACCOMPLISHED LIMITED REPAIR REF EA 8-5710-147784. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 24 MONTHS.
- [SDR FDEA201106132224](https://openairdocs.org/sdr/FDEA201106132224), Jun 13, 2011: ANGLE. CORRODED. AFT CARGO COMPARTMENT AT STA 1841 FLOOR AFT FRAME ANGLE FOUND CORRODED FROM UNDERNEATH AT NUT PLATE HOLES FROM LONGERON 42L TO 42R. FABRICATED NEW ANGLE WITH 70
- [SDR FDEA201106112207](https://openairdocs.org/sdr/FDEA201106112207), Jun 11, 2011: ROLLER TRAY. CORRODED. 4 ROLLER TRAYS HAVE CORROSION, CENTER PIT BETWEEN STA 1700 TO 1781 CLEANED SURFACE CORROSION ON 3 TRAYS IAW SRM 51-21-01, VOL III. FABRICATED ONE ROLLER TRAY IA
- [SDR FDEA201106112206](https://openairdocs.org/sdr/FDEA201106112206), Jun 11, 2011: FLOORBEAM. CORRODED. CTR CARGO, AFT WALL FLOORBEAM ANGLE CORRODED ON AFT SIDE (AS VIEWED FROM AFT CARGO). R & R LT FLOORBEAM ANGLE SECTION, REF AFA3871, CLEANED AND TREATED CTR AND 
- [SDR FDEA201106062129](https://openairdocs.org/sdr/FDEA201106062129), Jun 6, 2011: SUPPORT. CORRODED. CENTER CARGO AFT WALL, CORROSION ON VERTICAL SUPPORT BEAM JUST RIGHT OF CTR AND JUST ABOVE FLOOR LINE. INSTALLED NEW VERTICAL SUPPORT BEAM AT STA 1781 IAW DWG A
- [SDR FDEA201006162031](https://openairdocs.org/sdr/FDEA201006162031), Jun 16, 2010: RELIEF VALVE. LEAKING. ON CLIMBOUT, GOT HYD 3 ELEV OFF ALERT WITH DECREASING HYD 3 QTY. FOLLOW ON ALERTS HYD 3 OFF AND ON FINAL APPROACH BACK TO DEPARTURE GOT HYD 3 FAIL. LOST ALL HYD
- [SDR FDEA201004221292](https://openairdocs.org/sdr/FDEA201004221292), Apr 22, 2010: PRESSURE SWITCH. FAILED. AT CRUISE ALTITUDE, RECEIVED LEVEL 3 MANIFOLD NR 1 FAIL ALERT. AIR SYS ISOLATED PROPERLY AND ALERT WENT AWAY. DIVERTED AND LANDED WITHOUT INCIDENT. R & R LT WIN
- [SDR FDEA201002210480](https://openairdocs.org/sdr/FDEA201002210480), Feb 21, 2010: TRANSDUCER. MALFUNCTIONED. ANTI-SKID R FAIL ON LANDING CYCLED AND NO CHANGE,ON 2ND. ATTEMPT TO LAND CAME ON AGAIN THEN WENT OUT, FLAPS 50 LANDING 4L CKED CFDS FOUND MSG. 324355, NR 7 WHEE
- [SDR FDEA201001100077](https://openairdocs.org/sdr/FDEA201001100077), Jan 10, 2010: ANTI-SKID SYS. FAILED. LEVEL 2 ANTI-SKID R FAIL ON FINAL W/GEAR DOWN. ANTI-SKID WOULD NOT TEST W/GEAR UP AFTER GO AROUND. DID TEST AND FAIL ONCE GEAR DOWN. R & R NR 7 WHEEL SPEED TRAN
- [SDR FDEA201001090064](https://openairdocs.org/sdr/FDEA201001090064), Jan 9, 2010: ANTI-SKID SYS. FAILED. GOT LEVEL 2 ANTI SKID FAIL ON FINAL. EXECUTED GA RAN QRH. UNEVENTFUL LANDING. HAD FIRE TRUCK LOOK AT BRAKES WITH INFARED. THEY STATED BRAKES WERE WARM NOT HOT. 
- [SDR FDEA201001050014](https://openairdocs.org/sdr/FDEA201001050014), Jan 5, 2010: ANTI-SKID SYS. FAILED. WHILE CONDUCTING ILS APPROACH TO RWY 36R AT MEM RECEIVED LVL 2 ALERT ANTI SKID RT FAIL EXECUTED MISSED APPROCH, RAN QRH. FAILED MANUAL ANTI-SKID CHECK WERE VECT
- [SDR FDEA200907042475](https://openairdocs.org/sdr/FDEA200907042475), Jul 4, 2009: FITTING. CRACKED. RIGHT WING NR 2 SLAT FOUND CRACKED AT INBOARD FITTING. REMOVED AND REPLACED RT WING NR 2 SLAT AND ADJUSTED IAW AMM 27-80-01-4.
- [SDR FDEA200906152113](https://openairdocs.org/sdr/FDEA200906152113), Jun 15, 2009: WEB. CRACKED. N/R206- 5 IN CRACK ON UPPER WEB INBD SIDE NR 3 PYLON APPROX 12 IN. FROM AFT PYLON MOUNT. REMOVED UPPER WEB ATNR 3 PYLON REF SRM 51-00-01. FABRICATED NEW WEB REF
- [SDR FDEA200901290379](https://openairdocs.org/sdr/FDEA200901290379), Jan 29, 2009: PRESSURE PANEL. CRACKED. LT MLG WHEEL WELL INBD WALL UPPER AFT CORNER HAS CRACK FROM STIFFENER GOING FWD TOWARD PREVIOUS REPAIR, VERIFIED AND MARKED USING ET, LOCATED ABOVE NR 1 HYD SYS
- [SDR 06FDEA1650](https://openairdocs.org/sdr/06FDEA1650), Apr 30, 2006: SKIN. BULGED. FOUND CENTER PIT STA 1731 ABOVE L45R TORQUE BOX WEB (SILL AREA) SKIN BULGE AND SHEARED RIVET. ENTERED IN ERROR WRONG AIRCRAFT, NO NON-ROUTINE N00200 FOR AIRCRAF
- [SDR 06FDEA1245](https://openairdocs.org/sdr/06FDEA1245), Mar 27, 2006: REPAIR. UNKNOWN. RT FUSELAGE EXTERNAL REPAIR IS IN CRITICAL AREA OF PRIMARY STATIC PORT. REWORKED REPAIR IAW FEDX EA 8-5330-96383 FUSELAGE - SKIN AT FORWARD CARGO DOOR HAS REPAI
- [SDR 06FDEA0535](https://openairdocs.org/sdr/06FDEA0535), Feb 3, 2006: SENSOR. OUT OF ADJUST. ON APPROACH TO KSMF AT FLAPS 22, SLAT EXTEND SELECTION OF FLAPS 35 CAUSE A SLAT DISAGREE. RAN QRH LANDED FLAPS 22/SLATEXT. FOUND SENSOR GAP BEYOND MAX LIMIT. AD
- [SDR 05FDEA00097](https://openairdocs.org/sdr/05FDEA00097), Jan 15, 2005: COMPUTER. MALFUNCTIONED. DURING APPROACH TO RWY 35R AT MCO GOT TOO LOW TERRAIN WARNING. AT 400 FEET ON GLIDE SLOPE AND LOC EXECUTED MISSED APPROACH AND RETURNED TO SAME RWY. THE SAME TH
- [SDR 04FDEA02982](https://openairdocs.org/sdr/04FDEA02982), Oct 22, 2004: FITTING. WORN. LT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND ALL HOLES HAVE EVIDENCE OF PITTING. REMOVED CORROSION AND PITTING FROM LUG AND BORES. FABBED AN
- [SDR 04FDEA02981](https://openairdocs.org/sdr/04FDEA02981), Oct 22, 2004: ROLLER. WORN. RT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND HOLES HAVE EVIDENCE OF PITTING. REMOVED PITTING AND CORROSION FROM LUG AND BORE. FABBED AND INS
- [SDR 04FDEA02952](https://openairdocs.org/sdr/04FDEA02952), Oct 18, 2004: LAVATORY. NOT SEATED. LAVATORY PAPER AND WASTE RECEPTACLE DOES NOT SEAL CORRECTLY. RESEALED LAVATORY PAPER AND WASTE RECEPTALE IAW MD10-10 SRM 51-41-01 VOL II AND EA 8-2540- 82478, S
- [SDR 04FDEA02951](https://openairdocs.org/sdr/04FDEA02951), Oct 18, 2004: PANEL. MISALIGNED. NR 1 PYLON PRECOOLER VENTILATOR PANEL ASSY PN AUB7054-501 FASTENER HOLES DO NOT ALIGN TO PYLON STRUCTURE. COMPLIED WITH EA 8-5480-81485 REV. A, NR 1 ENGINE VENT
- [SDR 04FDEA02950](https://openairdocs.org/sdr/04FDEA02950), Oct 18, 2004: FRAME. CRACKED. NR 2 ENGINE RT THRUST REVERSER TRAILING EDGE AFT FLANGE CRACKED APPROXIMATELY 6 INCHES FROM BOTTOM. COMPLIED WITH MFG EA 8-7830-81496
- [SDR 04FDEA02937](https://openairdocs.org/sdr/04FDEA02937), Oct 15, 2004: HINGE FITTING. CORRODED. RIGHT HAND INBOARD FLAP PIVOT ATTACH POINT, OUTBOARD LUG FACE, OUTER SURFACE CORRODED. REMOVED CORROSION FROM LUG FACE, FOUND TO BE OUT OF LIMITS IAW DC10 CMM 5
- [SDR 04FDEA02914](https://openairdocs.org/sdr/04FDEA02914), Oct 11, 2004: HINGE. CORRODED. LT IB FLAP OB HINGE PIVOT BORE FACE PITTED AND GOUGED (AIRFRAME SIDE) LOCATION NR 3. REMOVED BUSHING, REMOVED CORROSION, AND COMPLIED WITH EA 8-5750-81473 REF N
- [SDR 04FDEA02917](https://openairdocs.org/sdr/04FDEA02917), Oct 11, 2004: FITTING. CRACKED. CRACKED LONGERON END FITTING, AFT OF RIGHT HAND AIR CONDITIONING DOOR CUTOUT, LONGERON 35R, STA 535. REMOVED END FITTING IAW FEDEX SRM 51-35-01 VOLUME II PAGE 1
- [SDR 04FDEA02916](https://openairdocs.org/sdr/04FDEA02916), Oct 11, 2004: HINGE FITTING. CORRODED. LEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DACCMM 57-52-01, BORE FOUND OUT OF LIMITS, GENERATED RFTS, RE
- [SDR 04FDEA02915](https://openairdocs.org/sdr/04FDEA02915), Oct 11, 2004: SUPPORT. CORRODED. RIGHT HAND OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE CORRODED (INBOARD SUPPORT). REMOVED CORROSION IAW DACCMM 57-52-02. ETCHED AND PEENED IA
- [SDR 04FDEA02913](https://openairdocs.org/sdr/04FDEA02913), Oct 11, 2004: LONGERON. WORN. NR 1 ENGINE LEFT HAND CORE COWL UPPER CHAFE STRIP WORN. FABRICATED DOUBLER, FILLERS, AND STRAP FOR LONGERON REPAIR IAW FEDEX EA8-7110-81487. INSTALLED LONGERON 
- [SDR 04FDEA02912](https://openairdocs.org/sdr/04FDEA02912), Oct 11, 2004: SUPPORT. CORRODED. LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCM
- [SDR 04FDEA02911](https://openairdocs.org/sdr/04FDEA02911), Oct 11, 2004: SUPPORT. CORRODED. RIGHT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY 
- [SDR 04FDEA02910](https://openairdocs.org/sdr/04FDEA02910), Oct 11, 2004: SUPPORT. CORRODED. LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 3 HAS CORROSION IN BORE. REMOVED CORROSION IAW DACCMM 57-44-07. BEGINNING BORE 2.5850 INCH FINAL 2.626 INCH
- [SDR 04FDEA02908](https://openairdocs.org/sdr/04FDEA02908), Oct 11, 2004: SUPPORT. CORRODED. LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCM
- [SDR 04FDEA02907](https://openairdocs.org/sdr/04FDEA02907), Oct 11, 2004: HINGE FITTING. CORRODED. RIGHT HAND INBOARD FLAP PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION BEGINNING BORE 1.1875 INCH FINAL 1.2583 INCH MATERIAL REMOVED .0708 INCH IAW
- [SDR 04FDEA02906](https://openairdocs.org/sdr/04FDEA02906), Oct 11, 2004: SUPPORT. CORRODED. BORE CORRODED RIGHT WING INBOARD FLAP OUTBOARD HINGE LOWER SWIVEL BEARING. REMOVED CORROSION IAW DACCMM 57-44-07. ORIGINAL BORE 2.530 INCH FINAL 2.543 INCH MATE
- [SDR 04FDEA02905](https://openairdocs.org/sdr/04FDEA02905), Oct 11, 2004: SUPPORT. CORRODED. RIGHT WING INBOARD FLAP OUTBOARD HINGE LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACC
- [SDR 04FDEA02904](https://openairdocs.org/sdr/04FDEA02904), Oct 11, 2004: SKIN. MISREPAIRED. RIGHT HAND PRIMARY STATIC PORT FAILS RVSM INSPECTION FOR EXTERNAL DOUBLER MISMATCH RATIO IAW DC10 SRM 53-00-02 NOTE 2 (FIG 1 SHEET 2). REMOVED EXISTING FUSELAGE
- [SDR 04FDEA02903](https://openairdocs.org/sdr/04FDEA02903), Oct 11, 2004: HINGE. CORRODED. LEFT WING OUTBOARD FLAP INBOARD HINGE, LOCATION NR 4 BORE CORRODED. REMOVED CORROSION IAW DACCMM 57-44-08, INSPECTED IAW DACCMM 57-44-08 AND 20-11-02. PEENED IA
- [SDR 04FDEA02902](https://openairdocs.org/sdr/04FDEA02902), Oct 11, 2004: FITTING. DAMAGED. RIGHT HAND INBD FLAP PIVOT POINT OUTBOARD BORE HAS GROOVE MARK. REMOVED CORROSION IAW DAC CMM 57-52-01. BEGINNING DIAMETER 1.1875 INCH FINAL 1.2552 INCH . FABBE
- [SDR 04FDEA02901](https://openairdocs.org/sdr/04FDEA02901), Oct 11, 2004: SKIN. CORRODED. LEFT WING SKIN LOWER SURFACE IS CORRODED, STATION XORS 799 APPROX 19 INCHES AFT OF FORWARD SPAR CAP. SKIN HAS SMALL AMOUNTS OF PITTING. REMOVED CORROSION AND FO

All 70: https://openairdocs.org/deregistered/N392FE-2024-01-29/reports.md

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