# N362FE: Mcdonnell Douglas MD-10-10F, registration cancelled 2024-03-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 2, 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: 48261
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 24, 2002
- Certificate issued: January 16, 2001
- Last registry action: August 4, 2023
- Mode S code: A4143C
- Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- 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/N362FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=362FE
- Page: https://openairdocs.org/deregistered/N362FE-2024-03-02

From the FAA registry file of November 4, 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 (37)

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

- [SDR FDEA201507152225](https://openairdocs.org/sdr/FDEA201507152225), Jul 15, 2015: WARNING SYSTEM. FALSE ACTIVATION. NUMBER 1 AIR MANIFOLD FAIL ALERT AT CRZ FL 340 ENG & WING A/ION, PACKS 1 & 3 ON. DIVERTED & LANDED WITHOUT INCIDENT. PERFORMED NR 1 DECAY CHECK, PASSES 9 SEC, 7
- [SDR FDEA201502060465](https://openairdocs.org/sdr/FDEA201502060465), Feb 6, 2015: INDICATOR. FAILED. L1 SLIDE TEST LIGHT DOES NOT ILLUMINATE WHEN PUSHED TO TEST. R & R L1 DOOR REMOTE SLIDE PACK PRESSURE PRESS TO TEST INDICATOR. OPERATIONS TESTED NORMAL.
- [SDR FDEA201406231527](https://openairdocs.org/sdr/FDEA201406231527), Jun 23, 2014: SKIN. CRACKED. EVIDENCE OF A CRACK IN THE NR 3 PACK BAY DOOR FRAME. NR 3 PACK DOOR FRAME/SKIN DAMAGE REPAIRED REF MD10/DC 10 SRM 53-50-00 FIG A SHEET 3.
- [SDR FDEA201406231528](https://openairdocs.org/sdr/FDEA201406231528), Jun 23, 2014: SUPPORT. CRACKED. SUSPECT CRACK ON UPPER AFT T CHORD OF DOOR CUT OUT STATION 535 ON INBD SIDE FROM RIVET HOLE TO EDGE. PERFORMED HFEC ON UPPER AFT T CHORD OF DOOR CUT OUT OF NR 3
- [SDR FDEA201405301230](https://openairdocs.org/sdr/FDEA201405301230), May 30, 2014: SKIN. CRACKED. ON WALK AROUND FOUND POSSIBLE CRACK ON LT WING AT FWD INBD CORNER OF FUEL PNL. CONFIRMED CRACK AT FWD INBD CORNER OF FUEL PNL BY HFEC INSPECTION IAW NDTSPM PT 6
- [SDR FDEA201403140509](https://openairdocs.org/sdr/FDEA201403140509), Mar 14, 2014: SPAR CAP. CRACKED. DURING C7, B9 CHECK AT LAX CRACK FOUND IN HOLE B & C IN REAR SPAR LOWER CAP AT XORS 345.75. ADDITIONAL INSPECTION FOUND UPPER SPAR CAP FLANGE TO HAVE A 2.8 INCH
- [SDR FDEA201212284394](https://openairdocs.org/sdr/FDEA201212284394), Dec 28, 2012: WIRE. DAMAGED. ON POST FLIGHT CHECK FOUND NR 3 AVIONICS RACK COOLING BREAKER POPPED. RESET BREAKER AND IT POPPED AGAIN. REMOVED DAMAGED WIRING AND REPAIRED FOLLOWING WIRES. B1
- [SDR FDEA201202260688](https://openairdocs.org/sdr/FDEA201202260688), Feb 26, 2012: SKIN. CORRODED. CORROSION FOUND ON EXTERNAL FUSELAGE SKIN AT BS 1109 AT S46R. REPAIRED SKIN IAW SRM 53-20-00, FIG 6, REPAIR CLASSIFED AS MAJOR.
- [SDR FDEA201202230673](https://openairdocs.org/sdr/FDEA201202230673), Feb 23, 2012: CARGO TRACK. WORN. MAIN DECK CARGO TRACK AT BS 1387.5, LBL 72 HAS TWO WORN AND BROKEN SCALLOP LOBES, REPAIRED CARGO TRACK IAW SRM 53-70-00 FIG 1.
- [SDR FDEA201202200627](https://openairdocs.org/sdr/FDEA201202200627), Feb 20, 2012: SKIN. TORN. RIGHT OTBD T/E FLAP LOWER SKIN HAS OIL CANNING ABOUT 45" OTBD OF FLAP VANE CARTRIDGE CUT-OUT AND 25" FWD OF T/E. REPAIRED RT WING OTBD T/E FLAP LOWER SKIN IAW S
- [SDR FDEA201202160595](https://openairdocs.org/sdr/FDEA201202160595), Feb 16, 2012: SKIN. CORRODED. EXTERNAL FUSELAGE SKIN BULGING AT BS 1621 BETWEEN S47-48R. REPAIRED EXTERNAL FUSELAGE SKIN IAW SRM 53-20-00, FIG 6, SHEET 5 AND 6, REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201202120563](https://openairdocs.org/sdr/FDEA201202120563), Feb 12, 2012: SEAT TRACK. WORN. MAIN DECK SEAT TRACK AT BS 755 AT LBL 47.5 HAS CHIPPED LOBES. REMOVED AND REPLACED MAIN DECK SEAT TRACK BETWEEN BS 725 TO 765 AT LBL 47.5 IAW SRM 51-31-01 AND S
- [SDR FDEA201102090510](https://openairdocs.org/sdr/FDEA201102090510), Feb 9, 2011: LIGHT. INOPERATIVE. L1 DOOR SLIDE PTT LIGHT INOP. WIRE THAT ATTACHES TO C BATTERY HOUSING BROKEN OFF. RELEASED FOR SERVICE IAW MEL: 25-61-01, PRESS VERIFIED IAW MEL 25-61-01. ACFT 
- [SDR FDEA201102090514](https://openairdocs.org/sdr/FDEA201102090514), Feb 9, 2011: ANTENNA. MALFUNCTIONED. CONSTANT ELT TONE ON 121.5 BOTH RADIOS. OVERHEAD COCKPIT ELT PANEL RESET NO HELP, RESET AT ELT NO HELP. TONE GOES AWAY THEN COMES BACK AFTER 5 TO 10 MINUTES. WI
- [SDR FDEA201004061088](https://openairdocs.org/sdr/FDEA201004061088), Apr 6, 2010: WEB. CRACKED. NR 1 RT SLAT DAMAGED AT INBD WEB/RIB STRUCTURE R & R FITTING PN ARB701602 IAW DWG ARB 7016 VIEW CC AND SRM 51-31-01, VOL II. R & R WEB PN ARB7128-24 IAW SRM 51-
- [SDR FDEA201003230968](https://openairdocs.org/sdr/FDEA201003230968), Mar 23, 2010: FEEDER CABLE. DAMAGED. WIRE NR C501-19-00A AT EXTERNAL POWER PLUG PIN "A" HAD OVERHEAT/ARCING DAMAGE AND POWER RECEPTACLE R5-1065 PIN "A" HOLE MELTED DUE TO OVERHEAT CONDITION. WIRE N
- [SDR FDEA200909173323](https://openairdocs.org/sdr/FDEA200909173323), Sep 17, 2009: RELAY. MALFUNCTIONED. REJECTED T/O DUE TO: LEVEL 1 ALERT: REV 1, PRESS FAIL T, DUPLICATED REV 1 PRESS FAULT ON 3 DIFFERENT TAXI/RUN-UP TESTS IAW JRH CHAPT 5 AND CHPT 4-8. REMOVED AND
- [SDR FDEA200908213070](https://openairdocs.org/sdr/FDEA200908213070), Aug 21, 2009: CYLINDER. SHEARED. WHILE CONFIGURING FOR LANDING, RECEIVED A LEVEL 2 SLAT DISAGREE ALERT. RAN QRH PROCEDURE WHICH REQUIRED A FLAPS 22/RETRACT LANDING. LANDED ILS 36C CAPTAINS LAND
- [SDR FDEA200903060858](https://openairdocs.org/sdr/FDEA200903060858), Mar 6, 2009: LINE. LOOSE. NR 2 ENG OIL QTY DROPPED FROM 12 QTS TO 3 QTS IN 2HRS. TEMP/PRESS NORMAL. DECREASED TO 2 QTS AT IDLE WITH DECREASING PRESSURE. SHUTDOWN NR 2. NR 2 ENG AND FOUND
- [SDR FDEA200903040835](https://openairdocs.org/sdr/FDEA200903040835), Mar 4, 2009: PUSH-PULL CABLE. DAMAGED. AT TOP OF DESCENT NR 2 ENG WOULD NOT RETARD BELOW 74 PERCENT N1. NR 2 THROTTLE WAS AT LEAST TWO KNOB WIDTHS ABOVE NR 1 AND NR 3 THROTTLES. SHUTDOWN NR 2 ENG ON 
- [SDR FDEA200812115180](https://openairdocs.org/sdr/FDEA200812115180), Dec 11, 2008: BEARING. FAILED. NR 1 TIRE ASSY OUTSIDE BEARING FAILURE. REMOVED WHEEL AND BRAKE ASSY FROM NR 1 AXLE LT MLG TRUCK ASSEMBLY TAG NR 5023BO. REPLACED LEFT MAIN LANDING GEAR TRUCK B
- [SDR 07FDEA02482](https://openairdocs.org/sdr/07FDEA02482), Jul 13, 2007: SKIN. CORRODED. CORROSION POSSIBLE ON FUSELAGE SKIN CORROSION LIMITED TO LONGERON DAMAGE WHICH WAS REPAIRED PER 53-10-00 VOL 1 OF MD10-10.
- [SDR 07FDEA01503](https://openairdocs.org/sdr/07FDEA01503), Apr 13, 2007: PROXIMITY SENSOR. UNKNOWN. ON DEPARTURE RECEIVED LVL 2 CARGO DOOR FWD "B" ALERT, RAN QRH AND ALERT DISAPPEARED, MEL 52-40-01-05: CARGO DOOR FWD "B" ALERT INOP. VERIFY DOOR IS CLOSED AND L
- [SDR 06FDEA03585](https://openairdocs.org/sdr/06FDEA03585), Oct 4, 2006: BRACKET. CRACKED. RT O/B SLAT DRIVE O/B BRACKET FWD FLANGE RADIUS IS CRACKED. SEQ CARD 735. REMOVED AND REPLACED RT O/B SLAT DRIVE MECHANISM.
- [SDR 05FDEA01029](https://openairdocs.org/sdr/05FDEA01029), Apr 16, 2005: KEELBEAM. CRACKED. AUXILIARY POWER UNIT KEEL CAP ASSEMBLY HAS 9 INCH CRACK FROM FUSELAGE STATION 2019 TO STATION 2028 AT STRINGER 45 RIGHT. REPAIRED STRINGER IAW EA 8-5310-83868, 
- [SDR 05FDEA01028](https://openairdocs.org/sdr/05FDEA01028), Apr 16, 2005: KEELBEAM. CRACKED. AUXILIARY POWER UNIT KEEL CAP ASSEMBLY HAS 9 INCH CRACK FROM FUSELAGE STATION 2019 TO STATION 2028 AT STRINGER 45 RIGHT. REPAIRED STRINGER IAW EA 8-5310-83868, 
- [SDR 04FDEA03168](https://openairdocs.org/sdr/04FDEA03168), Nov 18, 2004: DOOR. VIBRATES. 14000 FT HEAVY VIBRATION SLOWED AND LANDED WITH NO PROBLEM, EVEN WITH GEAR DOWN HAD VIBRATION. "DECLARED EMERGENCY" HAD FIRE TRUCKS STANDING BY. REMOVED AND REP
- [SDR 03FDEA01465](https://openairdocs.org/sdr/03FDEA01465), Sep 9, 2003: HINGE BRACKET. CORRODED. LT OUTBOARD FLAP INBOARD HINGE BRACKET, CORROSION REPAIR (P/N ARC0502-11) LT O/B FLAP I/B HINGE BRACKET CORROSION REPAIR,P/N ARC,0502-11 CLOSED ON 09/09/2003 FE
- [SDR 03FDEA01466](https://openairdocs.org/sdr/03FDEA01466), Sep 9, 2003: HINGE BRACKET. CORRODED. RT OUTBOARD FLAP- OB HINGE BRACKET CORROSION REPAIR (P/N ARC0503) COMPLIED WITH EA 8-5750-72274_WINGS RT O/B FLAP-O/B HINGE BRACKET CORROSION REPAIR P/N ARC, 05
- [SDR 03FDEA01455](https://openairdocs.org/sdr/03FDEA01455), Sep 7, 2003: ARM. CORRODED. WINGS-OUTBOARD FLAP REWORK OF CARRAGE SUPPORT ARM P/N ARC 2177. COMPLIED WITH E.A. 8-5740-72289. WINGS-OUTBD FLAPS REWORK OF CARRAGE SUPPORT ARM P/N ARC 2177.
- [SDR 03FDEA01456](https://openairdocs.org/sdr/03FDEA01456), Sep 7, 2003: BOLT. INACCURATE. WINGS-RIBS AND BULKHEADS-LT OUTBOARD FLAP HINGE STUD BOLT SUBSTITUTION. COMPLIED WITH E.A.8-5710-72287. WINGS-RIBS AND BKHDS- FLAP HINGE STUD BOLT SUBSTITUTION.
- [SDR 03FDEA01457](https://openairdocs.org/sdr/03FDEA01457), Sep 7, 2003: WEB. CRACKED. EXHAUST SYSTEM THRUST REVERSER SUPPORT WEB CRACK REPAIR. COMPLIED WITH E.A.8-7830-72281. EXHAUST SYSTEM THRUST REVERSER SUPPORT ASSY WEB CRACK REPAIR.
- [SDR 03FDEA01458](https://openairdocs.org/sdr/03FDEA01458), Sep 7, 2003: SUPPORT. CRACKED. THRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR. COMPLIED WITH E.A.8-7830-72283. EXHAUST-THRUST REVERSER-SUPPORT ASSY TORQUE BOX WEB REPAIR.
- [SDR 03FDEA01459](https://openairdocs.org/sdr/03FDEA01459), Sep 7, 2003: CASE. GOUGED. GOUGES IN EXTERIOR OF NR 2 FAN FRAME CASE. COMPLIED WITH E.A. 8-7220-72285 ENGINES-DISPOSITION OF GOUGES IN EXTERIOR OF NR 2 ENGINE FAN FRAME CASE.
- [SDR 03FDEA01387](https://openairdocs.org/sdr/03FDEA01387), Aug 26, 2003: SUPPORT. CRACKED. COMPLY WITH E.A. 8-7210-72270- ENGINE-BASIC- FAN STATOR SUPPORT HALF, CRACK REPAIR. ENGINE-BASIC FAN STATOR SUPPORT HALF CRACK REPAIR. CLOSED ON 08/25/2003 FEDE
- [SDR 03FDEA01383](https://openairdocs.org/sdr/03FDEA01383), Aug 25, 2003: THRUST REVERSER. CRACKED. COMPLY WITH EA 8-7832-72265 EXHAUST-THRUST REV- FIXED BODY UPPER ANGLE CRACK REPAIR. EXHAUST-THRUST REV FIXED BODY UPPER ANGLE CRACK REPAIR.
- [SDR 03FDEA01334](https://openairdocs.org/sdr/03FDEA01334), Aug 18, 2003: SUPPORT ANGLE. CRACKED. LEFT WING I/B FLAP FAIRING PANEL SUPPORT STRUCTURE ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-31-01 AT MAE ON N00420 WO 23696.

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