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Aircraft record

N140WE1975 Douglas DC-10-40F

DeregisteredUnclaimedSource: FAA, updated Oct 18, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 1, 2009.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched29 service difficulty reports

Registration
Deregistered
Last based in
Miami, FL
owner city / state
Owners
1
since 1998
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
29
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Last registered owner
Air Lease International One Lc
Owner type
Corporation
City, state
Miami, FL
Certificate issued
Sep 11, 1998
Canceled
May 1, 2009
Airworthiness
Standard · Transport
Airworthiness date
Sep 4, 1998

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Douglas
Model
DC-10-40F
Year
1975
Serial number
46920
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
380
Engines
3
Max takeoff weight
20,000 and over lb
Mode S code
A0A4A9

Engine

Make and model
P & W Jt9d Series
Type
Turbo-jet
Power
43,500 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 1998 – 2009Air Lease International One LcMiami, FL

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs published since 1998 that may apply (0)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

No ADs published since 1998 matched this airframe or engine model.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (29)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Flight controls · mechanism · lack of lubeOct 19, 2008

    UPON RETRACTING FLAPS 2 1/2 UNITS OF AILERON TRIM TO THE RT MUST BE USED TO KEEP WINGS LEVEL. PERFORMED AILERONS SYSTEM TEST IN ACCORDANCE WITH M/M 27-10-00. FOUND NORMAL, FLAP SYSTEM TEST IN ACCORDANCE WITH M/M 27-50-00. FOUND NORMAL SPOILER SYSTEM OPERATIONAL CHECK IN ACCORDANCE WITH M/M…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · warning system · malfunctionedAug 5, 2008

    ATC REPORT FOR DOOR OPEN ON ACFT. RETURN TO RAMP. INSPECTED ACFT. FOUND NO DOOR OPEN, NORMAL CONDITION IAW WITH MM 52-00-00. ALL CLOSED AND LIGHT OFF. (S)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine controls · throttle · obstructedJun 22, 2008

    UPON INITIATION OF TAKEOFF ROLL NR 3 POWER LEVER WOULD NOT ADVANCE BEYOND 128 EPR. RETURNED TO RAMP. OPENED ENGINE FOUND HYD TEMP C/P WIRE AROUND THROTTLE BELL CRANK BEHIND HYD FILTER MODULE. SECURED WIRE IAW M/M 20-30-07. OPS CHECK THROTTLE IAW MM 76-11-02 OPERATIONAL CHECK NORMAL. THROTTLE MOVES…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine indicating · indicator · faultyMay 17, 2008

    IN FLIGHT NR 2 ENGINE EGT INDICATOR FLUCTUATING 20 TO 30 DEGREES BOTH POINTER AND COUNTER ALL OTHER PARAMETERS NORMAL. REMOVED AND REPLACED NR 2 EGT INDICATOR CHECK GOOD IN ACCORDANCE WITH M/M 77-21-00 AND M/M 71-00-00.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · thermocouple · shortedMay 17, 2008

    IN FLIGHT NR 2 ENGINE EGT INDICATOR FLUCTUATING 20 TO 30 DEGREES BOTH POINTER AND COUNTER, ALL OTHER PARAMETERS NORMAL. TROUBLE SHOT IN ACCORDANCE WITH TAFY MANUAL 77-21-00, FOUND THERMO COUPLE SHORTED AT 6 O'CLOCK POSITION AND HARNESS ISOLATION HIGH, REMOVED AND REPLACED HARNESS IN ACCORDANCE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · door · damagedAug 3, 2007

    AFTER GEAR RETRACTION RED LEFT LGD GEAR LIGHT ON FWD AND F/E PANELS REMAINED ON. PERFORMED THE APPROPRIATE CHECK-LIST AND RETURN TO LANDING AFTER DUMPING FUEL TO MAX LANDING WEIGHT. REMOVED AND REPLACED MAIN LANDING GEAR DOOR IN ACCORDANCE WITH M/M 32-14-01; ACCOMPLISHED ADJ AND TEST IN ACCORDANCE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine oil · valve · unknownJun 6, 2007

    3 IDLE OIL PRESSURE 23 PSI. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE FILTER ADJUSTED OIL PRESSURE RELIEF VALVE IN ACCORDANCE WITH DC-10 M/M 71-00-01. PERFORMED ENGINE RUN OPERATIONAL NORMAL IN ACCORDANCE WITH 71-00-00.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · connector · looseMar 23, 2007

    ON ROTATION, NR 1 ENGINE REVERSER UNLOCK LIGHT CAME ON AND REMAINED ON; SHUT ENGINE DOWN AND RETURNED TO MIAMI. PERFORMED ELECTRICAL SYSTEM CHECK AND FOUND LOOSE CONNECTOR AT PRESSURE REG. S/O VALVE FROM PDM. TIGHTENED AND SECURED AS REQUIRED. NEEDS SYSTEM OPERATIONAL CHECK; REMOVED AND REPLACED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · cable · brokenMar 22, 2007

    ON TAKEOFF ROLL, NR 2 ENGINE REVERSER UNLOCK LIGHT CAME ON. ABORTED TAKEOFF AS SOON AS THROTTLES WERE ADVANCED. DEACTIVATED NR 2 ENGINE THRUST REVERSER AS PER MEL 78-1 (DDG) AFTER DEACTIVATION COMPLETED; CHECKED AT BLAST FENCE, VERIFIED SYSTEM AND FOUND NORMAL IN ACCORDANCE WITH M/M 71-00-00. NO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · line · damagedOct 12, 2006

    IN CRUISE FLIGHT TO MAINTAIN NR 1 ENGINE N1 ALIGNMENT WITH ALL OTHER ENGINES N1 NR 1 EPR INDICATING 1.15 NR 2 EPR 1.32 AND NR 3 EPR 1.32 ALL N2 ALIGNED. PERFORMED NR 1 CHECK AND CHECKED PT7, 4 SENSE AIR, FOUND LINE DAMAGE; REMOVED AND REPLACED LINE IAW MM 77-11-01; OPERATIONAL CHECK NORMAL ON…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 29 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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