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Aircraft record

N142WEDouglas DC-10-40F

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Feb 10, 2011.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched5 service difficulty reports

Registration
Deregistered
Last based in
Miami, FL
owner city / state
Owners
1
since 2009
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
5
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Air Lease International Three Lc
Owner type
Corporation
City, state
Miami, FL
Certificate issued
Feb 2, 2009
Canceled
Feb 10, 2011

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
Serial number
46966
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
A0AC17

Engine

Type
Turbo-jet

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

Ownership history

Ownership history from FAA records
  1. 2009 – 2011Air Lease International Three LcMiami, FL

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (5)

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.

  • Nacelles and pylons · skin · corrodedOct 12, 2000

    DURING C-CHECK AT ALITALIA, THE FITTING ELEMENT INSIDE THE AIR INTAKE DUCT ON THE NR 2 ENGINE SKIN PANEL ATTACHED TO BANJO''S 1, 2, 3 STRUCTURE IS CORRODED. REPAIRED IAW EO CH-00-015, BOEING TLX CAC-FCO 00-00008H, AND DRAWING AJC 7998. AN FAA FORM 8110-3 WAS ISSUED. RELEASED AIRCRAFT FOR REVENUE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Nacelles and pylons · skin · corrodedOct 12, 2000

    DURNIG C-CHECK AT ALITALIA, THE FITTING ELEMENT INSIDE THE AIR INTAKE DUCT ON THE NR 2 ENGINE SKIN PANEL ATTACHED TO BANJO''S 1, 2, 3 STRUCTURE IS CORRODED. REPAIRED IAW EO CH-00-015, BOEING TLX CAC-FCO 00-00008H, AND DRAWING AJC 7998. AN FAA FORM 8110-3 WAS ISSUED. RELEASED AIRCRAFT FOR REVENUE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · structure · corrodedJun 21, 2000

    DURING MAINTENANCE AT MIA, WHILE SB DC10-57A143, INTERGRANULAR CORROSION WAS FOUND ON THE FORWARD HORIZONTAL FLANGE (UPPER/INTERIOR SIDE) OF ARC1713-2 RIGHT OUTBOARD FLAP LOWER REAR SPAR CAP AT STATIONS XOF 549.672-557.489 AND XOF 722.235-2 - 728.653. REPAIRED IAW EO CH-00-008, SRM VOL 1 CHAP…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reports
  • Wings · flange · corrodedMar 2, 2000

    DURING MAINTENANCE AT MIA, WHILE COMPLYING WITH SB DC10-57A143, INTERGRANULAR CORROSION WAS FOUND ON THE FORWARD HORIZONTAL FLANGE (UPPER/INTERIOR SIDE) OF ARC1713-2 RIGHT OUTBOARD FLAP LOWER REAR SPAR CAP AT STATIONS XOF 549.672 - 557.489 AND XOF 722.235 - 728.653. REPLACED RIGHT OUTBOARD FLAP…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · adc · malfunctionedOct 13, 1999

    KMIA/MPTO - FLT 055 - AT 2:20 Z, ABORTED TAKEOFF, ON TAKEOFF ROLL FIRST OFFICER'S AIRPSPEED INDICATOR READS 20 KNOTS LOWER THAN THE CAPTAIN'S, AND STANDBY INDICATORS (THEY READ 100 KNOTS). FIRST OFFICER'S READS 75 KNOTS. NOTE: NO HIGH ENERGY STOP. PERFORMED PITOT STATIC LEAK CHECK ON FIRST…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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