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Aircraft record

N874TADouglas C-118A

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jun 30, 2017.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched49 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 1999
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
49
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Wells Fargo Bank Northwest NA Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Aug 11, 1999
Canceled
Jun 30, 2017
Airworthiness
Standard · Transport
Airworthiness date
Mar 8, 1991

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
C-118A
Serial number
44641
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
96
Engines
4
Max takeoff weight
20,000 and over lb
Mode S code
AC06DC

Engine

Make and model
P & W R-2800 Series
Type
Reciprocating
Power
2000 hp

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

Ownership history

Ownership history from FAA records
  1. 1999 – 2017Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

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

Accident history for this model

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 (49)

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.

  • Fuselage · skin · crackedOct 6, 1997

    SKIN CRACKED AT LAP SEAM ABOVE WINDOW LINE. CUTOUT DAMAGED SKIN AND REPAIRED PER SRM FIG 4-29. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedOct 6, 1997

    SKIN CORRODED AT SKIN LAP ABOVE WINDOW LINE STATION 500 RT SIDE. CUTOUT CORRODED SKIN AND REPAIRED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedOct 2, 1997

    POPPED RIVETS AT SKIN LAP 1 O'CLOCK POSITION APPROX STATION 530. CUT OUT DAMAGED SKIN AND REPAIRED PER SRM FIG 4-29. REPLACED POPPED RIVETS. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · skin · damagedOct 2, 1997

    RIVETS POPPED AT SKIN LAP 7 FOOT O'CLOCK POSITION STATION 178. REPLACED POPPED RIVETS. CUTOUT DAMAGED SKIN AND REPAIRED. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedOct 2, 1997

    POPPED RIVETS AT SKIN LAP 1 O'CLOCK POSITION APPROX 442. CUTOUT DAMAGED SKIN AND REPAIRED PER SRM FIG 4-29. REPLACED POPPED RIVETS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedSep 29, 1997

    RIVETS POPPED IN LAP SEAM AT 11 O'CLOCK POSITION AT APPROX 640. CUTOUT DAMAGED AREA. REPLACED IAW SRM 4 FIG 4-29. REPLACED FASTENERS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · rivets · poppedSep 26, 1997

    RIVETS POPPED IN LAP SEAM AT 10 O'CLOCK POSITION. REPLACED POPPED RIVETS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · damagedSep 26, 1997

    RIVETS POPPED IN LAP SEAM AT 11 O'CLOCK APPROX STATION 530. CUTOUT DAMAGED AREA AND REPAIRED PER SRM FIG 4-31. REPLACED POPPED RIVETS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedSep 24, 1997

    POPPED RIVETS AT LAP SEAM 2 O'CLOCK POSITION AT APPROX STATION 800. CUTOUT CORRODED SKIN AND REPAIRED PER SRM FIG 4-29. REPLACED POPPED RIVETS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedSep 24, 1997

    RIVETS POPPED AND SKIN CRACKED AT SKIN LAP 11 O'CLOCK POSITION. CUTOUT DAMAGED AREA. REPAIRED IAW SRM FIG 4-31.

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

Showing the 10 most recent of 49 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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