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Aircraft record

N801MXDehavilland DHC-8-102

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jun 27, 2000.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched6 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 2000
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
First Security Bank NA Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Apr 20, 2000
Canceled
Jun 27, 2000

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
Dehavilland
Model
DHC-8-102
Serial number
008
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
39
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
AAE6BD

Engine

Type
Turbo-prop

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

Ownership history

Ownership history from FAA records
  1. 2000First Security Bank NA TrusteeSalt Lake City, UT

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 (6)

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 · bolt · crackedJun 30, 1996

    DHC TASK 5310/08F DUE. PERFORMED ULTRASONIC TEST OF RIGHT BOLT, TEST REVEALED 30 PERCENT BACK REFLECTION. REMOVED AND REPLACED BOTH LEFT AND RIGHT FORWARD BOLTS. SUBSEQUENT ULTRASONIC TEST ON BOLT REMOVED FROM LEFT SIDE REVEALED 10 PERCENT BACK REFLECTION. MAGNETIC PARTICLE INSPECTION REVEALED A…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · lower arm assy · wornApr 7, 1996

    DURING A SCHEDULED RUDDER CHANGE, THE VERTICAL STABILIZER UPPER AND LOWER CENTER HINGE FITTING RUDDER ATTACH POINTS WERE FOUND WORN. THE BUSHINGS WOULD NOT INSTALL CORRECTLY DUE TO THE HOLES BEING OVERSIZED. REMOVED AND REPLACED UPPER AND LOWER CENTER HINGE FITTINGS IAW DEHAVILLAND DRAWINGS.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · upper arm assy · wornApr 7, 1996

    DURING A SCHEDULED RUDDER CHANGE, THE VERTICAL STABILIZER UPPER AND LOWER CENTER HINGE FITTING RUDDER ATTACH POINTS WERE FOUND WORN. THE BUSHINGS WOULD NOT INSTALL CORRECTLY DUE TO THE HOLES BEING OVERSIZED. REMOVED AND REPLACED UPPER AND LOWER CENTER HINGE FITTINGS IAW DEHAVILLAND DRAWINGS.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Landing gear · seq valve · failedMar 17, 1995

    WHEN LANDING GEAR WAS RETRACTED, NOSE GEAR ADVISORY LIGHT REMAINED ON. THE GEAR WAS SELECTED DOWN PER THE CHECK LIST; THE MAIN GEAR CAME DOWN AND LOCKED, THE NOSE GEAR INDICATED UNSAFE. THE CREW PERFORMED AN ALTERNATE EXTENSION. INSPECTED WIRING HARNESS FOR GEAR DOOR PROXIMITY SWITCH, FOUND TO BE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · prox cont box · failedMar 8, 1995

    AFTER DEPARTURE AND SELECTING GEAR UP, NOSE GEAR DOOR AMBER LIGHT STAYED LIT, FOLLOWED CHECK LIST, RECYCLED GEAR, NOSE WHEEL DID NOT COME DOWN. PERFORMED ALT GEAR EXT CHECK LIST, THEN RECEIVED 3 GREEN. REMOVED AND REPLACED PSEU DUE TO VARIOUS FAULT INDICATIONS. JACKED NOSE GEAR AND MANUALLY SWUNG…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · prox cont box · failedFeb 8, 1995

    THE LT DOOR OPEN ADVISORY LIGHT ILLUMINATED IN FLIGHT. CREW VERIFIED DOOR IS CLOSED. REMOVED AND REPLACED LT FWD GEAR DOOR ACTUATOR AND PSEU IAW MM, OPERATIONAL CHECK GOOD. ACFT RETURNED TO SERVICE. (W)

    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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