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Aircraft record

N921HADehavilland DHC-8-102

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jul 24, 2003.

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply7 service difficulty reports

Registration
Deregistered
Last based in
Lewisville, TX
owner city / state
Engine
PW120 · 1800 hp
P&W Canada
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
7
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Lewisville, TX
Canceled
Jul 24, 2003
Airworthiness
Standard · Transport
Airworthiness date
Dec 7, 1987

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
089
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
ACC291

Engine

Make and model
P&W Canada Pw120
Type
Turbo-prop
Power
1800 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. until 2003Individual ownerLewisville, TX

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (3)

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.

ADSubjectEffectiveApplies to
2014-14-02Pratt & Whitney Canada Corp. Turboprop EnginesAug 15, 2014Engine (PW120)Only with: PW120, PW121, PW121A engines with Post SB21610 configuration; PW124B, PW127, PW127E, PW127F engines with Post SB21607 and/or Post SB21705 configuration; PW127G and PW127M engines unconditionally.
2012-26-08Pratt & Whitney Canada Corp. Turboprop EnginesFeb 15, 2013Engine (PW120)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs.
2003-21-03Pratt & Whitney Canada Models PW118, PW120, PW120A, and PW121 Turboprop EnginesNov 20, 2003Engine (PW120)

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

Service Difficulty Reports (7)

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.

  • Propellers · tscu · failedAug 7, 2001

    AUTO FEATHER DID NOT ARM ON TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. REPLACED NR 1 AND NR 2 TSCU AND ADJUSTED POWER LEVER SWITCH 6121-S13.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · tscu · inoperativeAug 7, 2001

    AUTO FEATHER DID NOT ARM ON TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. REPLACED NR 1 AND 2 TSCU AND ADJUSTED POWER LEVER SWITCH 6121-S13.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · door · malfunctionedMar 19, 2000

    ON GEAR RETRACTION THE LT MLG FORWARD DOOR DID NOT CLOSE AND THE DOORS AMBER LIGHT REMAINED ILLUMINATED IN THE COCKPIT. AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE INSPECTED THE DOOR AND PERFORMED A BITE CHECK ON THE PSEU. NO DEFECTS WERE NOTED. AN EVALUATION FLIGHT WAS PERFORMED WITH NO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reports
  • Indicating and recording systems · t/o warning · activatedMay 30, 1999

    WARNING HORN SOUNDED ON TAKE-OFF ROLL. FOUND FLAP NEEDLE AT BOTTOM OF ARC BUT STILL IN WHITE AERA. CYCLED FLAPS 5-15-5, OPS CHECK GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · wire harness · failedMar 20, 1997

    FLT 3426 - PHF-PHL - WHEN AUTOFEATHER IS SELECTED, POWER UPTRIM LIGHT ILLUMINATES AND NR 1 ALTERNATE FEATHER PUMP LIGHT ILLUMINATES. REMOVED AND REPLACED NR 2 ENGINE STRUT HARNESS. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · bolt · looseOct 5, 1995

    LYN/PIT - FLT 3401 - AFTER LANDING IN PIT, THE AIRSTAIR DOOR WOULD NOT OPEN. FOUND UNSECURED BOLT ON FORWARD LOWER HANDRAIL ASSEMBLY. SECURED THE BOLT AS REQUIRED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · actuator · failedJul 19, 1995

    FLT 3017 - TPA-TLH - AFTER GEAR WAS SELECTED UP, THE LEFT MAIN FORWARD GEAR DOOR OPENED UP AFTER GEAR RETRACTION. RECYCLED GEAR AND THE DOOR CLOSED. CONTINUED ON TO TLH WITHOUT INCIDENT. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR FORWARD DOOR ACTUATOR.

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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