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Aircraft record

N890681982 Dehavilland DHC-7-102

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 5, 2022.

Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply10 service difficulty reports

Registration
Deregistered
Last based in
Fort Belvoir, VA
owner city / state
Engine
PT6A-50 · 1120 hp
P&W Canada
Owners
1
since 1998
NTSB events
None
since 1982
ADs may apply
1
confirm with A&P
Service reports
10
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Department Of Defense
Owner type
Government
City, state
Fort Belvoir, VA
Certificate issued
Jan 29, 1998
Canceled
Nov 5, 2022
Airworthiness
Standard · Transport
Airworthiness date
Mar 13, 1997

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-7-102
Year
1982
Serial number
88
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
59
Engines
4
Max takeoff weight
20,000 and over lb
Mode S code
AC489F

Engine

Make and model
P&W Canada Pt6a-50
Type
Turbo-prop
Power
1120 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. 1998 – 2022Department Of DefenseFort Belvoir, VA
  2. 1965 – 1973Co-ownersHouston, TX · different airframe: Cessna 140 S/N 8072

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.

Accident history for this model

ADs published since 1998 that may apply (1)

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
2002-23-13Pratt & Whitney Canada PT6A Series Turboprop EnginesDec 31, 2002Engine (PT6A-50)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed.

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

Service Difficulty Reports (10)

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.

  • Stabilizers · bracket · crackedJun 14, 2019

    ONE TIME INSPECTION FOR CRACK/BREAK OF THE RUDDER CONTROL MECHANISM BRACKET. THE INSPECTION RESULTED IN IDENTIFYING A CRACK AT BOTTOM OF RADIUS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · wire · chafedApr 30, 1996

    ON TEST FLIGHT, AC NR 2 GENERATOR LIGHT CAME ON. DURING TROUBLESHOOTING OF SYSTEM, FOUND WIRE 2420-20001E12A-1 GROUNDED OUT. CONDUIT PASSES BETWEEN REAR SPAR AND FLAP PRIMARY CONTROL TUBE. AREA WHERE WIRES PASS THROUGH IS PRESSED AND WIRE RUBS CONDUIT. SUBMITTER STATED IF AC GENERATOR LIGHT COMES…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · foreflap · corrodedOct 10, 1995

    ON D-INSPECTION OF FLIGHT CONTROLS OF LEFT FOREFLAP, FOUND CORROSION ON BOTTOM STR 12 AND STR 14 WITH BORESCOPE, STA YW242.17 TO YW257.35. FOREFLAP PANELS ARE NOT REQUIRED TO BE REMOVED ON INSPECTION. SUBMITTER STATED THEY NEED REMOVAL FOR INSPECTION OF CORROSION OF BOTTOM SKIN AND STRINGERS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Wings · foreflap · corrodedOct 10, 1995

    ON D-INSPECTION OF FLIGHT CONTROLS, FOUND A HINGE ARM WITH CORROSION AND, WITH THE OTHER FLAP PANELS OPEN, FOUND CORROSION AROUND PANEL NUTPLATES, STA YW367.90 TO STA YW423.30. SUBMITTER STATES PANELS NEED REMOVAL AT INSPECTION OF FOREFLAP.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · strut pin · corrodedOct 10, 1995

    ON A D-INSPECTION, REPLACED HARDWARE FOR UPPER DRAG STRUT AND WHEN STRUT PINS WERE REMOVED, THEY HAD CORROSION AND PITTING. SUBMITTER STATED WHEN HARDWARE IS SHOWING CORROSION, PINS NEED TO BE INSPECTED FOR CORROSION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · strut pin · corrodedOct 10, 1995

    ON A D-INSPECTION, REPLACED HARDWARE FOR UPPER DRAG STRUT AND WHEN STRUT PINS WERE REMOVED, THEY HAD CORROSION AND PITTING. SUBMITTER STATED WHEN HARDWARE IS SHOWING CORROSION, PINS NEED TO BE INSPECTED FOR CORROSION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · foreflap · arm corrodedOct 10, 1995

    ON D-INSPECTION OF FLIGHT CONTROLS, FOUND CORROSION ON INBD FORFLAP HINGE ARM UNDER PANEL COVER. PANELS ARE NOT REQUIRED TO BE REMOVED ON INSPECTION. PANELS NEED REMOVAL FOR CORROSION INSPECTION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · foreflap · corrodedOct 10, 1995

    ON D-INSPECTION, NDT DEBOND CHECK OF RIGHT FOREFLAP FOUND CORROSION OF STR 14 AT STA YW257.35. SUBMITTER STATED REAR FOREFLAP PANELS NEED REMOVAL AT INSPECTION AND INSPECT FOR CORROSION OF BOTTOM SKIN AND HINGE AREA BY BORECOPE AND DEBOND INSPECTIONS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · pin · corrodedSep 29, 1995

    DURING D-INSPECTION, RIGHT MLG UPPER DRAG STRUT PINS WERE REMOVED AND FOUND TO HAVE CORROSION AND PITTING. SUBMITTER STATED NEED TO INSPECT BY REMOVING PINS. PINS ARE NOT NORMALLY INSPECTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · pin · corrodedSep 29, 1995

    DURING D-INSPECTION, RIGHT MLG UPPER DRAG STRUT PINS WERE REMOVED AND FOUND TO HAVE CORROSION AND PITTING. SUBMITTER STATED NEED TO INSPECT BY REMOVING PINS. PINS ARE NOT NORMALLY INSPECTED.

    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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