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Aircraft record

N980HA1994 Dehavilland DHC-8-102

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 12, 2009.

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply39 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Engine
PW120 · 1800 hp
P&W Canada
Owners
1
since 1994
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
39
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
Jul 1, 1994
Canceled
Aug 12, 2009
Airworthiness
Standard · Normal
Airworthiness date
Mar 21, 1994

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
Year
1994
Serial number
376
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
ADABD4

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. 1994 – 2009Wells 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.

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 (39)

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.

  • Air conditioning and pressurization · unknown · odorJan 26, 2009

    DURING WORK ON A DIFFERENT PROBLEM ON THE ACFT, THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE AREA OF THE WARDROBE. MX INSPECTED THE AVIONICS COMPARTMENT AND THE WARDROBE AREAS AND FOUND NO SIGNS OF ELECTRICAL DEFECTS OR ODORS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · switch · failedJan 23, 2009

    WHILE ADVANCING THE POWER LEVERS TOWARD TAKE OFF POWER, THE NR 2 PROPELLER FEATHERED, THE AUXILIARY PUMP LIGHT ILLUMINATED AND THE PROP TORQUE SPIKED TO 100% FOR APPROXIMATELY 1 TO 2 SECONDS. THE TAKE OFF WAS ABORTED AND THE ACFT WAS RETURNED TO THE MX FACILITY. MX CONFIRMED THE PROBLEM AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · connector · dirtyJan 7, 2009

    NR 2 ENGINE OIL TEMPERATURE FLUCTUATES IN FLIGHT. CLEAN CONNECTOR PLUG, OPS CHECK GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine controls · switch · dirtyDec 19, 2008

    WHEN ADVANCING POWER LEVER FOR TAKEOFF AT APPROXIMATELY 30 PERCENT TORQUE NUMBER 2 PROPELLER FEATHERED. INSPECT ENGINE CONTROL PANEL NO FLAG NOTED. CLEANED POWER LEVER SWITCHES 6126-S6 THRU S 13. COMPLY WITH WORK CARD 61-20-03Q AND 61-20-04Q.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · radar · inoperativeAug 12, 2008

    WEATHER RADAR W/N PAINT, TX FAULT AND AFC MESSAGE. ACFT DIVERTED TO LGA. MAINTENANCE REMOVED AND REPLACED RADAR RT. OPS CHECK GOOD. (S)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · spar · crackedJun 18, 2008

    DURING C-CHECK INSP, THE REAR SPAR OF THE LT ELEVATOR SPRING TAB WAS FOUND TO BE CRACKED AT THE OTBD EDGE. THE SPAR WAS REPAIRED IAW RD8-55-068.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · skin panel · damagedJun 18, 2008

    DURING C-CHECK INSP, THE TRAIL RUDDER SKIN WAS FOUND TO BE DAMAGED ON THE LT SIDE NEAR THE LOWER HINGE POINT. THE DAMAGE WAS REPAIRED IAW SRM PROCEDURES AND EO8-55-08-3203.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · seat track · corrodedJun 17, 2008

    DURING C-CHECK INSPECTIONS, THE LT I/B FORWARD SEAT RAIL WAS FOUND TO BE CORRODED. THE SEAT RAIL SECTION WAS REMOVED AND REPLACED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · structure · corrodedJun 17, 2008

    DURING C-CHECK INSPECTIONS, THE INBOARD WIRING TROUGH (GUTTER) UNDER THE WARDROBE AREA WAS FOUND TO BE CORRODED ON THE LOWER SURFACE. A REPLACEMENT WAS FABRICATED AND INSTALLED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bracket · corrodedJun 16, 2008

    DURING C-CHECK INSP, THE PAX DOOR THRESHOLD WAS FOUND TO BE CORRODED. THIS ITEM WAS R&R IAW SRM PROCEDURES. A BRACKET UNDERNEATH THE THRESHOLD, P/N 85321069-101, WAS ALSO FOUND CORRODED. A REPLACEMENT WAS FABRICATED AND THE BRACKET REPLACED. ADDITIONALLY, THE FWD INBD LT SEAT RAIL P/N…

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

Showing the 10 most recent of 39 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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