N982HA1994 Dehavilland DHC-8-102
This N-number isn't registered right now. Below is its last known registration, canceled Oct 28, 2009.
Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply32 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Bank Of Utah Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Oct 22, 2009
- Canceled
- Oct 28, 2009
- Airworthiness
- Standard
- Airworthiness date
- Jul 7, 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 dataAirframe
- Manufacturer
- Dehavilland
- Model
- DHC-8-102
- Year
- 1994
- Serial number
- 380
- 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
- ADB342
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- 2009Bank Of Utah 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, 2026NTSB 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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-14-02 | Pratt & Whitney Canada Corp. Turboprop Engines | Aug 15, 2014 | Engine (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. |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (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. |
| 2003-21-03 | Pratt & Whitney Canada Models PW118, PW120, PW120A, and PW121 Turboprop Engines | Nov 20, 2003 | Engine (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 (32)
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.
- Lights · light · inoperativeMar 4, 2009
ONE EMERGENCY ESCAPE PATH FLOOR LIGHT AT ROW 7 INOP. REMOVED AND REPLACED LIGHT BULB.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · bypass switch · failedJan 7, 2009
NR 1 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED WHEN SETTING TAKE OFF POWER THEN EXTINGUISHED WHEN POWER REDUCED TO FLIGHT IDLE. R&R NR 1 HIGH PRESSURE FILTER AND BYPASS SWITCH. INSPECTED OLD FILTER NO DEBRIS FOUND. GROUND RUN ACFT OPS CHECK GOOD. LOW PRESSURE FUEL FILTER INDICATION NOT FLAGGED.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Airborne auxiliary power · apu · odorNov 30, 2008
UPON APU FAILURE, SMOKE ODOR FILLED THE CABIN AND COCKPIT. MAINTENANCE INSPECTED THE APU BAY AND FOUND NO LEAKS. APU WAS RUN FOR 10 MINUTES WITH AND WITHOUT BLEEDS ON. NO DEFECTS WERE NOTED AND NO ODORS WERE DETECTED. AIRCRAFT WAS THEN RELEASED FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · access panel · corrodedSep 13, 2008
RT WING ACCESS PANEL 622 AT (STRESS PANEL) HAS 2 HOLES CORRODED. CORROSION FOUND TO BE IN LIMIT PER RD8-57-1715. REPAIR HOLES IAW RD8-57-1715.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · panel · corrodedSep 13, 2008
DURING 'C' CHECK INSPECTIONS, THE LT WING STRESS PANEL, 522AT, WAS FOUND TO HAVE CORROSION IN SOME OF THE SCREW COUNTER SINKS THAT WAS BEYOND ACCEPTABLE LIMITS. THE PANEL WAS REPLACED. THIS IS AN AMENDMENT TO HNAA2009010900383 TO CORRECT ITEM 1C, REGISTRATION NR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · door frame · corrodedSep 11, 2008
DURING C-CHECK INSP, THE LAVATORY SERVICE DOOR FRAME WAS FOUND TO HAVE CORROSION ON IT. THE DOOR FRAME WAS REPLACED IAW SRM PROCEDURES. ADDITIONALLY, THE PAX DOOR THRESHOLD WAS FOUND TO BE CORRODED. THAT ITEM, P/N 85320686-101, WAS ALSO REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · door seal · dirtyDec 18, 2007
WITH ALL DOOR INDICATIONS NORMAL, DOOR SEAL WOULD NOT INFLATE. MAINTENANCE INSPECTED DOOR SEAL SUPPLY LINES AND PRESSURIZING VALVE, NOTING NO DEFECTS. DOOR SEAL WAS CLEANED OF DIRT AND GRIME. DOOR SEAL AT THIS TIME INFLATED PROPERLY AND AIRCRAFT WAS CHECKED FOR PRESSURIZATION. SYSTEM CHECKED GOOD…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Equipment and furnishings · galley · odorDec 17, 2007
ELECTRICAL ODOR IN CABIN. FLIGHT 4165, LGA TO ROA. LGA MNT PERFORMED HIDDEN DAMAGE INSPECTION AND FOUND HOT JUG IN NR 1 POSITION OVERHEATED AND CAUSING ODOR. REMOVED HOT JUG AS PRECAUTION, ITEM PLACED ON MEL. ROA MTN REMOVED AND REPLACED HOT JUG.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · smoke detector · defectiveDec 5, 2007
BAG BAY SMOKE WARNING AND MASTER WARNING LIGHT ILLUMINATED SEVERAL TIMES ON DESCENT TO HTS STARTING AT 6000 FEET THROUGH TOUCHDOWN. REMOVED AND REPLACED BOTH SMOKE DETECTORS IN THE BAG BAY, OPERATIONAL CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · mixer box · wornJul 26, 2007
CABIN GOT VERY HOT AFTER TAKEOFF FLIGHT DECK COLD. AFTER SEVERAL PAX GOT SICK, F/A INFORMED CREW THAT THE CABIN WAS TOO HOT TO CONTINUE. ACFT WAS APPROX 20 MILES OUT OF LGA, ACFT RETURNED TO FIELD. CONTACTED LGA MX. ACFT HAS BEEN WRITTEN UP TWICE BEFORE. DUCTING UNDER FLOOR APPEARS TO BE IN GOOD…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 32 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