# N982HA: 1994 Dehavilland DHC-8-102, registration cancelled 2009-10-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 28, 2009 - Exported to: Australia - Status when cancelled: Valid registration - Airframe: [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102) (registry code 2809003) - Engine: [Pratt & Whitney Canada PW120](https://openairdocs.org/engine/pratt-whitney-canada-pw120) (registry code 52114) - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 380 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard - Airworthiness date: July 7, 1994 - Certificate issued: October 22, 2009 - Last registry action: October 22, 2009 - Mode S code: ADB342 - Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N982HA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=982HA - Page: https://openairdocs.org/deregistered/N982HA-2009-10-28 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Dehavilland DHC-8-102: https://openairdocs.org/model/dehavilland-dhc-8-102.md ## Service difficulty reports (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HNAA2009031400091](https://openairdocs.org/sdr/HNAA2009031400091), Mar 4, 2009: LIGHT. INOPERATIVE. ONE EMERGENCY ESCAPE PATH FLOOR LIGHT AT ROW 7 INOP. REMOVED AND REPLACED LIGHT BULB. - [SDR HNAA200911200393](https://openairdocs.org/sdr/HNAA200911200393), Jan 7, 2009: BYPASS SWITCH. FAILED. 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 - [SDR HNAA2008113000333](https://openairdocs.org/sdr/HNAA2008113000333), Nov 30, 2008: APU. ODOR. 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 BLE - [SDR HNAA2009021200050](https://openairdocs.org/sdr/HNAA2009021200050), Sep 13, 2008: PANEL. CORRODED. 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. - [SDR HNAA2009020100041](https://openairdocs.org/sdr/HNAA2009020100041), Sep 13, 2008: ACCESS PANEL. CORRODED. 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. - [SDR HNAA2009010900382](https://openairdocs.org/sdr/HNAA2009010900382), Sep 11, 2008: DOOR FRAME. CORRODED. 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 DO - [SDR HNAA0800014](https://openairdocs.org/sdr/HNAA0800014), Dec 18, 2007: DOOR SEAL. DIRTY. WITH ALL DOOR INDICATIONS NORMAL, DOOR SEAL WOULD NOT INFLATE. MAINTENANCE INSPECTED DOOR SEAL SUPPLY LINES AND PRESSURIZING VALVE, NOTING NO DEFECTS. DOOR SEAL - [SDR HNAA0700295](https://openairdocs.org/sdr/HNAA0700295), Dec 17, 2007: GALLEY. ODOR. 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. RE - [SDR HNAA0700286](https://openairdocs.org/sdr/HNAA0700286), Dec 5, 2007: SMOKE DETECTOR. DEFECTIVE. 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 SM - [SDR HNAA0700156](https://openairdocs.org/sdr/HNAA0700156), Jul 26, 2007: MIXER BOX. WORN. 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 MILE - [SDR HNAA070156](https://openairdocs.org/sdr/HNAA070156), Jul 26, 2007: MIXER BOX. WORN. 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 MIL - [SDR HNAA0700079](https://openairdocs.org/sdr/HNAA0700079), Apr 16, 2007: HYDRAULIC LINE. LEAKING. WHILE CLIMBING THROUGH 17,000 FEET ABOUT 40 MILES EAST OF PIT, THE NUMBER 2 HYDRAULIC SYSTEM DROPPED TO 1/2 QUART. RETURNED TO PIT, DECLARED AN EMERGENCY. FLIGH - [SDR HNAA0700224](https://openairdocs.org/sdr/HNAA0700224), Jan 18, 2007: THRESHOLD. CORRODED. AIR STAIR DOOR MAIN ENTRANCE THRESHOLD MEMBER CORRODED. REPLACED THRESHOLD. - [SDR HNAA0700229](https://openairdocs.org/sdr/HNAA0700229), Jan 5, 2007: BRACKET. CORRODED. CORROSION FOUND ON BRACKET AND CARGO FLOOR AT X598 ZONE 144 NEAR ENTRANCE AFT. CORROSION ON CARGO FLOOR REMOVED AND BRACKET REPLACED. - [SDR HNAA0700228](https://openairdocs.org/sdr/HNAA0700228), Jan 5, 2007: SEAT TRACK. CORRODED. SURFACE CORROSION ON LEFT INBOARD SEAT TRACK IN CARGO AREA. REPLACED LEFT INBOARD SEAT TRACK AFT CARGO BAY. - [SDR HNAA0700227](https://openairdocs.org/sdr/HNAA0700227), Jan 5, 2007: SEAT TRACK. CORRODED. CORROSION ON RIGHT INBOARD SEAT TRACK AT X201.00. REPLACED SEAT RAIL. - [SDR HNAA0700226](https://openairdocs.org/sdr/HNAA0700226), Jan 5, 2007: FRAME. CORRODED. CORROSION FOUND ON FRAME UNDERFLOOR AT X201.1560 BETWEEN STR 32S AND 30S. REPAIRED FRAME IAW ENGINEERING ORDER. - [SDR HNAA0700225](https://openairdocs.org/sdr/HNAA0700225), Jan 5, 2007: SEAT TRACK. CORRODED. CORROSION ON FORWARD LEFT SEAT RAIL. REMOVED CORROSION AND RETREATED RAIL. - [SDR HNAA0600116](https://openairdocs.org/sdr/HNAA0600116), Sep 25, 2006: UNKNOWN. ODOR. HOT ELECTRICAL ODOR CENTER OF CABIN. PERFORMED HIDDEN DAMAGE INSPECTION AND PULLED ANC COLLARED RT MAIN CIRCUIT BREAKER S1 IAW SPECIAL PROCEDURES 33.1. SYSTEM M - [SDR HNAA0500096](https://openairdocs.org/sdr/HNAA0500096), Oct 26, 2005: ENGINE. SMOKE. IN FLIGHT SMOKE IN CABIN AND COCKPIT. USED COCKPIT 02 MASKS. TURNED 13 BLEED OFF AND OPENED OUTFLOW VALVE ON DESCENT TO CLEAR SMOKE AND FLY UNPRESSURIZED, THEN - [SDR HNAA0500088](https://openairdocs.org/sdr/HNAA0500088), Oct 6, 2005: ACTUATOR. BYPASSING. NOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN, GEAR DID EXTEND WHEN ALT. EXTENSION PROCEDURE WAS FOLLOWED. REMOVED AND REPLACED NOSE DOOR ACTUATOR. - [SDR HNAA0500072](https://openairdocs.org/sdr/HNAA0500072), Jul 28, 2005: ACTUATOR. LEAKING. NR 1 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED WHEN TAKING RUNWAY FOR TAKEOFF. NR 1 HYDRAULIC QUANTITY WENT TO 1.0 NORMAL BRAKING FAILED. CREW SHUT DO - [SDR HNAA0500026](https://openairdocs.org/sdr/HNAA0500026), Mar 18, 2005: SELECTOR VALVE. MALFUNCTIONED. GEAR WOULD NOT EXTEND ON 2ND ATTEMPT. FOLLOWED EMERGENCY CHECK LIST. PERFORMED ALT EXTENSION, GEAR DOWN AND LOCKED. INSPECTED PSEU FOR FAULT CODES NONE FOUND CY - [SDR HNAA0400072](https://openairdocs.org/sdr/HNAA0400072), Jul 29, 2004: THRESHOLD. CORRODED. PAX DOOR THRESHOLD CORRODED ON SILL PLATE. REMOVED AND REPLACED THRESHOLD. - [SDR HNAA0400071](https://openairdocs.org/sdr/HNAA0400071), Jul 29, 2004: PANEL. CORRODED. DURING C-CHECK INSPECTION FOUND STRESS PANELS 523 AND 623 AT WITH CORROSION IN COUNTERSINKS. REMOVED AND REPLACED PANELS. - [SDR PCAA0303050](https://openairdocs.org/sdr/PCAA0303050), Mar 3, 2003: HYDRAULIC LINE. LEAKING. SYR-FLIGHT#3963. CREW REPORTED THAT THE #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED AFTER GEAR EXTENSION. 1.4 QUARTS REMAINING IN #2 SYSTEM. MAINTENA - [SDR HNAA0100079](https://openairdocs.org/sdr/HNAA0100079), Dec 7, 2001: HYDRAULIC SYSTEM. MALFUNCTIONED. LOST NR 1 HYDRAULIC SYSTEM PRESSURE WITH NR 2 ENGINE RUNNING DURING SINGLE ENGINE TAXI. NO NORMAL BRAKING. I/B ROLL SPLR, RUD HYD AND RUD FULL PRESS CAUTION LIG - [SDR HNAA0100043](https://openairdocs.org/sdr/HNAA0100043), Aug 1, 2001: ENGINE. SMOKE. CREW REPORTED SMOKE/MIST FORMED IN THE CABIN AND COCKPIT. WHEN ENGINE BLEEDS WERE TURNED OFF SMOKE DISSIPATED. REPLACED #1 ENGINE. - [SDR HNAA0000041](https://openairdocs.org/sdr/HNAA0000041), May 16, 2000: CABLE. JAMMED. PAX DOOR WOULD NOT FULLY OPEN. FOUND THE DOOR COUNTERBALANCE CABLE OFF OF THE CABLE DRUM. REPLACED THE CABLE, COUNTERBALANCE GAS STRUTS AND INSTALLED MODIFIED C - [SDR HNAA0000004](https://openairdocs.org/sdr/HNAA0000004), Jan 11, 2000: WINDOW. CRACKED. THE CAPTAINS SIDE WINDOW OUTER PLY CRACKED IN FLIGHT. PIECES OF THE OUTER PLY SEPARATED FROM THE AIRCRAFT AND DAMAGED THE NR 1 PROP NR 1 BLADE. REPLACED THE CAP - [SDR HNAA9698232](https://openairdocs.org/sdr/HNAA9698232), May 21, 1996: PRPM INDICATOR. FAILED. FLT 3091 - PHL-DCA - WHILE IN CRUISE, AT 5000 FEET, THE NR 2 ENGINE ROLLED BACK LOSING TORQUE, ITT AND FUEL FLOW. NH STABILIZED AT 54 PERCENT. ENGINE WAS OPERAT - [SDR 96ZZZM1043](https://openairdocs.org/sdr/96ZZZM1043), May 21, 1996: EEC. FAILED. FLT 3091 - PHL-DCA - WHILE IN CRUISE, AT 5000 FEET, THE NR 2 ENGINE ROLLED BACK LOSING TORQUE, ITT AND FUEL FLOW. NH STABILIZED AT 54 PERCENT. ENGINE WAS OPERAT ## FAA accident and incident reports (3) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20030319007949I](https://openairdocs.org/incident/20030319007949I), Mar 19, 2003: Dhav DHC8102 (N982HA), Binghamton, NY. (-23) Crew reported the #2 hyd isolation valve caution light illuminated after gear extension. 1.4 quarts remaining in #2 system. The aircraft landed on runway… - [Incident 20020109000459I](https://openairdocs.org/incident/20020109000459I), Jan 9, 2002: Dhav DHC8102 (N982HA), Norfolk, VA, Substantial damage. (-23) At 20:45 hrs, at the Norfolk International Airport (orf) an aircraft was stationary at gate 9 with both engines powered up. Two piedmont mechanics were… - [Incident 20000111000409I](https://openairdocs.org/incident/20000111000409I), Jan 11, 2000: Dhav DHC8102 (N982HA), Elmira, NY. (-23) On Tuesday, 1/11/2000 at 1116 local, a piedmont airlines (d/b/a usair express) reported a captain's side window cracked. The aircraft landed on runway 28… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.