# N980HA: 1994 Dehavilland DHC-8-102, registration cancelled 2009-08-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 12, 2009 - Exported to: Canada - Status when cancelled: Triennial form not returned - 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: 376 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: March 21, 1994 - Certificate issued: July 1, 1994 - Last registry action: November 18, 2008 - Mode S code: ADABD4 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%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/N980HA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=980HA - Page: https://openairdocs.org/deregistered/N980HA-2009-08-12 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 (40) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HNAA2009012700030](https://openairdocs.org/sdr/HNAA2009012700030), Jan 26, 2009: UNKNOWN. ODOR. 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 COMPARTM - [SDR HNAA2009013000034](https://openairdocs.org/sdr/HNAA2009013000034), Jan 23, 2009: SWITCH. FAILED. 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% FO - [SDR HNAA200911200392](https://openairdocs.org/sdr/HNAA200911200392), Jan 7, 2009: CONNECTOR. DIRTY. NR 2 ENGINE OIL TEMPERATURE FLUCTUATES IN FLIGHT. CLEAN CONNECTOR PLUG, OPS CHECK GOOD. - [SDR HNAA2008121900353](https://openairdocs.org/sdr/HNAA2008121900353), Dec 19, 2008: SWITCH. DIRTY. WHEN ADVANCING POWER LEVER FOR TAKEOFF AT APPROXIMATELY 30 PERCENT TORQUE NUMBER 2 PROPELLER FEATHERED. INSPECT ENGINE CONTROL PANEL NO FLAG NOTED. CLEANED POWE - [SDR HNAA2009010900383](https://openairdocs.org/sdr/HNAA2009010900383), Sep 13, 2008: PANEL. CORRODED. DURING C-CHECK INSP, THE LT WING STRESS PANEL, 522AT, WAS FOUND TO HAVE CORROSION IN SOME OF THE SCREW COUNTER SINKS THAT WAS BEYOND ACCEPTABLE LIMITS. THE PANE - [SDR HNA2008F00044](https://openairdocs.org/sdr/HNA2008F00044), Aug 12, 2008: RADAR. INOPERATIVE. WEATHER RADAR W/N PAINT, TX FAULT AND AFC MESSAGE. ACFT DIVERTED TO LGA. MAINTENANCE REMOVED AND REPLACED RADAR RT. OPS CHECK GOOD. (S) - [SDR HNAA2009010900387](https://openairdocs.org/sdr/HNAA2009010900387), Jun 18, 2008: SKIN PANEL. DAMAGED. 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 - [SDR HNAA2009010900386](https://openairdocs.org/sdr/HNAA2009010900386), Jun 18, 2008: SPAR. CRACKED. 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. - [SDR HNAA2009021300056](https://openairdocs.org/sdr/HNAA2009021300056), Jun 17, 2008: STRUCTURE. CORRODED. 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 FABRICAT - [SDR HNAA2009021300055](https://openairdocs.org/sdr/HNAA2009021300055), Jun 17, 2008: SEAT TRACK. CORRODED. DURING C-CHECK INSPECTIONS, THE LT I/B FORWARD SEAT RAIL WAS FOUND TO BE CORRODED. THE SEAT RAIL SECTION WAS REMOVED AND REPLACED. - [SDR HNAA2009010900385](https://openairdocs.org/sdr/HNAA2009010900385), Jun 16, 2008: BRACKET. CORRODED. 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 - [SDR HNAA2009020100042](https://openairdocs.org/sdr/HNAA2009020100042), Jun 13, 2008: TAB. DENTED. DENT ON TRAILING ARM OF LT STRING TAB 3.3" FROM INBD EDGE. REPAIR DAMAGE IAW WITH RD8-55-037. - [SDR HNAA0800028](https://openairdocs.org/sdr/HNAA0800028), Jan 15, 2008: LIGHT. OUT OF POSITION. NUMBER 1 RED FLOOR EMERGENCY ESCAPE PATH LIGHT PULLED AWAY FROM FLOOR EXPOSING WIRING. REPAIRED EMERGENCY LIGHT ASSEMBLY. - [SDR HNAA0700264](https://openairdocs.org/sdr/HNAA0700264), Nov 5, 2007: LINE. LEAKING. ACID/CITRUS ODOR IN COCKPIT WHEN BLEEDS OFF ON APPROACH OK IN CRUISE. THERE WAS NO REPORT OF THIS ODOR IN THE CABIN. FOUND HOLES IN HYDRAULIC LINE BELOW FLIGHT - [SDR HNAA0700234](https://openairdocs.org/sdr/HNAA0700234), Oct 12, 2007: PRESSURE SWITCH. INOPERATIVE. FLIGHT WAS HEADED FROM PHL TO IPT AND DIVERTED TO MDT DUE TO NR 1 ENGINE FUEL LOW PRESSURE LIGHT ILLUMINATING IN FLIGHT. REMOVED AND REPLACE THE NR 1 PRESSURE S - [SDR HNAA0700184](https://openairdocs.org/sdr/HNAA0700184), Sep 27, 2007: TERMINAL. BURNED. CAPTAIN`S WINDSHIELD SELECTED TO WARM UP, SMOKED FROM ELEMENT LEADS. MEL'ED THE WINDSHIELD HEATER SYSTEMS. INSPECTION FOUND L1 TERMINAL BURNT, NO OTHER DAMAGE N - [SDR HNAA0700157](https://openairdocs.org/sdr/HNAA0700157), Jul 27, 2007: RADAR. FAILED. JUST AFTER TAKEOFF CREW NOTICED WX RADAR WAS NOT PAINTING ANY STORMS THEN RED DOTS BEGAN TO DISPLAY ON THE RADAR. AFTER TALKING WITH DISPATCH WITH DISPATCH AND - [SDR HNAA0700154](https://openairdocs.org/sdr/HNAA0700154), Jul 18, 2007: VALVE. MALFUNCTIONED. UPON DESCENT INTO TYS POWER LEVERS AT FLT IDLE FLT DECK/CABIN STARTED TO FILL WITH SMOKE WITH BOTH BLEEDS ON. TURNED OFF ENGINE BLEEDS AND SMOKE STARTED TO DISS - [SDR HNAA0700153](https://openairdocs.org/sdr/HNAA0700153), Jul 16, 2007: VALVE. STICKING. UPON DESCENT INTO HHH POWER LEVERS AT FLY IDLE FLT DECK/CABIN STARTED TO FILL WITH SMOKE WITH ENGINE BLEEDS ON. TURNED OFF BLEEDS AND SMOKE STARTED TO DISSIPATE - [SDR HNAA0700113](https://openairdocs.org/sdr/HNAA0700113), Jun 14, 2007: HYDRAULIC LINE. LEAKING. THE NUMBER 1 FUEL TEMP WAS DROPPING FOLLOWED BY THE ILLUMINATION OF THE NR 1 HYD ISO VALVE CAUTION LIGHT. THE HYD QTY WENT TO .5 QT. THE NUMBER 1 FUEL PRESSURE - [SDR HNAA0600024](https://openairdocs.org/sdr/HNAA0600024), Apr 9, 2006: WINDSCREEN. CRACKED. CAPTAINS FWD WINDSCREEN CRACKED IN FLIGHT. REMOVED AND REPLACED WINDSCREEN. - [SDR HNAA0400115](https://openairdocs.org/sdr/HNAA0400115), Aug 20, 2004: O-RING. LEAKING. FLIGHT NR 3818 REPORTED TOTAL LOSS OF NR 2 HYDRAULIC SYSTEM CONTENTS. PRESSURE LOSS WAS FOR APPROX. 7 MINUTES, WITH NR 2 ENGINE RUNNING. MAINTENANCE FOUND UNION - [SDR PCAA0310122](https://openairdocs.org/sdr/PCAA0310122), Oct 11, 2003: SWITCH. DIRTY. SYR-FLIGHT NR 3629. CREW REPORTED THAT THE NR 2 ENGINE POWER UPTRIM PARTIALLY ACTIVATED DURING TAKEOFF. CREW EXPERIENCED REPEATED NR 2 ENGINE SURGING. ENGINE WA - [SDR PCAA0308100](https://openairdocs.org/sdr/PCAA0308100), Aug 19, 2003: B-NUT. LEAKING. CREW REPORTED THAT THE RT ENGINE OIL PRESSURE FLUXUATED BETWEEN 40 AND 50 PSI AT CRUISE FLT OF 11,000 FT. NR 2 ENGINE WAS SHUT DOWN AND FLIGHT DIVERTED TO ACY. - [SDR PCAA0212144](https://openairdocs.org/sdr/PCAA0212144), Dec 8, 2002: ODOR. DETECTED. ITH- FLIGHT 3729 FLIGHT ATTENDANT REPORTED THAT WITH THE BLEEDS ON A BURNING SMELL WAS PRESENT AND CABIN WAS VERY HOT WITH TEMPERATURE GAUGE IN COCKPIT IN MIDDL - [SDR PCAA0209113](https://openairdocs.org/sdr/PCAA0209113), Sep 26, 2002: WIRE. BROKEN. DURING ROUTINE MAINTENANCE VISIT FLOOR EMERGENCY LIGHT SEAT 1DF FOUND INOPERATIVE DUE TO A BROKEN WIRE. BROKEN WIRE WAS REPAIRED, OPERATIONAL CHECK GOOD. AIRCRA - [SDR PCAA0207141](https://openairdocs.org/sdr/PCAA0207141), Jul 20, 2002: CONNECTOR. DIRTY. SYR-FLIGHT 3931. CREW REPORTED EMERGENCY LIGHTS WERE FLICKERING IN FLIGHT AND ON THE GROUND. MAINTENANCE CLEANED THE CONNECTOR ON THE EMERGENCY LIGHT CONTROL BO - [SDR PCAA0205061](https://openairdocs.org/sdr/PCAA0205061), May 29, 2002: FITTING. CRACKED. BGM-BUF FLIGHT#3779. CREW REPORTED RIGHT GEAR UNSAFE AND NOSE YELLOW DOOR LIGHT ILLUMINATED. BOTH GEAR CONFIRMED RETRACTED AND RIGHT MAIN DOORS OPEN. CHATTERING - [SDR HNAA0000046](https://openairdocs.org/sdr/HNAA0000046), May 26, 2000: SOCKET. ARCED. ON TAXI OUT FROM THE GATE THE FLIGHT ATTENDANT REPORTED FUMES IN THE CABIN AND ARCING FROM RT CABIN CEILING LIGHT AT ROW 1. REPLACED LAMP SOCKET. - [SDR HNAA9900004](https://openairdocs.org/sdr/HNAA9900004), Jan 8, 1999: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHT OVER AIRSTAIR DOOR INOPERATIVE. REPLACED EMERGENCY BATTERY POWER SUPPLY (P/N 61-0478-1X) (S/N PS034) AND EMERGENCY LIGHT BATTERY (P/N 60-13 - [SDR HNAA9898080](https://openairdocs.org/sdr/HNAA9898080), Nov 19, 1998: POWER SUPPLY. INOPERATIVE. HVN - FLT 3091 - NUMEROUS INTERIOR/EXTERIOR EMERGENCY LIGHTS OUT. REPLACED ALL EMERGENCY BATTERY POWER SUPPLIES. OPS CHECK GOOD. (M) - [SDR HNAA9598005](https://openairdocs.org/sdr/HNAA9598005), Nov 5, 1995: SPRING. MISSING. FLT NR 80 - ORF-PHF - DURING PREFLIGHT CHECK, UNABLE TO CLOSE MAIN CABIN DOOR. FOUND TOP STEP SPRING MISSING. DOOR OPERATES NORMALLY WITH STEP POSITIONED PROPER - [SDR 95ZZZX4235](https://openairdocs.org/sdr/95ZZZX4235), Aug 8, 1995: UPLOCK SENSORS. FAILED. DCA/GSO - FLT 3118 - ALL AMBER GEAR DOOR LIGHTS REMAINED ILLUMINATED AFTER RETRACTION. CENTER AND AFT GEAR DOORS COULD BE SEEN OPEN. CYCLED GEAR, AND GEAR RETRA - [SDR 95ZZZX4238](https://openairdocs.org/sdr/95ZZZX4238), Aug 3, 1995: RELAY. FAILED. DCA/GSO - FLT 3118 - AFTER TAKEOFF, WHEN GEAR WAS SELECTED UP, THE GEAR RETRACTED, BUT ALL DOOR LIGHTS REMAINED ON. GEAR DOORS REMAINED OPEN. THE AIRCRAFT TURNE - [SDR 95ZZZX4244](https://openairdocs.org/sdr/95ZZZX4244), Jul 28, 1995: PSEU. FAILED. HPN/PHL - FLT 3158 - WHEN THE GEAR WAS SELECTED UP AFTER TAKEOFF, THREE AMBER LIGHTS STAYED ON WITH GEAR UP. CREW SELECTED THE GEAR DOWN, TURNED BACK AND LANDED - [SDR 95ZZZX4243](https://openairdocs.org/sdr/95ZZZX4243), Jul 28, 1995: RELAY. FAILED. HPN/PHL - FLT 3158 - WHEN THE GEAR WAS SELECTED UP AFTER TAKEOFF, THREE AMBER LIGHTS STAYED ON WITH GEAR UP. CREW SELECTED THE GEAR DOWN, TURNED BACK AND LANDED - [SDR 95ZZZX4246](https://openairdocs.org/sdr/95ZZZX4246), Jul 27, 1995: RELAY. FAILED. GON/BWI - FLT 3157 - ON GEAR RETRACTION, ALL 3 GEAR DOOR LIGHTS STAYED ON. AFTER CYCLING THE GEAR, THE LIGHTS GO OUT. AIRCRAFT CONTINUED ON TO BWI WITHOUT INCID - [SDR 95ZZZX4245](https://openairdocs.org/sdr/95ZZZX4245), Jul 27, 1995: RELAY. FAILED. GON/BWI - FLT 3157 - ON GEAR RETRACTION, ALL 3 GEAR DOOR LIGHTS STAYED ON. AFTER CYCLING THE GEAR, THE LIGHTS GO OUT. AIRCRAFT CONTINUED ON TO BWI WITHOUT INCID - [SDR 95ZZZW557](https://openairdocs.org/sdr/95ZZZW557), Mar 3, 1995: SMOKE DETECTOR. FAILED. FLT 3068 - CLT-LYH - ON TAXI OUT RECEIVED FLASE BAG BAY SMOKE WARNING, THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR - [SDR 95ZZZW556](https://openairdocs.org/sdr/95ZZZW556), Mar 3, 1995: SMOKE DETECTOR. FAILED. FLT 3068 - CLT-LYH - ON TAXI OUT RECEIVED FALSE BAG BAY SMOKE WARNING, THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR ## FAA accident and incident reports (4) 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 20031011032639I](https://openairdocs.org/incident/20031011032639I), Oct 11, 2003: Dhav DHC8102 (N980HA), Syracuse, NY. (-23) On October 11, 2003, a DHC-8, flt. 3629, crew reported that the #2 engine power uptrim partially activated during takeoff. Crew experienced repeated #2… - [Incident 20020630016339I](https://openairdocs.org/incident/20020630016339I), Jun 30, 2002: Dhav DHC8102 (N980HA), Pittsburgh, PA. (-23) On June 30, 2002 allegheny airlines flight #3731 aborted take-off on runway 28R due to #1 engine low oil pressure annunciator illuminating. The pilot… - [Incident 20020529019299I](https://openairdocs.org/incident/20020529019299I), May 29, 2002: Dhav DHC8102 (N980HA), Binghamton, NY. (-23) On Wednesday, may 29, 2002, the crew of DHC-8, N980HA, reported a right gear unsafe and nose yellow door light illuminated on climbout. Both gear… - [Incident 20011214034289I](https://openairdocs.org/incident/20011214034289I), Dec 14, 2001: Dhav DHC8102 (N980HA), Middletown, PA. (-23) After takeoff there was a heading mismatch. Crew returned to MDT with no further incident. There was no fire or injuries resulting from this incident.… --- 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.