# N920HA: Dehavilland DHC-8-102, registration cancelled 2003-07-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 24, 2003 - Status when cancelled: Sale reported - 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: 084 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: July 17, 1987 - Last registry action: July 24, 2003 - Mode S code: ACBEDA - Location: [Lewisville, TX](https://openairdocs.org/faa-place/TX/Lewisville) - Owner type: Individual - Owner's area on the map: 33.0506° N, 96.9727° W: Placed by OpenAirDocs at the center of ZIP code 75057, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N920HA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=920HA - Page: https://openairdocs.org/deregistered/N920HA-2003-07-24 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 (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HNAA0000063](https://openairdocs.org/sdr/HNAA0000063), Aug 17, 2000: BATTERY PACK. DISCHARGED. FOUND MULTIPLE EMERGENCY LIGHTS INOP. FOUND EMERGENCY LIGHTS BATTERY PACKS 3351-PS1, 3351-PS2 AND 3351-PS4 DISCHARGED. REPLACED BATTERY PACKS. - [SDR HNAA0000048](https://openairdocs.org/sdr/HNAA0000048), Jun 11, 2000: STRUT. BROKEN. PASSENGER DOOR WOULD NOT OPEN. FOUND THE FWD UPPER DOOR SUPPORT STRUT BROKEN. REPLACED FWD UPPER SUPPORT STRUT. - [SDR HNAA0000036](https://openairdocs.org/sdr/HNAA0000036), Apr 30, 2000: SENSOR. OUT OF ADJ. THE PASSENGER DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. FOUND THE DOOR PROXIMITY SENSOR GAP WAS TOO WIDE WITH THE AIRCRAFT PRESSURIZED. ADJUSTED DOOR PROXIMITY - [SDR HNAA9900031](https://openairdocs.org/sdr/HNAA9900031), Feb 19, 1999: SEAT TRACK. CORRODED. LEFT FORWARD INBOARD SEAT TRACK HAS CORROSION BEYOND LIMITS. REPLACED SEAT TRACK. - [SDR HNAA9900022](https://openairdocs.org/sdr/HNAA9900022), Jan 30, 1999: STRUCTURE. CORRODED. CORROSION RIGHT FUSELAGE ON STRINGER SPLICE AT STR 32S FRAME 488, SPLICE ON STR 29 AND AT FRAME 488, FRAME 433 LEG AT ST 31S, STR 29 .021 DEEP AT FRAME 529, SUR - [SDR HNAA9900017](https://openairdocs.org/sdr/HNAA9900017), Jan 23, 1999: TAB. BROKEN. LOWER AFT CORNER OF PASSENGER DOOR ENTRANCE COMBING HAS TAB BROKEN OFF. REPAIRED AS NECESSARY. - [SDR HNAA9900015](https://openairdocs.org/sdr/HNAA9900015), Jan 15, 1999: SKIN. CHAFED. RIGHT HAND WING OUTBOARD FLAP INBOARD UPPER SKIN HAS CHAFE, DEPTH IS .009 LENGTH AND WIDTH .3 BY .3 LOCATED 2.5 INCHES FROM INBOARD EDGE. REPAIRED AS NECESSARY. - [SDR HNAA9900014](https://openairdocs.org/sdr/HNAA9900014), Jan 15, 1999: BRACKET. CRACKED. RIGHT HAND AILERON TRIM TAB ATTACH BRACKET CRACKED APPROXIMATELY 1 INCH RADIUS ON AFT SIDE FORWARD. REPLACED BRACKET. - [SDR HNAA9900013](https://openairdocs.org/sdr/HNAA9900013), Jan 15, 1999: CONDUIT. DAMAGED. RIGHT WING WIRE CONDUIT RIPPED OPEN AND BRACKET DAMAGED AT NR 4 FLAP JACKSCREW LOCATION. REPAIRED AS NECESSARY. - [SDR HNAA9900005](https://openairdocs.org/sdr/HNAA9900005), Jan 8, 1999: BOOTS. MALFUNCTIONED. EN ROUTE MULTIPLE DEICE BOOTS DID NOT INFLATE IN FREEZING CONDITIONS. CHECKED ALL BOOTS WITH SHOP AIR IN MANUAL AND AUTO MODE. REMOVED AND REINSTALLED DRAIN PLU - [SDR HNAA9892064](https://openairdocs.org/sdr/HNAA9892064), Oct 10, 1998: COVER. CORRODED. SBY - DURING C-CHECK INSPECTION, FOUND CORROSION ON THE RIGHT WING MIDDLE FUEL TANK LID THAT WAS MAINTENANCE MANUAL LIMITS. REPAIRED IAW PIEDMONT AIRLINES E08-5 - [SDR HNAA9892063](https://openairdocs.org/sdr/HNAA9892063), Oct 10, 1998: COVER. CORRODED. SBY - DURING C-CHECK INSPECTION, THE RIGHT WING MIDDLE FUEL CELL COVER PLATE WAS FOUND TO BE CORRODED BEYOND MAINTENANCE MANUAL LIMITS. REPAIRED THE COVER IAW P - [SDR HNAA9892061](https://openairdocs.org/sdr/HNAA9892061), Oct 10, 1998: PLATE. CORRODED. SBY - DURING C-CHECK INSPECTION, FOUND CORROSION PITS WERE FOUND IN THE FUEL CELL LID AND LADDER PLATE ON THE OUTBOARD END. REPAIRED IAW PIEDMONT AIRLINES E08-5 - [SDR HNAA9892057](https://openairdocs.org/sdr/HNAA9892057), Sep 16, 1998: VALVE. FAILED. CLT/HHH - FLT 3160 - LOST HYDRAULIC QUANTITY AND PRESSURE AFTER LANDING GEAR EXTENSION. DIVERTED TO SAV. REMOVED AND REPLACED SOLENOID SEQUENCE VALVE FOR NOSE G - [SDR HNAA9892044](https://openairdocs.org/sdr/HNAA9892044), Sep 2, 1998: VALVE. FAILED. FLT 3470 - CLT-CHA - UPON GEAR UP SELECTION AFTER TAKEOFF, 3 RED UNSAFE LIGHTS ILLUMINATED AND GEAR DID NOT MOVE. SELECTED GEAR DOWN AND 3 GEAR DOWN/LOCKED LIGH - [SDR HNAA9792025](https://openairdocs.org/sdr/HNAA9792025), Feb 23, 1997: WIRE. FAILED. FLT 3030 - PHL-DCA - AFTER TAKEOFF, SMELLED SMOKE AND NOTICED SMOKE COMING FROM CAPTAINS WINDSHIELD HEAT TERMINALS. TURNED WINDSHIELD HEAT OFF AND RETURNED TO P - [SDR HNAA9692011](https://openairdocs.org/sdr/HNAA9692011), Feb 13, 1996: BATTERY PACK. DISCHARGED. PHF/DCA - FLT 3091 - DURING PREFLIGHT WALK-AROUND, FOUND LEFT AND RIGHT UNDERWING INTERIOR AND EXTERIOR EEL LIGHTS INOPERATIVE. REMOVED AND REPLACED PS3 AND PS6 - [SDR 95ZZZW675](https://openairdocs.org/sdr/95ZZZW675), Apr 20, 1995: FUEL FILTER. FAILED. FLT 3289 - TPA - MIA - DURING TAKEOFF, THE NR 1 FUEL FILTER BYPASS CAUTION LIGHT CAME ON. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVE - [SDR 95ZZZW674](https://openairdocs.org/sdr/95ZZZW674), Apr 20, 1995: SWITCH. FAILED. FLT 3289 - TPA - MIA - DURING TAKEOFF, THE NR 1 FUEL FILTER BYPASS CAUTION LIGHT CAME ON. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVE - [SDR 95ZZZW555](https://openairdocs.org/sdr/95ZZZW555), Apr 1, 1995: ACTUATOR. FAILED. FLT 3465 - MIA-MCO - AFTER TAKEOFF AND AFTER GEAR RETRACTION, THE RIGHT MAIN GEAR DOOR FAILED TO CLOSE. AIRCRAFT TURNED BACK AND LANDED IN MIA WITHOUT INCIDENT. - [SDR 95ZZZW554](https://openairdocs.org/sdr/95ZZZW554), Mar 30, 1995: RETRACT MECH. MALFUNCTIONED. FLT NR 3442 - TPA-JAX - AFTER TAKEOFF AND DURING GEAR RETRACTION, THE RIGHT MAIN GEAR DOOR AMBER ADVISORY LIGHT ILLUMINATED. VISUAL INSPECTION CONFIRMED THE RIG ## FAA accident and incident reports (1) 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 19940511016549I](https://openairdocs.org/incident/19940511016549I), May 11, 1994: Dhav DHC8102 (N920HA), Lynchburg, VA. Fire warning NR1 engine. Shut engine down. Returned. No external fire noted. Found compressor turbine damage. ## Other aircraft with N920HA - [Registered now](https://openairdocs.org/aircraft/N920HA): Hiller UH-12D, S/N 1361, built 1962 --- 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.