# N925HA: Dehavilland DHC-8-102, registration cancelled 2003-06-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 18, 2003 - Exported to: Canada - 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: 111 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: August 19, 1988 - Certificate issued: April 25, 2003 - Last registry action: April 25, 2003 - Mode S code: ACD16D - Owner when cancelled: [Westinghouse Aircraft Leasing Inc](https://openairdocs.org/faa-owner/WESTINGHOUSE%20AIRCRAFT%20LEASING%20INC) - Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) - Owner type: Corporation - Owner's area on the map: 40.7598° N, 73.9907° W: Placed by OpenAirDocs at the center of ZIP code 10036, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N925HA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=925HA - Page: https://openairdocs.org/deregistered/N925HA-2003-06-18 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 (14) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HNAA0200049](https://openairdocs.org/sdr/HNAA0200049), Jun 22, 2002: LINE. LEAKING. NR 2 ENGINE OIL PRESSURE FLUX AND WARNING LIGHT ILLUMINATED, SHUT DOWN ENGINE QT 45 PSI, FOUND HOT SECTION SOAKED. CLEANED AND SERVICED ENGINE. NR 2 ENGINE LT N - [SDR HNAA0100052](https://openairdocs.org/sdr/HNAA0100052), Aug 30, 2001: ANGLE. CRACKED. NR 2 NACELLE HORSE COLLAR WAS FOUND CRACKED IN RADIUS OF FWD UPPER CLOSING ANGLE JUST ABOVE ENGINE HOIST ATTACH BRACKET. REPAIRED PER EO8-54-01-799. - [SDR HNAA0100026](https://openairdocs.org/sdr/HNAA0100026), Apr 13, 2001: LIGHT. INOPERATIVE. EMERGENCY LIGHTS OUT NR 3 & 4, FRONT RED LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY BASE. - [SDR HNAA0000080](https://openairdocs.org/sdr/HNAA0000080), Dec 3, 2000: LIGHT. INOPERATIVE. NUMBER 1 EMERGENCY FLOOR PATH LIGHT INOP. REPLACED LAMEP MODULE. - [SDR HNAA0000055](https://openairdocs.org/sdr/HNAA0000055), Jul 15, 2000: ANGLE. CRACKED. DURING AN UNRELATED INSPECTION FOUND THE KEEL STRUCTURE ANGLE AND WEB UNDER L/H CENTER SEAT RAIL AT STA 405.737 CRACKED FROM PREVIOUS IMPACT DAMAGE. PERFORMED M - [SDR HNAA0000047](https://openairdocs.org/sdr/HNAA0000047), Jun 9, 2000: ENGINE. OUT OF RIG. NR 1 ENGINE POWER LEVER WOULD NOT ADVANCE PAST 82 PERCENT TORQUE. AIRCRAFT RETURNED TO THE FIELD. RIGGED AND TRIMMED NR 1 ENGINE. - [SDR HNAA9900018](https://openairdocs.org/sdr/HNAA9900018), Jan 22, 1999: SHROUD. CRACKED. NR 1 ENGINE EXHAUST SHROUD HAS 1 INCH CRACK STA 223.4 AT 4 O'CLOCK POSITION, REAR I/B MOUNT BOLT OF FORWARD RADIATION SHIELD IS PULLED THROUGH, REAR O/B ANGLE B - [SDR HNAA9595504](https://openairdocs.org/sdr/HNAA9595504), Nov 4, 1995: EEL POWER SUPPLY. INOP. FLT NR 3040 - FLL TO TPA - DURING PREFLIGHT WALKAROUND, FOUND THE FIRST 2 RED FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE POWER SUPPLY AT 3352-PS2. (M - [SDR HNAA9592503](https://openairdocs.org/sdr/HNAA9592503), Nov 3, 1995: CONNECTOR. FAILED. FLT NR 3066 - MCO-TLH - AFTER GEAR EXTENSION, THE NOSE GEAR SHOWED UNSAFE. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED IN TLH WITHOUT INCIDENT. REMOVED AND RE - [SDR 95ZZZX6134](https://openairdocs.org/sdr/95ZZZX6134), Sep 29, 1995: AUTOFEATHER SW. FAILED. TPA/MIA - FLT 3005 - THE AUTOFEATHER ARM LIGHT FLICKERED AND WENT OUT DURING TAKEOFF. THE AIRCRAFT CONTINUED ON TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND - [SDR 95ZZZX6133](https://openairdocs.org/sdr/95ZZZX6133), Sep 29, 1995: ENGINE HARNESS. FAILED. TPA/MIA - FLT 3005 - THE AUTOFEATHER ARM LIGHT FLICKERED AND WENT OUT DURING TAKEOFF. THE AIRCRAFT CONTINUED ON TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND - [SDR 95ZZZX6128](https://openairdocs.org/sdr/95ZZZX6128), Sep 25, 1995: TQ CONTROL UNIT. FAILED. TPA/JAX - FLT 3166 - AFTER TAKEOFF DURING CLIMB, THE AUTOFEATHER ARM LIGHT ILLUMINATED INTERMITTENTLY. THE AIRCRAFT CONTINUED ON TO JAX AND LANDED WITHOUT INCID - [SDR 95ZZZM517](https://openairdocs.org/sdr/95ZZZM517), Sep 11, 1995: SWITCH. FAILED. FLT NR 3031 - TPA-JAX - THE AUTOFEATHER ARM LIGHT FLICKERED ON AND OFF SEVERAL TIMES DURING TAKEOFF. THE AIRCRAFT CONTINUED ON TO JAX AND LANDED WITHOUT INCIDEN - [SDR 95ZZZX5153](https://openairdocs.org/sdr/95ZZZX5153), Aug 25, 1995: AUTOFEATHER SW. DIRTY. MCO/TLH - FLT 3092 - ON TAKEOFF ROLL, AUTOFEATHER WOULD NOT ARM WHEN POWER LEVERS ADVANCED TO TAKEOFF SETTINGS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE --- 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.