# N817PH: Dehavilland DHC-8-102, registration cancelled 2018-01-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 29, 2018 - Status when cancelled: Registration expired, pending cancellation - 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: 056 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: December 9, 1986 - Certificate issued: February 8, 2002 - Last registry action: February 19, 2008 - Mode S code: AB24AA - Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N817PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=817PH - Page: https://openairdocs.org/deregistered/N817PH-2018-01-29 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 (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SABA980058](https://openairdocs.org/sdr/SABA980058), Oct 23, 1998: ENGINE. FAILED. CLT-CVG - FLT 5033 - THE LEFT ENGINE HAD A UNCOMMANDED SHUT DOWN AT 9000 FT AND ON APPROACH TO CINCINNATI. THERE WAS NO UNUSUAL TEMPS OR PRESSURE READINGS PRIOR - [SDR SABA980048](https://openairdocs.org/sdr/SABA980048), Sep 28, 1998: WX RADAR. MALFUNCTIONED. CLT - FLT 5069 - RADAR DOES NOT FUNCTION PROPERLY. WILL NOT PAINT WX. AIRCRAFT RETURNED CLT. NO INFLIGHT EMERGENCY DECLARED. AIRCRAFT LANDED CLT NO OTHER DISCRE - [SDR SABA290041](https://openairdocs.org/sdr/SABA290041), Aug 13, 1998: BLADE. BIRD STRIKE. GNV/CLT - FLT 5061 - UPON ARRIVAL INTO THE CHARLOTTE AREA, PILOT REPORTED HE TOOK A SMALL BIRD STRIKE ON THE RIGHT PROPELLER. NO IN-FLIGHT EMERGENCY WAS DECLARE - [SDR QXEA9800134](https://openairdocs.org/sdr/QXEA9800134), Jan 16, 1998: PLATE. DAMAGED. PDX - THE ELEVENTH HOLE FROM THE INBOARD SIDE ON THE FORWARD SIDE OF LADDER PLATE FOR 624AT IS ELONGATED APPROXIMATELY .030. REPAIRED IAW EA 9-57-337. - [SDR QXEA9800137](https://openairdocs.org/sdr/QXEA9800137), Jan 13, 1998: H MEMBER. CHAFED. PDX - NR 1 MAIN LANDING GEAR H-MEMBER CHAFFED FROM CONTACT WITH STANDBY PUMP HYDRAULIC PRESSURE FLEX LINE. REPAIRED IAW EA 9-32-62. - [SDR QXEA9800133](https://openairdocs.org/sdr/QXEA9800133), Jan 10, 1998: SKIN. DENTED. PDX - MAIN CABIN DOOR EXTERIOR SKIN HAS TWO SMOOTH DENTS BOTH .035 BY 1.5 WITHIN ON INCH OF FASTENERS ON THE TOP BEAM. REPAIRED IAW EA 9-52-77. - [SDR QXEA9800135](https://openairdocs.org/sdr/QXEA9800135), Jan 9, 1998: SKIN. DENTED. PDX - UPPER SKIN ON OUTBOARD FLAP HAS A SMALL DENT AND CHAFE AT INBOARD END OF FLAP. REPAIRED IAW EA 9-57-336. - [SDR QXEA9800136](https://openairdocs.org/sdr/QXEA9800136), Jan 8, 1998: FITTING. CORRODED. PDX - RIGHT MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING MATING SURFACE ON NACELLE FIREWALL AND MAIN LANDING GEAR FRAME STRUCTURAL ASSEMBLY HAS FRET - [SDR QXEA9700760](https://openairdocs.org/sdr/QXEA9700760), Nov 16, 1997: OIL SYSTEM. REQUIRED SERVICE. YKM- SHORTLY AFTER TAKEOFF, NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED. THE NR 2 OIL PRESSURE GAUGE WAS FLUCTUATING BELOW 40 PSI. AFTER LEVEL-OFF THE WARNING LI - [SDR QXEA9700165](https://openairdocs.org/sdr/QXEA9700165), May 4, 1997: LIGHT. INOPERATIVE. COCKPIT OVERHEAD EMERGENCY FLASHLIGHT INOP. REPLACED COCKPIT OVERHEAD LIGHT, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700139](https://openairdocs.org/sdr/QXEA9700139), Apr 21, 1997: BATTERY. DISCHARGED. RED LIGHT ON FLIGHT ATTENDANT FLASHLIGHT IS NOT FLASHING. REPLACED BATTERY PACK FOR FLASHLIGHT, OPERATIONAL CHECKS GOOD. - [SDR QXEA9600494](https://openairdocs.org/sdr/QXEA9600494), Dec 16, 1996: CONTROL BOX. MALFUNCTIONED. CABIN EMERGENCY LIGHTS WOULD NOT EXTINGUISH WHEN SELECTED OFF AT FIRST OFFICERS SWITCH. AIRCRAFT MUST BE POWERED DOWN AND CYCLED OFF TO EXTINGUISH. EMERGENCY LI - [SDR QXEA9600221](https://openairdocs.org/sdr/QXEA9600221), Jun 24, 1996: LIGHT. INOPERATIVE. BOI - COCKPIT EMERGENCY LIGHT IS INOP. LIGHT WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9600173](https://openairdocs.org/sdr/QXEA9600173), May 16, 1996: BULB. FAILED. EMERGENCY LIGHT IN COCKPIT IS INOP. LAMP WAS REPLACED AND BROKEN WIRE TO TEST SWITCH ON LANTERN REPAIRED, LIGHT OPS CHECKED GOOD. - [SDR QXEA9600164](https://openairdocs.org/sdr/QXEA9600164), Apr 30, 1996: CONTROLLER. MALFUNCTIONING. BOI - EMERGENCY LIGHTS REMAIN ON WITH SWITCH IN THE OFF POSITION AND AIRCRAFT POWER ON. AIRCRAFT INSPECTED AND FERRIED TO PDX FOR REPAIR. EMERGENCY LIGHT CONTRO - [SDR QXEA9600163](https://openairdocs.org/sdr/QXEA9600163), Apr 30, 1996: LIGHT. INOPERATIVE. PDX - COCKPIT EMERGENCY LIGHT IS INOPERATIVE. COCKPIT EMERGENCY LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9600145](https://openairdocs.org/sdr/QXEA9600145), Apr 8, 1996: LIGHT. INOPERATIVE. RIGHT HAND FORWARD EMERGENCY EXIT LIGHT IS INOP. SOCKET AND LAMP WERE REPLACED AND LIGHT OPS CHECKED GOOD. - [SDR QXEA950130](https://openairdocs.org/sdr/QXEA950130), Apr 29, 1995: EEL PWR SUPPLY. INOP. SEA - THE TWO FORWARD RED FLOOR PROXIMITY LIGHT ARE INO. REPLACED POWER SUPPLY AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ## 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 19870512022959I](https://openairdocs.org/incident/19870512022959I), May 12, 1987: Dhav DHC8102 (N817PH), Great Falls, MT. The aircraft returned after takeoff due to fluctuating torque on one engine. No malfunction found. ## Other aircraft with N817PH - [Registered now](https://openairdocs.org/aircraft/N817PH): Cirrus Design SR22T, S/N 9555, built 2023 --- 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.