# N814PH: Dehavilland DHC-8-102, registration cancelled 2001-05-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 23, 2001 - Exported to: Jamaica - Status when cancelled: Triennial form not returned - Airframe: [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102) (registry code 2809003) - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (OpenAirDocs) - Serial number: 043 - Type of aircraft: Fixed wing multi engine - Certificate issued: December 21, 1989 - Last registry action: July 18, 2000 - Mode S code: AB1985 - Owner when cancelled: [Cit Leasing Corporation](https://openairdocs.org/faa-owner/CIT%20LEASING%20CORPORATION) - Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) - Owner type: Corporation - Owner's area on the map: 40.7524° N, 73.9727° W: Placed by OpenAirDocs at the center of ZIP code 10017, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N814PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=814PH - Page: https://openairdocs.org/deregistered/N814PH-2001-05-23 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 (55, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR QXEA0100106](https://openairdocs.org/sdr/QXEA0100106), Feb 6, 2001: SEAT TRACK. CORRODED. PDX- FRETTING CORROSION ON INBOARD FLANGE OF LEFT INBOARD SEAT TRACK AT STATION X252.700 IN LINE WITH AFT EDGE OF MAIN CABIN DOOR. REPAIRED IAW PSM 1-GEN-5 CHAP - [SDR QXEA0100109](https://openairdocs.org/sdr/QXEA0100109), Feb 5, 2001: SKIN. DENTED. PDX- DENT IN AFT FUSELAGE SKIN 6 INCHES LONG, .020 INCH DEEP AFT OF FRAME X600.0 BETWEEN STRINGERS 22R AND 23R. REPAIRED IAW DHC-8 RD 8-53-436. - [SDR QXEA0100108](https://openairdocs.org/sdr/QXEA0100108), Feb 5, 2001: SEAT TRACK. CORRODED. PDX- FRETTING CORROSION ON INBOARD FLANGE OF LEFT HAND INBOARD SEAT TRACK AT STATION X252.700 IN LINE WITH AFT EDGE OF MAIN CABIN DOOR. REPAIRED IAW DHC-8 SRM 5 - [SDR QXEA0100100](https://openairdocs.org/sdr/QXEA0100100), Feb 4, 2001: SEAT TRACK. MISDRILLED. PDX- LEFT HAND INBOARD NR 4 SEAT TRACK SUPPORT ANGLE AT STATION 355.950 AND 354.250 HAS A 10:32 FASTENER HOLE THAT HAS BEEN MISDRILLED. REPAIRED IAW HORIZON AIR - [SDR QXEA0100113](https://openairdocs.org/sdr/QXEA0100113), Feb 2, 2001: ELEVATOR. INCORRECT. PDX- RIGHT HAND ELEVATOR INBOARD TRAILING EDGE DOES NOT FARE WITH ELEVATOR SKIN. REPAIRED IAW DHC-8 SRM 51-40-00. - [SDR QXEA0100114](https://openairdocs.org/sdr/QXEA0100114), Feb 1, 2001: ATTACH FITTING. CORRODED. PDX- LEFT HAND MAIN LANDING GEAR RETRACTION ACTUATOR ATTACH FITTING ATTACH POINT ON H-MEMBER HAS FRETTING CORROSION AT LEFT HAND SIDE OF UPPER MOUNT HOLES. REPA - [SDR QXEA0100116](https://openairdocs.org/sdr/QXEA0100116), Jan 31, 2001: STIFFENER. CRACKED. PDX- LOWER FINGERNAIL DECK OUTBOARD FORE/AFT STIFFENER IS CRACKED AT GEARWELL WALL VERTICAL STIFFENER OF LEFT HAND NACELLE. REPAIRED IAW DHC-8 SRM 51-40-11 AND - [SDR QXEA0100115](https://openairdocs.org/sdr/QXEA0100115), Jan 31, 2001: STIFFENER. CHAFED. PDX- FINGERNAIL DECK STIFFENER CHAFED THIN AT XN232.0 TOP SIDE. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-20-16. - [SDR QXEA0100110](https://openairdocs.org/sdr/QXEA0100110), Jan 31, 2001: SPLICE. CRACKED. PDX- FRAME JOINT SPLICE ANGLE AT STATION X136.80 AT STRINGER 15A RIGHT HAND IS CRACKED. REPAIRED IAW DHC-8 RD 8-53-576. - [SDR QXEA0100102](https://openairdocs.org/sdr/QXEA0100102), Jan 31, 2001: FLAP TRACK. DAMAGED. PDX- RIGHT HAND INBOARD FLAP, NR 2 OUTBOARD FLAP TRACK UPPER TRACK HAS A DIVET 10 INCHES AFT OF FORWARD END. REPAIRED IAW DHC-8 RD 8-57-986. - [SDR QXEA0100101](https://openairdocs.org/sdr/QXEA0100101), Jan 31, 2001: FLAP TRACK. DAMAGED. PDX- RIGHT HAND INBOARD FLAP, NR 1 INBOARD UPPER TRACK HAS DIVETS IN TOP AND BOTTOM 10 INCHES AFT OF FORWARD END. REPAIRED IAW DHC-8 RD 8-57-985. - [SDR QXEA0100112](https://openairdocs.org/sdr/QXEA0100112), Jan 30, 2001: SKIN. CRACKED. PDX- TOP RIGHT HAND SIDE OF TRAILING RUDDER SKIN HAS A CRACK PROGRESSING OUT FROM RIVET HOLE AT PREVIOUS REPAIR SKIN PATCH. REPAIRED IAW DHC-8 SRM 55-40-28 AND - [SDR QXEA0100111](https://openairdocs.org/sdr/QXEA0100111), Jan 30, 2001: SPLICE. CRACKED. PDX- CRACK FOUND IN LEFT HAND JOINT SPLICE FRAME AT STATION X136.80 AND STRINGER 15A. REPAIRED IAW DHC-8 RD 8-53-576. - [SDR QXEA0100117](https://openairdocs.org/sdr/QXEA0100117), Jan 29, 2001: DOOR FRAME. CORRODED. PDX- MAIN CABIN DOOR SURROUND FORWARD FRAME CORRODED AROUND NUTPLATE THAT IS BETWEEN 2ND AND 3RD STOPS FROM BOTTOM. REPAIRED IAW DHC-8 SRM 51-20-11 AND 53-00-16 - [SDR QXEA0100107](https://openairdocs.org/sdr/QXEA0100107), Jan 28, 2001: SEAT TRACK. CORRODED. PDX- CORROSION ON LEFT INBOARD SEAT TRACK FLANGE LOCATED IN CARGO AREA AT STATION 580.50. REPAIRED IAW DHC-8 SRM 51-20-16. - [SDR QXEA0003187](https://openairdocs.org/sdr/QXEA0003187), Dec 10, 2000: BALLAST. MALFUNCTIONED. PDX- BURNED ELECTRICAL INSULATION SMELL IN CABIN. REMOVED AND REPLACED BALLAST. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA0002065](https://openairdocs.org/sdr/QXEA0002065), Aug 2, 2000: ACTUATOR. MALFUNCTIONED. YVR- AFTER DEPARTURE LEFT HAND GEAR DOOR RETRACTED, THEN FELL OPEN. CYCLED GEAR, DOOR REMAINED CLOSED. REMOVED AND REPLACED LEFT HAND AFT AND CENTER GEAR DOOR A - [SDR QXEA0001824](https://openairdocs.org/sdr/QXEA0001824), Jul 7, 2000: SEQUENCE VALVE. MALFUNCTIONED. PSC- AFTER SELECTING GEAR UP, MAIN GEAR DOOR AMBER LIGHT ON AND VISUALLY CONFIRMED LIGHT GEAR DOOR FAILED TO CLOSE. PERFORMED ALTERNATE GEAR EXTENSION METHOD. L - [SDR QXEA0001823](https://openairdocs.org/sdr/QXEA0001823), Jul 6, 2000: PSEU. MALFUNCTIONED. SEA- AFTER SELECTING GEAR UP, MAIN GEAR DOOR AMBER LIGHT ON AND VISUALLY CONFIRMED LIGHT GEAR DOOR FAILED TO CLOSE. PERFORMED ALTERNATE GEAR EXTENSION METHOD. L - [SDR QXEA0001343](https://openairdocs.org/sdr/QXEA0001343), May 20, 2000: STOP. MALFUNCTIONED. SEA- MAIN CABIN DOOR IS HARD TO OPEN FROM THE OUTSIDE. REPLACED RUBBER STOP FOR EXTERIOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA0001127](https://openairdocs.org/sdr/QXEA0001127), Apr 17, 2000: FAIRING. DAMAGED. PDX- ON TAKEOFF AT GEAR RETRACTION, NOTED RUMBLING NOISE. LEFT DOOR, NOSE DOOR, RIGHT UNSAFE (RED) LIGHTS APPEARED. COMPLIED WITH LANDING GEAR NOT RETRACTING CH - [SDR QXEA0000751](https://openairdocs.org/sdr/QXEA0000751), Mar 14, 2000: INVERTER. MALFUNCTIONED. BOI- STRONG FISH SMELL COMING FROM BEHIND CAPTIN''S SEAT AREA. REMOVED AND REPLACED PRIMARY INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9902592](https://openairdocs.org/sdr/QXEA9902592), Dec 9, 1999: LIGHT. MALFUNCTIONED. PDX- COCKPIT EMERGENCY LIGHT ILLUMINATED WHEN EMERGENCY LIGHTS WERE ARMED. REPLACED COCKPIT LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD. - [SDR QXEA9902444](https://openairdocs.org/sdr/QXEA9902444), Nov 25, 1999: SWITCH. FAILED. SEA- EMERGENCY LIGHTS CIRCUIT BREAKER POPS EVEN WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED FLIGHT ATTENDENTS EMERGENCY LIGHTING SWITCH AND EMERGENCY LIGH - [SDR QXEA9901524](https://openairdocs.org/sdr/QXEA9901524), Jul 29, 1999: BOLT. LOOSE. SEA - MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE RESECURED HANDRAIL SUPPORT PIVOT BOLT. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. - [SDR QXEA9900510](https://openairdocs.org/sdr/QXEA9900510), Mar 22, 1999: ENGINE. FLAMED OUT. SEA- ON DESCENT INTO SEA, THE AIRCRAFT EXPERIENCED MODERATE TO SEVERE TURBULENCE WHILE IN INSTRUMENT METROLOGICAL CONDITIONS (IMC). DURING THIS PERIOD, BOTH ENG - [SDR QXEA9801057](https://openairdocs.org/sdr/QXEA9801057), Aug 3, 1998: VALVE. MALFUNCTION. SEA - LEFT GEAR DOOR LIGHT REMAINED ON WHEN THE LANDING GEAR WAS RETRACTED. DOOR VISUALLY INSPECTED AND VERFIED TO BE OPEN. WHEN GEAR CYCLED THE LIGHT WENT OUT. - [SDR QXEA9801052](https://openairdocs.org/sdr/QXEA9801052), Aug 2, 1998: VALVE. MALFUNCTION. LEFT MAIN GEAR DOOR REMAINED OPEN AFTER LANDING GEAR RETRACTION. AFTER CYCLING GEAR, THE DOOR CLOSED NORMALLY. FERRIED AIRCRAFT FROM SEA TO PDX FOR REPAIRS. IN - [SDR QXEA9801044](https://openairdocs.org/sdr/QXEA9801044), Jul 23, 1998: ACTUATOR. MALFUNCTION. DURING LANDING GEAR RETRACTION, THE LEFT GEAR DOOR LIGHT STAYED ON AND THE GEAR DOOR WAS NOTICED TO BE OPEN. CYCLED THE LANDING GEAR AND THE DOOR OPERATED PROPE - [SDR QXEA9801035](https://openairdocs.org/sdr/QXEA9801035), Jul 19, 1998: ACTUATOR. OUT OF ADJUST. AFTER GEAR SELECTED UP THE AMBER DOOR LIGHT REMAINED ON. VISUALLY VERIFIED THAT THE GEAR DOOR WAS OPEN. CYCLED LANDING GEAR AND ALL LIGHTS WENT OUT. ADJUSTED AF - [SDR QXEA9800949](https://openairdocs.org/sdr/QXEA9800949), Jul 15, 1998: STOP. MISSING. ALW - MAIN CABIN DOOR MISSING BLACK RUBBER STOPPER FOR THE EXTERNAL HANDLE. AIRCRAFT FERRIED FROM ALW TO SEA FOR REPAIRS. IN SEA, REPLACED THE BLACK RUBBER STOP - [SDR QXEA9800636](https://openairdocs.org/sdr/QXEA9800636), May 5, 1998: RETRACT MECH. OUT OF ADJUST. SEA - AFTER GEAR RETRACTION, THE LEFT GEAR DOOR REMAINED IN THE OPEN POSITION. CYCLED THE LANDING GEAR AND THE DOOR CLOSED NORMALLY. INSPECTED THE AIRCRAFT AND - [SDR QXEA9800534](https://openairdocs.org/sdr/QXEA9800534), Apr 17, 1998: RETRACT MECH. MALFUNCTIONED. LEFT MAIN FORWARD GEAR DOOR REMAINS OPEN AFTER TAKEOFF. GEAR WAS CYCLED, AND THE DOOR CLOSED. INSPECTED FORWARD GEAR DOOR ACTUATION MECHANISM, NO DEFECTS NOTED. - [SDR QXEA9800453](https://openairdocs.org/sdr/QXEA9800453), Mar 31, 1998: PSEU. MALFUNCTION. AFTER TAKEOFF, WHEN THE LANDING GEAR WAS SELECTED UP, ALL GEAR INDICATION LIGHTS WENT OUT NORMALLY. AFTER ABOUT 5 SECONDS THE LEFT GEAR DOOR LIGHT ILLUMINATED. - [SDR QXEA9800016](https://openairdocs.org/sdr/QXEA9800016), Jan 8, 1998: HYD LINE. LEAKING. AFTER TAKEOFF, NOTICED AN ODORLESS CHEMICAL IRRITANT IN THE COCKPIT. THE IRRITANT WAS NOTICED IN THE COCKPIT FOR A PERIOD OF ABOUT 20 SECONDS. MX PERFORMED AN E - [SDR QXEA9700673](https://openairdocs.org/sdr/QXEA9700673), Oct 17, 1997: SEAT MECHANISM. LACK OF LUBE. PDX - FIRST OFFICERS SEAT SLIPPED BACK IN ITS TRACK DURING FLIGHT. CLEANED AND LUBED FIRST OFFICERS SEAT TRACK MECHANISM. NO PARTS REPLACED, OPERATIONAL CHECK G - [SDR QXEA9700574](https://openairdocs.org/sdr/QXEA9700574), Sep 19, 1997: MECHANISM. OUT OF ADJUST. PDX - LEFT HAND GEAR DOOR LIGHT STAYED ON AFTER GEAR WAS RAISED. ADJUSTED MAIN LANDING GEAR DOOR (REAR AND CENTER) ACTUATORS. ADJUSTED MAIN LANDING GEAR FORWARD - [SDR QXEA9700610](https://openairdocs.org/sdr/QXEA9700610), Aug 28, 1997: BALL SCREW ACT. DAMAGED. PDX - NR 3 AND NR 4 BALL SCREW ACTUATORS HAVE SLIGHT BRINELLING DAMAGE. REPAIRED IAW EA 9-27-69. - [SDR QXEA9700609](https://openairdocs.org/sdr/QXEA9700609), Aug 28, 1997: BALL SCREW. DAMAGED. PDX - BALL SCREWS WITH SLIGHT BRINELLING DAMAGE. REPAIRED IAW EA 9-27-69. - [SDR QXEA9700607](https://openairdocs.org/sdr/QXEA9700607), Aug 27, 1997: ANGLE. CRACKED. PDX - CRACK FLANGE OF THE NACELLE DRAG ANGLE, (P/N 85710323). REPAIRED IAW EA 9-57-291. - [SDR QXEA9700608](https://openairdocs.org/sdr/QXEA9700608), Aug 25, 1997: WEB. CHAFED. PDX - RIGHT HAND NACELLE FINGERNAIL UPPER DECK CHAFE HOLE IN WEB. DAMAGE IS JUST OUTBOARD OF YN=0.00 AND JUST AFT OX XN=245. REPAIRED IAW 9-54-139. - [SDR QXEA9700606](https://openairdocs.org/sdr/QXEA9700606), Aug 25, 1997: HINGE BOLT. MISINSTALLED. PDX - RIGHT MAIN LANDING GEAR FORWARD DOOR AFT HINGE AFT FRAME (85410422) AND JOINT STRAP (85410426) THAT WAS DAMAGED BY THE HINGE BOLT BEING INSTALLED BACKWARD - [SDR QXEA9700322](https://openairdocs.org/sdr/QXEA9700322), Jul 10, 1997: PSEU. MALFUNCTION. ON APPROACH WHEN LANDING GEAR SELECTED DOWN, HAD 3 RED LANDING GEAR UNSAFE LIGHTS AND A LANDING GEAR HANDLE DISAGREEMENT LIGHT. PERFORMED AND ALTERNATE EXTENSIO - [SDR QXEA9700148](https://openairdocs.org/sdr/QXEA9700148), Apr 25, 1997: DIODE. DEFECTIVE. EMERGENCY EGRESS LIGHTS WILL NOT EXTINGUISH WHEN THE ARM-OFF SWITCH IS PLACED INTO THE OFF POSITION. AIRCRAFT FERRIED FROM SEA-PDX. REPLACED DIODE 3351-CR5, OPE - [SDR QXEA9700144](https://openairdocs.org/sdr/QXEA9700144), Apr 24, 1997: CONTROL BOX. DEFECTIVE. EMERGENCY LIGHTS WILL NOT EXTINGUISH USING THE ARM-OFF SWITCH. REPLACED LIGHT CONTROL UNIT AND PS2, PS1, P1, P2, P4, P5 POWER SUPPLIES AND BATTERIES, OPERATIONA - [SDR QXEA9700142](https://openairdocs.org/sdr/QXEA9700142), Apr 23, 1997: CONTROL BOX. DEFECTIVE. EMERGENCY EGRESS LIGHTS REMAIN ON EVEN WHEN THE SWITCH IS MOVED FROM ARM TO OFF. REPLACED EMERGENCY LIGHT CONTROLLER, OPERATIONAL CHECK GOOD. - [SDR QXEA9700135](https://openairdocs.org/sdr/QXEA9700135), Apr 20, 1997: DETECTOR. DEFECTIVE. PDX- NR 1 BAGGAGE SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED NR 1 SMOKE DETECTOR. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9700105](https://openairdocs.org/sdr/QXEA9700105), Apr 1, 1997: RADAR INDICATOR. FAILED. RADAR SCREEN WENT BLANK FOLLOWED BY STRONG ACRID SMELL IN COCKPIT, CREW TURNED RADAR OFF AND SMELL WENT AWAY. FLIGHT LANDED WITHOUT INCIDENT, RADAR DEFERRED PER - [SDR QXEA9700010](https://openairdocs.org/sdr/QXEA9700010), Jan 11, 1997: WIRE. BROKEN. PDX - ON APPROACH TO PDX RECEIVED 3 RED INTRANSIT LIGHT INDICATIONS, BUT LANDING GEAR DID NOT EXTEND. ALTERNATE GEAR EXTENSION PERFORMED AND GEAR EXTENDED. AIRC - [SDR QXEA9600415](https://openairdocs.org/sdr/QXEA9600415), Sep 29, 1996: LIGHT. MALFUNCTIONED. DURING OPS CHECK OF EMERGENCY LIGHTS, LIGHTS WOULD STAGGER OFF AND THEIR OWN WITHIN A COUPLE ON MINUTES. AIRCRAFT FERRIED TO PDX FOR REPAIR. PORTABLE EMERGENCY All 55: https://openairdocs.org/deregistered/N814PH-2001-05-23/reports.md ## FAA accident and incident reports (2) 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 19990513014319I](https://openairdocs.org/incident/19990513014319I), May 13, 1999: Dhav DHC8102 (N814PH), Portland, OR. After reaching 3000 ft, while departing from pdx, the flight crew was given a left turn by ATC. The fo noticed very still aileron control while in the left… - [Incident 19890105007529I](https://openairdocs.org/incident/19890105007529I), Jan 5, 1989: Dhav DHC8102 (N814PH), Portland, OR. Shortly after departure pilot shut NR2 engine down and returned to Portland. Landed without incident. Cause unknown --- 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.