# N821PH: Dehavilland DHC-8-102, registration cancelled 2000-04-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 14, 2000 - Exported to: Jamaica - Status when cancelled: Valid registration - 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: 104 - Type of aircraft: Fixed wing multi engine - Certificate issued: April 7, 2000 - Last registry action: April 7, 2000 - Mode S code: AB35DF - Owner when cancelled: [Bombardier Capital Inc](https://openairdocs.org/faa-owner/BOMBARDIER%20CAPITAL%20INC) - Location: [Colchester, VT](https://openairdocs.org/faa-place/VT/Colchester) - Owner type: Non-citizen corporation - Owner's area on the map: 44.5541° N, 73.2255° W: Placed by OpenAirDocs at the center of ZIP code 05446, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N821PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=821PH - Page: https://openairdocs.org/deregistered/N821PH-2000-04-14 From the FAA registry file of November 5, 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 (47) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR QXEA9901591](https://openairdocs.org/sdr/QXEA9901591), Jul 28, 1999: FRAME. CORRODED. PDX - NACELLE FRAME UNDER MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION. REPAIRED IAW HORIZON AIR EA 9-54-203. - [SDR QXEA9901585](https://openairdocs.org/sdr/QXEA9901585), Jul 24, 1999: ANGLE. CRACKED. PDX - LEFT FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-00, PAGE 4, TABLE 4. - [SDR QXEA9901605](https://openairdocs.org/sdr/QXEA9901605), Jul 20, 1999: SEAT TRACK. GOUGED. PDX - LEFT INBOARD SEAT TRACK HAS TWO GAUGES AT X268. REPAIRED IAW DHC-8 SRM 51-26-26. - [SDR QXEA9901600](https://openairdocs.org/sdr/QXEA9901600), Jul 20, 1999: SEAT TRACK. CORRODED. PDX - RIGHT OUTBOARD SEAT TRACK AT X312 HAS CORROSION PITS. REPAIRED IAW RD 8-53-1342. - [SDR QXEA9901599](https://openairdocs.org/sdr/QXEA9901599), Jul 20, 1999: SEAT TRACK. CORRODED. PDX - RIGHT OUTBOARD SEAT TRACK AT X327 HAS DEEP CORROSION PITS. REPAIRED IAW DHC8 SRM 51-26-26. - [SDR QXEA9901597](https://openairdocs.org/sdr/QXEA9901597), Jul 20, 1999: SEAT TRACK. CORRODED. PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION PITS IN THE HAT CHANNEL AT X364. REPAIRED IAW RD 8-53-1342. - [SDR QXEA9901596](https://openairdocs.org/sdr/QXEA9901596), Jul 20, 1999: SEAT TRACK. CORRODED. PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION PITS IN THE HAT CHANNEL AT X374. REPAIRED IAW RD 8-53-1342. - [SDR QXEA9901594](https://openairdocs.org/sdr/QXEA9901594), Jul 20, 1999: SEAT TRACK. CORRODED. PDX - LEFT OUTBOARD SEAT TRACK AT STATION 342 THERE IS CORROSION PITS. REPAIRED IAW RD 8-53-1342. - [SDR QXEA9901588](https://openairdocs.org/sdr/QXEA9901588), Jul 20, 1999: HOUSING. CHAFED. PDX - LEFT NR 5 FLAP CARRIAGE HOUSING ASSEMBLY IS CHAFED ON INBOARD SIDE WHERE FAIL/SAFE STRAP MOUNTS. REPAIRED IAW HORIZON AIR EA 9-57-437. - [SDR QXEA9901589](https://openairdocs.org/sdr/QXEA9901589), Jul 19, 1999: FLAP TRACK. OUT OF ADJUST. PDX - LEFT NR 4 FLAP TRACK ASSEMBLY TO CHECK GAPS. REPAIRED IAW HORIZON AIR EA 9-57-436. - [SDR QXEA9901584](https://openairdocs.org/sdr/QXEA9901584), Jul 19, 1999: FLAP TRACK. OUT OF POSITION. PDX- LEFT NR 4 FLAP TRACK AFT ATTACH GAPS DO NOT MEET MANUFACTURERS SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436. - [SDR QXEA9901583](https://openairdocs.org/sdr/QXEA9901583), Jul 19, 1999: FLAP TRACK. OUT OF POSITION. PDX - LEFT NR 5 FLAP TRACK AFT ATTACH GAPS DO NOT MEET MANUFACTURER SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436. - [SDR QXEA9901577](https://openairdocs.org/sdr/QXEA9901577), Jul 19, 1999: FLAP TRACK. OUT OF ADJUST. PDX - RIGHT NR 4 FLAP TRACK AFT MOUNT GAPS DO NOT MEET MANUFACTURERS GAP SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436. - [SDR QXEA9901576](https://openairdocs.org/sdr/QXEA9901576), Jul 19, 1999: MOUNT. OUT OF ADJUST. PDX - RIGHT NR 4 FLAP AFT MOUNT GAPS DO NOT MEET MANUFACTURERS GAP SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436. - [SDR QXEA9901582](https://openairdocs.org/sdr/QXEA9901582), Jul 17, 1999: SKIN. DAMAGED. PDX - LEFT OUTBOARD FLAP ASSEMBLY INBOARD SIDE HAS COMPOSITE DAMAGE. REPAIRED IAW DHC8 SRM 51-40-00, PAGE 201, FIGURE 2. - [SDR QXEA9901580](https://openairdocs.org/sdr/QXEA9901580), Jul 17, 1999: ANGLE. CRACKED. PDX - RIGHT AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-11. - [SDR QXEA9901592](https://openairdocs.org/sdr/QXEA9901592), Jul 16, 1999: HINGE. CORRODED. PDX - FORE RUDDER BOTTOM SAFETY HINGE LUG IS CHAFFED AND HAS FRETTING CORROSION ACROSS ENTIRE LUG TOP SURFACE. REPAIRED IAW RD 8-55-537. - [SDR QXEA9901586](https://openairdocs.org/sdr/QXEA9901586), Jul 16, 1999: ANGLE. CRACKED. PDX - LEFT AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-11. - [SDR QXEA9901590](https://openairdocs.org/sdr/QXEA9901590), Jul 15, 1999: SKIN. CRACKED. PDX - LEFT NACELLE LOWER INBOARD FORWARD CORNER CUTOUT IS CRACKED. REPAIRED IAW DHC-8 RD 8-54-724. - [SDR QXEA9901598](https://openairdocs.org/sdr/QXEA9901598), Jul 14, 1999: SEAT TRACK. GOUGED. PDX - RIGHT OUTBOARD SEAT TRACK AT X346 HAS A GOUGE. REPAIRED IAW DHC8 SRM 51-20-16. - [SDR QXEA9901595](https://openairdocs.org/sdr/QXEA9901595), Jul 14, 1999: SEAT TRACK. CORRODED. PDX - RIGHT OUTBOARD SEAT TRACK HAS PITS IN THE HAT CHANNEL AT X406. REPAIRED IAW DHC8 SRM 51-20-16. - [SDR QXEA9901593](https://openairdocs.org/sdr/QXEA9901593), Jul 14, 1999: SPAR. SCRATCHED. PDX - THERE IS A 3.5 INCH SCRATCH IN REAR SPAR AT YW RIGHT. REPAIRED IAW DHC8 SRM 51-20-11. - [SDR QXEA9901587](https://openairdocs.org/sdr/QXEA9901587), Jul 14, 1999: PANEL. CHAFED. PDX - FUEL PANEL 524CT IS CHAFED AT INBOARD EDGE. REPAIRED IAW RD 8-57-320. - [SDR QXEA9901579](https://openairdocs.org/sdr/QXEA9901579), Jul 14, 1999: PLATE. CORRODED. PDX - FRETTING CORROSION AT BOTH ENDS OF LADDER PLATE 624AT. REPAIRED IAW RD 8-57-611 AND DHC8 SRM 51-20-16. - [SDR QXEA9901578](https://openairdocs.org/sdr/QXEA9901578), Jul 14, 1999: PLATE. CORRODED. PDX - FRETTING CORROSION AT BOTH ENDS OF LADDER PLATE 624BT. REPAIRED IAW RD 8-57-633. - [SDR QXEA9901581](https://openairdocs.org/sdr/QXEA9901581), Jul 12, 1999: SKIN. CHAFED. PDX - RIGHT OUTBOARD FLAP HAS A SMALL CHAFED AREA ON OUTBOARD END OF TOP SURFACE. REPAIRED IAW 57-20-11. - [SDR QXEA9802101](https://openairdocs.org/sdr/QXEA9802101), Dec 12, 1998: WIRE. BROKEN. SEA - FOUND BROKEN WIRE ON NR 2 SMOKE DETECTOR CANNON PLUG. MAINTENANCE SOLDERED WIRE TO CANNON PLUG. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO P - [SDR QXEA9801548](https://openairdocs.org/sdr/QXEA9801548), Nov 1, 1998: BATTERY. DISCHARGED. COCKPIT EMERGENCY FLASHLIGHT IS NOT BLINKING. REPLACED BATTERY IN FLASHLIGHT, OPERATIONAL CHECKS GOOD. - [SDR QXEA9801680](https://openairdocs.org/sdr/QXEA9801680), Oct 24, 1998: WHEEL. CRACKED. NR 4 MAIN WHEEL BROKEN. THE OUTER RIM FAILED AT THE BEAD SEAT. THE CRACK RUNS APPROXIMATELY HALF OF THE WAY AROUND THE BEAD SEAT AREA. REPLACED THE NR 4 WHEEL A - [SDR QXEA9801380](https://openairdocs.org/sdr/QXEA9801380), Oct 3, 1998: ACTUATOR. MALFUNCTION. LEFT MAIN GEAR DOOR HANGS OPEN ABOUT 2 INCHES DURING FLIGHT. FERRIED AIRCRAFT FROM SEA TO PDX FOR REPAIRS. IN PDX REPLACED UPLOCK ACTUATOR, OPERATIONAL CHECK GO - [SDR QXEA9801447](https://openairdocs.org/sdr/QXEA9801447), Sep 7, 1998: ENGINE. MALFUNCTION. NR 1 ENGINE INDICATED OIL PRESSURE WAS BELOW 40 PSI. PERFORMED INFLIGHT SHUTDOWN OF NR 1 ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENG - [SDR QXEA9801274](https://openairdocs.org/sdr/QXEA9801274), Sep 7, 1998: ENGINE. FAILED. BOI- NR 1 ENGINE INDICATED OIL PRESSURE WAS BELOW 40 PSI. PERFORMED INFLIGHT SHUTDOWN OF NR 1 ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR - [SDR QXEA9800831](https://openairdocs.org/sdr/QXEA9800831), Jun 26, 1998: LIGHT. BROKEN. THRESHOLD EXIT SIGN BROKEN AT THE RIGHT UNDERWING EXIT DOOR. INSTALLED NEW SIGN AT THE RIGHT UNDERWING EXIT, OPERATIONAL CHECKS GOOD. - [SDR QXEA9800231](https://openairdocs.org/sdr/QXEA9800231), Feb 12, 1998: BRACKET. CHAFED. NACELLE AFT WALL GRAVEL GUARD MOUNT BRACKETS CHAFED. REPAIRED IAW HORIZON EA 9-54-154. - [SDR QXEA9800230](https://openairdocs.org/sdr/QXEA9800230), Feb 9, 1998: BRACKET. CHAFED. FIVE BRACKETS THAT RETAIN LEFT HAND MAIN LANDING GEAR GRAVEL GUARD ARE SEVERLY CHAFED. INSTALLED BRACKETS IAW DHC-8 SRM 51-40-00. INSTALLED CAM LOC RECEPTICALS - [SDR QXEA9700715](https://openairdocs.org/sdr/QXEA9700715), Oct 31, 1997: CONTROL VALVE. MALFUNCTION. PDX - NR 1 MAIN BRAKE IS INEFFECTIVE. REPLACED NR 1 DUAL SKID CONTROL VALVE, OPERATIONAL CHECK GOOD. - [SDR QXEA9700634](https://openairdocs.org/sdr/QXEA9700634), Oct 5, 1997: SMOKE DETECTOR. NO TEST. PDX - NUMBER 2 SMOKE DETECTOR WILL NOT TEST. PLACED ON MEL. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9700581](https://openairdocs.org/sdr/QXEA9700581), Sep 20, 1997: BULB. FAILED. PDX- FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH INOP. RELAMPED, OPERATION CHECK GOOD. - [SDR QXEA9700563](https://openairdocs.org/sdr/QXEA9700563), Sep 12, 1997: LAMP. FAILED. SEA- BAGGAGE SMOKE DETECTOR WILL NOT TEST IN POSITION NR 1. RELAMPED INTERNAL SMOKE DETECTOR LIGHT, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700319](https://openairdocs.org/sdr/QXEA9700319), Jul 8, 1997: BATTERY PACK. DISCHARGED. SEA- TWO FORWARD RED EGRESS LIGHTS ARE INOP. REPLACED BATTERY PACK AT 1ED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9700163](https://openairdocs.org/sdr/QXEA9700163), May 2, 1997: BATTERY. DISCHARGED. COCKPIT EMERGENCY FLASHLIGHT HAS A LOW BATTERY. REPLACED BATTERY PACK FOR FLASHLIGHT, OPERATIONAL CHECKS NORMAL. - [SDR QXEA9800229](https://openairdocs.org/sdr/QXEA9800229), Feb 7, 1997: BRACKET. FRETTING. FRETTING CORROSION IN NACELLE WHERE MAIN LANDING GEAR ACTUATOR BRACKET ATTACHES TO NACELLE. REPAIRED IAW HORIZON EA 9-54-155. - [SDR QXEA9600131](https://openairdocs.org/sdr/QXEA9600131), Mar 23, 1996: LIGHT. INOPERATIVE. COCKPIT OVERHEAD EMERGENCY LIGHT IS INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9500247](https://openairdocs.org/sdr/QXEA9500247), Aug 11, 1995: DETECTOR. MALFUNCTIONED. PDX - NR 1 CARGO SMOKE WARNING LIGHT INTERMITTENTLY ILLUMINATES. VERIFIED THAT THERE WAS NO SMOKE IN CARGO COMPARTMENT. NR 1 SMOKE DETECTOR WAS REPLACED AND TES - [SDR QXEA9500129](https://openairdocs.org/sdr/QXEA9500129), Apr 29, 1995: LAMP. FAILED. MFR - DURING PREFLIGHT TEST, FOUND NR 1 SMOKE DETECTOR INOP. PLACED ON MEL AND CONTINUED TO PDX. AT PDX FOUND REFERENCE LAMP BURNED OUT, REPLACED BOTH LAMPS, TE - [SDR QXEA9500041](https://openairdocs.org/sdr/QXEA9500041), Feb 9, 1995: EEL SIGN. BROKEN. SEA - EXIT SIGN AT 4A BROKEN. REPLACED SIGN AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9500015](https://openairdocs.org/sdr/QXEA9500015), Jan 15, 1995: PSEU. DEFECTIVE. PDX - THE LANDING GEAR INOP CAUTION LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED PSEU IAW, DEHAVILLAND -8 M.M. 32-61-50, PG. 201. OPERATIONALLY CHECKED GOOD. A --- 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.