# N823PH: Dehavilland DHC-8-102, registration cancelled 2000-04-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 21, 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: 110 - Type of aircraft: Fixed wing multi engine - Certificate issued: April 12, 2000 - Last registry action: April 12, 2000 - Mode S code: AB3D4D - 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/N823PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=823PH - Page: https://openairdocs.org/deregistered/N823PH-2000-04-21 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 (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR QXEA000038](https://openairdocs.org/sdr/QXEA000038), Jan 10, 2000: STOP. DIRTY. PDX - MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED MAIN CABIN DOOR STOP PADS. OPENED AND CLOSED DOOR NUMEROUS TIMES. DOOR OPERATIONS CHECK GOOD. AIRCRAFT RETURNED - [SDR QXEA9900451](https://openairdocs.org/sdr/QXEA9900451), Mar 5, 1999: SKIN. DENTED. PDX - THERE IS A DENT APPROXIMATELY 3 INCH DIAMETER IN THE FUSELAGE SKIN, UNDER THE RIGHT-HAND ICE SHIELD. REPAIRED IAW -8 MM 20-16-11. - [SDR QXEA9900450](https://openairdocs.org/sdr/QXEA9900450), Mar 5, 1999: SKIN. CORRODED. PDX - THERE IS LIGHT FRETTING CORROSION IN THE FUSELAGE SKIN AROUND SEVEN SCREW HOLES UNDER THE RIGHT-HAND ICE SHIELD. REPAIRED IAW -8 MM 20-13-11, PAGE 3. - [SDR QXEA9900443](https://openairdocs.org/sdr/QXEA9900443), Mar 5, 1999: SKIN. DENTED. PDX - DENT IN FUSELAGE SKIN JUST AFT OF LEFT-HAND ICE SHIELD AT STATION 312.350 AND STRINGER 12. REPAIRED IAW HORIZON AIR EA 9-53-442B. - [SDR QXEA9900427](https://openairdocs.org/sdr/QXEA9900427), Mar 3, 1999: TRACK. CORRODED. PDX - NR 3 RIGHT-HAND FLAP TRACK HAS LIGHT TO MODERATE SURFACE PITTING ON LOWER TRACK TOP SURFACE IN ROLLER PATH AND UPPER TRACK BOTTOM SURFACE IN ROLLER PATH. - [SDR QXEA9900456](https://openairdocs.org/sdr/QXEA9900456), Mar 2, 1999: SKIN. CORRODED. PDX - CORROSION ON BELLY SKIN AROUND TCAS ANTENNA DOUBLER RIVETS. REPAIRED IAW SRM 51-40-11. - [SDR QXEA9900440](https://openairdocs.org/sdr/QXEA9900440), Mar 2, 1999: FRAME. DAMAGED. PDX - CHAFE DAMAGE ON RIGHT-HAND CARGO PIT FRAME AT STATION 618 BETWEEN STRINGER 20 TO 22. REPAIRED IAW HORIZON AIR EA 9-53-443. - [SDR QXEA9900433](https://openairdocs.org/sdr/QXEA9900433), Mar 2, 1999: LINK. WORN. PDX - EXCESSIVE AXIAL PLAY ON INBOARD SIDE OF LINK ASSEMBLY. REPAIRED IAW HORIZON AIR EA 9-54-192. - [SDR QXEA9900438](https://openairdocs.org/sdr/QXEA9900438), Feb 28, 1999: FRAME. WORN. PDX - FRAME 646 AT STRINGER 18 HAS 2 WEAR MARKS FROM GILE LINER SUPPORT BRACKET. REPAIRED IAW SRM 53-20-21, FIGURE 6. - [SDR QXEA9900437](https://openairdocs.org/sdr/QXEA9900437), Feb 28, 1999: FRAME. DAMAGED. PDX - FRAME 618 AT STRINGER 18 HAS 2 WEAR MARKS FROM GILE LINER SUPPORT BRACKET. REPAIRED IAW SRM 51-20-11 AND 51-20-16. - [SDR QXEA9900442](https://openairdocs.org/sdr/QXEA9900442), Feb 27, 1999: SILL. DAMAGED. PDX - BAGGAGE DOOR CUTOUT UPPER SILL INNER STRAPS HAVE CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 9-53-440. - [SDR QXEA9900430](https://openairdocs.org/sdr/QXEA9900430), Feb 27, 1999: PLATE. CORRODED. PDX - LADDER PLATE UNDER PANEL 521AT HAS FRETTING CORROSION. REPAIRED IAW RD 8-57-592. - [SDR QXEA9900445](https://openairdocs.org/sdr/QXEA9900445), Feb 25, 1999: ANGLE. CRACKED. PDX - RIGHT-HAND AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-40-11. - [SDR QXEA9900444](https://openairdocs.org/sdr/QXEA9900444), Feb 25, 1999: ANGLE. CRACKED. PDX - LEFT-HAND AFT REAR WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-40-11. - [SDR QXEA9900441](https://openairdocs.org/sdr/QXEA9900441), Feb 25, 1999: FRAME. DENTED. PDX - RIGHT-HAND CARGO PIT FRAME IS DENTED AT STATION 580.5 AND STRINGER 22. REPAIRED IAW HORIZON AIR EA 9-53-437. - [SDR QXEA9900439](https://openairdocs.org/sdr/QXEA9900439), Feb 24, 1999: SILL. CRACKED. PDX - PILOT SIDE WINDOW LOWER SILL JOINT TO SIDE POST HAS A 1 INCH CRACK. REPAIRED IAW RD 8-53-576. - [SDR QXEA9900446](https://openairdocs.org/sdr/QXEA9900446), Feb 23, 1999: ANGLE. CRACKED. PDX - RIGHT-HAND FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-41-11. - [SDR QXEA9900453](https://openairdocs.org/sdr/QXEA9900453), Feb 22, 1999: CLIP. CORRODED. PDX - FRAME CLIP CORRODED AT STRINGER 31R AND STATION 510. REPAIRED IAW SRM 53-00-16. - [SDR QXEA9900447](https://openairdocs.org/sdr/QXEA9900447), Feb 22, 1999: ANGLE. CRACKED. PDX - LEFT-HAND FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-40-11. - [SDR QXEA9900455](https://openairdocs.org/sdr/QXEA9900455), Feb 21, 1999: CLIP. CORRODED. PDX - FRAME CLIP CORRODED AT STRINGER 32R AND STATION 545. REPAIRED IAW SRM 53-00-16, PARAGRAPH 1, TABLE 1. - [SDR QXEA9900454](https://openairdocs.org/sdr/QXEA9900454), Feb 21, 1999: CLIP. CORRODED. PDX - FRAME CLIP CORRODED AT STRINGER 31R AND STATION 545. REPAIRED IAW SRM 53-00-16, PARAGRAPH 1, TABLE 1. - [SDR QXEA9900452](https://openairdocs.org/sdr/QXEA9900452), Feb 21, 1999: CLIP. CRACKED. PDX - FRAME CLIP CRACKED AT STRINGER 31R AND STATION 222.7. REPAIRED IAW SRM 53-20-21, PAGE 1. - [SDR QXEA9900448](https://openairdocs.org/sdr/QXEA9900448), Feb 21, 1999: SILL. CORRODED. PDX - SLIGHT CORROSION ON TOP SURFACE OF LOWER SILL AT RIGHT-HAND CENTER EMERGENCY EXIT AT AFT INBOARD NUT PLATE. REPAIRED IAW SRM 51-00-04. - [SDR QXEA9900435](https://openairdocs.org/sdr/QXEA9900435), Feb 19, 1999: CASTELLATION. CRACKED. PDX - FRAME 4 HAS CRACKED CASTELLATION AT STRINGER 12S. REPAIRED IAW SRM 53-20-21. - [SDR QXEA9900434](https://openairdocs.org/sdr/QXEA9900434), Feb 19, 1999: CASTELLATION. CRACKED. PDX - FRAME 4 HAS CRACKED CASTELLATION AT STRINGER 12P. REPAIRED IAW SRM 53-20-21. - [SDR QXEA9900457](https://openairdocs.org/sdr/QXEA9900457), Feb 16, 1999: WALL. CRACKED. PDX - LEFT-HAND WALL OF NOSE GEAR WHEEL WELL IS CRACKED THROUGH A PREVIOUS REPAIR AT STATION 57. REPAIRED IAW RD 8-53-675. - [SDR QXEA9900449](https://openairdocs.org/sdr/QXEA9900449), Feb 15, 1999: SEAT TRACK. DAMAGED. PDX - PILOTS SEAT TRACKS HAVE LOOSE OR MISSING REPAIR BUSHINGS. REPLACED BUSHINGS IAW RD 8-53-219. - [SDR QXEA9900436](https://openairdocs.org/sdr/QXEA9900436), Feb 15, 1999: FITTING. CORRODED. PDX - LEFT-HAND NACELLE HAS MINOR FRETTING CORROSION UNDER MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING. REPAIRED IAW RD 8-54-735. - [SDR QXEA9900098](https://openairdocs.org/sdr/QXEA9900098), Jan 19, 1999: LIGHT. INOP. CREW EMERGENCY ESCAPE LIGHT INOP. MAINTENANCE REPLACED THE EMERGENCY ESCAPE LIGHT, OPERATIONAL CHECKS GOOD. - [SDR QXEA9802107](https://openairdocs.org/sdr/QXEA9802107), Dec 18, 1998: BATTERY. DISCHARGED. EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS, OPERATIONAL CHECK GOOD. - [SDR QXEA9800832](https://openairdocs.org/sdr/QXEA9800832), Jun 30, 1998: PWR SUPPLY. MALFUNCTION. PDX- FORWARD EMERGENCY TRACK LIGHTING OUT. REPLACED EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9800234](https://openairdocs.org/sdr/QXEA9800234), Mar 3, 1998: FAN. FAILED. ELECTRIC SMELL NOTED IN THE COCKPIT DURING EN ROUTE AND LANDING PHASE OF FLIGHT. ALL ELECTRICAL LOADS APPEAR TO BE NORMAL, WITH NO POPPED CIRCUIT BREAKERS. INSP - [SDR QXEA9800012](https://openairdocs.org/sdr/QXEA9800012), Jan 6, 1998: SWITCH. INOPERATIVE. PDX - FLIGHT ATTENDANT EMERGENCY LIGHTING SWITCH NORM LIGHT INOP. REPLACED SWITCH, OPERATIONAL CHECK GOOD. - [SDR QXEA9800001](https://openairdocs.org/sdr/QXEA9800001), Jan 1, 1998: BULB. FAILED. BOI- SMOKE DETECTOR WARNING LIGHT DOES NOT TEST IN THE NR 1 POSITION. RELAMPED SMOKE DETECTOR, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700687](https://openairdocs.org/sdr/QXEA9700687), Oct 22, 1997: CONNECTOR. LOOSE. SEA - FAULT B LIGHT ON RIGHT ENGINE FIRE PANEL WILL NOT LIGHT UP WHEN TESTED. WILL LIGHT UP DURING ADVISORY LIGHT TEST. RESEATED CAUTION ADVISORY TEST BOX. FAUL - [SDR QXEA9700406](https://openairdocs.org/sdr/QXEA9700406), Aug 1, 1997: BATTERY. DISCHARGED. MAIN CABIN DOOR OVERHEAD EXIT LIGHT AND FORWARD EMERGENCY EXIT LIGHT ON LEFT SIDE ARE INOP. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECKS GOOD. - [SDR QXEA9500036](https://openairdocs.org/sdr/QXEA9500036), Feb 5, 1995: EEL POWER SUPPLY. FAILED. PDX - THE TWO FORWARD EMERGENCY LIGHTS IN THE STRIP LIGHTING ARE INOP. REPLACED BATTERY POWER SUPPLY AT SEAT 1DE AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED T ## 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 19920626030369I](https://openairdocs.org/incident/19920626030369I), Jun 26, 1992: Dhav DHC8102 (N823PH), Portland, OR. Ground spoilers extended in flight. Landed safely at destination. Right side ground spoilers actuators replaced. - [Incident 19910911058159I](https://openairdocs.org/incident/19910911058159I), Sep 11, 1991: Dhav DHC8102 (N823PH), Portland, OR. Rudder would not move on preflight. Engines shut down. Mechanic left screwdriver in the rudder pedal quadrant. --- 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.