# N822PH: Dehavilland DHC-8-102, registration cancelled 2001-12-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 4, 2001
- Exported to: Antigua and Barbuda
- 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: 106
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 23, 1988
- Certificate issued: November 30, 2001
- Last registry action: November 30, 2001
- Mode S code: AB3996
- Owner when cancelled: [Jetfleet III](https://openairdocs.org/faa-owner/JETFLEET%20III)
- Location: [Burlingame, CA](https://openairdocs.org/faa-place/CA/Burlingame)
- Owner type: Corporation
- Owner's area on the map: 37.5719° N, 122.3751° W: Placed by OpenAirDocs at the center of ZIP code 94010, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N822PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=822PH
- Page: https://openairdocs.org/deregistered/N822PH-2001-12-04

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 (90, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR QXEA0100227](https://openairdocs.org/sdr/QXEA0100227), Mar 6, 2001: BEARING. FAILED. PDX - ON APPROACH TO PDX AN INCREASING ITT ON NR 2 ENGINE NOTED ALONG WITH VIBRATION. AFTER GEAR AND FLAP EXTENSION SMOKE SMELL NOTED. DECLARED AN EMERGENCY. AF
- [SDR QXEA0100014](https://openairdocs.org/sdr/QXEA0100014), Jan 9, 2001: LIGHT. INOPERATIVE. PDX - FLIGHT COMPARTMENT OVERHEAD EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED OVERHEAD EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE
- [SDR QXEA0003050](https://openairdocs.org/sdr/QXEA0003050), Nov 17, 2000: ROD. LACK OF LUBE. SEA- MAIN CABIN DOOR SOMETIMES JAMS WHEN OPEN. LEVER AT ABOUT HALFWAY POSITION. LUBED MAIN CABIN DOOR OVERCENTER RODS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNE
- [SDR QXEA0002725](https://openairdocs.org/sdr/QXEA0002725), Sep 27, 2000: SIGN. INOPERATIVE. PDX- LOWER EMERGENCY EXIT SIGN IN SEAT 4A IS MISSING COVER. REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002486](https://openairdocs.org/sdr/QXEA0002486), Aug 28, 2000: STRAP. OUT OF ADJ. YKM- MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND TEFLON STRIP UNDER DOOR HINGE IMPINGING ON DOOR. ADJUSTED TEFLON STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED
- [SDR QXEA0002347](https://openairdocs.org/sdr/QXEA0002347), Aug 22, 2000: SKIN. LIGHTNING STRIKE. YXX- LIGHTNING STRIKES ON AIRCRAFT SKIN. REPAIRED IAW DHC-8 SRM 5-50-31.
- [SDR QXEA0002338](https://openairdocs.org/sdr/QXEA0002338), Aug 21, 2000: STIFFENER. CRACKED. YXX- CRACKS AT UPPER END OF VERTICAL STIFFENERS, 4 INCHES OUTBOARD OF CENTER LINE OF AIRCRAFT LEFT AND RIGHT ON BULKHEAD AT FUSELAGE STATION X66.00. REPAIRED IA
- [SDR QXEA0002357](https://openairdocs.org/sdr/QXEA0002357), Aug 20, 2000: FIREWALL. DAMAGED. YXX- LEFT HAND NACELLE FORWARD FIREWALL INBOARD LOWER AREA HAS TWO RIVETS WITH HEADS CHAFED OFF AND AREA OF CHAFING JUST ABOVE XM107-80 AND ZM1.5-00. REPAIRED I
- [SDR QXEA0002328](https://openairdocs.org/sdr/QXEA0002328), Aug 20, 2000: SHIELD. CRACKED. YXX- CARGO DOOR SHIELD AT CEILING IS CRACKED IN SEVERAL LOCATIONS. REPAIRED IAW DHC-8 SRM 51-70-00 PAGE 401.
- [SDR QXEA0002374](https://openairdocs.org/sdr/QXEA0002374), Aug 18, 2000: SKIN. GOUGED. YXX- MAIN CABIN DOOR OUTER SHELL HAS A GOUGE ON SEALING SURFACE OF DOOR SHELL AT LOWER FORWARD CORNER. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA0002368](https://openairdocs.org/sdr/QXEA0002368), Aug 18, 2000: DRAG STRUT. CHAFED. YXX- LEFT HAND MAIN LANDING GEAR DRAG STRUT FOUND WITH CHAFE MARKS. REPAIRED IAW DHC-8 RD 8-32-474, HORIZON AIR EA 9-32-102 AND CONAIR EO 2869.
- [SDR QXEA0002366](https://openairdocs.org/sdr/QXEA0002366), Aug 18, 2000: STRUCTURE. LOOSE. YXX- RIGHT HAND NACELLE TO REAR SPAR INBOARD AND OUTBOARD END OF LINK HAS LOOSE HARDWARE. REPLACED WORN HARDWARE AS PER DHC-8 100 MM.
- [SDR QXEA0002363](https://openairdocs.org/sdr/QXEA0002363), Aug 18, 2000: SKIN. GOUGED. YXX- GOUGE ON LOWER WING SKIN AT FORWARD END OF LEFT HAND NR 5 FLAP TRACK, LYW373. REPAIRED IAW DHC-8 SRM 57-10-16, 51-00-06, 51-20-16 PAGE 1-4 AND 51-20-36 PAG
- [SDR QXEA0002358](https://openairdocs.org/sdr/QXEA0002358), Aug 18, 2000: STRUCTURE. LOOSE. YXX- LEFT HAND NACELLE TO REAR SPAR INBOARD AND OUTBOARD END OF LINK HAS LOOSE HARDWARE. REPLACED WORN HARDWARE PER DHC-8 MM.
- [SDR QXEA0002356](https://openairdocs.org/sdr/QXEA0002356), Aug 18, 2000: FIREWALL. CHAFED. YXX- CHAFE DAMAGE ON NR 2 FORWARD OUTBOARD FIREWALL WEB AT STATION YN107.18 AND ZN-10.50. REPAIRED IAW DHC-8 RD 8-54-1330, 8-54-081, AND SRM 51-00-06.
- [SDR QXEA0002350](https://openairdocs.org/sdr/QXEA0002350), Aug 18, 2000: MOUNT. CHAFED. YXX- LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR MOUNT SURFACE ON NACELLE FRAME CHAFED. BLENDED AREA.
- [SDR QXEA0002329](https://openairdocs.org/sdr/QXEA0002329), Aug 18, 2000: SKIN. DENTED. YXX- LEFT HAND FUSELAGE HAS A DENT BETWEEN STRINGER 19 AND 20 FORWARD OF FRAME X405.737. REPAIRED IAW DHC-8 RD 8-53-457 AND DHC-8 SRM 51-00-05, 53-00-16.
- [SDR QXEA0002324](https://openairdocs.org/sdr/QXEA0002324), Aug 18, 2000: DOOR FRAME. GOUGED. YXX- CARGO DOOR CUTOUT UPPER WEB IS GOUGED BESIDE DOOR STOPS AT FUSELAGE STATION X564.5X AND X580.5. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 7 AND HORIZON AIR EA 9
- [SDR QXEA0002349](https://openairdocs.org/sdr/QXEA0002349), Aug 17, 2000: SKIN. DENTED. YXX- DENT IN UPPER RIGHT HAND SIDE OF FORWARD RUDDER 4 INCHES FORWARD OF AFT SPAR AT UPPER HINGE LINE. REPAIRED IAW DHC-8 SRM 55-40-16, 55-40-28, AND 51-00-06.
- [SDR QXEA0002364](https://openairdocs.org/sdr/QXEA0002364), Aug 16, 2000: PLATE. CRACKED. YXX- RIGHT HAND LADDER PLATE HAS A CRACK FROM DEUTCH NUT HOLE. REPAIRED IAW DHC-8 RD 8-57-876.
- [SDR QXEA0002352](https://openairdocs.org/sdr/QXEA0002352), Aug 16, 2000: FIREWALL. CRACKED. YXX- LEFT HAND NACELLE FIREWALL EXTENSION TUBE IS CRACKED AT WELD AND BOLT HOLES. REPAIRED IAW DHC-8 RD 8-54-16, AND 8-54-8.
- [SDR QXEA0002351](https://openairdocs.org/sdr/QXEA0002351), Aug 16, 2000: MOUNT. CHAFED. YXX- RIGHT HAND MAIN LANDING GEAR RETRACT ACTUATOR MOUNT SURFACE ON NACELLE FRAME CHAFED. REPAIRED IAW DHC-8 RD 8-54-523 AND SRM 51-00-06.
- [SDR QXEA0002372](https://openairdocs.org/sdr/QXEA0002372), Aug 15, 2000: SKIN. LIGHTNING STRIKE. YXX- MAIN CABIN DOOR OUTER SHELL EXTERIOR SKIN HAS LIGHTNING STRIKES. REPARIED IAW DHC-8 SRM 51-20-11, 52-00-16, 51-00-05 AND 20-34-11 PAGE 17.
- [SDR QXEA0002371](https://openairdocs.org/sdr/QXEA0002371), Aug 15, 2000: SKIN. LIGHTNING STRIKE. YXX- RIGHT HAND EMERGENCY EXIT DOOR HAS LIGHTNING STRIKES. REPAIRED IAW DHC-8 SRM 51-20-11, 52-00-16, 51-00-05 AND 51-20-00 PAGE 5.
- [SDR QXEA0002359](https://openairdocs.org/sdr/QXEA0002359), Aug 15, 2000: SKIN. DAMAGED. YXX- LEFT HAND WING TIP LEADING EDGE ERRODED. REPAIRED IAW DHC-8 RD 8-57-071.
- [SDR QXEA0002348](https://openairdocs.org/sdr/QXEA0002348), Aug 15, 2000: ANTENNA. DAMAGED. YXX- DAMAGE ON LEFT HAND VOR ANTENNA AND FORWARD MOUNT ON VERTICAL FIN RIB 9 AND X848. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-55-955.
- [SDR QXEA0002342](https://openairdocs.org/sdr/QXEA0002342), Aug 15, 2000: SKIN. DENTED. YXX- DENT AT FUSELAGE STATION X282.400 BETWEEN STRINGER 10 AND 11 JUST FORWARD OF ICE SHIELD. REPAIRED IAW DHC-8 SRM 53-00-16, 51-00-06 AND 51-00-05.
- [SDR QXEA0002369](https://openairdocs.org/sdr/QXEA0002369), Aug 12, 2000: SKIN. DENTED. YXX- AIRSTAIR DOOR OUTER SKIN HAS MANY DENTS AND SCRATCHES. REPAIRED IAW DHC-8 SRM 51-20-26 PAGE 6, 51-20-11, 52-00-16 AND 51-00-06.
- [SDR QXEA0002367](https://openairdocs.org/sdr/QXEA0002367), Aug 12, 2000: SKIN. CHAFED. YXX- RIGHT HAND UPPER WING SKIN AFT OF NR 2 ENGINE HAS CHAFE DAMAGE FROM PANEL 422ET. REPAIRED IAW DHC-8 SRM 57-10-16, 51-00-06 AND 51-20-00.
- [SDR QXEA0002362](https://openairdocs.org/sdr/QXEA0002362), Aug 12, 2000: SKIN. GOUGED. YXX- LEFT HAND UPPER WING SKIN AFT OF NR 1 ENGINE NACELLE HAS A GOUGE FROM PANEL 412ET. REPAIRED IAW DHC-8 SRM 57-10-16, 51-20-11 AND 51-20-00 PAGE 5.
- [SDR QXEA0002361](https://openairdocs.org/sdr/QXEA0002361), Aug 12, 2000: SKIN. GOUGED. YXX- LEFT HAND WING CENTER SECTION OF UPPER SKIN AT YW70.00 HAS GOUGE. REPAIRED IAW DHC-8 SRM 51-20-11, 57-10-16 PAGE 2 AND 51-20-00 PAGE 5.
- [SDR QXEA0002360](https://openairdocs.org/sdr/QXEA0002360), Aug 12, 2000: SKIN. GOUGED. YXX- THREE GOUGES ON LEFT HAND UPPER WING SKIN BETWEEN YW139.000 AND YW171.000. REPAIRED IAW DHC-8 SRM 51-20-11, AND 57-10-16 PAGE 2.
- [SDR QXEA0002355](https://openairdocs.org/sdr/QXEA0002355), Aug 12, 2000: STRUCTURE. CRACKED. YXX- RIGHT HAND NACELLE FOUND TO HAVE TWO CRACKS ABOVE ACCESS HOLES FOR MAIN LANDING GEAR RETRACT ACTUATOR ATTACH HARDWARE. REPAIRED IAW DHC-8 RD 8-54-109 PAGE 
- [SDR QXEA0002353](https://openairdocs.org/sdr/QXEA0002353), Aug 12, 2000: STRUCTURE. CRACKED. YXX- CRACKED STRUCTURE ON NR 2 NACELLE BETWEEN MID DOOR''S FORWARD HINGE AND FORWARD BRACKET OF EXTENSION HANDLE. REPAIRED IAW DHC-8 RD 8-54-239 AND SRM 51-40-1
- [SDR QXEA0002337](https://openairdocs.org/sdr/QXEA0002337), Aug 12, 2000: SKIN. DENTED. YXX- LEFT HAND FUSELAGE HAS A DENT JUST AFT OF STATION X636.00 BETWEEN STRINGER 16 AND 15. REPAIRED IAW DHC-8 SRM 53-00-16, 51-00-06, 51-00-05, RD 8-53-5230 AND
- [SDR QXEA0002336](https://openairdocs.org/sdr/QXEA0002336), Aug 12, 2000: SKIN. DENTED. YXX- LEFT HAND FUSELAGE JUST FORWARD OF MAIN CABIN DOOR THERE IS A DENT FORWARD OF STATION X545.00 BETWEEN STRINGER 22 AND 23. REPAIRED IAW DHC-8 SRM 51-20-26, 
- [SDR QXEA0002373](https://openairdocs.org/sdr/QXEA0002373), Aug 11, 2000: SKIN. CHAFED. YXX- MAIN CABIN DOOR OUTER SHELL HAS CHAFE DAMAGE ON INTERIOR LIP, 18 INCHES FROM DOOR CABLE ATTACH POINT. REPAIRED IAW DHC-8 SRM 52-00-16 AND 51-20-16 PAGE 1-5
- [SDR QXEA0002354](https://openairdocs.org/sdr/QXEA0002354), Aug 11, 2000: FIREWALL. CRACKED. YXX- RIGHT HAND NACELLE FIREWALL FOUND CRACKED ABOVE INBOARD END OF OIL COOLER. REPAIRED IAW DHC-8 SRM 51-40-11, 54-00-00 PAGE 1 AND 20-21-18.
- [SDR QXEA0002326](https://openairdocs.org/sdr/QXEA0002326), Aug 11, 2000: SKIN. DENTED. YXX- LEFT HAND FUSELAGE HAS DENTS BETWEEN 30 AND 31 AT STATION X151.600. REPAIRED IAW DHC-8 RD 8-53-5206, DHC-8 SRM 53-00-16 AND 51-00-05.
- [SDR QXEA0002325](https://openairdocs.org/sdr/QXEA0002325), Aug 11, 2000: SKIN. DENTED. YXX- RIGHT HAND FUSELAGE HAS DENT BETWEEN STRINGER 29 AND 30 AT STATION X182.00. REPAIRED IAW HORIZON AIR EA 9-53-561 AND DHC-8 SRM 51-00-05.
- [SDR QXEA0002312](https://openairdocs.org/sdr/QXEA0002312), Aug 11, 2000: THRESHOLD. CORRODED. YXX- SEVERAL AREAS OF PITTING AND SURFACE CORROSION ON THRESHOLD OF MAIN CABIN DOOR CUTOUT, AT FLOOR LEVEL BETWEEN FUSELAGE STATION 222.000AND X252.700. REPAIRE
- [SDR QXEA0002332](https://openairdocs.org/sdr/QXEA0002332), Aug 10, 2000: SKIN. DENTED. YXX- LEFT HAND FUSELAGE HAS DENT AND GOUGE BETWEEN STRINGER 17 AND 19 AT FRAME 151.600. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-11 AND 51-00-06.
- [SDR QXEA0002315](https://openairdocs.org/sdr/QXEA0002315), Aug 10, 2000: SEAT TRACK. CORRODED. YXX- LEFT HAND OUTBOARD FORWARD SEAT TRACK HAS PITTING CORROSION WHERE SEATS ATTACH TO TRACK. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11.
- [SDR QXEA0002370](https://openairdocs.org/sdr/QXEA0002370), Aug 9, 2000: STRUCTURE. CHAFED. YXX- RIGHT HAND EMERGENCY EXIT DOOR, BOTTOM AFT CORNER OF DOOR HAS CHAFE DAMAGE TO DOOR STRUCTURE AND RIVETS. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5, 51-40-11 P
- [SDR QXEA0002346](https://openairdocs.org/sdr/QXEA0002346), Aug 8, 2000: INTERCOSTAL. CORRODED. YXX- RIGHT HAND FORWARD OUTBOARD SEAT TRACK INTERCOSTAL TO FRAME X356, Z102 AND Y42 HAVE CORROSION. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-00 PAGE 5 AND 51-20-1
- [SDR QXEA0002343](https://openairdocs.org/sdr/QXEA0002343), Aug 4, 2000: FRAME. GOUGED. YXX- AFT FACE OF FRAME X240.50 BETWEEN STRINGER 19 AND 22 HAVE MINOR SCRATCHES AND GOUGES. REPAIRED IAW DHC-8 SRM 51-20-11, 53-00-16 AND 51-20-00.
- [SDR QXEA0002323](https://openairdocs.org/sdr/QXEA0002323), Aug 3, 2000: SKIN. CORRODED. YXX- CORROSION AROUND MARKER BEACON ANTENNA. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-11 AND 51-20-00.
- [SDR QXEA0002316](https://openairdocs.org/sdr/QXEA0002316), Aug 3, 2000: SEAT TRACK. CORRODED. YXX- LEFT HAND INBOARD FORWARD SEAT TRACK HAS EVIDENCE OF PITTING CORROSION AT SEAT ATTACH SPOTS. REPAIRED IAW DHC-8 AD 8-53-3074 AND 8-53-1339.
- [SDR QXEA0002365](https://openairdocs.org/sdr/QXEA0002365), Aug 2, 2000: SKIN. UNBONDED. YXX- RIGHT HAND AILERON TIP TRAILING EDGE IS DISBONDING. REPAIRED IAW DHC-8 SRM 57-60-63.
- [SDR QXEA0002345](https://openairdocs.org/sdr/QXEA0002345), Aug 2, 2000: SEAT TRACK. CORRODED. YXX- SURFACE CORROSION ON RIGHT HAND INBOARD SEAT TRACK AT CARGO HOLD DOWN ATTACH POINT X597.500 AND 9.250. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5 AND RD 8-53-4

All 90: https://openairdocs.org/deregistered/N822PH-2001-12-04/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA01FA059](https://openairdocs.org/ntsb/SEA01FA059), Mar 6, 2001: de Havilland DHC-8-102 (N822PH), Portland, OR, substantial damage. Probable cause: The failure of the number 5 engine bearing assembly followed by the disconnection of the P2.5/P3 switching valve to rear inlet case sealing air tube and the melting of the NL probe port (sealing…

## FAA accident and incident reports (4)

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 20010306005709I](https://openairdocs.org/incident/20010306005709I), Mar 6, 2001: Dhav DHC8102 (N822PH), Portland, OR, Substantial damage. (-23) A/c enroute from sea to pdx, crew noticed vibration on #2 engine and smell of smoke in cabin. Crew declared an emergency and landed at pdx. During…
- [Incident 19921004045669I](https://openairdocs.org/incident/19921004045669I), Oct 4, 1992: Dhav DHC8102 (N822PH), Seattle, WA. Smoke and sparks erupted from overhead passenger service unit. Feeder cable had failed at the bus bar.
- [Incident 19911220062499I](https://openairdocs.org/incident/19911220062499I), Dec 20, 1991: Dhav DHC8102 (N822PH), Medford, OR. W.o.w. light on descent. Had a ground spoiler deployment upon power reduction. W.o.w. sensors improperly adjusted.
- [Incident 19890105007039I](https://openairdocs.org/incident/19890105007039I), Jan 5, 1989: Dhav DHC8102 (N822PH), Medford, OR. NR1 engine oil pressure problem. Engine shut down. Returned to Medford. Landed without incident.

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