# N825PH: Boeing DHC-8-102, registration cancelled 2009-09-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 16, 2009
- Exported to: Kenya
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102) (registry code 1386002)
- 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: 213
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 5, 1990
- Certificate issued: July 22, 2005
- Last registry action: August 19, 2008
- Mode S code: AB44BB
- Owner when cancelled: [Wells Fargo Delaware Trust Co Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20DELAWARE%20TRUST%20CO%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N825PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=825PH
- Page: https://openairdocs.org/deregistered/N825PH-2009-09-16

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 Boeing DHC-8-102: https://openairdocs.org/model/boeing-dhc-8-102.md

## Service difficulty reports (93, newest 50)

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

- [SDR CBR2006F00003](https://openairdocs.org/sdr/CBR2006F00003), Apr 3, 2006: WARNING HORN. INTERMITTENT. ABORTED TAKEOFF, DURING TAKEOFF ROLL, TAKEOFF CONFIGURATION HORN CAME ON. FLAP CYCLED. SYSTEM FUNCTIONED SATISFACTORY, HORN NO LONGER EVIDENT ON TAKEOFF REF MM.
- [SDR QXEA0101304](https://openairdocs.org/sdr/QXEA0101304), Aug 2, 2001: STRUCTURE. DAMAGED. PDX - CARGO DOOR DAMAGED AT FORWARD STRUCTURE CABLE FEED-THROUGH BY CABLE CHAFING.REPAIRED IAW HORIZON AIR EA 9-52-122.
- [SDR QXEA0101305](https://openairdocs.org/sdr/QXEA0101305), Aug 2, 2001: STRUCTURE. DENTED. PDX - BAGGAGE DOOR INNER STRUCTURE DENTED WITH CRACK ON VERTICAL MEMBER ABOVE FORWARD COUNTERBALANCE ASSEMBLY. REPAIRED DAMAGE IAW E.A. 9-52-123.
- [SDR 1304](https://openairdocs.org/sdr/1304), Aug 2, 2001: STRUCTURE. DAMAGED. PDX - CARGO DOOR DAMAGED AT FORWARD STRUCTURE CABLE FEED-THROUGH BY CABLE CHAFING. REPAIRED IAW HORIZON AIR EA 9-52-122.
- [SDR QXEA011300](https://openairdocs.org/sdr/QXEA011300), Aug 1, 2001: INVERTER. DEFECTIVE. GEG-ELECTRICAL SMELL NOTICED IN FLIGHT. REMOVED AND REPLACED INVERTER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100015](https://openairdocs.org/sdr/QXEA0100015), Jan 10, 2001: CONTROLLER. WILL NOT TEST. LWS - AUTOFEATHER WILL NOT TEST. CYCLED POWER LEVERS AND CONDITION LEVERS FULL TRAVEL NUMEROUS TIMES. TEST NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVI
- [SDR QXEA0100002](https://openairdocs.org/sdr/QXEA0100002), Jan 2, 2001: POWER SUPPLY. INOPERATIVE. PDX - FOUND LEFT HAND SIDE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002509](https://openairdocs.org/sdr/QXEA0002509), Sep 18, 2000: ACM. MALFUNCTIONED. SEA- FLIGHT ATTENDANT REPORTED SMELL OF SMOKE ON SHORT AND FINAL APPROACH JUST AFTER BLEED AIR TURNED OFF FOR LANDING. REPLACED AIR CYCLE MACHINE. OPERATIONAL C
- [SDR QXEA0001425](https://openairdocs.org/sdr/QXEA0001425), May 31, 2000: SIGN. MALFUNCTIONED. PDX- FORWARD ENTRY DOOR LOWER EMERGENCY EGRESS EXIT SIGN BROKEN. REPLACED ENTRY DOOR LOWER EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED 
- [SDR QXEA0001126](https://openairdocs.org/sdr/QXEA0001126), Apr 19, 2000: INVERTER. MALFUNCTIONED. SEA- DURING FLIGHT AIRCRAFT COCKPIT/CABIN BEGAN TO SMELL OF SMOKE. AUXILIARY INVERTER MASTER CAUTION LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY CHECKLIST. AIRCR
- [SDR QXEA9902718](https://openairdocs.org/sdr/QXEA9902718), Dec 23, 1999: WEB. CORRODED. PDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN286.0. REPAIRED IAW DHC-8 SRM 51-40-4.
- [SDR QXEA9902701](https://openairdocs.org/sdr/QXEA9902701), Dec 23, 1999: SKIN. CRACKED. PDX - RIGHT NACELLE EXTERIOR OUTBOARD SKIN HAS .250 CRACK FROM RIVET HOLE TO SKIN PANEL EDGE AT STATION XN122.00 AND YW171.200, ALSO HAS LOOSE WORKING RIVET IN 
- [SDR QXEA9902699](https://openairdocs.org/sdr/QXEA9902699), Dec 23, 1999: WEB. CORRODED. PDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN280.00. REPAIRED IAW DHC-8 SRM 51-40-00 AND S
- [SDR QXEA9902674](https://openairdocs.org/sdr/QXEA9902674), Dec 23, 1999: SKIN. DENTED. PDX - 4 DENT ON OUTER SKIN AT STATION 507, WL100, BL40RH. REPAIRED IAW HORIZON AIR EA 9-53-531.
- [SDR QXEA9902696](https://openairdocs.org/sdr/QXEA9902696), Dec 21, 1999: GUARD. WORN. PDX - INBOARD MIDDLE GRAVEL GUARD ATTACH POINT WORN EXCESSIVELY THIN. REPAIRED IAW RD8-54-41.
- [SDR QXEA9902673](https://openairdocs.org/sdr/QXEA9902673), Dec 21, 1999: SKIN. CHAFED. PDX - CHAFE DAMAGE AT STATION 242.20 AND STRINGER 11S, ABOVE RIGHT FORWARD EXIT. IT IS APPROXIMATELY .035 DEEP. REPAIRED IAW HORIZON AIR EA 9-53-535.
- [SDR QXEA9902669](https://openairdocs.org/sdr/QXEA9902669), Dec 21, 1999: BRACKET. CORRODED. PDX - CORROSION IN ANGLE BRACKET AT FRAME X600.0 AND STRINGER 21S. REPAIRED IAW HORIZON AIR EA 9-53-536.
- [SDR QXEA9902663](https://openairdocs.org/sdr/QXEA9902663), Dec 21, 1999: STRINGER. GOUGED. PDX - SMALL GOUGE IN LEFT-HAND STRINGER 31 AT APPROXIMATELY STATION 550. REPAIRED IAW HORIZON AIR EA 9-53-532.
- [SDR QXEA9902652](https://openairdocs.org/sdr/QXEA9902652), Dec 21, 1999: FRAME. CORRODED. PDX - CORROSION ON UNDER SIDE OF HORIZONTAL STIFFENING RIB ON AFT FLANGE OF FRAME 253.400, BETWEEN STRINGERS 24 LT AND 25 LT. REPAIRED IAW HORIZON AIR EA 9-53-5
- [SDR QXEA9902700](https://openairdocs.org/sdr/QXEA9902700), Dec 19, 1999: SKIN. CRACKED. PDX - RIGHT NACELLE EXTERIOR INBOARD SKIN HAS 1.5 CRACK AT STATION XN127.5 AND YW139.200, JUST AFT OF PANEL 425AL TOP EDGE. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902698](https://openairdocs.org/sdr/QXEA9902698), Dec 19, 1999: WEB. PUNCTURED. PDX - AFT NACELLE TOP DECK HAS A PUNCTURE HOLE AT APPROXIMATELY STATION X236.00 AND YW139.900. REPAIRED IAW HORIZON AIR EA 9-54-237.
- [SDR QXEA9902697](https://openairdocs.org/sdr/QXEA9902697), Dec 19, 1999: STRINGER. DAMAGED. PDX - HOLE IN STRINGER XN176.5 AT STATION ZN17.04. REPAIRED IAW HORIZON AIR EA 9-54-238, FIGURE 2.
- [SDR QXEA9902694](https://openairdocs.org/sdr/QXEA9902694), Dec 19, 1999: STRINGER. CRACKED. PDX - EXHAUST DECK AFT LATERAL STRINGER HAS ONE CRACK. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-40-11.
- [SDR QXEA9902660](https://openairdocs.org/sdr/QXEA9902660), Dec 19, 1999: STRINGER. CORRODED. PDX - CORROSION INBOARD SIDE OF RIGHT-HAND STRINGER 32 AT FRAME STATION 488. INSTALLED NEW STRINGER SPLICE IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902683](https://openairdocs.org/sdr/QXEA9902683), Dec 18, 1999: SPLICE. CORRODED. PDX - CORROSION ON STRINGER SPLICE AT STATION 488.5 AND STRINGER 30RH. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902682](https://openairdocs.org/sdr/QXEA9902682), Dec 18, 1999: SPLICE. CORRODED. PDX - CORROSION ON STRINGER SPLICE AT STATION 488.5, STRINGER 29RH. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902651](https://openairdocs.org/sdr/QXEA9902651), Dec 18, 1999: FLOOR PANEL. CORRODED. PDX - MAIN ENTRY THRESHOLD WHERE FLOOR PANEL ATTACHES HAD NUMEROUS SPOTS OF CORROSION. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902692](https://openairdocs.org/sdr/QXEA9902692), Dec 17, 1999: ICE SHIELD. SCRATCHED. PDX - TWO DEEP SCRATCHES FOUND ABOVE RIGHT ICE SHIELD. REPAIRED IAW HORIZON AIR EA 9-53-530.
- [SDR QXEA9902691](https://openairdocs.org/sdr/QXEA9902691), Dec 17, 1999: THRESHOLD. CORRODED. PDX - MINOR SURFACE CORROSION AROUND NUT PLATES UNDER MAIN CABIN DOOR THRESHOLD. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 6, PARAGRAPH 2C.
- [SDR QXEA9902720](https://openairdocs.org/sdr/QXEA9902720), Dec 16, 1999: FITTING. CORRODED. PDX - RIGHT MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION ON H MEMBER MOUNTING PADS. REPAIRED IAW HORIZON AIR EA 9-54-233 AND EA 9-54-233
- [SDR QXEA9902719](https://openairdocs.org/sdr/QXEA9902719), Dec 16, 1999: FITTING. CORRODED. PDX - LEFT MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION ON H MEMBER. REPAIRED IAW HORIZON AIR EA 9-54-233 AND EA 9-54-233A.
- [SDR QXEA9902687](https://openairdocs.org/sdr/QXEA9902687), Dec 16, 1999: SEAT TRACK. CHAFED. PDX - RIGHT INBOARD SEAT TRACK CHAFFED AND LUG LIP WORN AT APPROXIMATELY STATION 282. REPAIRED IAW DHC-8 SRM 51-40-00.
- [SDR QXEA9902653](https://openairdocs.org/sdr/QXEA9902653), Dec 16, 1999: SPLICE. CORRODED. PDX - CORROSION ON STRINGER SPLICE AT STATION 531 AND STRINGER 30 RT. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-40-11 AND SRM 51-20-36.
- [SDR QXEA9902643](https://openairdocs.org/sdr/QXEA9902643), Dec 16, 1999: CLIP. CORRODED. PDX - CLIP CORROSION BETWEEN LEFT-HAND STRINGER 32 AND 33 AT FRAME STATION 445. REPAIRED IAW DHC-8 SRM 53-20-21, FIGURE 1.
- [SDR QXEA9902642](https://openairdocs.org/sdr/QXEA9902642), Dec 16, 1999: CLIP. CORRODED. PDX - CLIP CORROSION BETWEEN RIGHT-HAND STRINGER 32 AND 33 AT FRAME STATION 445. REPAIRED IAW DHC-8 SRM 53-20-21, FIGURE 1.
- [SDR QXEA9902690](https://openairdocs.org/sdr/QXEA9902690), Dec 15, 1999: SILL. DAMAGED. PDX - NICKS BELOW CARGO DOOR SILL. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2.
- [SDR QXEA9902672](https://openairdocs.org/sdr/QXEA9902672), Dec 15, 1999: SKIN. CHAFED. PDX - CHAFE DAMAGE AT STATION 262.400 AND STRINGER 11S, ABOVE RIGHT FORWARD EXIT, IT IS APPROXIMATELY .003 DEEP. REMOVAL WAS .001. FOUND TO BE WITHIN LIMITS IAW
- [SDR QXEA9902668](https://openairdocs.org/sdr/QXEA9902668), Dec 15, 1999: FRAME. GOUGED. PDX - GOUGE AT FRAME X618.0, BETWEEN STRINGERS 21S AND 20S. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902644](https://openairdocs.org/sdr/QXEA9902644), Dec 15, 1999: CONNECTOR. CORRODED. PDX - INSPECT DEICE DISTRIBUTOR CANNON PLUGS AND PRESSURE SWITCHES FOR CORROSION AND SERVICEABILITY. REMOVED AND REPLACED PRESSURE SWITCHES. (S/N 6503, 3509, 70
- [SDR QXEA9902689](https://openairdocs.org/sdr/QXEA9902689), Dec 14, 1999: SEAT TRACK. CHAFED. PDX - LEFT INBOARD SEAT TRACK CHAFFED AND LUG LIP WORN AT STATION 300. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
- [SDR QXEA9902688](https://openairdocs.org/sdr/QXEA9902688), Dec 14, 1999: SEAT TRACK. CHAFED. PDX - LEFT INBOARD SEAT TRACK CHAFFED IN BOTTOM OF TRACK APPROXIMATELY AT STATION 330. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
- [SDR QXEA9902686](https://openairdocs.org/sdr/QXEA9902686), Dec 14, 1999: SEAT TRACK. GOUGED. PDX - SMALL GOUGE IN BOTTOM OF LEFT INBOARD SEAT TRACK, APPROXIMATELY STATION 377. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
- [SDR QXEA9902664](https://openairdocs.org/sdr/QXEA9902664), Dec 14, 1999: SEAT TRACK. CHAFED. PDX - LEFT OUTBOARD SEAT TRACK HAS CHAFING PITS ON INBOARD LIP APPROXIMATELY STATION 242. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
- [SDR QXEA9902693](https://openairdocs.org/sdr/QXEA9902693), Dec 12, 1999: SEAT TRACK. CORRODED. PDX - LIGHT SURFACE CORROSION ON RIVET HEADS AND WEB PLATE FROM RIGHT-HAND OUTBOARD SEAT TRACK TO STRINGER 23, BETWEEN FRAMES 387.350 AND 405.737. REPAIRED IAW 
- [SDR QXEA9902639](https://openairdocs.org/sdr/QXEA9902639), Dec 12, 1999: STRINGER. CORRODED. PDX - CORROSION AROUND RIVET LEFT-HAND SIDE OF STRINGER 33 AT FRAME STATION 488. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902685](https://openairdocs.org/sdr/QXEA9902685), Dec 11, 1999: FRAME. CORRODED. PDX - CORROSION ON FRAME FLANGE AT STATION 531 BETWEEN STRINGERS 30 AND 31 RT. REMOVED LIGHT CORROSION IAW PSM 1-GEN-5, CHAPTER 4, PAGE 4-21, PARAGRAPH 8D. FOUN
- [SDR QXEA9902684](https://openairdocs.org/sdr/QXEA9902684), Dec 11, 1999: FRAME. CORRODED. PDX - CORROSION ON FRAME FLANGE AT STATION 510 BETWEEN STRINGERS 30 AND 31 RT. REPAIRED IAW 20-32-02, PAGE 2, PARAGRAPH A, B AND C.
- [SDR QXEA9902667](https://openairdocs.org/sdr/QXEA9902667), Dec 11, 1999: FRAME. CORRODED. PDX - CORROSION NUMEROUS PLACED AROUND RIVETS ON TOP OF FRAME X653.349, BETWEEN STRINGER 23S AND 23P. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND
- [SDR QXEA9902661](https://openairdocs.org/sdr/QXEA9902661), Dec 11, 1999: CLIP. CORRODED. PDX - CLIP HAS CORROSION BETWEEN RIGHT-HAND STRINGER 31 AND 32 AT FRAME STATION 531. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2 AND SRM 51-20-
- [SDR QXEA9902655](https://openairdocs.org/sdr/QXEA9902655), Dec 11, 1999: SPLICE. CORRODED. PDX - MINOR CORROSION ON TOP FLANGE OF STRINGER SPLICE AT STATION 531 AND STRINGER 28 RT. ACID ETCHED, ALODINED, AND PRIMED. REMOVED CORROSION FOUND TO BE WITHI

All 93: https://openairdocs.org/deregistered/N825PH-2009-09-16/reports.md

## 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 20010602018459I](https://openairdocs.org/incident/20010602018459I), Jun 2, 2001: Dhav DHC8102 (N825PH), Vancouver Bc, CN, Minor damage. (-23) Number 4 brake assembly overheated and caught fire due to failure of filter fitting p/n 20011-4-10W. Filter assembly became dislodged and blocked the…

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