# N353PH: 1997 Dehavilland DHC-8-202, registration cancelled 2011-07-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 25, 2011
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [Dehavilland DHC-8-202](https://openairdocs.org/model/dehavilland-dhc-8-202) (registry code 2809007)
- Engine: [Pratt & Whitney Canada PW123](https://openairdocs.org/engine/pratt-whitney-canada-pw123) (registry code 52129)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 496
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: September 25, 1997
- Certificate issued: August 6, 2008
- Last registry action: August 6, 2008
- Mode S code: A3F13F
- Owner when cancelled: [Win Win Services LLC](https://openairdocs.org/faa-owner/WIN%20WIN%20SERVICES%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.8187° N, 75.5062° W: Placed by OpenAirDocs at the center of ZIP code 19810, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N353PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=353PH
- Page: https://openairdocs.org/deregistered/N353PH-2011-07-25

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-8-202: https://openairdocs.org/model/dehavilland-dhc-8-202.md

## Service difficulty reports (200, newest 50)

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

- [SDR QXEA200800522](https://openairdocs.org/sdr/QXEA200800522), May 25, 2008: SWITCH. BROKEN. SEA - FLIGHT 2090 - JUST AFTER TAKEOFF, AND GEAR SELECTED UP, THE FIRST OFFICER USED THE RUDDER TRIM SWITCH, AND IN DOING SO, THE SWITCH BROKE TO THE RIGHT POSI
- [SDR QXEA200800393](https://openairdocs.org/sdr/QXEA200800393), Apr 19, 2008: UNKNOWN. UNKNOWN. SEA - BRAKES ARE MUSHY. SIGNIFICANT EFFORT ON PEDALS RESULTS IN NO BRAKING. HIGH FORCE APPLIED TO PEDALS RESULTS IN ADEQUATE BRAKING. MAINTENANCE TAXIED THE AIR
- [SDR QXEA200800281](https://openairdocs.org/sdr/QXEA200800281), Mar 8, 2008: ROD. BROKEN. ALW - UPON TRYING TO OPEN THE MAIN CABIN DOOR, THE GROUND CREW REPORTED THAT THE WERE UNABLE TO DO SO. MAINTENANCE ENTERED AIRCRAFT THROUGH THE CARGO DOOR AND F
- [SDR QXEA200800057](https://openairdocs.org/sdr/QXEA200800057), Feb 3, 2008: SPRING. MALFUNCTIONED. PDX - MAIN CABIN DOOR DIFFICULT TO OPEN. PDX MAINTENANCE REMOVED AND REPLACED MAIN CABIN DOOR GAS SPRINGS WITH NEW SPRINGS. OPS CHECKS GOOD, AIRCRAFT RETURNED T
- [SDR QXEA200701776](https://openairdocs.org/sdr/QXEA200701776), Nov 29, 2007: GENERATOR. MALFUNCTIONED. RDM - EMERGENCY LIGHTS IN THE CABIN FLICKER SOMETIMES THROUGH THE DURATION OF THE FLIGHT. SOME LIGHTS ARE ON UP TO 5 SECONDS. THE LIGHTS THAT FLICKER ARE THE EX
- [SDR QXEA200701767](https://openairdocs.org/sdr/QXEA200701767), Nov 28, 2007: POWER SUPPLY. INOPERATIVE. PDX - ON FLIGHT 2139, EMERGENCY LIGHTS IN CABIN FLICKER AFTER TAKEOFF. TURNING OFF THEN ON, ARM STOPS THE FLICKERING. LIGHTS FLICKERING ARE THE EXIT SIGNS AND O
- [SDR QXEA200701165](https://openairdocs.org/sdr/QXEA200701165), Jul 18, 2007: NONE. NONE. PDX - FOUL ODOR THROUGHOUT CABIN AND FLIGHT DECK WORSE DURING TIMES PARKED AT GATE AND ALSO DURING APPROACH AND LANDING. CLEANED REFUSE AND SPILLED BEVERAGES FR
- [SDR QXEA200701100](https://openairdocs.org/sdr/QXEA200701100), Jul 10, 2007: UNKNOWN. UNKNOWN. PDX FLIGHT NR 2164, NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED ON TAXI OUT. CYCLED ENGINE MANUAL CIRCUIT BREAKER. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAF
- [SDR QXEA200701379](https://openairdocs.org/sdr/QXEA200701379), Jul 4, 2007: CIRCUIT BREAKER. TRIPPED. SEA - WHEN SELECTING NR 1 STANDBY HYDRAULIC PRESSURE ON DURING APPROACH CHECKLIST NR 1 STANDBY HYDRAULIC PRESSURE INDICATED ZERO. AFTER FLAP SELECTION INDICATOR
- [SDR QXEA200701040](https://openairdocs.org/sdr/QXEA200701040), Jun 28, 2007: NONE. NONE. SEA - FLIGHT CREW NOTICED ACRID BURNING ODOR IN COCKPIT, NO SMOKE NOTED. ODOR IS STILL NOTICEABLE AFTER PARKING. FOUND CAPTAINS HAT WAS HUNG ON OBSERVERS MAP LI
- [SDR QXEA200700821](https://openairdocs.org/sdr/QXEA200700821), May 19, 2007: GENERATOR. MALFUNCTIONED. PDX FLIGHT NR 2149 - DURING TAKEOFF, NR 1 AC GENERATOR CAUTION ILLUMINATED AFTER CYCLING NR 1 AC GENERATOR PER CHECK LIST NR 1 STALL WARNING CAUTION ILLUMINATED
- [SDR QXEA200700389](https://openairdocs.org/sdr/QXEA200700389), Feb 26, 2007: UNKNOWN. UNKNOWN. YVR FLIGHT NR 2029, AFTER TAKEOFF DURING FLAP RETRACTION GOT NR 1 ENGINE HYD PUMP CAUTION LIGHT. PRESSURE INDICATED 2000 PSI ON BOTH STANDBY AND MAIN NR 1 HYDRA
- [SDR QXEA200700206](https://openairdocs.org/sdr/QXEA200700206), Feb 15, 2007: UNKNOWN. UNKNOWN. PUW FLIGHT NR 2197, NR 1 DC GENERATOR CAUTION LIGHT BECAME ILLUMINATED DURING TAXI OUT TO RUNWAY. FOLLOWED EMERGENCY CHECKLIST, CAUTION LIGHT STAYED ILLUMINATED
- [SDR QXEA200700043](https://openairdocs.org/sdr/QXEA200700043), Jan 20, 2007: TSCU. MALFUNCTIONED. SEA FLIGHT NR 2257, NR 1 WOULD NOT FEATHER WHEN TESTED DURING DAILY CHECKS. MAINTENANCE REPLACED NR 1 TSCU. PERFORMED GROUND RUNS IAW MTC 9720019. OPERATIONAL C
- [SDR QXEA200700005](https://openairdocs.org/sdr/QXEA200700005), Jan 4, 2007: POTENTIOMETER. OUT OF ADJUST. PSC FLIGHT NR 2094, AUTO FEATHER FAILED TO ARM ON TAKEOFF ROLL, AUTO FEATHER SYSTEM INOP. MAINTENANCE ADJUSTED THE POTENTIOMETER. OPERATIONAL CHECK GOOD. NO PAR
- [SDR QXEA200603152](https://openairdocs.org/sdr/QXEA200603152), Dec 8, 2006: FLAP SYSTEM. MALFUNCTIONED. SEA FLIGHT NR 2194 ON CLIMB-OUT, APPROXIMATELY 2 MINUTES AFTER SELECTING FLAPS UP, FLAP POWER CAUTION LIGHT ILLUMINATED. ALL SYSTEMS INDICATED NORMAL. LIGHT EXT
- [SDR QXEA200603000](https://openairdocs.org/sdr/QXEA200603000), Nov 16, 2006: WARNING SYSTEM. MALFUNCTIONED. PDX FLIGHT NR 2228, FLAP POWER CAUTION LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200601699](https://openairdocs.org/sdr/QXEA200601699), Jun 26, 2006: PANEL. DISLODGED. SEA FLIGHT NR 2273, CEILING PANEL FELL DOWN. MAINTENANCE SECURED. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200601471](https://openairdocs.org/sdr/QXEA200601471), Jun 17, 2006: RESISTOR. MALFUNCTIONED. SEA - NR 2 ENGINE TORQUE LIMITED DUE TO HIGH ITT. MAINTENANCE SECURED TRIM RESISTOR HARDWARE. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SE
- [SDR QXEA200601273](https://openairdocs.org/sdr/QXEA200601273), May 18, 2006: GCU. MALFUNCTIONED. SEA - ON FLIGHT 2222, RETURNED TO GATE, NR 2 DC GENERATOR CAUTION LIGHT ILLUMINATED. MAINTENANCE, REMOVED AND REPLACED THE NR 2 GCU. FUNCTIONAL TEST GOOD. OPERA
- [SDR QXEA200601258](https://openairdocs.org/sdr/QXEA200601258), May 15, 2006: LIGHT. LOOSE. SEA - ON FLIGHT 2229, PART OF THE EMERGENCY LIGHT STRIP ON CABIN FLOOR LOOSE. REPLACED FWD SECTION OF EMERGENCY LIGHTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETUR
- [SDR QXEA200601218](https://openairdocs.org/sdr/QXEA200601218), May 8, 2006: BATTERY. INOPERATIVE. PDX - FLIGHT 2207 FLIGHT ATTENDANT ADVISES THAT THE EXIT LIGHT ABOVE THE DOOR FLICKERS ON AND OFF ACCOMPANIED BY A POPPING SOUND. MAINTENANCE REPLACED RELAY 335
- [SDR QXEA200601217](https://openairdocs.org/sdr/QXEA200601217), May 7, 2006: SWITCH. MALFUNCTIONED. GEG - FLIGHT 2206 EMERGENCY LIGHTS FLICKERED ON AND OFF FOUR TIMES DURING CLIMBOUT, ACCORDING TO THE FLICHT ATTENDANT. MAINTENANCE REPLACED THE EMERGENCY LIGHT 
- [SDR QXEA200601031](https://openairdocs.org/sdr/QXEA200601031), Apr 12, 2006: STOP FITTING. WORN. YYC - C4 FUSELAGE RIGHT HAND EMERGENCY EXIT DOOR SURROUND STOP FITTINGS WORN IN EIGHT LOCATIONS. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-36, 51-20-51 AND RD 
- [SDR QXEA200601068](https://openairdocs.org/sdr/QXEA200601068), Apr 11, 2006: SKIN. DENTED. YYC - C4 LEFT HAND HORIZONTAL STABILIZER LOWER SKIN HAS TWO DENTS AT YH102 AND YH104.5, BETWEEN STRINGER 1 AND 2. REPAIRED IAW RD 8-55-1685, ISSUE 1.
- [SDR QXEA200601052](https://openairdocs.org/sdr/QXEA200601052), Apr 10, 2006: STRUCTURE. CRACKED. YYC - C4 RIGHT NACELLE LOWER COWL RIGHT SIDE FORWARD LATCH MATTING SURFACE CRACKED. REPAIRED IAW RD 8-71-030, ISSUE 3.
- [SDR QXEA200601032](https://openairdocs.org/sdr/QXEA200601032), Apr 10, 2006: ANGLE. CRACKED. YYC - C4 LEFT NACELLE, INBOARD DRAG ANGLE IS CRACKED AT LAST RIVET, AFT ON WING SIDE. REPARIED IAW RD 8-57-1053, ISSUE 2.
- [SDR QXEA200601016](https://openairdocs.org/sdr/QXEA200601016), Apr 10, 2006: ATTACH FITTING. WORN. YYC - C4 LEFT NACELLE AFT HEAT SHIELD, OUTLET SHROUD ATTACHMENT TABS ARE WORN THROUGH AT STATION 262 - 280 ON INBOARD SIDE AND OUTBOARD SIDE. REPAIRED IAW RD 8-
- [SDR QXEA200601057](https://openairdocs.org/sdr/QXEA200601057), Apr 7, 2006: BUSHING. WORN. YYC - C4 TRAILING RUDDER CENTER HINGE UPPER ATTACHMENT BOLT HOLE WORN EXCESSIVE AND LOWER BUSHING WORN. REPAIRED IAW RD 8-55-554, ISSUE 1.
- [SDR QXEA200601055](https://openairdocs.org/sdr/QXEA200601055), Apr 7, 2006: PUSH-PULL ROD. GOUGED. YYC - C4 TRAILING RUDDER LOWER HINGE PUSH/PULL ROD ATTACHMENT BRACKET HAS A DEEP GOUGE AND BOLT OPENING HOLE WORN EXCESSIVE. REPAIRED IAW RD 8-55-168, ISSUE 5.
- [SDR QXEA200601067](https://openairdocs.org/sdr/QXEA200601067), Apr 6, 2006: SKIN. DAMAGED. YUYC C4 - LEFT NACELLE INBOARD SIDE SKIN HAS LOOSE RIVETS ABOVE AND BEHIND ACCESS DOOR 416AR. ONE RIVET WORN THROUGH COUNTER SINK. REPAIRED IAW RD 8-54-1193, IS
- [SDR QXEA200601066](https://openairdocs.org/sdr/QXEA200601066), Apr 6, 2006: HINGE. GOUGED. YYC - C4 RIGHT MAIN LANDING GEAR DOOR FORWARD HINGE GOUGED AT AFT SIDE OF FORWARD LUG BY BRG BRACKET AND SPACER CONTACT SURFACE WORN. REPAIRED IAW HORIZON AIR E
- [SDR QXEA200601059](https://openairdocs.org/sdr/QXEA200601059), Apr 6, 2006: SKIN. CHAFED. YYC - C4 LEFT INBOARD FLAP UPPER SKIN HAS CHAFED MARK. REPAIRED IAW DHC-8-200 RD 8-57-1023 AND DHC-8-200 AMM 20-30-11.
- [SDR QXEA200601019](https://openairdocs.org/sdr/QXEA200601019), Apr 6, 2006: STOP FITTING. CHAFED. YYC - C4 PASSENGER DOOR AFT NR 1 AND NR 2 STOP ASSEMBLIES LIGHTLY CHAFED. REPARIED IAW RD 8-52-8222, ISSUE 1 AND HORIZON AIR EA 2-52-237.
- [SDR QXEA200601020](https://openairdocs.org/sdr/QXEA200601020), Apr 6, 2006: SKIN. DAMAGED. YYC - C4 FUSELAGE EXTERIOR BELLY SKIN BETWEEN STATION X530 - X566 AND STRINGERS 23P - 28P HAS A LARGE AREA OF NICKS IN SKIN. REPAIRED IAW DHC-8-200 SRM 51-20-11
- [SDR QXEA200601022](https://openairdocs.org/sdr/QXEA200601022), Apr 5, 2006: SKIN. DENTED. YYC - C4 FUSELAGE EXTERIOR SKIN AT STATION X302, BETWEEN STRINGERS 17S - 20S HAS SEVERAL DENTS. REPAIRED IAW DHC-8-200 SRM 51-20-91, RD 8-53-4984, ISSUE 1 AND H
- [SDR QXEA200601062](https://openairdocs.org/sdr/QXEA200601062), Apr 4, 2006: HINGE. WORN. YYC - C4 VERTICAL STABILIZER REAR SPAR TOP FORE RUDDER ATTACH SAFETY HINGE HAS WEAR DAMAGE ON TOP FACE. REPARIED IAW DHC-8-200 SR, 51-40-11, PAGES 1-4 AND RD 8-
- [SDR QXEA200601063](https://openairdocs.org/sdr/QXEA200601063), Apr 4, 2006: HINGE. WORN. YYC - C4 VERTICAL STABILIZER REAR SPAR FORE RUDDER ATTACH BOTTOM SAFETY HINGE HAS WEAR DAMAGE ON TOP FACE. REAPIRED IAW RD 8-51-102, ISSUE 1 AND DHC-8-200 SRM 5
- [SDR QXEA200601043](https://openairdocs.org/sdr/QXEA200601043), Apr 4, 2006: FASTENER. LOOSE. YYC - C4 LEFT WING INTERIOR, STATION YW138.0 ON FRONT SPAR HAS TWO LOWER LOOSE HILOCKS. REPLACED IAW DHC-8-200 SRM 51-40-00.
- [SDR QXEA200601035](https://openairdocs.org/sdr/QXEA200601035), Apr 4, 2006: FITTING. WORN. YYC - C4 LEFT ELEVATOR SPRING TAB DRIVE HINGE FITTING IS WORN. REPARIED IAW DHC-8-200 SRM 51-40-11, PAGES 1-4.
- [SDR QXEA200601024](https://openairdocs.org/sdr/QXEA200601024), Apr 4, 2006: STOP FITTING. WORN. YYC - C4 FUSELAGE AFT BAGGAGE DOOR SURROUND STOP FITTINGS WORN AT EIGHT LOCATIONS. REPAIRED IAW DHC-8-200 SRM 52-30-00-820-001 AND RD 8-104, ISSUE 3.
- [SDR QXEA200601033](https://openairdocs.org/sdr/QXEA200601033), Apr 3, 2006: CLIP. CRACKED. YYC - C4 FUSELAGE INTERIOR AT STATION X240 UNDER PASSENGER DOOR SILL, CLIP IS CRACKED. REPAIRED IAW DHC-8-200 SRM, 51-40-11, PAGES 1-4.
- [SDR QXEA200601034](https://openairdocs.org/sdr/QXEA200601034), Apr 3, 2006: SILL. CORRODED. YYC - C4 FUSELAGE INTERIOR PASSENGER DOOR OPENING, LOWER SILL ASSEMBLY HAS PITTING CORROSION ON TOP SURFACE UNDER TEFLON RUB STRIP. REPAIRED IAW DHC-8-200 SRM 5
- [SDR QXEA200601064](https://openairdocs.org/sdr/QXEA200601064), Apr 2, 2006: ACCESS PANEL. CORRODED. YYC - C4 RIGHT HAND WING ACCESS PANEL 622AT COUNTER SINK SCREW HOLES HAVE FRETTING CORROSION. REPAIRED IAW RD 8-57-1715, ISSUE 3, DHC-8-200 SRM 51-20-16, PARAGR
- [SDR QXEA200601048](https://openairdocs.org/sdr/QXEA200601048), Apr 2, 2006: SKIN. CORRODED. YYC - C4 RIGHT INBOARD LEADING EDGE 611AR LOWER ATTACHMENT REBATE INBOARD HAS FRETTING CORROSION. REPAIRED IAW RD 8-57-811, DHC-8-200 SRM 51-40-11, PAGES 1-4 AN
- [SDR QXEA200601061](https://openairdocs.org/sdr/QXEA200601061), Apr 1, 2006: STRUCTURE. CORRODED. YYC - C4 RIGHT HORIZONTAL STABILIZER ELEVATOR HORN HAS FRETTING DAMAGE ON INTERNAL REBATE ALONG INBOARD EDGE. REPAIRED IAW DHC-8-200 CORROSIOON PREVENTION MANUA
- [SDR QXEA200601038](https://openairdocs.org/sdr/QXEA200601038), Apr 1, 2006: LINE. CHAFED. YYC - C4 LEFT WING FUEL BAY 524AT HAS RUBBING LINE ON STRUCTURE AT YW207. REPAIRED IAW DHC-8-200 SRM 51-20-11 AND AMM SUB TASK 28-43-11-120-001.
- [SDR QXEA200601030](https://openairdocs.org/sdr/QXEA200601030), Apr 1, 2006: STRINGER. CORRODED. YYC - C4 FUSELAGE INTERIOR, RIGHT SIDE SUPPORT CHANNEL X240, STRINGER 22S HAS CORROSION ON END. REPAIRED IAW CORROSION PREVENTION CONTROL MANUAL, CHAPTER, PART 
- [SDR QXEA200601029](https://openairdocs.org/sdr/QXEA200601029), Apr 1, 2006: SILL. CORRODED. ICY - C4 FUSELAGE RIGHT EMERGENCY EXIT DOOR SURROUND STRUCTURE, LOWER SILL HAS AREA OF CORROSION FROM X240 TO X264. REPAIRED YAW CORROSION PREVENTION MANUAL, CH
- [SDR QXEA200601028](https://openairdocs.org/sdr/QXEA200601028), Apr 1, 2006: DOUBLER. CORRODED. YYC - C4 FUSELAGE INTERIOR, RIGHT EMERGENCY EXIT LOWER FRAME DOUBLER HAS AREA OF CORROSION FROM X240 TO X264, STRINGER 24S. REPAIRED IAW DHC-8-200 SRM 51-40-00.

All 200: https://openairdocs.org/deregistered/N353PH-2011-07-25/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 20020311003679I](https://openairdocs.org/incident/20020311003679I), Mar 11, 2002: Dhav DHC8202 (N353PH), Seattle, WA, Minor damage. (-23) A food & beverage (fab) cart ran into the tail cone of N353PH during push-back ground operations at sea-tac intl. Airport. The aircraft sustained minor…
- [Incident 19990114008599I](https://openairdocs.org/incident/19990114008599I), Jan 14, 1999: Dhav DHC8202 (N353PH), Pasco, WA. During descent, aircraft encountered unforcast severe turbulence, flight attendant hit nose and possibly broke nose.

## Other aircraft with N353PH

- [Cancelled 2017-08-08](https://openairdocs.org/deregistered/N353PH-2017-08-08): Bombardier CL-600-2B19, S/N 7385. Exported to Canada. Owner: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)

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