# N354PH: 1997 Dehavilland DHC-8-202, registration cancelled 2011-07-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 21, 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: 498 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: October 2, 1997 - Certificate issued: August 6, 2008 - Last registry action: August 6, 2008 - Mode S code: A3F4F6 - 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/N354PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=354PH - Page: https://openairdocs.org/deregistered/N354PH-2011-07-21 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-8-202: https://openairdocs.org/model/dehavilland-dhc-8-202.md ## Service difficulty reports (224, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR QXEA200800285](https://openairdocs.org/sdr/QXEA200800285), Mar 6, 2008: ATTACH FITTING. CORRODED. PDX - C5 - MCD LAY SHAFT FWD AND AFT GOOSE NECK ATTACH FITTINGS ARE PITTING AND CORRODED. REMOVED MCD LAY SHAFT REF -8/200 AMM 52-10-00FIG 501 SHEETS (3&4). REM - [SDR QXEA200800284](https://openairdocs.org/sdr/QXEA200800284), Mar 6, 2008: BRACKET. CORRODED. PDX - C5 - MCD SURROUND FWD END OF SILL PLATE BRACKET FOR SILL PLATE CORRODED AGAINST FUSELAGE. REMOVED THE MCD THRESHOLD BY DRILLING OUT THE RIVETS HOLDING THE - [SDR QXEA200800283](https://openairdocs.org/sdr/QXEA200800283), Mar 6, 2008: SILL. CORRODED. PDX - C5 - MCD SURROUND FWD SIDE OF SILL PLATE AREA, CORROSION AT SEAL INFLATION FEED THROUGH, IPC 52-05-00 FIG 5 ITEM 490. REMOVED MCD SEAL INFLATION TUBE AND - [SDR QXEA200800282](https://openairdocs.org/sdr/QXEA200800282), Mar 6, 2008: SILL. CORRODED. PDX- C5 - CORROSION ON LOWER SURFACE OF MCD SILL PLATE STATION X250 AT AFT NUT PLATE. BLENDED TO REMOVE CORROSION IAW RD8-53-8921. HFEC INSPECTION OF BLENDED AR - [SDR QXEA200800272](https://openairdocs.org/sdr/QXEA200800272), Mar 6, 2008: BRACKET. CRACKED. PDX - C5 - ANGLE BRACKET FORWARD OF STATION 600 AND INBOARD OF STRINGER 31R WEB UNDER FLOOR PANEL 441CZ IS CRACKED IN UPPER RADIUS. DRILLED OUT RIVETS IN THE AN - [SDR QXEA200800270](https://openairdocs.org/sdr/QXEA200800270), Mar 6, 2008: ATTACH ANGLE. CORRODED. PDX - C5 - CARGO BAY ENTRYWAY THRESHOLD ATTACHMENT ANGLE AT APPROXIMATELY STA 580.5 HAS CORROSION AROUND NUT PLATES. REMOVED CARGO BAY THRESHOLD PLATE BY REMOVI - [SDR QXEA200800277](https://openairdocs.org/sdr/QXEA200800277), Mar 6, 2008: SKIN. CHAFED. PDX - C5 - UPPER SURFACE OF LEFT INBOARD FLAP 5" AFT OF THE LEADING EDGE AT STATION YW139.00 IS CHAFED APPROXIMATELY .30" BY .35". BLENDED OUT CHAFE IAW -8 200 - [SDR QXEA200800276](https://openairdocs.org/sdr/QXEA200800276), Mar 6, 2008: CHANNEL. DENTED. PDX - C5 - LOWER FORWARD EMERGENCY EXIT THRESHOLD CHANNEL PN 85320693 REQUIRES REPLACEMENT IN ACCORDANCE WITH EA 2-53-733 PERMANENT REPAIR FOR DENT IN CHANNEL. - [SDR QXEA200800275](https://openairdocs.org/sdr/QXEA200800275), Mar 6, 2008: FLOOR SUPPORT. CORRODED. PDX - C5 - CORROSION ON FLOOR BOARD NUT PLATE FLANGE UNDER PANEL 144BZ AT STATION 199.5 INBOARD OF SEAT TRACK. REMOVED NUTPLATE, BLENDED OUT CORROSION IAW DASH - [SDR QXEA200800274](https://openairdocs.org/sdr/QXEA200800274), Mar 6, 2008: FLOORBOARD. CORRODED. PDX - C5 - CORROSION ON FLOORBOARD FLANGE UPPER SURFACE AT STATION 599.5 OUTBOARD OF STRINGER 28R TO END OF FLANGE. REMOVED NUT PLATE, BLENDED OUT CORROSION IAW - [SDR QXEA200800269](https://openairdocs.org/sdr/QXEA200800269), Mar 6, 2008: THRESHOLD. CHAFED. PDX - C5 - CARGO BAY ENTRYWAY THRESHOLD HAS SEVERAL AREAS OF LIGHT CHAFING. REPAIRED CHAFE BY BLENDING, MAX MATERIAL REMOVED WAS .005" WITHIN LIMITS REFERENCE T - [SDR QXEA200701902](https://openairdocs.org/sdr/QXEA200701902), Dec 14, 2007: ROD. BROKEN. FLIGHT 2035. LT MAIN GEAR DOORS WERE OPEN WITH NO INDICATION FROM THE COCKPIT, ONLY THE LT SIDE OF THE DOOR IS OPEN. MAINTENANCE REPLACED THE SPRING, CONNECT RO - [SDR QXEA200701586](https://openairdocs.org/sdr/QXEA200701586), Oct 20, 2007: OUTFLOW VALVE. MALFUNCTIONED. SEA FLIGHT NR 2190 AT LEVEL FLIGHT CABIN DIFFERENTIAL PRESSURE GRADUALLY DECREASED FROM 5.4 PSID TO 0 PSID. UNABLE TO CONTROL CABIN PRESSURE IN MANUAL MODE. MAI - [SDR QXEA200701504](https://openairdocs.org/sdr/QXEA200701504), Sep 25, 2007: GENERATOR. MALFUNCTIONED. YVR FLIGHT NR 2450, NR 1 AC GENERATOR CAUTION LIGHT WOULD NOT RESET PER CHECKLIST. FERRIED TO PDX. REPLACED NR 1 AC GENERATOR IAW 24-21-00-400-801. ALSO, REPLAC - [SDR QXEA200701410](https://openairdocs.org/sdr/QXEA200701410), Sep 10, 2007: PRESSURE SWITCH. MALFUNCTIONED. PDX FLIGHT NR 2107, 18 PSI BLEED AIR INDICATES 10 PSI WITH POWER LEVERS AT FLIGHT IDLE. INSTALLED NEW 55 AND 65 PSI SWITCHES IN BOTH RIGHT AND LEFT NACELLES IAW - [SDR QXEA200701166](https://openairdocs.org/sdr/QXEA200701166), Jul 18, 2007: SMOKE DETECTOR. INOPERATIVE. SEA FLIGHT NR 2064, NR 1 ENGINE START SMOKE MASTER WARNING ILLUMINATED. NR 2 SMOKE DETECTOR INOP. PLACED ON MEL 372270. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA200700963](https://openairdocs.org/sdr/QXEA200700963), Jun 14, 2007: LENS. DISLODGED. SEA FLIGHT NR 2026 PLASTIC PIECE FELL OFF FROM CEILING ABOUT 6" LONG. REPORTED BY FLIGHT ATTENDANT. MAINTENANCE RESECURED SIDE WALL LIGHT LENS. PERFORMED GUI OF - [SDR QXEA200700393](https://openairdocs.org/sdr/QXEA200700393), Mar 18, 2007: WIRE. CHAFED. SEA FLIGHT 2070 SHORTLY AFTER LIFTOFF NR 2 DC GENERATOR DC GEN HOT CAUTION ILLUMINATED. CAUTION REMAINED ON FOR ENTIRE DURATION OF FLIGHT EVEN AFTER TURNING OFF - [SDR QXEA200700361](https://openairdocs.org/sdr/QXEA200700361), Mar 11, 2007: GENERATOR. OVERHEATED. SEA FLIGHT NR 2116 - DURING TAXI, NR 2 DC GEN HOT CAUTION ILLUMINATED. AFTER TURNING OFF NR 2 DC GENERATOR (AS PER CHECKLIST) CAUTION EXTINGUISHED AFTER APPROXI - [SDR QXEA200602066](https://openairdocs.org/sdr/QXEA200602066), Aug 13, 2006: GALLEY. ODIFEROUS. SEA FLIGHT NR 2054 ON DESCENT, AIRCRAFT SMELLS LIKE A DIRTY LAV. LAV FLUID HAS BEEN EXCHANGED TWICE, WARDROBE CLOSET HAS BEEN CLEANED. AIRCRAFT STILL SMELLS LIK - [SDR QXEA200600999](https://openairdocs.org/sdr/QXEA200600999), Apr 7, 2006: STOP. WORN. PDX - C4 LEFT HAND UNDERWING EMERGENCY EXIT AFT UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200601000](https://openairdocs.org/sdr/QXEA200601000), Apr 7, 2006: STOP. WORN. PDX - C4 LEFT UNDER WING EMERGENCY EXIT AFT LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600998](https://openairdocs.org/sdr/QXEA200600998), Apr 7, 2006: STOP. WORN. PDX - C4 LEFT UNDER WING EMERGENCY EXIT FORWARD UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600997](https://openairdocs.org/sdr/QXEA200600997), Apr 7, 2006: STOP. WORN. PDX - C4 LEFT UNDER WING EMERGENCY EXIT FORWARD LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600996](https://openairdocs.org/sdr/QXEA200600996), Apr 7, 2006: STOP. WORN. PDX - C4 RIGHT UNDERWING EMERGENCY EXIT AFT LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600995](https://openairdocs.org/sdr/QXEA200600995), Apr 7, 2006: STOP. WORN. PDX - C4 RIGHT UNDERWING EMERGENCY EXIT AFT UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600992](https://openairdocs.org/sdr/QXEA200600992), Apr 7, 2006: STOP. WORN. PDX - C4 LEFT UNDER WING EMERGENCY EXIT AFT LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-52-350. - [SDR QXEA200600991](https://openairdocs.org/sdr/QXEA200600991), Apr 7, 2006: STOP. WORN. PDX - C4 LEFT UNDER WING EMERGENCY EXIT AFT UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-52-350. - [SDR QXEA200600990](https://openairdocs.org/sdr/QXEA200600990), Apr 7, 2006: STOP. WORN. PDX - C4 LEFT HAND UNDER WING EMERGENCY EXIT FORWARD LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-350. - [SDR QXEA200600993](https://openairdocs.org/sdr/QXEA200600993), Apr 7, 2006: STOP. WORN. PDX - C4 RIGHT HAND UNDERWING EMERGENCY EXIT FORWARD UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600994](https://openairdocs.org/sdr/QXEA200600994), Apr 7, 2006: STOP. WORN. PDX - C4 RIGHT HAND UNDER WING EMERGENCY EXIT FORWARD LOWER STOP WORN ON CONTACT. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600989](https://openairdocs.org/sdr/QXEA200600989), Apr 7, 2006: STOP. WORN. PDX - C4 LEFT UNDER WING EMERGENCY EXIT FORWARD UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-350. - [SDR QXEA200601001](https://openairdocs.org/sdr/QXEA200601001), Apr 6, 2006: STRINGER. CORRODED. PDX - C4 CORROSION FOUND ON STRINGER 32R ON AFT SIDE OF FRAME X151.600. REPAIRED IAW DHC-8-200 SRM 51-40-11 AND HORIZON AIR EA 2-53-375. - [SDR QXEA200601003](https://openairdocs.org/sdr/QXEA200601003), Apr 5, 2006: SKIN. CORRODED. PDX - C4 CORROSION ON INTERNAL SKIN BAGGAGE COMPARTMENT JUST AFT OF DOOR CUTOUT FLOOR LEVEL. SEVERAL AREAS OF SURFACE CORROSION APPROXIMATELY X600-X535 AND STRI - [SDR QXEA200600938](https://openairdocs.org/sdr/QXEA200600938), Apr 3, 2006: THRESHOLD. DENTED. PDX - C4 DENT IN FORWARD EMERGENCY EXIT THRESHOLD HAS TRANSFER THROUGH TO INSIDE LYING STRUCTURE AT X248-249, YW40. REPAIRED IAW HORIZON AIR EA 2-53-733. - [SDR QXEA200600921](https://openairdocs.org/sdr/QXEA200600921), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 31L AND 32L. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-21-10 AND SRM 51-25-15. - [SDR QXEA200600925](https://openairdocs.org/sdr/QXEA200600925), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 30R AND 31R. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND SRM 51-25-15. - [SDR QXEA200600931](https://openairdocs.org/sdr/QXEA200600931), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 30L AND 31L. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600924](https://openairdocs.org/sdr/QXEA200600924), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 28L AND 29L. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600932](https://openairdocs.org/sdr/QXEA200600932), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 29L AND 30L. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND SRM - [SDR QXEA200600930](https://openairdocs.org/sdr/QXEA200600930), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 31L AND 32L. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND 51- - [SDR QXEA200600929](https://openairdocs.org/sdr/QXEA200600929), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 32L AND 33L. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-21-10, 51-25-10 AND SRM 51-25-15. - [SDR QXEA200600928](https://openairdocs.org/sdr/QXEA200600928), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 30R AND 31R. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND 51- - [SDR QXEA200600923](https://openairdocs.org/sdr/QXEA200600923), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 29L AND 30L. REPAIRED IAW DHC-82 SRM 51-00-02, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600934](https://openairdocs.org/sdr/QXEA200600934), Apr 3, 2006: STRINGER. CORRODED. PDX - C4 STRINGER 31R APPEARS CORRODED WHERE PAINT IS MISSING AT STATION 175.0. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-00-04, 51-40-11, 51-21-10, 51-25-10 AND - [SDR QXEA200600926](https://openairdocs.org/sdr/QXEA200600926), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 32R AND 33R. REPAIRED IAW DHC-8-200 SRM 51-40-11, 51-20-10 AND SRM 51-25-15. - [SDR QXEA200600922](https://openairdocs.org/sdr/QXEA200600922), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 30L AND 31L. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-11, 51-25-10 AND SRM 51-25-15. - [SDR QXEA200600927](https://openairdocs.org/sdr/QXEA200600927), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 31R AND 32R. REPAIRED IAW DHC-8-200 SRM 51-70-16, 51-40-11, 51-21-10, 51-25-10 AND SRM 51-25-15. - [SDR QXEA200600933](https://openairdocs.org/sdr/QXEA200600933), Apr 3, 2006: FRAME. CORRODED. PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 28L AND 29L. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600915](https://openairdocs.org/sdr/QXEA200600915), Apr 3, 2006: SILL. DENTED. PDX - C4 RIGHT FORWARD EMERGENCY EXIT LOWER SILL HAS DENT BY FORWARD DOOR LUG RECEPTACLE. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND HORIZON AIR EA 2-53-729. All 224: https://openairdocs.org/deregistered/N354PH-2011-07-21/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 20020713025289I](https://openairdocs.org/incident/20020713025289I), Jul 13, 2002: Dhav DHC8202 (N354PH), Portland, OR. (-23) Aircraft experienced roll control binding in flight. Pilot returned to field without incident. Maintenance troubleshot system and discovered safety wire… - [Incident 19971109041439I](https://openairdocs.org/incident/19971109041439I), Nov 9, 1997: Dhav DHC8202 (N354PH), Portland, OR, Minor damage. Aircraft was marshalled into a parked aircraft. Failure in communication between marshaller/wingwalker. ## Other aircraft with N354PH - [Cancelled 2017-12-07](https://openairdocs.org/deregistered/N354PH-2017-12-07): Boeing 737-700, S/N 28583. 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) --- 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.