# N355PH: 1997 Dehavilland DHC-8-202, registration cancelled 2013-01-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 24, 2013
- Status when cancelled: First renewal notice
- 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: 500
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: October 31, 1997
- Certificate issued: November 3, 2008
- Last registry action: November 3, 2008
- Mode S code: A3F8AD
- 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/N355PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=355PH
- Page: https://openairdocs.org/deregistered/N355PH-2013-01-24

From the FAA registry file of October 31, 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 (223, newest 50)

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

- [SDR QXEA200800697](https://openairdocs.org/sdr/QXEA200800697), Jun 28, 2008: OIL SYSTEM. OVERSERVICED. PDX - CREW REPORTS OIL ODOR IN CABIN. FOUND ENGINE OIL FOR NR 1 OVER SERVICED. ADJUSTED LEVEL. GROUND RUN CHECKS OK. RETURNED TO SERVICE. NO PARTS REPLACED. (A)
- [SDR QXEA200800418](https://openairdocs.org/sdr/QXEA200800418), Apr 18, 2008: INTERCOSTAL. CORRODED. C4-CHECK - SUSPECT CORROSION ON AVIONICS BAY INTERCOSTAL AT BELLY SKIN, JUST OB OF STRINGER 31P FROM STA X190 TO X201. REPAIRED IAW SRM. (K)
- [SDR QXEA200800417](https://openairdocs.org/sdr/QXEA200800417), Apr 18, 2008: KEELBEAM. CORRODED. C4-CHECK- SUSPECT CORROSION ON BOTTOM OF VERT KEEL BEAM AT STR 31P AND STA X201. REPAIRED IAW SRM. (K)
- [SDR QXEA200800425](https://openairdocs.org/sdr/QXEA200800425), Apr 18, 2008: HINGE FITTING. CORRODED. PDX C4 CHECK - MCD LAY SHAFT, AFT HINGE FITTING HAS PITTING AROUND BOLT HOLES. REMOVED MCD LAY SHAFT. SEPARATED LAYSHAFT AND DRILLED OUT AFT HINGE FITTING. DRIL
- [SDR QXEA200800442](https://openairdocs.org/sdr/QXEA200800442), Apr 18, 2008: STRUT. CHAFED. PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE AT LOWER O/B SURFACE WHERE O/B WOW HARNESS CONDUIT HAS CONTACTED. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 3
- [SDR QXEA200800441](https://openairdocs.org/sdr/QXEA200800441), Apr 18, 2008: STRUT. CHAFED. PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE ON FWD SURFACE AT STRUT FAIRING MID ATTACH HOLE. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015 P
- [SDR QXEA200800440](https://openairdocs.org/sdr/QXEA200800440), Apr 18, 2008: STRUT. CHAFED. PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE ON FWD SURFACE AT STRUT FAIRING UPPER ATTACH HOLE. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015
- [SDR QXEA200800424](https://openairdocs.org/sdr/QXEA200800424), Apr 18, 2008: CASTING. CORRODED. PDX C4 CHECK. FWD CORNER CASTING ON MCD HAS CORROSION AROUND NUTPLATE, TOP AND BOTTOM. REMOVED FWD CORNER MCD CASTINGS AND INSTALL NEW CASTING REF -8 200 SRM 51
- [SDR QXEA200800426](https://openairdocs.org/sdr/QXEA200800426), Apr 18, 2008: FITTING. CORRODED. PDX C4 CHECK. TENSION FITTING LOCATED AT FRAME X201 STR 31S HAS CORROSION. REMOVED TENSION FITTING AND INSTALLED NEW FITTING IAW 8 200 SRM 51-40-11, 51-20-36.
- [SDR QXEA200800423](https://openairdocs.org/sdr/QXEA200800423), Apr 18, 2008: STOP FITTING. WORN. PDX C4 CHECK. MCD SURROUND STOP FITTINGS ALL HAVE SIGNS OF WEAR. BLENDED FITTINGS IAW -8 200 RD8-53-3933 PG 4, PARA 1.2. WITHIN LIMITS. INSPECTED AS PER RD8-53-
- [SDR QXEA200800421](https://openairdocs.org/sdr/QXEA200800421), Apr 18, 2008: SEAT TRACK. CORRODED. PDX C4 CHECK. CORROSION ON SEAT TRACK NR 4 CAMLOCK RECEP. STA X222. REMOVED NR 4 SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 2
- [SDR QXEA200800420](https://openairdocs.org/sdr/QXEA200800420), Apr 18, 2008: SEAT TRACK. CORRODED. PDX C4 CHECK. SURFACE CORROSION ON SEAT TRACK NR 7 BETWEEN STA X220 AND X226. REMOVED NR 7 SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRAC
- [SDR QXEA200800419](https://openairdocs.org/sdr/QXEA200800419), Apr 18, 2008: SEAT TRACK. CORRODED. PDX C4 CHECK. LT SEAT TRACK NR 2 HAS CORROSION AT APPROX STA 438 STA 466.5, STA 485, AND STA 498. REMOVED SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INS
- [SDR QXEA200800422](https://openairdocs.org/sdr/QXEA200800422), Apr 18, 2008: SEAT TRACK. CORRODED. PDX C4 CHECK. CORROSION ON SEAT TRACK NR 1 AT APPROX. STA X360. REMOVED NR 4 SEAT TRACK IAW -8 200 SRM 51-40-00. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 S
- [SDR QXEA200800415](https://openairdocs.org/sdr/QXEA200800415), Apr 18, 2008: FITTING. CORRODED. PDX C4 CHECK FITTING CORRODED JUST AFT OF CARGO DOOR FUSELAGE CUTOUT, LOWER AFT CORNER. REMOVED CORRODED FITTING AT AFT LOWER CORNER IAW -8 200 SRM 51-40-11. IN
- [SDR QXEA200800416](https://openairdocs.org/sdr/QXEA200800416), Apr 18, 2008: FLOOR SKIN. CORRODED. PDX C4 CHECK CORROSION AT CARGO PIT DECK SKIN I/B AND BELOW CORNER FITTING STA X597.5, Y40.95. REMOVED CORROSION USING SCOTCH BRITE PAD IAW -8 200 SRM 51-40-11 
- [SDR QXEA200800414](https://openairdocs.org/sdr/QXEA200800414), Apr 18, 2008: FLOOR SKIN. CORRODED. PDX C4 CHECK CARGO PIT LOWER FLOOR DECK SKIN HAS CORROSION ALONG RIVET ROW AT STA X600 BETWEEN Y10L AND Y24L. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS CHE
- [SDR QXEA200800413](https://openairdocs.org/sdr/QXEA200800413), Apr 18, 2008: SUPPORT BRACKET. CRACKED. PDX C4 CHECK SUPPORT BRACKET UNDER MCD SILL IS CRACKED. R&R SUPPORT BRACKET WITH NEW FROM STOCK REF -8 200 SRM 51-40-11 FOR RIVETING.
- [SDR QXEA200800412](https://openairdocs.org/sdr/QXEA200800412), Apr 18, 2008: DOOR. GOUGED. PDX C4 CHECK CARGO DOOR HAS SEVERAL GOUGES ON CENTER FWD LOWER SIDE. REMOVED DAMAGE IAW -8 200 51-20-11. HFEC INSP IAW -8 200 NDTM PT6, 51-00-01 NO CRACKS NOTED
- [SDR QXEA200800410](https://openairdocs.org/sdr/QXEA200800410), Apr 18, 2008: SEAT TRACK. CORRODED. PDX C4 CHECK FUSELAGE INTERIOR WEB THAT TIES INTO LT O/B SEAT TRACK HAS AN OVERSIZED HOLE LOCATED 2" AFT OF FRAME 333.300. REMOVED WEB BETWEEN FRAMES 333.30 AND
- [SDR QXEA200800411](https://openairdocs.org/sdr/QXEA200800411), Apr 18, 2008: SUPPORT BRACKET. DAMAGED. PDX C4 CHECK LT O/B SEAT TRACK SUPPORT BRACKET ON FWD SIDE OF FRAME AT STA X333.3 HAS DAMAGED HOLE, 2ND HOLE AFT TOP. REMOVED LT O/B SEAT TRACK SUPPORT BRACKET 
- [SDR QXEA200800408](https://openairdocs.org/sdr/QXEA200800408), Apr 18, 2008: FLAP. CHAFED. PDX C4 CHECK RT O/B FLAP HAS A CHAFFED AREA AT THE O/B END APPROX 10" FROM THE TRAILING END. BLENDED ARE OF CHAFE, FOUND OUT OF LIMITS IAW -8 200 SRM 57-50-16. 
- [SDR QXEA200800409](https://openairdocs.org/sdr/QXEA200800409), Apr 18, 2008: SEAT TRACK. CORRODED. PDX C4 CHECK BRACKET FOR NR 1 SEAT TRACK WEB AFT OF FRAME 354 IS DAMAGED. REMOVED BRACKET IAW -8 200 SRM 51-40-11. INSTALLED NEW BRACKET IAW -8 200 SRM 51-40-00
- [SDR QXEA200800407](https://openairdocs.org/sdr/QXEA200800407), Apr 18, 2008: SEAT TRACK. CORRODED. PDX C4 CHECK CORROSION ON RT O/B SEAT TRACK AT APPROX X488.5. BLENDED OUT CORROSION IAW RD8-53-10103. ALODINE PRIMED IAW -8 200 SRM 51-20-16, 51-20-36.
- [SDR QXEA200800405](https://openairdocs.org/sdr/QXEA200800405), Apr 18, 2008: KEELBEAM. CORRODED. PDX C4 CHECK SUSPECT CORROSION AT I/B BOTTOM OF VERTICAL KEELBEAM AT STA X370 AND STR 31P. REMOVED CORROSION AT BOTTOM OF VERTICAL KEEL BEAM STA 370.8. REF CPM 
- [SDR QXEA200800406](https://openairdocs.org/sdr/QXEA200800406), Apr 18, 2008: STRINGER. CORRODED. PDX C4 CHECK CORROSION ON STR 23S (X387 TO X392) AND CONNECTING CLIP TO FRONT SPAR MAIN FRAME ON AFT SIDE AT X387.35. REMOVED LIGHT SURFACE FROM STRINGER AND CO
- [SDR QXEA200800404](https://openairdocs.org/sdr/QXEA200800404), Apr 18, 2008: STRUCTURE. DAMAGED. PDX C4 CHECK CORROSION ON FORE AND AFT LOWER CORNER COMBING PIECES, I/B FLANGE, ON PAX DOOR APERTURE LOWER EDGE. REMOVED NUTPLATE FROM CASTING AND REMOVED CORRO
- [SDR QXEA200800403](https://openairdocs.org/sdr/QXEA200800403), Apr 18, 2008: FRAME. CORRODED. PDX C4 CHECK SUSPECT CORROSION OF FRA X201 AT STR 31S. REMOVED CORROSION IAW CPM CHAP 4 PARA 9A-B(1-6(A)). UT THICKNESS CHECK IAW -8 200 NDTM PT 1, 51-00-04 HI 
- [SDR QXEA200800399](https://openairdocs.org/sdr/QXEA200800399), Apr 18, 2008: FLOORBEAM. CORRODED. PDX C4 CHECK ZONE 144 AFT FLOOR SUPPORT ANGLE AT STA X600 IS CORRODED AT Y20L AND Y24L. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS IAW -8 200 PT 1, 51-00-04
- [SDR QXEA200800401](https://openairdocs.org/sdr/QXEA200800401), Apr 18, 2008: STRUCTURE. CORRODED. PDX C4 CHECK ZONE 144 SUBFLOOR IS CORRODED AT Y565 AND Y25L-Y27L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED .002 MATERIAL FROM ORIGINAL THICKNESS, .043 MATERIAL
- [SDR QXEA200800402](https://openairdocs.org/sdr/QXEA200800402), Apr 18, 2008: STRUCTURE. CORRODED. PDX C4 CHECK ZONE 144 SUBFLOOR IS CORRODED AT Y546 AND Y35.5L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED .003 MATERIAL FROM .045 ORIGINAL THICKNESS, .042 MATERI
- [SDR QXEA200800400](https://openairdocs.org/sdr/QXEA200800400), Apr 18, 2008: STRUCTURE. CORRODED. PDX C4 CHECK ZONE 144 SUBFLOOR TOP SURFACE IS CORRODED AT Y580-X581 AND Y24L-Y26L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED .002 MATERIAL FROM ORIGINAL THICKNE
- [SDR QXEA200800398](https://openairdocs.org/sdr/QXEA200800398), Apr 18, 2008: FLOORBEAM. CORRODED. PDX C4 CHECK ZONE 144 AFT FLOOR SUPPORT ANGLE AT STA X600 IS CORRODED AT Y29.5R. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS IAW -8 200 PT 1, 51-00-04, HI .0
- [SDR QXEA200800389](https://openairdocs.org/sdr/QXEA200800389), Apr 16, 2008: UNKNOWN. ODOR. SEA - LAVATORY SMOKE DETECTOR WENT OFF FOR THE SECOND TIME. NO SMOKE OR FIRE NOTED. ON THE FLIGHT DECK THOUGH NOTICED A ODOR IN THE AIR AND BOTH PILOTS SENSED A
- [SDR QXEA200800388](https://openairdocs.org/sdr/QXEA200800388), Apr 16, 2008: SMOKE DETECTOR. MALFUNCTIONED. SEA - LAVATORY SMOKE DETECTOR WENT OFF. NO EVIDENCE OF SMOKE, OR FIRE. MAINTENANCE COMPLIED WITH A OPERATIONAL CHECKS OF THE SYSTEM AND FOUND NO DEFECTS. AIRCRA
- [SDR QXEA200800377](https://openairdocs.org/sdr/QXEA200800377), Apr 12, 2008: DOOR. OPEN. SEA - AFTER TAKEOFF, TRIED TO RAISE THE GEAR AND THE GEAR DOOR LIGHTS WERE STILL ILLUMINATED ALONG WITH THE LEFT AND RIGHT UNSAFE LIGHTS. A LOUD FLAPPING SOUND 
- [SDR QXEA20080339](https://openairdocs.org/sdr/QXEA20080339), Mar 29, 2008: CONNECTOR. DAMAGED. SEA - FLIGHT 2101 - LAVATORY SMOKE DETECTOR GOES OFF INTERMITTENTLY IN FLIGHT. MAINTENANCE PLACED ON MEL 26-4. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED ON 3/31
- [SDR QXEA200800298](https://openairdocs.org/sdr/QXEA200800298), Mar 16, 2008: ACM. MALFUNCTIONED. PDX - FLIGHT 2193, ON APPROACH THE LAVATORY SMOKE DETECTOR WENT OFF TWICE. BOTH TIMES THE FLIGHT ATTENDANT REPORTED NO INDICATIONS OF SMOKE. AIR WAS SMOOTH AND 
- [SDR QXEA200800279](https://openairdocs.org/sdr/QXEA200800279), Mar 9, 2008: SMOKE DETECTOR. FALSE ACTIVATION. YKM - FLIGHT 2002 - LAVATORY SMOKE DETECTOR WENT OFF WITH NO SMOKE DETECTED. MAINTENANCE PLACED THE SYSTEM ON MEL 26-4. AIRCRAFT RETURNED TO SERVICE. CLEARED BY
- [SDR QXEA200800229](https://openairdocs.org/sdr/QXEA200800229), Feb 26, 2008: INDICATOR. SMOKE. PDX - FLIGHT 2058 - WHEN APPLYING ELECTRICAL POWER TO THE IRU AND FMS. SMOKE NOTICED FROM THE AREA BETWEEN THOSE UNITS AND THE RADAR INDICATOR. MAINTENANCE POWE
- [SDR QXEA200800206](https://openairdocs.org/sdr/QXEA200800206), Feb 18, 2008: ALTIMETER. MALFUNCTIONED. SEA - FLIGHT 2027, RETURNED TO THE FIELD FOR THE CAPTAIN'S ALTIMETER FLAGGING AT 420 FEET. MAINTENANCE REPLACED THE NR 1 ALTIMETER. OPS CHECKS GOOD. AIRCRAFT RE
- [SDR QXEA200800179](https://openairdocs.org/sdr/QXEA200800179), Feb 11, 2008: SERVO. JAMMED. PDX - FLIGHT 2193 (OTH-PDX) ON APPROACH WITH THE AUTOPILOT ON, EXPERIENCED A UNCOMMANDED ROLL TO THE LEFT. AUTOPILOT WAS TURNED OFF AND THE WHEEL APPEARED TO BE
- [SDR QXEA200702031](https://openairdocs.org/sdr/QXEA200702031), Dec 25, 2007: DRAIN MAST. FROZEN. RDM - FLIGHT 2191 - ON SHUTDOWN AT THE GATE, RAMP NOTICED SMOKE FROM THE TOP OF NR 1 ENGINE. MAINTENANCE CHECKED NACELLE AND ENGINE AREA AND FOUND NO SOURCE FOR
- [SDR QXEA200701771](https://openairdocs.org/sdr/QXEA200701771), Dec 1, 2007: LAMP. INOPERATIVE. PDX - FLIGHT 2011 - HEATER LIGHT ON LEFT ENGINE INTAKE BYPASS DOOR DOES NOT TEST. RETURNED TO THE GATE. MAINTENANCE REPLACED THE LAMP. OPERATIONAL CHECKS GOOD. 
- [SDR QXEA200701342](https://openairdocs.org/sdr/QXEA200701342), Aug 17, 2007: BLADE. MALFUNCTIONED. BOI FLIGHT NR 2115, SPARKS OBSERVICED FROM NR 2 PROP ON CLIMB-OUT. REPLACED BLADES NR 1 AND NR 4 ON NR 2 PROP PER TC 9611003. S/N 9801028-23, TSN 89.53, CSN 134
- [SDR QXEA200700776](https://openairdocs.org/sdr/QXEA200700776), May 9, 2007: RELAY. MALFUNCTIONED. SEA FLIGHT NR 2019 ON TAKEOFF, AUTOFEATHER FAILED TO ARM. REPLACED NR 1 POWER LEVER LIMIT SWITCH 6121-S7, ADJUSTED SWITCH. REPLACED RELAY 6121-K15. OPERATIONAL 
- [SDR QXEA200700641](https://openairdocs.org/sdr/QXEA200700641), Apr 17, 2007: AUTOFEATHER SYS. NONE. SEA FLIGHT NR 2110 ON TAKEOFF, AUTOFEATHER SWITCH LIGHT DAR. TAKEOFF ABORTED AT 60KTS. MAINTENANCE PERFORMED AUTOFEATHER SYSTEM AND POWER UPTRIM TEST IAW -8200 
- [SDR QXEA200700395](https://openairdocs.org/sdr/QXEA200700395), Mar 19, 2007: UNKNOWN. ODOR. SEA FLIGHT NR 2017, BURNING RUBBER ODOR FROM MAPCO, GALLEY EQUIPMENT INOP. MAINTENANCE PLACED MAPCO ON MEL.
- [SDR QXEA200700127](https://openairdocs.org/sdr/QXEA200700127), Feb 3, 2007: TRANSDUCER. MALFUNCTIONED. PDX FLIGHT NR 2200, IMMEDIATELY AFTER TAKEOFF, NR 1 STALL WARNING CAUTION LIGHT ILLUMINATED STALL WARNING INOP. MAINTENANCE REPLACED THE NR 1 STALL WARNING TRAN
- [SDR QXEA200603228](https://openairdocs.org/sdr/QXEA200603228), Dec 23, 2006: LATCH. UNSECURE. SEA - ON FLIGHT 2224, RETURNED TO GATE. ENGINE COWL NR 2 LATCH OPEN. MAINTENANCE SECURED LATCH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

All 223: https://openairdocs.org/deregistered/N355PH-2013-01-24/reports.md

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