# N350PH: 1997 Dehavilland DHC-8-202, registration cancelled 2009-11-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 3, 2009 - Exported to: Canada - Status when cancelled: Triennial form not returned - 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: 488 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: September 9, 1997 - Certificate issued: March 22, 2004 - Last registry action: March 20, 2007 - Mode S code: A3E61A - Owner when cancelled: [Wells Fargo Bank Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N350PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=350PH - Page: https://openairdocs.org/deregistered/N350PH-2009-11-03 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 Dehavilland DHC-8-202: https://openairdocs.org/model/dehavilland-dhc-8-202.md ## Service difficulty reports (283, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR QXEA2009012600035](https://openairdocs.org/sdr/QXEA2009012600035), Jan 21, 2009: SWITCH. MALFUNCTIONED. SEA - ON TAKEOFF, NR 1 ENG LAGS BEHIND NR 2 DOESN'T ACCELERATE. REPLACED THE SWITCH ROLLER ASSEMBLY. OPS CHECK GOOD. RETURNED TO SERVICE. - [SDR QXEA2009012300032](https://openairdocs.org/sdr/QXEA2009012300032), Jan 19, 2009: SWITCH. CONTAMINATED. SEA - NR 1 ENGINE FAILED TO ACCELERATE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. UPON INSPECTION FOUND MAX AND MIN POSITION ON THE CONDITION LEVERS - [SDR QXEA200800809](https://openairdocs.org/sdr/QXEA200800809), Jul 18, 2008: LAMP. MALFUNCTIONED. PDX-FLIGHT 2096 (PDT-PDX). ON APPROACH THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED ALTERNATE EXTENSION AND RECEIVED 3 GREEN LIGHTS. FLEW BY TOWER TO CONFI - [SDR QXEA200800173](https://openairdocs.org/sdr/QXEA200800173), Jan 30, 2008: STRINGER CLIP. CORRODED. PDX - C5 CHECK - THE STRINGER CLIP AND RIVETS ON STRINGER 23R AT THE FORWARD SIDE OF THE REAR SPAR FRAME X424.124 IS CORRODED. REMOVED CLIP AND INSTALLED NEW CL - [SDR QXEA200800160](https://openairdocs.org/sdr/QXEA200800160), Jan 30, 2008: FITTING. CORRODED. PDX - C5 CHECK - RIGHT MLG RETRACTION ACTUATOR FITTING HAS CORROSION ON FRAME JUST ABOVE TOP BOLT HOLE IN CENTER. REPAIRED IAW DHC8 200 RD8-54-1178, NDTM PT-6 5 - [SDR QXEA200800157](https://openairdocs.org/sdr/QXEA200800157), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - AT APPROXIMATELY STATION X545 TO X549 ON LEFT OUTBOARD SEAT TRACK NR 3 THERE IS LIGHT CORROSION IN THE CENTER OF THE TRACK. REPAIRED IAW DHC8 2 - [SDR QXEA200800220](https://openairdocs.org/sdr/QXEA200800220), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - NR 6 SEAT TRACK FLOORBOARD MOUNT FLANGE (INBOARD) SIDE OF FLANGE APPROXIMATELY STA X565.00 IS CORRODED. REPAIRED IAW DHC 8 200 RD8-53-784, NDTM - [SDR QXEA200800172](https://openairdocs.org/sdr/QXEA200800172), Jan 30, 2008: FRAME. CORRODED. PDX - C5 CHECK - FRAME CASTELLATION AT STATION X333.3 AFT FACE OF FRAME BETWEEN STRINGERS 23L AND 24L HAS SUSPECT CORROSION. REPAIRED IAW DHC8 200 CPM CHAPTER 4 - [SDR QXEA200800171](https://openairdocs.org/sdr/QXEA200800171), Jan 30, 2008: KEELBEAM. CORRODED. PDX - C5 CHECK - SUSPECT CORROSION UNDER BRACKET AT VERTICAL KEEL FRAME APPROXIMATELY STATION 202 X 31P. REPAIRED IAW DHC8 200 CPM CHAPTER 4 STEP 8, NDTM PT-1 5 - [SDR QXEA200800170](https://openairdocs.org/sdr/QXEA200800170), Jan 30, 2008: STRINGER CLIP. CORRODED. PDX - C5 CHECK - FOUND CORROSION ON STRINGER CLIP, STRINGER 23R AT FRAME 387 AFT SIDE. REMOVED AND INSTALLED NEW STRINGER CLIP IAW DHC8 200 SRM 51-40-11. - [SDR QXEA200800169](https://openairdocs.org/sdr/QXEA200800169), Jan 30, 2008: SKIN. GOUGED. PDX - C5 CHECK - RIGHT SIDE OF FUSELAGE EXTERNAL SKIN HAS GOUGE AT BASE OF V-STAB APPROXIMATELY 10 INCHES AFT OF FRAME 5. REPAIRED IAW DHC8 RD8-53-2181 AND NDTM - [SDR QXEA200800168](https://openairdocs.org/sdr/QXEA200800168), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - NR 6 SEAT TRACK OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGE SUSPECT CORROSION FROM STATION X582.00 - 600.00. REPAIRED IAW DHC8 200 RD8-53-4936, ND - [SDR QXEA200800167](https://openairdocs.org/sdr/QXEA200800167), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - NR 6 SEAT TRACK FLOORBOARD SUPPORT MOUNT FLANGE HAS CORRODED NUTPLATE AT STATION X593.00. REPAIRED IAW DHC8 200 RD8-53-784, NDTM PT-6 51-00-01 - [SDR QXEA200800166](https://openairdocs.org/sdr/QXEA200800166), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGES SUSPECTED CORROSION AT STATION X545.00 TO X600.00. REPAIRED IAW DHC8 200 - [SDR QXEA200800165](https://openairdocs.org/sdr/QXEA200800165), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGES SUSPECTED CORROSION AT STATION X582.00. REPAIRED IAW DHC8 200 RD8-53-784, - [SDR QXEA200800164](https://openairdocs.org/sdr/QXEA200800164), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGES SUSPECTED CORROSION AT STATION X545.00. REPAIRED IAW DHC8 200 RD8-53-4936 - [SDR QXEA200800163](https://openairdocs.org/sdr/QXEA200800163), Jan 30, 2008: BRACKET. CHAFED. PDX - C5 CHECK - NR 2 ENGINE COWLING NR 3 BRACKET ON INBOARD SIDE IS CHAFED. REMOVED FIRE SEAL BRACKET FROM LOWER COWL AND INSTALLED NEW FIRE SEAL BRACKET IAW D - [SDR QXEA200800162](https://openairdocs.org/sdr/QXEA200800162), Jan 30, 2008: INTERCOSTAL. CORRODED. PDX - C5 CHECK - SUSPECT CORROSION ON FLOOR PAN INTERCOSTAL AT STR 24P FROM STA X510 TO X531. REPAIRED IAW DHC8 200 SRM 51-20-11 AND 51-20-16. - [SDR QXEA200800161](https://openairdocs.org/sdr/QXEA200800161), Jan 30, 2008: INTERCOSTAL. CORRODED. PDX - C5 CHECK - SUSPECT CORROSION ON AVIONICS BAY INTERCOSTAL INBOARD AND OUTBOARD SIDES OF INTERCOSTAL AT STATION X201.15 AND STR 31P. REPAIRED IAW DHC8 200 C - [SDR QXEA200800159](https://openairdocs.org/sdr/QXEA200800159), Jan 30, 2008: FRAME. CORRODED. PDX - C5 CHECK - LEFT MLG RETRACTION ACTUATOR FITTING HAS CORROSION ON ATTACHMENT FRAME ON LOWER OUTBOARD BOLT HOLE. REPAIRED IAW DHC8 200 RD8-54-1178, NDTM PT- - [SDR QXEA200800158](https://openairdocs.org/sdr/QXEA200800158), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - AT APPROXIMATELY STATION X547 TO X549 ON LEFT INBOARD SEAT TRACK NR 6 THERE IS CORROSION IN THE CENTER OF THE TRACK. REPAIRED IAW DHC8 200 RD8- - [SDR QXEA200800156](https://openairdocs.org/sdr/QXEA200800156), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - AT APPROXIMATELY STATION X532 ON LEFT OUTBOARD SEAT TRACK NR 3 HAS CORROSION ON THE TOP OF THE TRACK. REPAIRED IAW DHC8 200 RD8-53-3644, NDTM P - [SDR QXEA200800155](https://openairdocs.org/sdr/QXEA200800155), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - AT APPROXIMATELY STATION X504 ON THE LEFT INBOARD SEAT TRACK NR 5 THERE IS CORROSION IN THE CENTER OF THE TRACK. REPAIRED IAW DHC8 200 RD8-53-3 - [SDR QXEA200800154](https://openairdocs.org/sdr/QXEA200800154), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C4 CHECK - AT APPROXIMATELY STATION X488 THE LEFT OUTBOARD SEAT TRACK NR 2 HAS CORROSION ON TOP OF TRACK. REPAIRED IAW DHC8 200 RD8-53-1342, NDTM PT-6 51- - [SDR QXEA200800153](https://openairdocs.org/sdr/QXEA200800153), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - AT APPROXIMATELY STATION X468 THE LEFT OUTBOARD SEAT TRACK NR 2 HAS A GOUGE ON THE EDGE OF THE CLAW ON TOP OF TRACK. REPAIRED IAW DHC8 200 RD8- - [SDR QXEA200800152](https://openairdocs.org/sdr/QXEA200800152), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - AT APPROXIMATELY STATION X455 LEFT OUTBOARD SEAT TRACK NR 2 HAS CORROSION ON TOP OF TRACK. REPAIRED IAW DHC8 200 RD8-53-1342, NDTM PT-6 51-00-0 - [SDR QXEA200800151](https://openairdocs.org/sdr/QXEA200800151), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - AT APPROXIMATELY STA X350 TO X356 LEFT OUTBOARD SEAT TRACK NR 1 HAS GOUGES ON THE TOP AT THE INBOARD EDGE. REPAIRED IAW DHC8 200 RD8-53-1342, N - [SDR QXEA200800150](https://openairdocs.org/sdr/QXEA200800150), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - AT APPROXIMATELY STA X265 THE LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP OF TRACK. REPAIRED IAW DHC 8 200 RD8-53-1342, NDTM PT-6 51-00- - [SDR QXEA200800192](https://openairdocs.org/sdr/QXEA200800192), Jan 30, 2008: FLAP TRACK. DAMAGED. PDX - C5 CHECK - THERE IS ONE DIVOT ON THE UPPER SIDE OF THE OUTBOARD LOWER FLANGE OF THE RIGHT NR 4 FLAP TRACK. REPAIRED IAW DHC8 200 RD8-57-988, NDTM PT-6 51- - [SDR QXEA200800182](https://openairdocs.org/sdr/QXEA200800182), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - SEAT TRACK NR 10 HAS CORROSION AT STA Y265. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW DHC 8 200 SRM 51-40-11, 51-40-00. - [SDR QXEA200800191](https://openairdocs.org/sdr/QXEA200800191), Jan 30, 2008: MOUNT. DAMAGED. PDX - C5 CHECK - THE OUTBOARD STATIC WICK MOUNT PAD APPEARS TO HAVE LIGHTNING STRIKE DAMAGE ON THE RIGHT AILERON. REMOVED AILERON TRAILING EDGE AND INSTALLED A - [SDR QXEA200800190](https://openairdocs.org/sdr/QXEA200800190), Jan 30, 2008: SKIN. DAMAGED. PDX - C5 CHECK - LEFT AILERON OUTBOARD TRAILING EDGE JUST OUTBOARD OF STATIC WICK APPEARS TO BE A LIGHTING EXIT POINT. REMOVED TRAILING EDGE AND INSTALLED NEW T - [SDR QXEA200800189](https://openairdocs.org/sdr/QXEA200800189), Jan 30, 2008: FLAP TRACK. CORRODED. PDX - C5 CHECK - LEFT NR 5 FLAP TRACK HAS PITTING ON THE LOWER SURFACE OF THE UPPER INBOARD FLANGE AT THE ROLLERS ZERO DEGREE POSITION. REPAIRED IAW DHC 8 200 R - [SDR QXEA200800188](https://openairdocs.org/sdr/QXEA200800188), Jan 30, 2008: FLAP TRACK. CORRODED. PDX - C5 CHECK - LEFT NR 5 FLAP TRACK HAS PITTING ON UPPER SURFACE OF THE LOWER OUTBOARD FLANGE AT THE ROLLERS ZERO DEGREE POSITION. REPAIRED IAW DHC 8 200 RD8- - [SDR QXEA200800187](https://openairdocs.org/sdr/QXEA200800187), Jan 30, 2008: MOUNT. LOOSE. PDX - C5 CHECK - THE BOTTOM RIVETS ON THE AILERON TRIM ACTUATOR HINGE ARM MOUNTING PLATE ARE LOOSE AND WORKING. REMOVED AND REPLACED RIVET AT AILERON TRIM ACTUA - [SDR QXEA200800186](https://openairdocs.org/sdr/QXEA200800186), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGE SUSPECTED CORROSION AT STATION X565.00. REPAIRED IAW DHC 8 200 RD8-53-784, - [SDR QXEA200800185](https://openairdocs.org/sdr/QXEA200800185), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - NR 6 SEAT TRACK INBOARD FLOORBOARD MOUNT FLANGE, SUSPECTED CORROSION FROM STA X545.00 - X600.00. REPAIRED IAW DHC 8 200 RD8-53-784, NDTM PT-6 5 - [SDR QXEA200800184](https://openairdocs.org/sdr/QXEA200800184), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - NR 6 SEAT TRACK FLOORBOARD MOUNT FLANGE (INBOARD) SIDE OF FLANGE APPROXIMATELY STATION X582.00 IS CORRODED. REPAIRED IAW DHC 8 200 RD 8-53-784, - [SDR QXEA200800183](https://openairdocs.org/sdr/QXEA200800183), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - SEAT TRACK NR 7 HAS CORROSION ON THE TOP BETWEEN STA Y213 TO Y240. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW DHC 8 200 SRM 51-40-11, AND R - [SDR QXEA200800181](https://openairdocs.org/sdr/QXEA200800181), Jan 30, 2008: SEAT TRACK. CORRODED. PDX - C5 CHECK - AT APPROXIMATELY STATION X264 THE LEFT INBOARD SEAT TRACK NR 4 HAS CORROSION ON TOP OF TRACK. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW DH - [SDR QXEA200702035](https://openairdocs.org/sdr/QXEA200702035), Dec 26, 2007: TRANSDUCER. MALFUNCTIONED. PDX - FLIGHT 2094 - LEFT DE-ICE PRESSURE GAUGE SHOWS GREATER THEN 30 PSI. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 30-8B. AIRCRAFT RETURNED TO - [SDR QXEA200701718](https://openairdocs.org/sdr/QXEA200701718), Nov 12, 2007: ACTUATOR. MALFUNCTIONED. PDX FLIGHT NR 2119, NR 2 ENGINE BYPASS DOOR DOES NOT INDICATE OPEN (LIGHT TEST OK) FROM CRUISE (FL230/-20'C) TO PARKING (+10"C). REPAIRED CHAFFED WIRES AND REPL - [SDR QXEA200701275](https://openairdocs.org/sdr/QXEA200701275), Aug 10, 2007: WARNING LIGHT. NONE. PDX FLIGHT NR 2184 ECU MANUAL CAUTION LIGHT. MAINTENANCE CYCLED BETA LOCKOUT CIRCUIT BREAKER. MANUAL LIGHT EXTINGUISHED. NO PARTS REPLACED. AIRCRAFT RETURNED TO - [SDR QXEA200701211](https://openairdocs.org/sdr/QXEA200701211), Jul 21, 2007: UNKNOWN. UNKNOWN. PSC - DURING INITIAL CLIMB NR 1 AC GENERATOR CAUTION ILLUMINATED. FOLLOWING THE CHECKLIST, THE LIGHT EXTINGUSHED. 90 SECONDS LATER, THE LIGHT RE-ILLUMINATED. A - [SDR QXEA200700778](https://openairdocs.org/sdr/QXEA200700778), May 11, 2007: INDICATOR. MALFUNCTIONED. IDA FLIGHT NR 2165, AFTER TURNING ON ALL ELECTRONICS IN THE FLIGHT DECK THERE WAS A SLIGHT ELECTRICAL ODOR AFTER ONE MINUTE IT WAS VERY STRONG AND REACHED BACK - [SDR QXEA200700388](https://openairdocs.org/sdr/QXEA200700388), Feb 28, 2007: UNKNOWN. UNKNOWN. SEA FLIGHT NR 2077 INFLIGHT, NR 2 SPU AUX POWER CAUTION LIGHT ILLUMINATED RAN APPROPRIATE CHECKLIST NO OTHER CAUTION LIGHTS AT THE TIME. MAINTENANCE GROUND RAN - [SDR QXEA200700124](https://openairdocs.org/sdr/QXEA200700124), Feb 3, 2007: BRAKE ASSY. VIBRATION. SEA FLIGHT NR 2010, VIBRATION COMING FROM LEFT SIDE BRAKES. MAINTENANCE REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. BLED AND LEAK CHECKED BRAKES. OPERATIONAL CHECK - [SDR QXEA200602688](https://openairdocs.org/sdr/QXEA200602688), Oct 5, 2006: THRESHOLD. CORRODED. BAGGAGE COMPARTMENT THRESHOLD PLATE SUPPORT ANGLE ON VERTICAL WEB AT STA X600 LBL30.0 HAS CORROSION ON BOTH TOP AND BOTTOM SURFACE. REPAIRED IAW SRM 51-40-11. - [SDR QXEA200602674](https://openairdocs.org/sdr/QXEA200602674), Oct 1, 2006: SKIN. DAMAGED. C4 YYC - RIGHT FORWARD FUSELAGE EXTEROIR SKIN AT STATION 222.7 AND STRINGER 26 HAS NICKS ON SKIN. REPAIRED IAW RD8-53-5384 AND SRM 51-20-51. - [SDR QXEA200602673](https://openairdocs.org/sdr/QXEA200602673), Oct 1, 2006: SKIN. GOUGED. C4 YYC - RIGHT FORWARD FUSELAGE EXTEROIR SKIN AT STATION 222.7 AND STRINGER 27 SKIN IS GOUGED. REPAIRED IAW RD8-53-5384 AND SRM 51-20-51. All 283: https://openairdocs.org/deregistered/N350PH-2009-11-03/reports.md ## Other aircraft with N350PH - [Registered now](https://openairdocs.org/aircraft/N350PH): Bombardier BD-100-1A10, S/N 20571, built 2015 --- 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.