# N195WQ: 2008 Bombardier DHC-8-402, registration cancelled 2016-11-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 30, 2016 - Exported to: United Kingdom - Status when cancelled: Valid registration - Airframe: [Bombardier DHC-8-402](https://openairdocs.org/model/bombardier-dhc-8-402) (registry code 1390042) - Engine: [Pratt & Whitney Canada PW150A](https://openairdocs.org/engine/pratt-whitney-canada-pw150a) (registry code 52167) - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E00062EN](https://openairdocs.org/tcds/E00062EN) (OpenAirDocs) - Serial number: 4195 - Year built: 2008 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: March 3, 2008 - Certificate issued: June 24, 2015 - Last registry action: June 24, 2015 - Mode S code: A17CC1 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%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/N195WQ - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=195WQ - Page: https://openairdocs.org/deregistered/N195WQ-2016-11-30 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 Bombardier DHC-8-402: https://openairdocs.org/model/bombardier-dhc-8-402.md ## Service difficulty reports (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR R61A201509290697](https://openairdocs.org/sdr/R61A201509290697), Sep 29, 2015: LAMP. INOPERATIVE. CREW REPORTED THAT THE NORMAL F/A EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LAMP IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201509280666](https://openairdocs.org/sdr/R61A201509280666), Sep 28, 2015: POWER SUPPLY. INOPERATIVE. MAINTENANCE REPORTED THAT THE RT FORWARD DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE R & R FOWARD EMERGENCY LIGHT POWER SUPPLY IAW AMM AND OPS CHECKED - [SDR R61A201506120363](https://openairdocs.org/sdr/R61A201506120363), Jun 12, 2015: LAMP. INOPERATIVE. CREW REPORTED THAT THE RT MLG GREEN LIGHT DID NOT ILLUMINATE. ABORTED APPROACH, RAN THE QRH AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE INSP - [SDR R61A201504270265](https://openairdocs.org/sdr/R61A201504270265), Apr 27, 2015: SWITCH. MALFUNCTIONED. CREW REPORTED THAT WITH THE SWITCH OFF AND THE ACFT POWERED DOWN, THE EMERGENCY LIGHTS CAME ON. MAINTENANCE R & R EMERGENCY LIGHT SWITCH ON FORWARD BULKHEAD IAW - [SDR R61A201502260120](https://openairdocs.org/sdr/R61A201502260120), Feb 26, 2015: CHECK VALVE. FAILED. CREW RECEIVED A FUSELAGE DOORS WARNING LIGHT. WHILE RUNNING QRH, CAPTAIN NOTICED CABIN ALTITUDE STARTING TO CLIMB. CREW STARTED DECENT AND RECEIVED CABIN PRESSU - [SDR R61A201502080079](https://openairdocs.org/sdr/R61A201502080079), Feb 8, 2015: RELAY. MALFUNCTIONED. CREW REPORTED THAT THE EMERGENCY LIGHTS WERE STAYING ON WITH THE ACFT POWERED OFF. MAINTENANCE R & R THE K1 AND K2 EMERGENCY LIGHT RELAYS IAW AMM AND OPS CHECKE - [SDR R61A201408291027](https://openairdocs.org/sdr/R61A201408291027), Aug 29, 2014: BATTERY PACK. DISCHARGED. CREW REPORTED THAT THE FLIGHT DECK FLASHLIGHT BATTERY WAS VERY LOW. MAINTENANCE R & R FLIGHT DECK FLASHLIGHT BATTERIES IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201408050961](https://openairdocs.org/sdr/R61A201408050961), Aug 5, 2014: LANDING GEAR. MALFUNCTIONED. CREW REPORTED THAT WHEN THE GEAR WERE RETRACTED, THE RT GEAR AND THE AFT GEAR DOOR DID NOT RETRACT. CREW FOLLOWED QRH AND CYCLED THE GEAR DOWN. DID NOT DECLARE - [SDR R61A201406040721](https://openairdocs.org/sdr/R61A201406040721), Jun 4, 2014: BYPASS VALVE. FAILED. FLYING AT 10,000 FT CREW REPORTED NR 2 OIL TEMP WAS 107. CREW RAN QRH, REDUCED TORQUE AND OIL TEMP ROSE TO 119 WHERE IT REMAINED FOR 10 MINUTES. BECAUSE TEMP WA - [SDR R61A201405290711](https://openairdocs.org/sdr/R61A201405290711), May 29, 2014: WIRE HARNESS. DAMAGED. CREW REPORTED THAT THE LT MLG DOOR REMAINED OPEN AFTER GEAR EXTENSION AND LOST GEAR INDICATION. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. - [SDR R61A201405280702](https://openairdocs.org/sdr/R61A201405280702), May 28, 2014: DOOR. MALFUNCTIONED. CREW REPORTED THAT THE LT GEAR DOOR OPENED AND THE LIGHT CAME ON. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE RAN ENGINES AND PE - [SDR R61A201309040839](https://openairdocs.org/sdr/R61A201309040839), Sep 4, 2013: GLOWSTRIP. DAMAGED. CREW REPORTED THAT THE PHOTO LUMINESCENT STRIP WAS DAMAGED. MX INSTALLED PHOTO LUMINESCENT STRIP IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201309010831](https://openairdocs.org/sdr/R61A201309010831), Sep 1, 2013: BATTERY PACK. DISCHARGED. CREW REPORTED THAT THE FWD CABIN FLASHLIGHT BATTERIES ARE DEAD. MX REPLACED FLASHLIGHT IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201308260801](https://openairdocs.org/sdr/R61A201308260801), Aug 26, 2013: FLAP SYSTEM. MALFUNCTIONED. CREW RECEIVED A FLAP POWER UNIT FAIL MESSAGE AFTER SELECTING FLAPS FROM 5 TO 10. CREW ELECTED TO GO AROUND, ADVISED ATC OF SITUATION AND RAN QRH. CREW CORRECTED - [SDR R61A201307220641](https://openairdocs.org/sdr/R61A201307220641), Jul 22, 2013: RIVET. BROKEN. WHILE OPERATING AND CLOSING MAIN CABIN DOOR THERE WAS A SOUND OF LOOSE MATERIAL SLIDING WITHIN THE DOOR. MX REMOVED THE OUTER PART OF THE MAIN CABIN DOOR AND FO - [SDR R61A201304120410](https://openairdocs.org/sdr/R61A201304120410), Apr 12, 2013: SKIN PANEL. DENTED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED MULTIPLE DENTS JUST AFT OF THE LEFT ICE SHIELD, ABOVE AND BELOW WINDOW BETWEEN STATION X281.0 TO X30 - [SDR R61A201304120409](https://openairdocs.org/sdr/R61A201304120409), Apr 12, 2013: SKIN PANEL. DENTED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED MULTIPLE DENTS JUST AFT OF THE LEFT ICE SHIELD, ABOVE AND BELOW WINDOW BETWEEN STATION X281.0 TO X30 - [SDR R61A201304100386](https://openairdocs.org/sdr/R61A201304100386), Apr 10, 2013: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK - LEVEL 2 CORROSION WAS FOUND ON THE RIGHT INBOARD SEAT RAIL BETWEEN STATION X -39.0 TO X9.50. (AT FWD LAV ATTACH FITTING) - [SDR R61A201301250391](https://openairdocs.org/sdr/R61A201301250391), Jan 25, 2013: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE AFT GALLEY INBOARD SEAT RAIL AT STATION X705 TO X712 & Y-9.250. MAINTENANCE REMOVED & - [SDR R61A201301210423](https://openairdocs.org/sdr/R61A201301210423), Jan 21, 2013: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT RAIL BETWEEN STATIONS X236.0 TO X564.5 MAINTENANCE REMOVED AND REPL - [SDR R61A201301210392](https://openairdocs.org/sdr/R61A201301210392), Jan 21, 2013: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LEFT INBOARD SEAT RAIL BETWEEN STATIONS X564.5 TO X664.5. MAINTENANCE REMOVED AND REPL - [SDR R61A201301210390](https://openairdocs.org/sdr/R61A201301210390), Jan 21, 2013: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT RAIL BETWEEN STATION X94.8 TO X236.0, MAINTENANCE REMOVED AND REPL - [SDR R61A201301210389](https://openairdocs.org/sdr/R61A201301210389), Jan 21, 2013: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RIGHT INBOARD SEAT RAIL BETWEEN STATION X116.0 TO X236.0, MAINTENANCE REMOVED AND REPL - [SDR R61A201301210388](https://openairdocs.org/sdr/R61A201301210388), Jan 21, 2013: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RIGHT INBOARD SEAT RAIL BETWEEN STATION X236.0 & X564.5, MAINTENANCE REMOVED & REPLACE - [SDR R61A201301210387](https://openairdocs.org/sdr/R61A201301210387), Jan 21, 2013: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RIGHT INBOARD SEAT RAIL BETWEEN STATION X614 & X664.5. MAINTENANCE REMOVED & REPLACED - [SDR R61A201301210385](https://openairdocs.org/sdr/R61A201301210385), Jan 21, 2013: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK - LEVEL 2 CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT RAIL IN SEVERAL AREAS BETWEEN FS X236.0 & X564.5. MAINTENANCE REM - [SDR R61A201301160424](https://openairdocs.org/sdr/R61A201301160424), Jan 16, 2013: SKIN PANEL. DENTED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED FUSELAGE SKIN DENTS AT FS X-98.0 TO X-69.4, S-31S TO S-32S. MAINTENANCE PERFORMED A MAJOR REPAIR TO - [SDR R61A201301160411](https://openairdocs.org/sdr/R61A201301160411), Jan 16, 2013: SKIN PANEL. BURNED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED A BURN MARK ON THE SKIN ADJACENT TO THE FORWARD JACKING POINT LOCATED AT STATION X-39.0 AND BETWEEN - [SDR R61A201301160383](https://openairdocs.org/sdr/R61A201301160383), Jan 16, 2013: SKIN PANEL. CRACKED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK - MAINTENANCE FOUND A .5" CRACK/PUNCTURE ON THE AIRSTAIR DOOR INNER SKIN AT THE DOOR SUPPORT CABLE BRACKET, FORWARD INBOAR - [SDR NSVA2011409](https://openairdocs.org/sdr/NSVA2011409), Jan 25, 2012: PRESSURE GAUGE. ERRATIC. AFTER TAKEOFF NR 2 ENGINE OIL PRESSURE GAUGE BECAME IRRATIC. CA DECLARED EMERGENCY AND RETURNED TO THE FIELD IN IAH. - [SDR NSVA2011152](https://openairdocs.org/sdr/NSVA2011152), Jul 5, 2011: BRACKET. UNSECURE. DURING DESCENT THE FWD CARGO DOOR LIGHT ILLUMINATED. THE CREW FOLLOWED THE QRH AND CONTINUED TO THE NEAREST SUITABLE AIRPORT WHICH IS ALSO THE DESTINATION. THE - [SDR NSVA2011128](https://openairdocs.org/sdr/NSVA2011128), Jun 2, 2011: SEQUENCE VALVE. FAULTY. UPON GEAR RETRACTION NOSE AND RIGHT MAIN RETRACTED, LEFT MAIN DOOR CLOSED, LEFT RED AND GEAR HANDLE ILLUMINATED, THEN LEFT GEAR DOOR OPENED AND LEFT GEAR RETRAC - [SDR NSVA2011027](https://openairdocs.org/sdr/NSVA2011027), Feb 15, 2011: SELECTOR VALVE. FAULTY. PILOT LOGBOOK ENTRY "LANDING GEAR FAILED TO RETRACT ON TAKEOFF. ONLY THE RED UNSAFE LIGHTS REMAINED ON, INCLUDING HANDLE. THREE GREEN WORK FINE. TWO ATTEMPTS TO - [SDR NSVA2010213](https://openairdocs.org/sdr/NSVA2010213), Nov 20, 2010: DOOR. UNSECURE. RETURNED TO FIELD DUE TO THE AFT CARGO DOOR LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. SECURED DOOR. - [SDR NSV2008F00019](https://openairdocs.org/sdr/NSV2008F00019), Aug 7, 2008: RELIEF VALVE. LEAKING. NR 1 HYD FAILURE IN FLIGHT, NO FLUID IN NR 1 RESERVOIR. NO PRESSURE IN NR 1 SYSTEM. RAN QRH, LANDED FLAPS 0 AND EMERGENCY BRAKE. SKYDORL LEAKING FROM LT SIDE OF ## 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 20090516006509I](https://openairdocs.org/incident/20090516006509I), May 16, 2009: Bombdr DHC8402 (N195WQ), Boston, MA, No damage. (-23) On two mile final requested be met by medical personnel due to possible injury to a flight attendant. F/a was taken to hospital. Injury determined to be… --- 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.