# N196WQ: 2008 Bombardier DHC-8-402, registration cancelled 2018-11-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 14, 2018
- Exported to: Canada
- 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: 4196
- Year built: 2008
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 11, 2008
- Certificate issued: July 16, 2015
- Last registry action: June 12, 2018
- Mode S code: A18078
- Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%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/N196WQ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=196WQ
- Page: https://openairdocs.org/deregistered/N196WQ-2018-11-14

From the FAA registry file of November 3, 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 (54, newest 50)

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

- [SDR R61A201406230783](https://openairdocs.org/sdr/R61A201406230783), Jun 23, 2014: TIRE. FAILED. CREW FELT A VIBRATION AND NOTICED SMALL BLACK OBJECT FLY IN FRONT OF ACFT. ASKED TOWER FOR RUNWAY INSPECTION FOR TIRE DEBRIS AND WAS ADVISED THAT EXTENSIVE DEBR
- [SDR R61A201403110362](https://openairdocs.org/sdr/R61A201403110362), Mar 11, 2014: DOOR. UNSECURE. FLYING, CREW RECEIVED AN AFT CARGO DOOR OPEN LIGHT AND LEVELED OFF AT 11,000 FT. CREW ELECTED TO RETURN TO DEPARTURE AND DURING DECENT CABIN LOST PRESSURIZATION
- [SDR R61A201311101120](https://openairdocs.org/sdr/R61A201311101120), Nov 10, 2013: DOOR. OUT OF ADJUST. CREW REPORTED THAT THE ACFT WOULD NOT PRESSURIZE. CREW RAN QRH AND WENT TO MANUAL MODE THEN AUTO MODE WITH SOME POSITIVE RESULTS. CONTROL AND INDICATION BECAME 
- [SDR R61A201310201039](https://openairdocs.org/sdr/R61A201310201039), Oct 20, 2013: HANDLE. UNSECURE. CREW RECEIVED A FUSELAGE MASTER WARNING LIGHT. CREW FOLLOWED QRH, DID NOT DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND AFT 
- [SDR R61A201310151010](https://openairdocs.org/sdr/R61A201310151010), Oct 15, 2013: PSU. DISLODGED. CREW REPORTED THAT THE PASSENGER SERVICE UNIT OVER SEATS 20 C & D FELL OUT. MAINTENANCE SECURED PSU IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201309220905](https://openairdocs.org/sdr/R61A201309220905), Sep 22, 2013: HANDLE. UNSECURE. CREW RECEIVED AN AFT CARGO DOOR WARNING INDICATION. CREW LEVELED OFF AT 10,000 FT, CABIN WAS NOT PRESSURIZING AND CREW ELECTED TO RETURN. AN EMERGENCY WAS NOT D
- [SDR R61A201308190767](https://openairdocs.org/sdr/R61A201308190767), Aug 19, 2013: SKIN. DENTED. MULTIPLE DENTS ON LT SIDE AFT OF ICE SHIELD IAW RD NR 8/4-53-5620. MX FABRICATED PATCH FOR INSTALL OVER SKIN.
- [SDR R61A201308310822](https://openairdocs.org/sdr/R61A201308310822), Aug 17, 2013: ATTACH FITTING. CORRODED. DURING HEAVY CHECK, MX FOUND CORROSION ON FWD FLOOR FITTING ATTACHMENT POINT FOR G3 GALLEY. MX R & R FWD FLOOR FITTING IAW SRM 51-41-00.
- [SDR R61A201308310823](https://openairdocs.org/sdr/R61A201308310823), Aug 11, 2013: BEAM. CORRODED. DURING HEAVY CHECK, MX FOUND CORROSION ON FWD EMERGENCY EXIT DOOR SURROUND LOWER BEAM TO BE OUT OF ALLOWABLE LIMITS. MX R & R LOWER EDGE BEAM IAW SRM 51-42-05,5
- [SDR R61A201308300812](https://openairdocs.org/sdr/R61A201308300812), Aug 10, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK. MX FOUND RT INBD SEAT TRACK, CORRODED BEYOND ALLOWABLE LIMITS. MX R & R SEAT TRACK IAW IAW SRM 51-42-05, 51-40-15, AND 51-40-07.
- [SDR R61A201308070712](https://openairdocs.org/sdr/R61A201308070712), Aug 7, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, FOUND CORROSION OUT OF LIMITS ON RT OTBD SEAT TRACK AT X32.4 TO X71.2. MX R & R SEAT TRACK IAW SRM 51-42-00.
- [SDR R61A201308300817](https://openairdocs.org/sdr/R61A201308300817), Aug 2, 2013: ACCESS PANEL. CORRODED. DURING HEAVY CHECK, FOUND CORRODED COUNTERSINKS ON FUEL PANEL 521BT TO BE OUT OF ALLOWABLE LIMITS. MX R & R FUEL PANEL IAW AMM 57-11-06.
- [SDR R61A201308300816](https://openairdocs.org/sdr/R61A201308300816), Jul 30, 2013: DUCT. CORRODED. DURING HEAVY CHECK. MX FOUND TUBE ON BLEED AIR DUCT CORRODED BEYOND ALLOWABLE LIMITS. MX R & R BLEED AIR DUCT IAW AMM 21-51-66.
- [SDR R61A201308310819](https://openairdocs.org/sdr/R61A201308310819), Jul 29, 2013: ACCESS PANEL. CORRODED. DURING HEAVY CHECK, MX FOUND COROSION IN COUNTERSINKS ON FUEL ACCESS PANEL 623AT TO BE OUT OF ALLOWABLE LIMITS. MX R & R FUEL ACCESS PANEL IAW AMM 57-11-01.
- [SDR R61A201308300815](https://openairdocs.org/sdr/R61A201308300815), Jul 29, 2013: ACCESS PANEL. CORRODED. DURING HEAVY CHECK. MX FOUND CORROSION ON FUEL PANEL 521AT COUNTERSINKS, FOUND TO BE OUT OF ALLOWABLE LIMITS. MX R & R FUEL PANEL IAW AMM 57-11-06.
- [SDR R61A201308300814](https://openairdocs.org/sdr/R61A201308300814), Jul 27, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, MX FOUND LT INBD SEAT TRACK, CORRODED BEYOND ALLOWABLE LIMITS. MX R & R SEAT TRACK IAW SRM 51-40-05, AND 51-40-15.
- [SDR R61A201307270770](https://openairdocs.org/sdr/R61A201307270770), Jul 27, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, FOUND RT INBD SEAT TRACK AT BS 116 TO 176 CORRODED BEYOND LIMITS. MX REPLACED SEAT TRACK IAW SRM 51-40-07, 51-40-15.
- [SDR R61A201307270711](https://openairdocs.org/sdr/R61A201307270711), Jul 27, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, FOUND RT INBD SEAT TRACK AT BS X229.5 TO X569.5 CORRODED BEYOND LIMITS. MX R & R SEAT TRACK IAW SRM 51-40-15, 51-41-00, AND 51-42-05.
- [SDR R61A201308300811](https://openairdocs.org/sdr/R61A201308300811), Jul 26, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK. MX FOUND RT OTBD SEAT TRACK, CORRODED BEYOND ALLOWABLE LIMITS. MX R & R SEAT TRACK IAW SRM 51-40-7 AND 51-40-15.
- [SDR R61A201308300810](https://openairdocs.org/sdr/R61A201308300810), Jul 26, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK. MX FOUND RT OTBD SEAT TRACK, CORRODED BEYOND ALLOWABLE LIMITS. MX R & R SEAT TRACK IAW SRM 51-40-07 AND 51-40-15.
- [SDR R61A201308300809](https://openairdocs.org/sdr/R61A201308300809), Jul 26, 2013: SEAT TRACK. CORRODED. WHILE ACFT WAS IN FOR MX. MX FOUND SEAT TRACK, CORRODED BEYOND ALLOWABLE LIMITS. MX R & R SEAT TRACK IAW SRM 51-42-05; 51-42-15; AND 51-40-15. ACFT OUT OF SERVI
- [SDR R61A201308300808](https://openairdocs.org/sdr/R61A201308300808), Jul 26, 2013: SEAT TRACK. CORRODED. WHILE ACFT WAS IN FOR HEAVY CHECK. MX FOUND RT OTBD SEAT TRACK, PN 85328261-105, CORRODED BEYOND ALLOWABLE LIMITS. MX R & R SEAT TRACK IAW IAW SRM 51-42-05; 51-
- [SDR R61A201307260771](https://openairdocs.org/sdr/R61A201307260771), Jul 26, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, FOUND LT OTBD SEAT TRACK CORRODED. MX R & R SEAT TRACK IAW SRM 51-42-05, 51-40-15, 51-40-07.
- [SDR R61A201307260769](https://openairdocs.org/sdr/R61A201307260769), Jul 26, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, FOUND LT OTBD SEAT TRACK CORRODED OUT OF LIMITS FROM BS 346 TO 377. MX R & R SEAT TRACK IAW SRM 51-40-07, 51-42-45, 51-40-15,51-42-05.
- [SDR R61A201308180740](https://openairdocs.org/sdr/R61A201308180740), Jul 26, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, MX FOUND LT FORWARD INBD SEAT TRACK, BS 61 & 94 CORRODED BEYOND ALLOWABLE LIMITS. MX R & R SEAT TRACK IAW SRM 51-42-05 & 51-40-15.
- [SDR R61A201308180739](https://openairdocs.org/sdr/R61A201308180739), Jul 26, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, MX FOUND CORROSION TO BE OUT OF LIMITS ON RT INBD SEAT TRACK LOCATED AT FUSELAGE BS 236 TO 321. MX R & R SEAT TRACK IAW SRM 51-40-07 & 51-40
- [SDR R61A201308180738](https://openairdocs.org/sdr/R61A201308180738), Jul 26, 2013: ATTACH ANGLE. CORRODED. DURING HEAVY CHECK. MX FOUND CORROSION ON SUPPORT ANGLE ON FWD PAX DOOR LOCATED UNDER FORWARD HINGE SHAFT TO BE OUT OF LIMITS. MX R & R SUPPORT ANGLE IAW SRM 51
- [SDR R61A201307260710](https://openairdocs.org/sdr/R61A201307260710), Jul 26, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, FOUND CORROSION ON THE NR 1 LT OTBD SEAT TRACK. MX R & R SEAT TRACK IAW SRM 51-40-01 AND 51-40-15.
- [SDR R61A201307260708](https://openairdocs.org/sdr/R61A201307260708), Jul 26, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, FOUND CORROSION ON THE LT OTBD SEAT TRACK, MX R & R SEAT TRACK IAW SRM 51-40-07 AND 51-40-15.
- [SDR R61A201308180737](https://openairdocs.org/sdr/R61A201308180737), Jul 25, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK. MX RT INBD SEAT TRACK AT FUSELAGE BS -39.00 TO 1.00 CORRODED BEYOND ALLOWABLE LIMITS. MX R & R SEAT TRACK IAW SRM 51-40-07 & 51-40-15.
- [SDR R61A201308180736](https://openairdocs.org/sdr/R61A201308180736), Jul 25, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK. MX FOUND RT INBD SEAT TRACK CORRODED BEYOND ALLOWABLE LIMITS AT FUSELAGE BS 321. MX R & R SEAT TRACK IAW SRM 51-40-07 & 51-40-05.
- [SDR R61A201308180735](https://openairdocs.org/sdr/R61A201308180735), Jul 25, 2013: SEAT TRACK. CORRODED. DURING HEAVY MAINTENCANCE. MX FOUND RT INBD SEAT TRACK CORRODED AND OUT OF LIMITS AT FUSELAGE BS 644. R & R SEAT TRACK IAW SRM 51-40-07 & 51-40-15.
- [SDR R61A201307250709](https://openairdocs.org/sdr/R61A201307250709), Jul 25, 2013: SEAT TRACK. CORRODED. DURING HEAVY CHECK, FOUND RT INBD SEAT TRACK HAS CORROSION AT BS 644. MX R & R SEAT TRACK IAW SRM 51-40-07 AND 51-40-15.
- [SDR R61A201307230768](https://openairdocs.org/sdr/R61A201307230768), Jul 23, 2013: FITTING. CORRODED. DURING HEAVY CHECK, FOUND FWD EMERGENCY DOOR LOWER DOOR BRACKETS ON THRESHOLD SHOWS EVIDENCE OF CORROSION. MX R & R TWO STOP FITTINGS IAW SRM 51-41-00, AND AMM 
- [SDR NSVA20120209446](https://openairdocs.org/sdr/NSVA20120209446), Feb 9, 2012: HANDLE. OUT OF POSITION. FLIGHT 4864 RETURNED TO THE FIELD IS AUS DUE TO THE CARGO DOOR LIGHT ILLUMINATED. NO EMERGENCY WAS DECLARED. THE FLIGHT LANDED SAFELY AND IT WAS FOUND THAT THE 
- [SDR NSVA2011255](https://openairdocs.org/sdr/NSVA2011255), Oct 7, 2011: CABLE ASSY. BENT. WHILE PERFORMING TC32-000-0C2 CABLE FROM CAN MECH TO MLG UNLOCK ACTUATOR IN RT NACELLE IS BENT AT THE SWAGED END. CABLE ASSY IS PART OF THE EMERGENCY ALTERNATE 
- [SDR NSVA2011254](https://openairdocs.org/sdr/NSVA2011254), Oct 7, 2011: CABLE. BENT. WHILE PERFORMING TC 32-000-0C2 CABLE FROM CAM MECH GOING FWD IS BENT WHERE CABLE TURNS INTO ADJUSTABLE TURNBUCKLE. OTHER END OF TURNBUCKLE CONNECTS TO CLEVIS FO
- [SDR NSVA2011163](https://openairdocs.org/sdr/NSVA2011163), Jul 20, 2011: DOOR. UNSECURE. AT ABOUT 70 KTS REAR CARGO DOOR LIGHT ILLUMINATED. NORMAL BREAKING. PERFORMED OPERATIONAL CHECK OF THE AFT CARGO DOOR IAW Q400 AMM 52-31-00-710-801, OPS CHECKED
- [SDR NSVA2011114](https://openairdocs.org/sdr/NSVA2011114), May 21, 2011: PROXIMITY SENSOR. MALFUNCTIONED. LEFT MAIN GEAR UNSAFE LIGHT INTERMITTENTLY COMES ON. GEAR HANDLE INTERMITTENTLY COMES ON AT SAME TIME. REPLACED LT MLG NR 1 DOWNLOCK PROXIMITY SENSOR IAW 32-61-
- [SDR NSVA2011119](https://openairdocs.org/sdr/NSVA2011119), May 20, 2011: UNKNOWN. MALFUNCTIONED. IN CRUISE THE LEFT ITT SHOWED 257 DEG C AND THE RIGHT SHOWED 706 DEG C ALL OTHER INDICATIONS WERE NORMAL AND NO CAUTION LIGHTS. FOLLOWED Q400 FIM 73-20-00 SUB T
- [SDR NSVA2011097](https://openairdocs.org/sdr/NSVA2011097), Apr 23, 2011: UNKNOWN. ODOR. DURING CRUISE CLOSE TO TOD, F/A NOTIFIED FLIGHT CREW THAT THERE WAS A STRANGE SMELL IN THE CABIN. THE FIRST OFFICER INSPECTED THE CABIN AND DETERMINED THAT THER
- [SDR NSVA2010194](https://openairdocs.org/sdr/NSVA2010194), Oct 22, 2010: HANDLE. UNSECURE. CARGO LIGHT ILLUMINATED DURING FLIGHT. THERE WAS NO LOSS OF PRESSURIZATION. CREW DESCENDED BELOW FL100 AS A PRECAUTION AND LANDED IN CLE WITHOUT FURTHER COMPLIC
- [SDR NSVA2010193](https://openairdocs.org/sdr/NSVA2010193), Oct 21, 2010: PROXIMITY SENSOR. OUT OF ADJUST. AFT BAGGAGE DOOR LIGHT ILLUMINATED IN FLIGHT, RETURNED TO FIELD. RE-ADJUSTED AFT BAG DOOR PROX SENSOR.
- [SDR NSVA2010192](https://openairdocs.org/sdr/NSVA2010192), Oct 20, 2010: DOOR. UNSECURE. AFT BAGGAGE DOOR NOT SECURED PROPERLY, LANDED WITH NO FURTHER INCEDENT. PERFORMED OPS CHECK OF AFT BAGGAGE DOOR OPS CHECKED GOOD. NO FAULT FOUND.
- [SDR NSVA2010148](https://openairdocs.org/sdr/NSVA2010148), Aug 31, 2010: HANDLE. UNSECURE. DURING CRUISE, CREW NOTICED "FUSELAGE DOOR" INDICATION. THERE WAS NO INDICATION OF PRESSURIZATION LOSS, BUT CREW ELECTED TO DIVERT TO ALB AS A PRECAUTION. MECHA
- [SDR NSVA2010142](https://openairdocs.org/sdr/NSVA2010142), Aug 28, 2010: WARNING SYSTEM. MALFUNCTIONED. NUMBER 2 BLEED HOT LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAXIED OFF THE RUNWAY, RAN CHECKLIST AND CHECKED WITH MAINTENANCE. ALL INDICATIONS WENT BACK TO NORMAL
- [SDR NSVA2010015](https://openairdocs.org/sdr/NSVA2010015), Jan 20, 2010: LOCK. ENGAGED. THE NOSE LANDING GEAR DID NOT RETRACT UPON SELECTION OF THE LANDING GEAR HANDLE TO THE UP POSITION. THE SUBSEQUENT LANDING GEAR SYSTEM INSPECTION REVEALED THAT 
- [SDR NSVA2009016](https://openairdocs.org/sdr/NSVA2009016), Apr 4, 2009: TRANSDUCER. FAILED. AT 13000 LT ENGINE OIL PRESSURE WAS AT 117 PSI, OIL PRESSURE WAS FLUCTUATION. LT ENGINE SHUTDOWN AND DIVERTED TO ALB. REMOVED AND REPLACED LEFT ENGINE OIL PRESS
- [SDR NSVA2009014](https://openairdocs.org/sdr/NSVA2009014), Apr 3, 2009: CONNECTOR. DIRTY. LEFT ENGINE OIL PRESS AT 178 PSI, ENGINE SHUTDOWN IN FLIGHT, DIVERTED TO KDTV DUE TO OIL PRESSURE. DISCONNECT P55 CONNECTOR OIL PRESS TRANSDUCER, CLEANED CONNEC
- [SDR NSVA2009004](https://openairdocs.org/sdr/NSVA2009004), Jan 23, 2009: SENSOR. MALFUNCTIONED. FORWARD EMERGENCY EXIT LIGHT ILLUMINATED IN FLIGHT. OPENED DOOR AND INSPECTED SENSOR, CLEANED 7 LUBED SENSOR. OPERATIONAL CHECK OF DOOR CHECKS GOOD. LIGHT IS EX

All 54: https://openairdocs.org/deregistered/N196WQ-2018-11-14/reports.md

## 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 20090404010139I](https://openairdocs.org/incident/20090404010139I), Apr 4, 2009: Bombdr DHC8402 (N196WQ), Albany, NY, No damage. (-23) On 04/04/2009, during a re-positioning flight from burlington VT, (kbtv) to newark liberty airport (kewr), flight crew noticed an anomaly with the #1…

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