# Service difficulty reports: N196WQ, cancelled Nov 14, 2018

A list on [N196WQ, cancelled Nov 14, 2018](https://openairdocs.org/deregistered/N196WQ-2018-11-14.md).

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

Page 1 of 2 · 54 reports

- [SDR R61A201406230783](https://openairdocs.org/sdr/R61A201406230783.md): Tire · failed · Jun 23, 2014 · N196WQ · Bombdr DHC8402 · Tire
  > 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 DEBRIS WAS FOUND ON RUNWAY. CREW LOWERED GEAR EARLY AND WAS ADVISED THAT LT INBD MAIN TIRE HAD BLOWN O
- [SDR R61A201403110362](https://openairdocs.org/sdr/R61A201403110362.md): Door · unsecure · Mar 11, 2014 · N196WQ · Bombdr DHC8402 · Cargo/Baggage Doors
  > 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. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. AFTER LANDING, MAINTENANCE FOUND
- [SDR R61A201311101120](https://openairdocs.org/sdr/R61A201311101120.md): Door · out of adjust · Nov 10, 2013 · N196WQ · Bombdr DHC8402 · Emergency Exits
  > 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 INTERMITTENT WITH PRESSURIZATION FLUCUATIONS. CREW ELECTED TO RETURN TO DEPARTURE, DID NOT DECLAR
- [SDR R61A201310201039](https://openairdocs.org/sdr/R61A201310201039.md): Handle · unsecure · Oct 20, 2013 · N196WQ · Bombdr DHC8402 · Cargo/Baggage Doors
  > CREW RECEIVED A FUSELAGE MASTER WARNING LIGHT. CREW FOLLOWED QRH, DID NOT DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND AFT CARGO DOOR HANDLE POPPED OUT AND NOT SECURE. MAINTENANCE PERFORMED OPS CHECKED OF AFT CARGO DOOR
- [SDR R61A201310151010](https://openairdocs.org/sdr/R61A201310151010.md): Psu · dislodged · Oct 15, 2013 · N196WQ · Bombdr DHC8402 · Emergency Equipment
  > 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.md): Handle · unsecure · Sep 22, 2013 · N196WQ · Bombdr DHC8402 · Cargo/Baggage Doors
  > 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 DECLARED AND LANDED WITHOUT INCIDENT. ON ARRIVAL, MX FOUND DOOR HANDLE WAS IN THE OUT POSITION. MX
- [SDR R61A201308190767](https://openairdocs.org/sdr/R61A201308190767.md): Skin · dented · Aug 19, 2013 · N196WQ · Bombdr DHC8402 · Fuselage Main, Plate/Skin
  > 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.md): Attach Fitting · corroded · Aug 17, 2013 · N196WQ · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > 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.md): Beam · corroded · Aug 11, 2013 · N196WQ · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > 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 51-42-05,51-40-07, AND DWG 85329511.
- [SDR R61A201308300812](https://openairdocs.org/sdr/R61A201308300812.md): Seat Track · corroded · Aug 10, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Aug 7, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Access Panel · corroded · Aug 2, 2013 · N196WQ · Bombdr DHC8402 · Wing, Plate/Skin
  > 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.md): Duct · corroded · Jul 30, 2013 · N196WQ · Bombdr DHC8402 · Pneumatic Distribution System
  > 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.md): Access Panel · corroded · Jul 29, 2013 · N196WQ · Bombdr DHC8402 · Wing, Plate/Skin
  > 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.md): Access Panel · corroded · Jul 29, 2013 · N196WQ · Bombdr DHC8402 · Wing, Plate/Skin
  > 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.md): Seat Track · corroded · Jul 27, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 27, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 27, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 SERVICE.
- [SDR R61A201308300808](https://openairdocs.org/sdr/R61A201308300808.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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; 51-40-15;51-40-07; AND 51-42-15. ACFT IS STILL CURRENTLY OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
- [SDR R61A201307260771](https://openairdocs.org/sdr/R61A201307260771.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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 & 51-40-15.
- [SDR R61A201308180738](https://openairdocs.org/sdr/R61A201308180738.md): Attach Angle · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > 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 51-40-07 & 51-42-05.
- [SDR R61A201307260710](https://openairdocs.org/sdr/R61A201307260710.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 26, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 25, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 25, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 25, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Jul 25, 2013 · N196WQ · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Fitting · corroded · Jul 23, 2013 · N196WQ · Bombdr DHC8402 · Fuselage Main, Structure
  > 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 52-23-00, SHEET 4, FIG 504 RT.
- [SDR NSVA20120209446](https://openairdocs.org/sdr/NSVA20120209446.md): Handle · out of position · Feb 9, 2012 · N196WQ · Bombdr DHC8402 · Cargo/Baggage Doors
  > 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 HANDLE WAS POPPED OUT.
- [SDR NSVA2011255](https://openairdocs.org/sdr/NSVA2011255.md): Cable Assy · bent · Oct 7, 2011 · N196WQ · Bombdr DHC8402 · Landing Gear Retraction/Extension System
  > 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 EXTENSION FOR THE LANDING GEAR SYSTEM. TC32-000-0C2 IS THE REPEAT INSPECTION REQUIRED BY AD 2011-1
- [SDR NSVA2011254](https://openairdocs.org/sdr/NSVA2011254.md): Cable · bent · Oct 7, 2011 · N196WQ · Bombdr DHC8402 · Landing Gear Retraction/Extension System
  > 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 FORKEND/BARREL SPRING ASSY. TC 32-000-0C2 IS THE REPEAT INSPECTION REQUIRED BY AD 2011-15-09.
- [SDR NSVA2011163](https://openairdocs.org/sdr/NSVA2011163.md): Door · unsecure · Jul 20, 2011 · N196WQ · Bombdr DHC8402 · Cargo/Baggage Doors
  > 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 GOOD. WARNING LIGHT WENT OUT WHEN DOOR SECURED.
- [SDR NSVA2011114](https://openairdocs.org/sdr/NSVA2011114.md): Proximity Sensor · malfunctioned · May 21, 2011 · N196WQ · Bombdr DHC8402 · Landing Gear Position and Warning
  > 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 32-61-06. ALSO REPLACED LT MLG NR 2 DOWNLOCK PROXIMITY SENSOR IAW Q400 AMM 32-61-06. PERFORMED OPERATI
- [SDR NSVA2011119](https://openairdocs.org/sdr/NSVA2011119.md): Unknown · malfunctioned · May 20, 2011 · N196WQ · Bombdr DHC8402 · Engine EGT/TIT Indicating System
  > 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 TASK 73-20-00-810-006 SECTION A UP TO AND INCLUDING STEP 3, NO MAJOR ITT DIFFERENCE WAS NOTED DURING
- [SDR NSVA2011097](https://openairdocs.org/sdr/NSVA2011097.md): Unknown · odor · Apr 23, 2011 · N196WQ · Bombdr DHC8402 · Air Distribution System
  > 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 THERE WAS AN UNKNOWN SMELL THAT DID NOT SEEM TO BE CAUSED BY SOMETHING BURNING. AS A PRECAUTION, CREW
- [SDR NSVA2010194](https://openairdocs.org/sdr/NSVA2010194.md): Handle · unsecure · Oct 22, 2010 · N196WQ · Bombdr DHC8402 · Cargo/Baggage Doors
  > CARGO LIGHT ILLUMINATED DURING FLIGHT. THERE WAS NO LOSS OF PRESSURIZATION. CREW DESCENDED BELOW FL100 AS A PRECAUTION AND LANDED IN CLE WITHOUT FURTHER COMPLICATIONS. CAPTAIN INSTRUCTED CLE GROUND PERSONNEL NOT TO TOUCH THE CARGO DOOR UNTIL HE VISUALLY INS
- [SDR NSVA2010193](https://openairdocs.org/sdr/NSVA2010193.md): Proximity Sensor · out of adjust · Oct 21, 2010 · N196WQ · Bombdr DHC8402 · Door Warning System
  > AFT BAGGAGE DOOR LIGHT ILLUMINATED IN FLIGHT, RETURNED TO FIELD. RE-ADJUSTED AFT BAG DOOR PROX SENSOR.
- [SDR NSVA2010192](https://openairdocs.org/sdr/NSVA2010192.md): Door · unsecure · Oct 20, 2010 · N196WQ · Bombdr DHC8402 · Cargo/Baggage Doors
  > 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.md): Handle · unsecure · Aug 31, 2010 · N196WQ · Bombdr DHC8402 · Doors
  > DURING CRUISE, CREW NOTICED "FUSELAGE DOOR" INDICATION. THERE WAS NO INDICATION OF PRESSURIZATION LOSS, BUT CREW ELECTED TO DIVERT TO ALB AS A PRECAUTION. MECHANIC VERIFIED THAT THE DOOR HANDLE WAS POPPED OUT ANT THE INDICATION WENT AWAY ONCE HANDLE WAS SECU
- [SDR NSVA2010142](https://openairdocs.org/sdr/NSVA2010142.md): Warning System · malfunctioned · Aug 28, 2010 · N196WQ · Bombdr DHC8402 · Pneumatic Indicating System
  > 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 AND REQUESTED TO GO BACK IN SEQUENCE.
- [SDR NSVA2010015](https://openairdocs.org/sdr/NSVA2010015.md): Lock · engaged · Jan 20, 2010 · N196WQ · Bombdr DHC8402 · Landing Gear Retraction/Extension System
  > 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 THE NOSE GEAR GROUND LOCK WAS STILL ENGAGED. THE NOSE GEAR GROUND LOCK WAS DISENGAGED AND THE AIR
- [SDR NSVA2009016](https://openairdocs.org/sdr/NSVA2009016.md): Transducer · failed · Apr 4, 2009 · N196WQ · Bombdr DHC8402 · Engine Oil Pressure
  > 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 PRESSURE TRANSDUCER IAW AMM 79-31-01-000-801 AND 79-31-01-400-801 FOUND OPERATIONAL CHECKS GOOD, NO LEA
- [SDR NSVA2009014](https://openairdocs.org/sdr/NSVA2009014.md): Connector · dirty · Apr 3, 2009 · N196WQ · Bombdr DHC8402 · Turbine Engine System Wiring
  > 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 CONNECTOR AND RE-CONNECTED IAW AMM 70-00-15. OPS CHECK GOOD IAW AMM.
- [SDR NSVA2009004](https://openairdocs.org/sdr/NSVA2009004.md): Sensor · malfunctioned · Jan 23, 2009 · N196WQ · Bombdr DHC8402 · Door Warning System
  > FORWARD EMERGENCY EXIT LIGHT ILLUMINATED IN FLIGHT. OPENED DOOR AND INSPECTED SENSOR, CLEANED 7 LUBED SENSOR. OPERATIONAL CHECK OF DOOR CHECKS GOOD. LIGHT IS EXTINGUISHED.

Next page: https://openairdocs.org/deregistered/N196WQ-2018-11-14/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N196WQ' AND deregistration_id = 'N196WQ-2018-11-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N196WQ-2018-11-14/reports

---
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.
