# Service difficulty reports: N809WP, cancelled Oct 25, 2012

A list on [N809WP, cancelled Oct 25, 2012](https://openairdocs.org/deregistered/N809WP-2012-10-25.md).

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

- [SDR KPVA2012FA0000156](https://openairdocs.org/sdr/KPVA2012FA0000156.md): Flap System · stuck · Mar 15, 2012 · N809WP · Dhav DHC8103 · Trailing Edge Flap Control System
  > FLAPS STUCK AT 5 DEGREES.
- [SDR KPVA201203](https://openairdocs.org/sdr/KPVA201203.md): Indicator · faulty · Mar 6, 2012 · N809WP · Dhav DHC8103 · Trailing Flap Position Indicating System
  > FLAPS STUCK AT 5 DEGREES DURING TAKEOFF. DECLARED EMERGENCY. RETURNED TO HNL. REMOVED AND REPLACED FLAP POSITION INDICATOR. GROUND OPERATION CHECKED GOOD.
- [SDR KPVA201107](https://openairdocs.org/sdr/KPVA201107.md): Mount Bracket · cracked · Jul 19, 2011 · N809WP · Dhav DHC8103 · Drag Control Actuator
  > LEFT OUTBOARD SPOILER ACTUATOR BRACKET CRACKED. REPLACED WITH POST MOD P/N 8570558-001.
- [SDR KPVA201104](https://openairdocs.org/sdr/KPVA201104.md): Inverter · failed · Mar 6, 2011 · N809WP · Dhav DHC8103 · AC Inverter
  > ON DESCENT, THE FLIGHT CREW OBSERVED THE AUX INV CAUTION LIGHT ILLUMINATED. AT THAT TIME AN ELECTRICAL ODOR WAS NOTICED BUT NO SMOKE. THE FLIGHT CREW DONNED THEIR O2 MASKS AND PROCEEDED WITH THEIR CHECKLIST. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED
- [SDR KPVA 201004](https://openairdocs.org/sdr/KPVA%20201004.md): Engine · malfunctioned · Nov 6, 2010 · N809WP · Dhav DHC8103 · Engine (Turbine/Turboprop)
  > IN FLIGHT AT LOW POWER SETTING WHEN HIGH PRESSURE VALVE OPENS, A VERY STRONG SMELL OF CHEMICAL SMELL COMING OUT OF VENTS, ALSO LIGHT HAZE. (MX) REPLACED NR 2 ENGINE IAW AIAM-105. OPS & LEAK CHECK GOOD. S/N ON AC0044.
- [SDR KPVA200910001](https://openairdocs.org/sdr/KPVA200910001.md): Structure · contaminated · Sep 25, 2009 · N809WP · Dhav DHC8103 · Nacelle/Pylon, Main Frame
  > LT NACELLE, AFT TAIL CONE, OUTBOARD SIDE HONEYCOMB HAS OIL CONTAMINATION. REMOVED APPROXIMATELY 750SQ/IN OF CONTAMINATED HONEYCOMB. REPLACED HONEYCOMB AND FIBERGLASS PLIES IAW BOMBARDIER RD 8-57-2752.
- [SDR KPVA 200908](https://openairdocs.org/sdr/KPVA%20200908.md): Warning System · malfunctioned · Jul 16, 2009 · N809WP · Dhav DHC8103 · Smoke Detection
  > (PIREP) SMOKE WARNING LIGHT ILLUMINATED FOR APPROX 10 SECONDS DURING CLIMBOUT. RETURN TO HNL, EMERGENCY DECLARED. (MX) INSPECTED SMOKE DETECTION SYSTEM AND PERFORMED TEST IAW DHC-8 MM 26-12-00 PAGE 201. NO DEFECTS NOTED.
- [SDR KPVA 200906](https://openairdocs.org/sdr/KPVA%20200906.md): Smoke Detector · intermittent · Jul 8, 2009 · N809WP · Dhav DHC8103 · Smoke Detection
  > (PIREP) SMOKE LIGHT FLICKERS IN FLIGHT. (MX) DEFER PER MEL 26-8-1 CATEGORY C. (MX) CLEAR MEL 26-8-1; REPLACED NR 2 BAGGAGE SMOKE DETECTOR.
- [SDR KPVA2008-05](https://openairdocs.org/sdr/KPVA2008-05.md): Wire · intermittent · Dec 20, 2008 · N809WP · Dhav DHC8103 · Engine Oil System Wiring
  > IN CRUISE, NR1 OIL PRESSURE 50 TO 55 PSI. MX NR1 OIL PRESSURE TRANSMITTER CONNECTOR P1 WIRE 2D20 REPAIRED IAW WD 79-32-00 SHEET 1 OF 2. PERFORMED OPS CHECK GOOD. C/W NR1 AND NR2 ENGINE RUN-UP IAW MM 71-00-00 PG. 529-531. NO DEFECTS NOTED.
- [SDR KPVA200714](https://openairdocs.org/sdr/KPVA200714.md): Turbine Blades · separated · Aug 31, 2007 · N809WP · Dhav DHC8103 · Turbine Section
  > NR 2 ENGINE TURBINE FAILURE, 2ND STAGE LP TURBINE BLADE SEPARATION WITH DAMAGE TO THE 1ST STAGE LP TUBINE BLADES AND 2ND STAGE GUIDE VANES. LP SECTION FROZEN BUT PROP SHAFT TURNS.
- [SDR KPVA200713](https://openairdocs.org/sdr/KPVA200713.md): Unknown · odor · Aug 31, 2007 · N809WP · Dhav DHC8103 · Air Distribution System
  > (PIREP) FLIGHT ATTENDANT REPORTED BURNING ODOR IN CABIN AFTER LANDING. (MX) INSPECTED FOR BURNING ODOR IN CABIN, LAV COMPARTMENTS. NO SMELL NOTED.
- [SDR KPVA20077](https://openairdocs.org/sdr/KPVA20077.md): Control Unit · inoperative · Jun 30, 2007 · N809WP · Dhav DHC8103 · Landing Gear Retraction/Extension System
  > (PIREP) PLACED GEAR HANDLE DOWN, GOT 3 RED INDICATIONS ONLY. GEAR CAME DOWN ON IT'S OWN AFTER GO AROUND WITH CLIMB TO 3000 FT. ALTERNATE GEAR EXTENSION LIGHTS SHOWED 3 DOWN. ANTI-SKID TESTED OK. (MX) REMOVED AND REPLACED LANDING GEAR CONTROL UNIT IAW DHC-8
- [SDR KPVA20076](https://openairdocs.org/sdr/KPVA20076.md): Tscu · malfunctioned · Jun 21, 2007 · N809WP · Dhav DHC8103 · Propeller Feathering/Reversing
  > (PIREP) WITH CONDITION LEVERS MAX WHEN TAXIING ON TO RUNWAY FOR TAKEOFF, NR 2 PROP EXPERIENCED AN UNCOMMANDED FEATHER. POWER LEVERS SLIGHTLY ABOVE IDLE, NR 2 TQ INCREASED TO 60 PERCENT, NR 2 PROP DOWN TO APPROX 300. (MX) REMOVED AND REPLACED NR 2 ENGINE TORQ
- [SDR KPVA20075](https://openairdocs.org/sdr/KPVA20075.md): Sequence Valve · inoperative · May 11, 2007 · N809WP · Dhav DHC8103 · Landing Gear Retraction/Extension System
  > (PIREP) NOSE GEAR WOULD NOT EXTEND USING NORMAL HYDRAULIC SYSTEM. GEAR EXTENSION USING ALTERNATE SYSTEM. (MX) REMOVED AND REPLACED RELAYS 3261-K11 AND 6231-K7 IAW DHC-8 WD 32-30-00 PG 1 SHEET 4. DID NOT SOLVE PROBLEM. (MX) REMOVED AND REPLACED NOSE GEAR DO
- [SDR KPVA20074](https://openairdocs.org/sdr/KPVA20074.md): Smoke Detector · faulty · May 8, 2007 · N809WP · Dhav DHC8103 · Smoke Detection
  > (PIREP) CLIMBING OUT AT 6000 FT FROM HNL THE SMOKE WARNING LIGHT KEPT COMING ON INTEMITTANTLY AND STAYED ON. (MX) REMOVED AND REPLACED NR 2 BAGGAGE SMOKE DETECTOR AND PERFORMED OPS CHECK IAW DHC-8 MM 26-12-00 PG 201.
- [SDR KPVA200617](https://openairdocs.org/sdr/KPVA200617.md): Generator · malfunctioned · Sep 6, 2006 · N809WP · Dhav DHC8103 · AC Generation System
  > (PIREP) L TRU AND NR 1 AC GEN LIGHT ILLUMINATED ON TAKEOFF ROLL. (MX) REMOVED AND REPLACED NR 1 AC GENERATOR IAW MM 24-21-00 PG. 201-203. OPS CHECK NORMAL IAW MM 24-21-00 PG. 203.
- [SDR KPVA20063](https://openairdocs.org/sdr/KPVA20063.md): Pcu · malfunctioned · Jan 21, 2006 · N809WP · Dhav DHC8103 · Propeller Controlling System
  > EXPERIENCED PROP OVERSPEED NR 2 ENGINE ON SHORT FINAL. ALSO, BETA WARNING HORN ANNOUNCED JUST PRIOR TO TOUCHDOWN (WHISTLE SOUND) WHEN POWER LEVERS ABOVE FLIGHT IDLE. REMOVED & REPLACED NR 2 ENGINE PCU IAW HAMILTON SUNDSTRAND 61-22-00 PG 703-706. ENGINE RUN
- [SDR 20018](https://openairdocs.org/sdr/20018.md): Indicator · false indication · Dec 11, 2005 · N809WP · Dhav DHC8103 · Flight Control System
  > ON TAKE OFF ROLL, PFCS INDICATOR SHOWED RT SIDE SPOILERS DEPLOYED AFTER ADVANCING TAKEOFF POWER WITH CONTROLS IN NEUTRAL POSITION. REMOVED AND REPLACED PFCS INDICATOR IAW PSM 1-8-2, 27-05-00 PG. 201-203. OPS CHECK PASS IAW PSM 1-8-2, 27-00-05 PG. 204-206.
- [SDR 200515](https://openairdocs.org/sdr/200515.md): Indicator · fluctuates · Oct 26, 2005 · N809WP · Dhav DHC8103 · Engine BMEP/Torque Indicating
  > ROUGH NR 2 ENG, TQ FLUCTUATION +/-2 PERCENT NON-STOP, CONTINUOUS. REMOVED AND REPLACED NR 2 ENGINE TORQUE GAUGE IAW MM CHAP. 77-10-00 PG. 201-202. NOTE: SUBSEQUENT TEST FLIGHT GOOD.
- [SDR KPV2005F00001](https://openairdocs.org/sdr/KPV2005F00001.md): Link · damaged · Aug 5, 2005 · N809WP · Dhav DHC8103 · Landing Gear Steering System
  > DURING TAXI INTO GATE THE NOSE STEERING WAS SLUGGISH. CONTINUED TO GATE. REPLACED NLG STEERING LINK AND BOTH NOSE WHEELS. OPS CHECK GOOD. (K)

## 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 = 'N809WP' AND deregistration_id = 'N809WP-2012-10-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N809WP-2012-10-25/reports

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