# Service difficulty reports: Pratt & Whitney Canada PW119B

A list on [Pratt & Whitney Canada PW119B](https://openairdocs.org/engine/pratt-whitney-canada-pw119b.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 33 · 1,612 reports

- [SDR CA160203014](https://openairdocs.org/sdr/CA160203014.md): Engine · malfunctioned · Jan 28, 2016 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) ON FOUR SEPARATE OCCASIONS, THE CREW EXPERIENCED A REDUCTION OF TORQUE ON THE RIGHT ENGINE. ON ALL OCCASIONS, THE POWER LEVER WAS FREE TO MOVE BUT MOVEMENT HAD NO EFFECT. THEY ALSO NOTED THAT ON ALL OCCASIONS, THE TORQUE BEGINS TO REDUCE AT LOW OAT AND O
- [SDR CA151019003](https://openairdocs.org/sdr/CA151019003.md): Wheel · failed · Oct 15, 2015 · Dorner DO328100 · Wheel/Ski/Float
  > (CAN) WHEEL ASSY INNER HALF WAS FOUND WITH THE BEAD AREA SEPARATED AND TIRE DEFLATED. ALL OTHER TIRES FULLY INFLATED. THE BEAD AREA HAD A DARK CAST TO THE METAL THAT LOOKED LIKE THE POSSIBLE START OF A POSSIBLE CRACK. THIS ASSEMBLY HAD THE LAST NDT COMPLETED J
- [SDR CA140326009](https://openairdocs.org/sdr/CA140326009.md): Blade · damaged · Mar 12, 2014 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTED NOISE FROM RT ENGINE IN TRANSIENT FROM CLIMB TO CRUISE, APPROXIMATELY 15 MINUTES INTO FLIGHT, AND WITH A LOSS OF POWER. PILOT INDUCED THE IFSD FOLLOWED BY ACFT RETURNING TO AIRPORT AND PERFORMED UNEVENTFUL SINGLE ENGINE LANDING. ON GRO
- [SDR CA140225021](https://openairdocs.org/sdr/CA140225021.md): Relay · failed · Feb 20, 2014 · Dorner DO328100 · DC Power Distribution System
  > (CAN) ON DEPARTURE AFTER ROTATION "MC" RT ALT FAIL ILLUMINATED. "MC" WAS AWKNOWLEDGED AND DEPATURE PROCEDURE WAS FOLLOWED AS NORMAL. WHEN SAFE CREW RAN "MC" R ALT FAIL CHECKLIST. TIEING LT ALT CAUSED LT ALT TO FAIL ALSO. IAW QRH AC TIE WAS UNTIED AND LT ALT
- [SDR CA130808004](https://openairdocs.org/sdr/CA130808004.md): Stator · damaged · Jul 16, 2013 · Dorner DO328100 · Turbine Section
  > (CAN) ON A WALK AROUND INSPECTION OF THE DO 328-100 AS LISTED ABOVE, IT WAS NOTED THAT WHILE ROTATING THE NR 2 PROPELLER BY HAND THAT A SLIGHT RUB AND SLOWING OF THE PROP OCCURRED. A BOROSCOPE INSPECTION WAS COMPLETED AND FOUND SLIGHT RUBBING OF THE PT BLADES
- [SDR CA130212001](https://openairdocs.org/sdr/CA130212001.md): Engine · power loss · Jan 24, 2013 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) "DURING REPOSITIONING FLIGHT AFTER MAINTENANCE (NO MAINTENANCE DONE ON THE ENGINE, ABOUT 1.5 HR INTO THE FLIGHT THE ENGINE NR 2 TORQUE AND FUEL FLOW GRADUALLY DROPPED SLOWLY. THE PILOT TRIED MANUAL ECU BUT NO EFFECT. THE ENGINE WAS SHUTDOWN AND THE ACFT
- [SDR CA121228004](https://openairdocs.org/sdr/CA121228004.md): Fuel Control · malfunctioned · Nov 16, 2012 · Dorner DO328100 · Fuel Control/Turbine Engines
  > (CAN) DURING FLIGHT AT FL240, TORQUE FLUCTUATIONS ON TH RT ENGINE WITH A DROP OF APPROXIMATELY 40 OCCURRED. THE ACFT EXPERIENCED A YAW AND ROLL MOMENT. EMERGENCY PROCEDURES WERE FOLLOWED AND THE ACFT RETURNED TO DESTINATION WHERE AN UNEVENTFUL LANDING WAS MA
- [SDR CA121119021](https://openairdocs.org/sdr/CA121119021.md): Gear · damaged · Nov 12, 2012 · Dorner DO328100 · Turbine Engine Reduction Gear
  > (CAN) DURING CLIMB, CREW REPORTED A CHIP DETECTOR INDICATION MESSAGE FOLLOWED BY LOSS OF OIL PRESSURE. THE ENGINE WAS SHUTDOWN AND SECURED BEFORE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED AT THE DEPARTURE AIRPORT. POST FLIGHT INSPECTION FOUND A CR
- [SDR CA120925004](https://openairdocs.org/sdr/CA120925004.md): Control Unit · malfunctioned · Sep 24, 2012 · Dorner DO328100 · Propeller Controlling System
  > (CAN) DURING GROUND RUN OF THE ENGINES, THE CREWS NOTICED THAT THE LT PROPRELLER WOULD NOT FEATHER WHILE IN GROUND IDLE POSITION EITHER ELECTRICALLY USING FEATHER PUMP, OR MANUALLY USING THE CONDITION LEVERS. BUT THE PROP WOULD FEATHER WHEN POWER LEVERS ARE I
- [SDR CA110606009](https://openairdocs.org/sdr/CA110606009.md): Bearing · making metal · Jun 1, 2011 · Turbine Engine Reduction Gear
  > EIR PW100 2011-034 WAS ABLE TO CONFIRM THE OPERATORS REPORT OF METAL CONTAMINATION IN THE RGB OIL SYS. THE SOURCE OF THE METAL CONTAMINATION WAS DETERMINED TO BE THE RT NR 14 BEARING WHICH HAD A CRACKED AND SPALLED INNER RACE. THE CAUSE OF THE FAILURE COULD
- [SDR XV6A2009101400009](https://openairdocs.org/sdr/XV6A2009101400009.md): Light · inoperative · Oct 14, 2009 · N329MX · Dorner DO328100 · Emergency Lighting
  > EMERGENCY STRIP FLOOR LIGHTING OUT ROWS 4-7.
- [SDR CA090911007](https://openairdocs.org/sdr/CA090911007.md): Eec · failed · Sep 5, 2009 · Fuel Controlling System
  > (CAN) ENGINE TORQUE WAS SEEN TO FLUCTUATE FOLLOWING TAKE-OFF AND THE ENGINE WAS SHUT DOWN. TROUBLESHOOTING LED TO REPLACEMENT OF A FAULT EEC. (TC# 20090911007)
- [SDR CA090701002](https://openairdocs.org/sdr/CA090701002.md): Pseu · malfunctioned · Jun 28, 2009 · Dorner DO328100 · Hydraulic System, Main
  > ON CLIMB AFTER TAKEOFF, PILOT RECEIVED A CAS MESSAGE "PRIORITY VALVE CLOSED" GEAR AND FLAPS IN-TRANIST STOPPED, HYD PRESSURE CAS MESSAGE HIGH. THEN ALL HYD PRESSURE WAS LOST. PILOT RETURNED TO AIRPORT OF DEPARTURE TO LAND. HAD EMERGENCY CREWS STANDBY FOR P
- [SDR CA080924013](https://openairdocs.org/sdr/CA080924013.md): Engine · fluctuates · Sep 22, 2008 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) AT ABOUT 50 METERS FROM THE ARRIVAL GATE, THE ENG PARAMETERS STARTED FLUCTUATING. PILOT SHUTDOWN THE ENG. NO REPORTED DAMAGE. TROUBLESHOOTING IN PROGRESS. MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.
- [SDR CA080220007](https://openairdocs.org/sdr/CA080220007.md): Oil System · low pressure · Jan 15, 2008 · Dorner DO328100 · Engine Oil Pressure
  > (CAN) DURING CRUISE, THE OIL PRESSURE WAS NOTED TO DROP. THE CREW SHUTDOWN THE ENGINE AND PERFORMED A SINGLE ENGINE LANDING. ENGINE IS BEING SENT FOR INVESTIGATION. MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 200
- [SDR CA070209016](https://openairdocs.org/sdr/CA070209016.md): Engine · failed · Jan 23, 2007 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE THE ENGINE CHIP DETECTOR AND LOW OIL PRESSURE WARNINGS ACTIVATED AND THE ENGINE FLAMED OUT IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED.
- [SDR R019617](https://openairdocs.org/sdr/R019617.md): Bearing · corroded · Apr 15, 2006 · Dorner DO328100 · Propeller Blade Section
  > INSTALLED NEW BEARINGS AND FORK AND COMPLIED WITH ALL APPLICABLE SERVICE BULLETINS. PROP WAS DISASSEMBLED FOR SHIPMENT. TSN 14711:35, TSO 2101:09. 1/26/03 - PROP WAS ASSEMBLED AND INSTALLED ON AC302. 4/11/06 - PROP HAS ACCUMULATED 546 HOURS. ALL SIX C-743
- [SDR 2006F00008](https://openairdocs.org/sdr/2006F00008.md): Lug · cracked · Jan 26, 2006 · N462PS · Dorner DO328100 · Empennage Structure
  > WHILE PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.
- [SDR 2006F00009](https://openairdocs.org/sdr/2006F00009.md): Lug · cracked · Jan 26, 2006 · N462PS · Dorner DO328100 · Empennage Structure
  > WILL PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.
- [SDR VNAA0408015](https://openairdocs.org/sdr/VNAA0408015.md): Gcu · failed · Aug 29, 2004 · N424JS · Dorner DO328100 · AC Generation System
  > DURING TAKEOFF, THE CREW RECEIVED A LT GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE LT GENERATOR CONROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-31-03. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT W
- [SDR VNAA0408014](https://openairdocs.org/sdr/VNAA0408014.md): Valve · failed · Aug 24, 2004 · N439JS · Dorner DO328100 · Pneumatic System
  > DURING CLIMBOUT, THE CREW RECEIVED A RT LOW PRESSURE VALVE FAILED INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND LOW PRESSURE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED A
- [SDR VNAA0408012](https://openairdocs.org/sdr/VNAA0408012.md): Circuit Breaker · tripped · Aug 19, 2004 · N424JS · Dorner DO328100 · Stabilizer Control System
  > DURING CLIMBOUT, THE CREW RECEIVED AN ELEVATOR ASYMMETRY CAS MESSAGE THEN FLIGHT 2540 RETURNED TO PIT. MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND TRIM CIRCUIT BREAKER POPPED. MAINTENANCE THEN RESET THE CIRCUIT BREAKER IN ACCORDANCE WITH WIRING MANUAL 20
- [SDR VNAA0408009](https://openairdocs.org/sdr/VNAA0408009.md): Proximity Sensor · out of adjust · Aug 16, 2004 · N441JS · Dorner DO328100 · Door Warning System
  > DURING FLIGHT, THE DOORS LIGHT ON THE RED WARNING PANEL CAME ON. THE CREW THEN DIVERTED TO ELM. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE THEN ADJUSTED THE PROXI SENSOR AND THE OVERCENTER LEVER IN ACCORDANCE WITH DORNIER MAITNENANCE MANUAL 52-00-00.
- [SDR VNAA0408010](https://openairdocs.org/sdr/VNAA0408010.md): Chip Detector · failed · Aug 16, 2004 · N440JS · Dorner DO328100 · Turbine Engine Reduction Gear
  > DURING FLIGHT, THE CREW RECEIVED A RT REDUCTION GEARBOX CHIP DETECTOR INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND FOUND ALLOWABLE DEBRIS ON THE DETECTOR. MAINTNENANCE THEN CLEANED THE CHIP DETECTOR AND REPLACED THE FILTER IN ACCORDANCE WITH DOR
- [SDR VNAA0408007](https://openairdocs.org/sdr/VNAA0408007.md): Relay · failed · Aug 15, 2004 · N440JS · Dorner DO328100 · Air Conditioning System Wiring
  > IN FLIGHT, THE CREW REPORTED SMOKE IN THE CABIN AND DIVERTED TO TRI. MAINTENANCE CONTROL DISPATCHED MECHANICS FROM PIT. MAINTENANCE FOUND THAT THE RECIRC FAN WOULD NOT TURN OFF AND OVERHEATED CAUSING SMOKE DUE TO A FAILED 36HB RELAY. THE RECIRC FAN WAS MEL
- [SDR VNAA0408003](https://openairdocs.org/sdr/VNAA0408003.md): Pump · failed · Aug 8, 2004 · N438JS · Dorner DO328100 · Engine Fuel Pump
  > DURING TAKEOFF, THE CREW RECEIVED A LOW FUEL PRESSURE MESSAGE AND ABORTED TAKEOFF. MAINTENANCE CONTROL DEFERRED THE ASSOCIATED FUEL PUMP SYSTEM WITH MEL 28-9 CODE-C.
- [SDR VNAA0408002](https://openairdocs.org/sdr/VNAA0408002.md): Power Supply · failed · Aug 2, 2004 · N425JS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY WAS DEAD. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0407009](https://openairdocs.org/sdr/VNAA0407009.md): Smoke Detector · failed · Jul 31, 2004 · N441JS · Dorner DO328100 · Smoke Detection
  > THE CREW REPORTED RECEIVING A LAV SMOKE MESSAGE. MAINTENANCE CONTROL DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH MEL 26-3 CODE-C. THE MEL WAS CLEARED BY REPLACING THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATI
- [SDR VNAA0407008](https://openairdocs.org/sdr/VNAA0407008.md): Battery · failed · Jul 29, 2004 · N439JS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS OUT. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0407007](https://openairdocs.org/sdr/VNAA0407007.md): Valve · failed · Jul 26, 2004 · N429JS · Dorner DO328100 · Landing Gear Brake System
  > DURING CLIMBOUT, THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR LOW CAS MESSAGE AND RETURNED TO PHL. MAINTENANCE CONTROL FERRIED THE AIRCRAFT TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER M
- [SDR VNAA0407006](https://openairdocs.org/sdr/VNAA0407006.md): Door · failed · Jul 24, 2004 · N438JS · Dorner DO328100 · Emergency Exits
  > THE CREW REPORTED THAT THE EMERGENCY DOOR AT ROW 9A WAS NOT OPENING PROPERLY. MAINTENANCE INSPECTED AND REPOSITIONED SEATS 2A THROUGH 8A IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 25-00-00. OPERATION CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR
- [SDR VNAA0407004](https://openairdocs.org/sdr/VNAA0407004.md): Engine · bird ingestion · Jul 17, 2004 · N440JS · Dorner DO328100 · Engine (Turbine/Turboprop)
  > DURING LANDING, FLIGHT 2576 HAD A BIRD STRIKE. MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05-57-04. FURTHER INSPECTION FOUND FOD DAMAGE TO THE LEFT HAND ENGINE IMPELLER BLADES. THE DAMAGE REQUIRED REMOVAL OF
- [SDR VNAA0407002](https://openairdocs.org/sdr/VNAA0407002.md): Light · failed · Jul 13, 2004 · N430JS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT A EMERGENCY FLOOR LIGHT STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RE
- [SDR VNAA0407001](https://openairdocs.org/sdr/VNAA0407001.md): Sensor · failed · Jul 4, 2004 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE VISUALLY INSPECTED THE SYSTEM AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. THE SYSTEM WAS RESET AND THE
- [SDR VNAA0406014](https://openairdocs.org/sdr/VNAA0406014.md): Dau · failed · Jun 21, 2004 · N425JS · Dorner DO328100 · Stall Warning System
  > ON CLIMBOUT, THE CREW RECEIVED AN ON SIDE BLUE STICK SHAKER CAS MESSAGE. THE AIRCRAFT THEN RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED, AND REPLACED THE NR 2 DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL
- [SDR VNAA0406015](https://openairdocs.org/sdr/VNAA0406015.md): Terminal Block · failed · Jun 21, 2004 · N429JS · Dorner DO328100 · Electrical Power System Wiring
  > THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED FUSES AND A TERMINAL BLOCK UNDER THE CAPTAIN'S SEAT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE
- [SDR VNAA0406013](https://openairdocs.org/sdr/VNAA0406013.md): Fire Loop · failed · Jun 17, 2004 · N430JS · Dorner DO328100 · Smoke Detection
  > ON CLIMBOUT, THE CREW RECEIVED A RIGHT HAND FIRE LOOP FAIL MESSAGE. FLIGHT 2490 RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FIRE DETECTION BOX IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS
- [SDR VNAA0406012](https://openairdocs.org/sdr/VNAA0406012.md): Gcu · failed · Jun 16, 2004 · N426JS · Dorner DO328100 · DC Generating System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL INDICATION AND ABORTED TAKEOFF. ON TAXI BACK, THE CREW RECEIVED A DC GENERATOR FAIL CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE GENERATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER M
- [SDR VNAA0406011](https://openairdocs.org/sdr/VNAA0406011.md): Warning Light · illuminated · Jun 15, 2004 · N426JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND STICK SHAKER PUSHER ON SIDE FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE SHAKER PUSHER RESET ITSELF AND FLIGHT 2417 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 2417 THEN DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0406010](https://openairdocs.org/sdr/VNAA0406010.md): Dau · failed · Jun 14, 2004 · N425JS · Dorner DO328100 · Stall Warning System
  > DURING CLIMBOUT, THE CREW RECEIVED A RT STICK SHAKER CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT
- [SDR VNAA0406009](https://openairdocs.org/sdr/VNAA0406009.md): Smoke Detector · failed · Jun 14, 2004 · N440JS · Dorner DO328100 · Smoke Detection
  > THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0406007](https://openairdocs.org/sdr/VNAA0406007.md): Power Supply · failed · Jun 13, 2004 · N441JS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLIES FAILED TO TEST. MAINTENANCE HAD THE CREW RUN THE ENGINES FOR 10 MINUTES AND PERFORM AN OPERATIONAL CHECK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.
- [SDR VNAA0406008](https://openairdocs.org/sdr/VNAA0406008.md): Sensor · out of position · Jun 13, 2004 · N438JS · Dorner DO328100 · Stall Warning System
  > DURING TAKEOFF, THE ANGLE OF ATTACK VANE WAS OUT OF POSITION AND THE CREW ABORTED TAKEOFF. THE ANGLE OF ATTACK VANE WAS RESET AND FLIGHT 2572 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.
- [SDR VNAA0406001](https://openairdocs.org/sdr/VNAA0406001.md): Handle · failed · Jun 2, 2004 · N434JS · Dorner DO328100 · Landing Gear Selector
  > AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT GO UP AND THE CREW RETURNED TO CAK. MAINTENANACE INSPECTED AND REPLACED THE GEAR RETRACT CIRCUIT BREAKER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS R
- [SDR VNAA0406002](https://openairdocs.org/sdr/VNAA0406002.md): Power Supply · failed · Jun 2, 2004 · N429JS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT DURING THE EMERGENCY POWER SUPPLY TEST, ONLY THE TOP LIGHT CAME ON. MAINTENANCE INSPECTED AND REPLACED THE FORWARD EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENACE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE
- [SDR VNAA0405012](https://openairdocs.org/sdr/VNAA0405012.md): Smoke Detector · failed · May 22, 2004 · N434JS · Dorner DO328100 · Smoke Detection
  > THE CREW REPORTED GETTING A LAV SMOKE FAIL CAS MESSAGE. MAINTENANCE DEFERRED THE LAV SMOKE DETECTION SYSTEM WITH THE CREW PER 26-3 CODE C.
- [SDR VNAA0405011](https://openairdocs.org/sdr/VNAA0405011.md): Control Unit · failed · May 18, 2004 · N426JS · Dorner DO328100 · Fire Detection
  > THE CREW REPORTED THAT A FIRE SQUIB WAS FAILING TO TEST. MAINTENANCE INSPECTED AND REPLACED THE FIRE WARNING CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0406016](https://openairdocs.org/sdr/VNAA0406016.md): Tail Cone · failed · May 14, 2004 · N430JS · Dorner DO328100 · Aerodynamic Fairings
  > UPON LANDING AT GSO, IT WAS FOUND THAT THE APU ACCESS DOOR HAD OPENED IN FLIGHT. MAINTENANCE WAS SENT TO GSO AND REPLACED THE APU TAIL CONE ASSMEBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 53-00-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.
- [SDR VNAA0405004](https://openairdocs.org/sdr/VNAA0405004.md): Door · open · May 3, 2004 · N441JS · Dorner DO328100 · Passenger/Crew Doors
  > AFTER TAKEOFF, THE MAIN CABIN DOOR OPENED, AND FLIGHT 2447 RETURNED TO ABE, AIRCRAFT N441JS WAS THEN FERRIED TO CAK. THIS IS CURRENTLY STILL UNDER INVESTIGATION. AN UPDATED ODR WILL BE PROCESSED WHEN THE INVESTIGATION HAS BEEN COMPLETED.
- [SDR VNAA0404016](https://openairdocs.org/sdr/VNAA0404016.md): Pin · installed · Apr 19, 2004 · N429JS · Dorner DO328100 · Rudder Control System
  > FLIGHT 2597 RETURNED TO GATE WITH RUDDER PEDDLES JAMMED. MAINTENANCE INSPECTED AND REMOVED RIG PIN FROM RUDDER PEDDLES IN ACCORDANCE WITH THE DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE.

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pw119b/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 engine_model_key = 'PW119B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw119b/reports

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