Pratt & Whitney Canada PW119B
Service difficulty reports · 1,612
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Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA160203014Engine · malfunctioned(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 OSDR CA151019003Wheel · failed(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 JSDR CA140326009Blade · damaged(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 GROSDR CA140225021Relay · failed(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 CA130808004Stator · damaged(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 BLADESSDR CA130212001Engine · power loss(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 ACFTSDR CA121228004Fuel Control · malfunctioned(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 MASDR CA121119021Gear · damaged(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 CRSDR CA120925004Control Unit · malfunctioned(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 ISDR CA110606009Bearing · making metalEIR 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 COULDSDR XV6A2009101400009Light · inoperativeEMERGENCY STRIP FLOOR LIGHTING OUT ROWS 4-7.SDR CA090911007Eec · failed(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 CA090701002Pseu · malfunctionedON 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 PSDR CA080924013Engine · fluctuates(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 CA080220007Oil System · low 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 200SDR CA070209016Engine · failed(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 R019617Bearing · corrodedINSTALLED 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-743SDR 2006F00008Lug · crackedWHILE PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.SDR 2006F00009Lug · crackedWILL PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.SDR VNAA0408015Gcu · failedDURING 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 WSDR VNAA0408014Valve · failedDURING 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 ASDR VNAA0408012Circuit Breaker · trippedDURING 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 20SDR VNAA0408009Proximity Sensor · out of adjustDURING 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 VNAA0408010Chip Detector · failedDURING 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 DORSDR VNAA0408007Relay · failedIN 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 MELSDR VNAA0408003Pump · failedDURING 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 VNAA0408002Power Supply · failedTHE 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 VNAA0407009Smoke Detector · failedTHE 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. OPERATISDR VNAA0407008Battery · failedTHE 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 VNAA0407007Valve · failedDURING 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 MSDR VNAA0407006Door · failedTHE 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 FORSDR VNAA0407004Engine · bird ingestionDURING 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 OFSDR VNAA0407002Light · failedTHE 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 RESDR VNAA0407001Sensor · failedDURING 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 VNAA0406014Dau · failedON 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 VNAA0406015Terminal Block · failedTHE 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 SERVICESDR VNAA0406013Fire Loop · failedON 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 CHECKSSDR VNAA0406012Gcu · failedDURING 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 MSDR VNAA0406011Warning Light · illuminatedDURING 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 VNAA0406010Dau · failedDURING 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 AIRCRAFTSDR VNAA0406009Smoke Detector · failedTHE 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 VNAA0406007Power Supply · failedTHE 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 VNAA0406008Sensor · out of positionDURING 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 VNAA0406001Handle · failedAFTER 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 RSDR VNAA0406002Power Supply · failedTHE 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 THESDR VNAA0405012Smoke Detector · failedTHE 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 VNAA0405011Control Unit · failedTHE 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 VNAA0406016Tail Cone · failedUPON 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 VNAA0405004Door · openAFTER 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 VNAA0404016Pin · installedFLIGHT 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.
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