Pratt & Whitney Canada PW119C
Service difficulty reports · 49
Newest first. General aviation reporting is voluntary.
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 = 'PW119C' 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 = 'PW119C' 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 2016FA0000002Control Wheel · crackedAFTER INITIAL CLIMB THE CO-PILOT ATTEMPTED TO LOWER THE NOSE OF THE ACFT FOR CRUISE CLIMB. AS SOON AS FORWARD FORCE WAS APPLIED TO THE CONTROL WHEEL THE RT HORN CRACKED AND ARTICULATED FORWARD. CONTROL OF THE ACFT WAS TAKEN OVER BY THE F/O WHO MADE DECENT ANSDR J8UR2015FA0000515Actuator · activatedAIRCRAFT STICK PUSHER FAILED IN THE RETRACTED POSITION, ELEVATORS BEING HELD IN FULL NOSE DOWN DEFLECTION, AFTER BEING TESTED BY THE AIRCREW ON PREFLIGHT CHECKS. THE FAILURE WAS NOT DISCOVERED UNTIL THE ACFT WAS LINED UP AND CLEARED FOR TAKEOFF FROM RUNWAY 22SDR 2014F00085Alternator · crackedWHILE CLIMBING THROUGH, FL 140, THE FLIGHT CREW REPORTED LOSS OF OIL PRESSURE ON THE RT ENGINE. THEY IMMEDIATELY FEATHERED THEN SHUTDOWN THE ENGINE AND RETURNED TO THE DEPARTURE AIRPORT. THE MAINTENANCE REPAIR TEAM DISCOVERED THE RT ENGINE'S ALTERNATOR HALVESDR CA121105006Engine · malfunctioned(CAN) ON START UP FOR A RE-POSITIONING FLIGHT, THE CAPTAIN WAS ADVISED BY GROUND HANDLERS OF A PROBLEM WITH THE LT ENGINE. THE ENGINE WAS SHUTDOWN AND INSPECTION FOUND THAT A QTY OF OIL FROM ENGINE HAD BEEN LOST. OIL WAS ALSO FOUND IN THE NR 5 BEARING VENT TSDR CA120815001Turbine · damaged(CAN) FRONT INLET CASE REPLACEMENT REPLACEMENT AND LATER DURING TEST CELL PERFORMANCE CHECKS, THE HOT SECTION HAD A MAJOR FAILURE.SDR XV6A201109010013Shutoff Valve · defectiveBLEED SOV FAIL MSG. TIME ON UNIT NOT TRACKED.SDR CA110330008Wheel · damaged(CAN) LT I/B MAIN WHEEL ASSY WAS REPLACED ON 28-MAR-11 DUE TO A VERY BAD LEAK. THIS MAIN WHEEL ASSYÏ¿½S TIRE PRESSURE WAS ADJUSTED TO THE CORRECT SETTING ON 25-MAR-11 AND WAS THEN FOUND TO HAVE ONLY 40 PSI IN IT 3 DAYS LATER AFTER NO FLYING. THIS WAS VERY CONSDR CA110331013Computer · malfunctioned(CAN) FLIGHT MANAGEMENT SYSTEM DATA BASE CAUSES THE FMS TO RESET ON APPROACH INTO AIRPORT. MFG ENGINEERS ARE WORKING ON A SOFTWARE FIX. FMS DATA BASE IS FUNCTIONING NORMALLY AT ALL OTHER COMPANY AIRPORTS.SDR CA100726017Starter Gen · failed(CAN) LT STATER-GENERATOR FAILED PRIOR TO DESCENT. PILOTS FOLLOWED QRH CHECKLIST AND ATTEMPTED TO RESET IT. STARTER-GEN WOULD NOT RESET. REMAINDER OF THE FLIGHT WAS COMPLETED WITH DC-TIE ON. MX TROUBLESHOT THE ISSUE TO A FAILURE OF THE STARTER-GEN. THE STARTSDR XV6A2010042400006Light · inoperativeLT REAR EMERGENCY EXTERNAL EXIT LIGHT INOP.SDR CA090806012Control Unit · malfunctionedFLIGHT CREW WAS TAXING OUT FOR ITS FIRST FLIGHT OF THE DAY WHEN THEY STARTED TO SMELL SMOKE IN THE COCKPIT. FA INFORMED THE CREW THAT THERE WAS ALSO SMOKE IT THE CABIN. ENGINES WERE SHUTDOWN AND QRH WAS CONSULTED. CREW NOTED THAT SMOKE WAS ELIMINATED ONCE THE SDR XV6A2009030600001Structure · crackedREPETITIVE EDDY CURRENT INSPECTION IAW RAS-328-57-3051 AND AD 2008-10-15.SDR XV62008F00000Control Cable · obstructedR/S POWER LEVER WOULD NOT GO INTO GROUND IDLE AFTER LANDING. FOUND HINGE FROM COCKPIT DOOR INTERFERING WITH CABLES/ PULLEYS TRAVEL AT RT AVIONICS AFT SIDE. REMOVED FOD AS REQUIRED. CABLES/ PULLEYS GROUND RUN SATISFACTORY. A/C APPROVED FOR RTS. (K)SDR CA080207007Elt · failed(CAN) NUMEROUS UNCOMMANDED ELT ACTIVATIONS WITH ELT97. HAVE HAD ACTIVATIONS WITH THE AC INFLIGHT AND PARKED ON THE APRON. THE LASTEST WAS WITH ELT S/N-4584 ON JANUARY 30, 2008. THE AC HAD BEEN PARKED ON THE APRON FOR ROUGHLY 2 HOURS WHEN THE ELT SIGNAL WAS DSDR CA071121004Turbine · seized(CAN) AIRCRAFT DEVELOPED WHITE SMOKE IN CABIN WHILE TAXING FOR TAKEOFF. PILOTS NOTICED A CAS LT PACK FAIL LIGHT AND AN AFT LAV SMOKE DETECT CAS MESSAGE. AIRCRAFT RETURNED TO BLOCKS AND PASSENGERS DEBOARDED. CAUSE OF SMOKE WAS TURBINE SEIZED CAUSING A LT PACK OSDR CA070725004Boot · loose(CAN) PILOTS REPORTED LT HORIZONTAL STAB. DE-ICER BOOT APPEARS LOOSE. MAINTENANCE INSPECTED THE DE-ICER BOOT AND FOUND THE BOOT HAD COME LOOSE FROM THE AIRCRAFT AT THE AFT EDGES. THE ADHESIVE (3M 1300L) DID NOT SECURE THE DE-ICER BOOT TO THE STAB. THE BOOT WASDR CA061107008Trim Panel · shorted(CAN) ENROUTE THE PILOT REPORTED A STRONG SMELL AND A FLASH OF LIGHT FROM CENTER CONSOLE AREA. THEY TURNED THE INTERIOR DOME LIGHT ON A CONFIRMED THAT A PLASTIC LIGHTING PANEL WAS MELTING ON THE RUDDER LIMITER AND STANDBY ELEVATOR BUTTONS. HE POKED THE SPOT WISDR CA060906022Seal · leaking(CAN) FOLLOWING TAKEOFF ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND DECAY TO ZERO. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED A LEAKING ALTERNATOR DRIVE SEAL. (TC NR 20060906022)SDR CA060831006Hydraulic System · failed(CAN) AIRCRAFT READIED AND RT ENGINE START PARAMETERS NORMAL. RT CONDITION LEVER ADVANCED TO MIN. RT PROP DOES NOT UNFEATHER. RT CONDITION LEVER RETARDED TO FEATHER. RT CONDITION LEVER ADVANCED TO MIN. RT PROP DOES NOT UNFEATHER. MAINTENANCE CALLED TO SISDR CA051223016Boot · splitCREW REPORTED A FAIL INDICATION FOR THE RT HORIZONTAL STAB DEICE BOOT. UPON INSPECTION BY MAINTENANCE THE BOOT HAD A 12 INCH SPLIT AND WAS REPLACED. NO IN FLIGHT HANDLING PROBLEMS WHERE REPORTED.)SDR CA050901005Wire Harness · shortedA/C DEPARTED YYC, DURING CLIMB-OUT LIGHTS FLICKERED LT GEN KICKED OFFLINE AND CREW LOST FMS SCREEN AND PROP SYNC CB POPPED. AS DEPARTING MX BASES, ELECTED TO RETURN TO YYC. PAX`S WHERE DISEMBARKED AND A/C RETURNED TO HANGAR. GENERATOR CAME ON LINE DURING STSDR A6WA200330006Oil System · overservicedIN CRUISE AT 29,000 FEET, NR 2 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 51-55. INSPECTED AND FOUND OIL OVERSERVICED. REMOVED ONE QUART OF OIL. INSPECTED AND CLEANED OIL PSI CANNON PLUG. GROUND RAN GOOD. (M)SDR CA020606006Restrictor Valve · failed(CAN) LEFT OUTBOARD GROUND SPOILER FAILED TO DEPLOY ON LANDING. REPACED R/H RESTRICTOR VALVE P/N ZRV 87-3, S/N 90213160 AND CHECK VALVE P/N ZCV 157-1, S/N 80356276. AIRCRAFT RETURNED TO SERVICE AND GROUND SPOILER SYSTEM CHECKED SERVICEABLE. ALL PARTS SENT TO VSDR A6WA200100069Boot · defectiveRIGHT ENGINE HAD FLUCTUATING TORQUE INDICATION OF 10 - 25 PERCENT IN FLIGHT. MAINTENANCE FOUND INTAKE DE-ICE BOOT INFLATING AND CHOKING OFF ENGINE AIR INLET SUPPLY. REMOVED AND REPLACED INTAKE.SDR A6WA200100066Oil Filter · obstructedLEFT ENGINE OIL PSI HIGH IN CRUISE. MAINTENANCE FOUND LT BYPASS FILTER CAS MESSAGE. REMOVED AND REPLACED NR 1 OIL FILTER AND SCAVENGE FILTERS.SDR A6WA200100055Transducer · faultyRIGHT OIL PRESSURE HIGH. MAINTENANCE REMOVED AND REPLACED ENG PSI TRANSDUCER, MAIN ENGINE SCAVENGE FILTERS, OIL PUMP REGULATOR VALVE, AND NR 2 ENG KB HARNESS.SDR A6WA200100028Gearbox · defectiveDESCENT OUT OF FL240, LT ENGINE SURGED FROM 0 PERCENT TO 30 PERCENT TORQUE AND LT PROP IMMEDIATELY WENT TO 103 PERCENT NP. FLEW FOR 4 MINUTES WITH ENGINE AT FLT IDLE AND NP AT 103 PERCENT. ENGINE SURGED 2ND TIME CAUSING ACFT TO YAW. ELECTED TO SHUTDOWN ENGISDR A6WA200000081Hmu · failedLEFT ENGINE UNCOMMANDED POWER LOSS. POWER LEVER MOVEMENT HAS NO EFFECT. ENGINE SHUTDOWN. MAINTENANCE REMOVED AND REPLACED ENGINE HMU.SDR A6WA200000069Impeller · damagedLT ENGINE POWER LOSS AND STOPPAGE ON TAKE-OFF AFTER TAKE-OFF POWER WAS SET. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. LP IMPELLER BLADE WAS FOUND DAMAGED CAUSE WAS DETERMINED TO BE ICE INGESTION.SDR 99ZZZX1140Fuel Pump · failedPILOT REPORTED ON 10 MILE FINAL AT 3,000 FEET MSL, THE LEFT ENGINE ROLLED BACK WITH THE POWER LEVER PULLED BACK TO FLIGHT IDLE. REPLACED LT HMU AND FUEL PUMP WITH SERVICABLE, CONTINUED TIME HMU AND FUEL PUMP. ENGINE TSN: 8,473.6 HOURS, CSN: 9,993.SDR 99ZZZX1141Hmu · failedPILOT REPORTED ON 10 MILE FINAL AT 3,000 FEET MSL, THE LEFT ENGINE ROLLED BACK WITH THE POWER LEVER PULLED BACK TO FLIGHT IDLE. REPLACED LT HMU AND FUEL PUMP WITH SERVICABLE, CONTINUED TIME HMU AND FUEL PUMP. ENGINE TSN: 8,473.6 HOURS, CSN: 9,993.SDR M8XA9800014Dau · defectiveSHORTLY AFTER TAKEOFF, THE FLIGHT CREW REPORTED A PROBLEM WITH THE NR 1 ALTERNATOR. THEY WERE ALERTED BY AC VOLT FAIL MESSAGE ON THE EICAS SCREEN. AIRCRAFT RETURNED TO DEN, LANDED WITHOUT FURTHER INCIDENT. DENVER MAINTENANCE REPLACED THE NR 1 DAU IAW AMM 31SDR M8XA9800013Windshield · defectiveAIRCRAFT RETURNED TO DEN BECAUSE OF A CRACKED RIGHT FRONT WINDSHIELD AS A RESULT OF ENCOUNTERING A HAIL STORM SHORTLY AFTER TAKEOFF. AIRCRAFT LANDED IN DEN WITHOUT FURTHER INCIDENT. DENVER MAINTENANCE INSPECTED THE AIRCRAFT FUSELAGE IAW SRM 53-00-11 AND WINDSDR M8XA9800010Flap Control · malfunctionedSHORTLY AFTER TAKE-OFF, THE FLIGHT CREW REPORTED A FLAP CONTROL FAULT AND ASYMMETRY WARNING MESSAGE. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER INCIDENT. ON-CALL MAINTENANCE CONTRACTOR RESET THE FLAP CONTROL UNIT IAW AMM JIC 27-50-00-810-001-ASDR M8XA9800009Air Distr · odorCREW REPORTED RECEIVING AN EICAS. LEFT PACK FAIL MESSAGE DURING TAXI. PILOT CYCLED THE LT PACK SWITCH,THE FAIL MESSAGE THEN CLEARED ITSELF. FAIL MESSAGE ILLUMINATED AGAIN AFTER T/O. THIS WAS ACCOMPANIED WITH AN AMBER LAV SMOKE EICAS. CREW REPORTED, NO EVIDSDR M8XA9800012Controller · defectiveSHORTLY AFTER T/O, THE FLIGHT CREW REPORTED A PROBLEM WITH THE AIRCRAFT PRESSURIZATION SYSTEM. AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL MODE. AIRCRAFT RETURNED TO THE FIELD LANDED WITHOUT FURTHER INCIDENT. DENVER MX PERSONNEL REPLACED THE CABIN PRESSSDR M8XA9800008Indication · malfunctionedEN ROUTE FROM DEN TO DRO, THE FLIGHT CREW NOTICED ON THE FLAP POSITION INDICATION PORTION OF THE EICAS. SCREEN THAT THE RIGHT FLAP INDICATED A ONE DEGREE DEFLECTION AND THE LEFT FLAP WAS AT ZERO DEGREE DEFLECTION. THIS WAS NOT ASSOCIATED WITH A FAULT OR ASSESDR M8XA9800007Pitot Heat · failedEN ROUTE FROM DEN TO CYS, AIRCRAFT ENCOUNTERED ICING CONDITIONS. SINCE THE PITOT HEAT SYSTEM WAS MEL'D, AIRCRAFT WAS FORCED TO RETURN TO DEN. AIRCRAFT LANDED IN DEN WITHOUT FURTHER INCIDENT. DEN MAINTENANCE PERSONNEL REPLACED THE NR 2 PITOT TUBE IAW AMM 34-SDR M8XA9800005Seal · failedDURING CLIMBOUT, THE CREW REPORTED A PROBLEM WITH AIR LEAKING AROUND THE DOCUMENT DOOR. CREW THEN ELECTED TO RETURN TO DEN. AIRCRAFT LANDED IN DEN WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE DOCUMENT DOOR AND FOUND NO DISCREPANCIES. ALSO, CONDUCTEDSDR M8XA9800004Radar Unit · defectiveCREW REPORTED THAT THE RADAR APPEARED TO BE INOPERATIVE, NO GROUND PAINT. CREW ELECTED TO RETURN TO DENVER. AIRCRAFT LANDED IN DEN WITH NO FURTHER INCIDENTS. MX REPLACED WEATHER RADAR UNIT IAW AMM 34-41-01, OPERATIONAL CHECK IAW AMM 34-41-00 WAS CONDUCTED WSDR M8XA9800002Indication · malfunctionedCREW REPORTED THAT THEY RECEIVED NO VISUAL EICAS INDICATION THAT THE GROUND SPOILERS WERE ARMED AFTER THE CONDITION LEVERS WERE ADVANCED TO THE TAKEOFF POSITION. CREW ELECTED TO ABORT TAKEOFF AND RETURN TO THE GATE. CONTRACT MAINTENANCE PERFORMED GROUND SPOISDR M8XA9700022Bracket · failedEN ROUTE, THE CREW RECEIVED A DOOR WARNING INDICATION. ACFT RETURNED, LANDED WITHOUT FURTHER INCIDENT. MX DISCOVERED THE PAX DOOR PROXIMITY SENSOR TARGET WAS MISRIGGED. ALSO, THE PROXIMITY SENSOR BRACKET WAS DAMAGED SEVERAL ATTACH RIVETS WERE LOOSE. ACFT SDR M8XA9700020Hinge · defectiveSHORTLY AFTER THE A/C ARRIVED IN (DIA) MX WAS REQUESTED TO INSPECT THE PAX DOOR AS A RESULT OF DOOR BEING DIFFICULT TO CLOSE FROM TUL. MX INSPECT DOOR AND DISCOVERED AFT MAIN DOOR SUPPORT HINGE CRACKED ALMOST INTO, CRACK WAS COMPLETELY THROUGH THE UPPER FLANGSDR M8XA9700018Press Switch · defectiveEN ROUTE, RECEIVED A CAS MESSAGE EMERGENCY/PARKING BRAKE ACCUMULATOR PRESSURE ALERT. DIVERTED TO COS WHERE MX WAS AVAILABLE. ACFT LANDED WITH NO FURTHER INCIDENT. NOTE: THIS WAS THE SECOND PILOT REPORT OF THE SAME DISCREPANCY IN AS MANY DAYS. MX UNABLE TO SDR M8XA9700019Valve · defectiveEN ROUTE, THE FLIGHT CREW REPORTED A PROBLEM WITH THE EMERGENCY/ PARKING BRAKE ACCUMULATOR PRESSURE INDICATION. THIS IS A REPEAT OF SAME PROBLEM EXPERIENCED EARLIER IN THE DAY. REPLACEMENT OF THE PRESSURE SWITCH DID NOT CORRECT THE PREVIOUS DISCREPANCY. THESDR M8XA9700017Warning · activatedDURING THE TAKEOFF ROLL, THE FLIGHT CREW WAS ALERTED BY A GROUND SPOILERS NOT STOWED CAS MESSAGE. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MX CONDUCTED A THROUGH INSPECTION OF THE AIRCRAFT AS WELL AS PERFORMING AN OPERATION CHECK OF THE GROUND SPOSDR M8XA9700015Bearing · defectivePROPELLER SERIAL NUMBER HL-146, WAS REMOVED FROM AIRCRAFT N331MX (S/N 3067) FOR SCHEDULED MAINTENANCE. WHEN THE PROPELLER WAS BEING DISASSEMBLED IN PREPARATION FOR SHIPMENT TO THE OEM FOR INSPECTION, MAINTENANCE PERSONNEL NOTICED THE THRUST BEARING AT THE NR SDR M8XA9700014Cas Warning · activatedDURING THE TAKEOFF ROLL PRIOR TO REACHING V1, THE CREW WAS ALERTED BY THE CAS SYSTEM THAT THEY HAD ENCOUNTERED AN INVERTER BUS FAIL. THIS WAS ACCOMPANIED BY AN AMBER MESSAGE ON THE EICAS SCREEN. THE FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO GATE. MTN SDR M8XA9700012Boost Pump · failedDURING THE TAKEOFF ROLL, THE FLT WAS ALERTED BY A ELPMP AUTO FAIL CAS MESSAGE. THE FLT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. DENVER MX INSPECTED THE A/C AND CONDUCTED GROUND RUNS IAW AMM JIC. 28-00-00. ALL CHECKS WERE SATISFACTORY. MX UNABLE T
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