Pratt & Whitney Canada PW617F-E
Service difficulty reports · 63
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 = 'PW617FE' 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 = 'PW617FE' 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 CA131105010Manifold · blocked(CAN) FUEL MANIFOLD DETERMINED TO EXHIBIT CARBON BLOCKAGE OF INTERNAL PASSAGES DISRUPTING FUEL FLOW TO INTEGRAL FUEL NOZZLES AND LIMITING MAXIMUM AVAILABLE FLOW. THIS RESULTS IN PRESSURE RELIEF VALVE ACTIVATION AND APR HEADROOM FAULT INDICATIONS. MFG IS INVESTSDR CA121206008Lead · failed(CAN) MOC RECEIVED A CALL FROM THE FLIGHT CREW. THE CREW REPORTED DURING THE START OF ENGINE NR 1 THERE WAS NO ITT INCREASE ABOVE 12 DEGREE DURING ROTATION. CREW RESET THE ACFT AND CYCLED THE IGNITION SWITCH TO OFF AND ATTEMPTED ANOTHER START. ON THE 2ND ATSDR 2012FA0000741Gear · obstructedON APPROACH, PILOT UNABLE TO RETARD THE RT THROTTLE COMPLETELY. A SUCCESSFUL LANDING WAS ACCOMPLISHED. INSPECTION REVEALED ONE OF THE DUST COVER SEGMENTS FOR THAT THROTTLE WAS NOT MOVING IN SEQUENCE WITH THROTTLE MOVEMENT. ON FURTHER INVESTIGATION, IT WAS FSDR E07A2012092000001Relay · defectiveBRAKES FADED AND THEN FAILED ON LANDING ROLL OUT. HYDRAULIC PRESSURE INDICATED 0. SUSPECT PRESSURE SWITCH OR HYDRAULIC PUMP RELAY FAILED.SDR E07A2012092000002Pressure Switch · defectiveON LANDING ROLL, BRAKES FADED THEN FAILED. ACFT WAS STOPPED USING EMERGENCY BRAKES. CREW NOTED HYDRAULIC PRESSURE INDICATED 0 ALSO HAS BRAKE FAIL MESSAGE AND LOW HYD PRESSURE CAS MESSAGE. DETERMINED FAULT TO BE PRESSURE SWITCH OR PUMP CONTROL RELAY.SDR CA120917019Shutoff Valve · failed(CAN) ON CLIMB OUT THE ACFT HAD A NR 1 BLEED AIR FAILURE. THE ACFT DIVERTED BACK AND LANDED WITHOUT INCIDENT. LT PYLON PRESSURE REGULATING SHUTOFF VALVE, PRSOV REPLACED.SDR CA120903003Engine · faulted(CAN) DURING TAKE OFF ROLL, THE PILOT RECEIVED A NR 1 ENGINE CONTROL FAULT, WARNING AND ABORTED TAKE OFF. TAXIED BACK TO THE TERMINAL AND RESET THE POWER AND FADEC CIRCUIT BREAKERS BEFORE MAKING A SUBSEQUENT NORMAL TAKE OFF. THE SAME PROBLEM, OCCURRED ON TSDR CA120717008Powerpack · failed(CAN) WHILE IN CLIMB THREW ABOUT 12,000, MLG DROPPED OUT AND AFTER WE REDUCED POWER AND BROUGHT A/S FROM 200 IAS TO 160 IAS THE ACFT WAS THEN LEVELED OFF AND RAN QRH FOR HYD LOW PRESSURE GEAR WAS SELECTED DOWN AND ACFT RETURNED. DURING THE TAXI THE HYD PUMP WSDR CA111123012Control Unit · failed(CAN) UPON LANDING, SKIDDED DUE TO THE RNWY BEING WET. THE WX AT TIME OF LANDING WAS HEAVY RAIN. WHEN THE ACFT STARTED TO SKID, THE CREW DEPLOYED THE EMER BRAKE. BOTH MAIN GEAR TIRES HAVE BEEN FLAT SPOTTED. UPDATED BY THE CREW NOT EXACTLY, WE LANDED & APPLSDR 2011FA0000460Fuel Filter · missingDURING THE FIRST SCHEDULED INSP (600HR/12 MONTH) THE RT ENGINE FUEL FILTER WAS FOUND TO HAVE NEVER BEEN INSTALLED AT THE FACTORY. THE MFG WAS NOTIFIED AND THEY REQUESTED AN ENGINE HOT SECTION BOROSCOPE INSP BE PERFORMED. NO ENGINE DISTRESS WAS OBSERVED AND COSDR CA110614002Fuel Control · malfunctionedPOWER ROLL BACK DURING INITIAL CLIMB N1 SPEED DROPPED TO 50 PERCENT AND T/O RESERVE WAS ACTIVATED. AFTER A FEW SECONDS, THE ENGINE RECOVERED AND OPERATED NORMALLY. AFTER LANDING AT HOME BASE, THE ENGINE WAS VISUALLY INSPECTED AND NO DAMAGE WAS FOUND. ANALYSISSDR CA110223006Heater · failedSTANDBY PITOT/STATIC TUBE HEATER FAILED IN FLIGHT CAUSING THE"STBY HTR FAIL CAS MESSAGE TO ILLUMINATE. TROUBLESHOOTING CONFIRMS THAT THE HEATER ELEMENT HAD BURNED OUT IN THE PROBE. THIS IS THE SECOND PROBE THAT HAS BEEN CHANGED IN THE LAST 3 WEEKS. THE 1STSDR CA110214004Fmu · failedPOWER ROLLBACK, PILOT REPORTED THAT JUST AFTER TAKEOFF (WHILE IN CLIMB), THE LT SIDE ENGINE ROLLED BACK TO 60 PERCENT N2. THE RT SIDE ENGINE REMAINED NORMAL. PILOT PERFORMED AN UNEVENTFUL LANDING AT AIRPORT OF ORIGIN. TROUBLESHOOTING IS ONGOING WITH MFG ASSIS
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