Pratt & Whitney Canada PW308A
Service difficulty reports · 18
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 = 'PW308A' 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 = 'PW308A' 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 2023FA0000407Engine · stalledIN CRUISE THE # 1 ENGINE DID AN UNCOMMANDED SHUTDOWN. THE CREW RESTARTED THE ENGINE BUT OBSERVED THAT THE ITT WAS HIGHER THAN THE OTHER ENGINES. THE POWER LEVER FOR THE # 1 ENGINE WAS BROUGHT BACK TO IDLE AND THE AIRCRAFT DIVERTED TO KTEB.SDR 9JLA2021120731804None · noneTHE FLIGHT CREW REPORTED THAT THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALL DURING TAKEOFF POWER. THIS CONDITION WAS ALLOWED PER MEL AND OPERATIONS WERE CONTINUED WITH NO RESTRICTIONS. THE MAINTENANCE VENDOR DETERMINED THE FAULT WAS INTERNAL WITH THE ENGINE RESDR OZTA2021060323Windshield · failedA/C EXPERIENCED A FAILURE OF THE OUTER PANEL OF THE CO-PILOTS SIDE REAR WINDOW WHILE PASSING THRU FL250 & WITHIN MOMENTS OF CHECKING THE CHECKLIST THE WINDOW HAD A COMPLETE FAILURE FOLLOWED BY DECOMPRESSION. CREW EXECUTED AN EMERGENCY DESENT PROCEDURES & DECLASDR 2020F00108Anti-Ice Valve · bindsFLT. CREW REPORTS DURING CRUISE NUMEROUS CAS MESSAGES RELATED TO AIRCRAFT ANTI-ICE FAIL. AIRCRAFT DIVERTS BACK TO MAINTENANCE BASE KFRG, AFTER TROUBLESHOOTING FAILURE DETERMINED TO BE RH ENGINE ANTI-ICE VALVE INOPERATIVE. VALVE IS REPLACED WITH SERVICEABLE UNISDR 2020F00086Starter · overheatedAIR TURBINE STARTER SEVERE OVERHEAT RH ENGINE CAUSED FLIGHT CREW TO RECEIVE A RH ENGINE FIRE INDICATION DURING TAKEOFF. TAKEOFF WAS ABORTED AT 100 KTS. AIRCRAFT TAXIED BACK TO RAMP AIRPORT FIRE RESCUE DID RESPOND AND DETERMINE THERE WAS NO FIRE BUT AIR TURBINESDR CA160216008Warning Light · illuminated(CAN) THE AIRCRAFT WAS FLYING AT 43000 FT, WHEN THE PILOT EXPERIENCED FADEC FAULT BLUE WARNING THEN FADEC FAULT YELLOW WITH THE EVENTUAL UNCOMMANDED IN FLIGHT SHUTDOWN. THE AIRCRAFT WAS DIVERTED AND LANDED. TROUBLESHOOTING ONGOING.SDR CA151030008Warning System · activated(CAN) DURING TAKEOFF WITH AUTO-THROTTLE ENGAGED AT AN SPEED OF 60KTS, THE LEFT ENGINE FADEC FAULT CAME ON. THE TAKEOFF WAS ABORTED. THE FAULT MESSAGE DISAPPEARED WHEN THE THROTTLES WERE RETARDED TO IDLE. A 2ND TAKEOFF WAS ATTEMPTED WITHOUT AUTO-THROTTLE. WITH SDR CA150713007Vane · damaged(CAN) CUSTOMER REPORTS ENG SURGE AT FL 430. ACFT DESCENDED TO FL 330 & CONTINUED TO DESTINATION. UNEVENTFUL LANDING WAS COMPLETED. NO INJURIES REPORTED, DURING TROUBLESHOOTING, HPC BORESCOPE REVEALED COATING DAMAGES AT THE 4TH STAGE VANE COATING. THE ENG WSDR 7SSA2015102801Radome · cockedAIRCRAFT WAS ON ITS 2ND LEG OF THE DAY ENROUTE. THE LANDING GEAR DID NOT DEPLOY WHEN SELECTED GEAR DOWN. DURING INVESTIGATION IT WAS DETERMINED THE RADOME HAD MOVED AFT ALLOWING THE AFT PORTION TO COVER THE FRONT LIP OF THE NOSE LANDING GEAR DOORS PREVENTING TSDR OZTA20150513001Reservoir · bypassingDURING CRUISE FL 410, THE RT HYD OVERHEAT CAS MSG POSTED. CREW FOLLOWED CHECKLIST DESCENDING TO FL350, CREW NOTED HYD TEMP RISING. AS TEMP STEADILY ROSE CREW ACCOMPLISHED A PRECAUTIONARY RT ENG SHUTDOWN. CREW DECLARED AN EMER & DIVERTED.SDR OZTA2015F00033Manifold · failedCREW EXPERIENCED AN ABNORMAL GEAR EXTENSION. WHEN THE GEAR WAS SELECTED DOWN THE NOSE GEAR DOORS OPENED AND THE NOSE GEAR DID NOT EXTEND. CREW DECLARED A MISS APPROACH AND HELD. CREW CYCLED GEAR 4 TIMES WITH NOSE GEAR NOT DEPLOYING. EMERGENCY GEAR EXTENSION SDR CA141025005Oil System · low pressure(CAN) AIRCRAFT WAS EN ROUTE AT 41,000 FT. WHEN THE RIGHT HAND ENGINE OIL PRESSURE SUDDENLY DROPPED FROM 70 PSI TO ZERO. THE CREW HEARD A RUMBLING NOISE AFTER ENGINE WAS SHUT DOWN. THE AIRCRAFT DIVERTED AND MADE AN UNEVENTFUL LANDING. TROUBLESHOOTING ONGOING.SDR CA131007003Engine · failed(CAN) 5 MINUTES AFTER TAKEOFF, THE PILOT NOTICED A VIBRATION AND OBSERVED THE NR 2 ENGINE OIL PRESSURE HAD DROPPED TO ZERO. THE ENGINE THEN SHUTDOWN BY ITSELF. THE ACFT RETURNED TO THE DEPARTURE AIRPORT WHERE A SINGLE ENGINE LANDING WAS SAFELY ACCOMPLISHED. SDR 2012FA0000629Module · faultedON CLIMBOUT, FADEC FAULT INDICATED, AT 15000 FT ALTITUDE ENGINE NR 1 (LT) ROLLED BACK TO IDOL WITH FADEC FAIL INDICATION. PILOTS WERE UNABLE TO GET CONTROL OF ENGINE. DECLARED AN EMERGENCY AND LANDED WITH LT ENGINE AT IDLE. CONTROL OF RT ENGINE WAS NORMAL. SDR CA110818003Line · damaged(CAN) CUSTOMER REPORTED FUEL LEAK INBOARD IGNITER AREA. DURING WET MOTORING TEST FOUND FUEL COMING FROM BRAIDED FUEL LINE NEXT TO THE IGNITER GUIDE BOSS. PARTICULAR FUEL LINE IS CRIMPPED AND APPEARS TO BE BUBBLING OUT OF THE BOTTOM OF THE CRIMP. AS FUEL PRESSUSDR 2010F00110Pump · making metalDPI FOUND EXTENDED DURING PF INSPECTION. REMOVED FILTER AND FOUND MINOR METAL IN FILTER AND FILTER HOUSING. REPLACE RT HYDRAULIC ENGINE DRIVEN PUMP.SDR 2010F00109Pump · making metalDPI FOUND EXTENDED DURING INITIAL 100 HOUR INSPECTION. REMOVED FILTER AND FOUND METAL IN FILTER AND FILTER HOUSING. REPLACE RT HYDRAULIC ENGINE DRIVEN PUMP.SDR ZES2008F00000Case · corrodedABORTED TAKEOFF, DUE TO RT ENGINE CHIP LIGHT. REMOVED CHIP PLUG FOR INSPECTION, FOUND SMALL DEBRIS, CLEANED, DRAINED AND FLUSHED OIL SYS, INSPECTED OIL FILTER, FOUND NO SIGNIFICANT CONTAMINATION. REINSTALLED FILTER AND SERVICED OIL. GROUND RUN, FOUND NO CHI
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