Pratt & Whitney Canada PW305
Service difficulty reports · 78
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 = 'PW305' 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 = 'PW305' 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 JBGA20050002Engine · flamed outENGINE FLAME OUT FOLLOWED BY AMBER ENGINE LIGHT. ENGINE RELIGHT NORMAL. ENGINE CONTINUED OPERATION NORMAL.SDR 2005FA0000407Strut · damagedDURING 300 HOUR INSPECTION (GEAR SERVICE) THE INNER STRUT CHROME WAS FOUND DAMAGED APPROXIMATELY .001 INCH DEEP. PROBABLE CAUSE: WEAR OF SEALS CAUSING THE UPPER CAM TO CONTACT THE INNER CYLINDER. INSPECTION REPACK OF THE NOSE LANDING GEAR ASSY AT 3,000 LANDISDR DXTA200400503Oil System · overservicedIMMEDIATELY AFTER AIRBORNE & SELECTING MAIN AIR VALVE TO ON, SMOKE BEGAN TO BELLOW THROUGHOUT THE COCKPIT AND CABIN AREAS. MAIN AIR VALVES WERE IMMEDIATELY SELECTED OFF AND RAM AIR SELECTED TO FULL ON, TO HELP CLEAR THE COCKPIT. ON THE GROUND, ON REINSPECTIOSDR REXA04044Control Unit · inoperativeFLAPS FAILED AT 20 ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAP ON 72 HOUR WATCH IAW AD 98-20-01.SDR 2005FA0000088Holder · destroyedAIRCRAFT WAS SQUAWKED WITH NR 1 ALTERNATOR DROPPING OFF IN FLIGHT. DURING TROUBLESHOOTING THE TECHNICIAN FOUND SMOKE TRAILS ON THE GG PANEL. LOCATED ON THE AFT SIDE OF THE REAR FACE OF THE PRESSURE BULKHEAD. A MORE CLOSE INSPECTION REVEALED A DESTROYED FUSESDR 2005FA0000260Alternator · failedAIRCRAFT WAS SQUAWKED WITH NR 1 ALTERNATOR DROPPING OFF IN FLIGHT. DURING TROUBLESHOOTING THE TECHNICIAN FOUND SMOKE TRAILS ON THE (GG PANEL), LOCATED ON THE AFT SIDE OF THE REAR FACE OF THE PRESSURE BULKHEAD. A MORE CLOSE INSPECTION REVEALED A DESTROYED FUSDR DXTA200400428Brake Assy · malfunctionedWHEN APPLYING THE BRAKES FROM THE LT SEAT, THE FIRST APPLICATION RESULTS IN ALMOST NO BRAKING ACTION. THE PEDALS GO TO THE STOPS WITH VERY LITTLE RESULTS. BREAKING ACTION RETURNS TO NORMAL AFTER THE PEDALS ARE RELEASED AND RE-APPLIED. ITEM IS UNDER INVESTISDR 4122Line · blownAIRCRAFT IN ROUTE TO BTV FROM LNS SELECTED GEAR DOWN. DID NOT GET ALL THREE DOWN AND LOCK INDICATIONS, DIVERTED TO BDL BLEW GEAR DOWN AND LANDED NO PROBLEMS. MAINTENANCE FOUND HYD. LINE ON RT ENGINE PRESSURE LINE HAD BLOWN DEPLETING ALL FLUID FROM RESERVOIR.SDR DXTA200400391Coalescer Bag · dirtyON DESCENT WITH POWER LEVERS AT IDLE NOTICED EXHAUST FUME ODOR IN CABIN. REMOVED COALESOR SOCK AND INSTALLED NEW IAW MFG M/M CHAPTER 21-50-13. RAN AIRCRAFT AND LEAK CHECKED, NO LEAKS NOTED, COULD NOT DUPLICATE SMELL AT IDLE ON GROUND.SDR O2G2004F00009Overheat Loop · malfunctionedDURING DEPARTURE, BOTH RED BLEED AIR LIGHTS ILLUMINATED. TURNED RT BLEED AIR SWITCH OFF, LIGHTS STAYED ON. TURNED RT BLEED AIR SWITCH ON, TURNED 1 BLEED AIR SWITCH OFF, LIGHTS STAYED ON. WITH RT BLEED AIR SWITCH ON AND RT ENGINE TO IDLE AND LEFT BLEED AIR SSDR DXTA200300009Engine · overservicedIN FLIGHT DENSE BLACK SMOKE CAME OUT OF THE COPILOTS AIR CONDITIONER VENT. SHORTLY AFTER THAT REAR BAGGAGE SMOKE ANNUNCIATOR ON THE MASTER WARNING PANEL ILLUMINATED.SDR WVE2002F00017Duct · damagedDURING 300 HOUR INSPECTION, THE UPPER COWLING WAS REMOVED FOR MINOR INSPECTION. DAMAGE WAS NOTED TO THE UPPER BYPASS DUCT. DURING FURTHER INVESTIGATION, DAMAGE WAS ALSO NOTED ON THE RIGHT AND LEFT INNER CORE COWLS. TO BE EVALUATED BY MFG.SDR WVE2002F00003Control Cable · wornDURING ROUTINE MAINTENANCE THE LEFT AND RIGHT FLAP CABLE (PN 2300003-152/155) ASSEMBLIES WERE FOUND WORN AND FRAYED AT WS 82 PULLEY SECTOR. A.C.T.T. 4174:52 A.C.T.C. 2945. PROBABLE CAUSE: FATIGUE OF CABLE AROUND A SMALL DIAMETER PULLEY. RECOMMENDATION: SDR BAC2002F00000Bleed Valve · stuckLEFT AND RIGHT BLEED LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM AND FOUND RIGHT HAND BLEED AIR MIXING VALVE TO BE STUCK IN THE FULL OPEN POSITION CAUSING EXCESSIVE HIGH PRESSURE BLEED AIR AND TEMSDR UXF2002F00000Lamp · inoperativeFLUORESCENT LAMP 22 INCHES LONG, MODEL F00100 HAS EVIDENCE OF SEVERE OVERHEATING (CHARRING) AT ONE END OF LAMP. LAMP USED IN GALLEY/CABIN LIGHTING SYSTEM.SDR 20000406SH057Ignitor · failedRECEIVED 3 EACH IGNITORS FROM SUPPLY. THE 4TH IGNITOR OPS CHECKED OK. BATCH NUMBER UNKNOWN. THE IGNITOR USED NORMALLY IS INSTALLED ON P&W 305 SERIES ENGINES. P/N 34682. (X)SDR 20000707SH014Igniter · defectiveRECEIVED 3 EACH IGNITERS. THE 4TH IGNITER OPS CHECKED OK. BATCH NUMBER UNKNOWN. THE IGNITER USED NORMALLY IS INSTALLED IN P&W 305 SERIES ENGINES. (PN 34682). (X)SDR 20000707SH013Igniter · failedRECEIVED 2 EACH IGNITERS. THE THIRD IGNITER OPS CHECKED OK. BATCH NUMBER UNKNOWN. THE IGNITER USED NORMALLY IS INSTALLED IN PWA 305 SERIES ENGINES. (P/N CH34682). (X)SDR 98ZZZX4206P3 Line · brokePILOTS DISCREPANCY WAS NR 1 ENGINE TEMPORARILY LIMITED ABOVE CRUISE DETENT. REMOVED THE OUTBOARD INNER BYPASS ACCESS TO CHECK BLEED VALVES. UPON INVESTIGATION, FOUND THE BLEED AIR (P3 LINE) BROKEN AT B-NUT, P/N 3081695. IT APPEARED THE FIT OF THE LINE HAD CSDR 98ZZZX4648Line · brokenPILOT'S DISCREPANCY WAS NR 1 ENIGNE IS TEMP LIMITED ABOVE CRUISE DETENT. REMOVED THE OUTER AND INNER BYPASS ACCESS TO CHECK BLEED VALVES. UPON INVESTIGATION, FOUND THE BLEED AIR (P3 LINE) BROKEN AT B-NUT, P/N 3081695. IT APPEARED THE FIT OF THE LINE HAD CAUSDR 98ZZZX3222Tube · brokenRIGHT HAND ENGINE OUTBOARD BLEED AIR VALVE P3 LINE FOUND BROKEN AT WELDED 'L' FITTING. BY VISUAL INSPECTION, SUSPECTED CAUSE IS VIBRATION AND FATIGUE AND POSSIBILITY OF FLAW IN WELD.SDR AU971506O-Ring · failed(AUS) NO1 ENGINE HYDRAULIC PUMP HIGH PRESSURE FITTING `O' RING SEAL FAILED. LOSS OF HYDRAULIC FLUID.SDR 97ZZZX4737N2 Probe · defectiveDURING 40-HOUR FLT, LT ENG COMPUTER LIGHT ILLUMINATED. UPON LANDING, AN 'EA' FAULT (N2 INPUT INTERFACE) IN THE ENG (EDU) CLEARED AFTER CYCLING PWR. HANDBOOK STATED 'CONT NORMAL ENG OPER". ON NEXT LEG DURING DESCENT THRU 25K FT, LT ENG SHUT DOWN. EDU CONTAISDR CA971112006Hmu · faulty(CAN) DURING LEVEL FLIGHT AT FL 140, THE NR 1 ENGINE LOW FUEL PRESSURE WARNING LIGHT ILLUMINATED FOLLOWED BY AN AUDIBLE ENGINE SHUTDOWN. THE AIRCRAFT DIVERTED AND AN UNEVENTFUL LANDING WAS CARRIED OUT. POST-FLIGHT INVESTIGATION FOUND A PROBLEM WITH THE HYDRO SDR CA970910017Lpt Disk · mis manufacture(CAN) A TURBINE DISK MACHINED, AS A TRIAL, TO AN UNAPPROVED PROCESS WAS ERRONEOUSLY ASSEMBLED INTO A MODULE AND SUBSEQUENTLY BUILT INTO ENGINE CA0043 CURRENTLY ON LEARJET 60-103. THE UNAPPROVED PART WAS REPLACED. THIS IS AN ISOLATED CASE AND NO OTHER DISKS ARESDR 97ZZZX375Eec · failedDURING INITIAL CLIMB, AT 15,500 FEET, THE LT ENGINE AMBER COMPUTER LIGHT ILLUMINATED. FIFTEEN SECONDS LATER THE LT ENGINE FLAMED OUT. TWO RESTART ATTEMPTS WERE UNSUCCESSFUL. INVESTIGATION REVEALED A BLEED AIR CLAMP HAD COME OFF ALLOWING BLEED AIR TO FLOW INSDR 96ZZZX4015Pump · housing crackedEXCESSIVE OIL LEAK ON LEFT ENGINE. FOUND OIL PUMP HOUSING CRACKED AT UPPER LEFT BOLT HOLE AREA. SUBMITTER STATED THIS IS TURNING INTO A FLEET-WIDE CONCERN AS THIS CAN CAUSE AN ENGINE SHUTDOWN IN FLIGHT. OTHER OPERATORS HAVE EXPERIENCED THIS SAME CRACK. AD SDR 96ZZZX2242Eec · malfunctionAMBER AND WHITE COMPUTER LIGHTS CAME ON AND ITT INDICATION WAS LOST FOR THE LEFT ENGINE; OTHERWISE, OPERATION WAS NORMAL IN-FLIGHT. ENGINE WOULD NOT START ON GROUND. NO ITT INDICATION CAUSED THE FADER TO ABORT START ATTEMPTS. REPLACED E.E.C. OPERATION NORM
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