Pratt & Whitney Canada PW305

Service difficulty reports · 78

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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 = '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.

SDR JBGA20050002Engine · flamed outENGINE FLAME OUT FOLLOWED BY AMBER ENGINE LIGHT. ENGINE RELIGHT NORMAL. ENGINE CONTINUED OPERATION NORMAL.Apr 15, 2005 · N529KF · Lear 60LEAR · Engine (Turbine/Turboprop)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 LANDIMar 8, 2005 · N247FX · Lear 60LEAR · Main Landing Gear Strut/Axle/TruckSDR 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 REINSPECTIODec 30, 2004 · N544QS · Braero HAWKER1000 · Turbine Engine Oil SystemSDR 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.Dec 13, 2004 · N8505Q · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR 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 FUSEDec 9, 2004 · N533QS · Braero BAE1251000A · AC Power Distribution SystemSDR 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 FUDec 9, 2004 · N533QS · Braero BAE1251000A · AC Power Distribution SystemSDR 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 INVESTIOct 17, 2004 · N548QS · Braero HAWKER1000 · Landing Gear Brake SystemSDR 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.Sep 26, 2004 · N560AN · Lear 60LEAR · Hydraulic System, MainSDR 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.Sep 14, 2004 · N505QS · Braero BAE1251000 · Humidity Control SystemSDR 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 SJun 11, 2004 · N14TU · Lear 60LEAR · Overheat DetectionSDR 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.Mar 16, 2003 · N551QS · Braero HAWKER1000 · Turbine Engine Oil SystemSDR 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.Aug 19, 2002 · N229FX · Lear 60LEAR · Pneumatic SystemSDR 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: Mar 4, 2002 · N220FX · Lear 60LEAR · Trailing Edge Flap Control SystemSDR 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 TEMFeb 13, 2002 · N8271 · Lear 60LEAR · Compressor Bleed ValveSDR 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.Nov 16, 2001 · N119U · Braero BAE1251000 · Passenger Compartment LightingSDR 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)Feb 9, 2000 · Spark Plug/IgniterSDR 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)Feb 9, 2000 · Spark Plug/IgniterSDR 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)Jan 26, 2000 · Spark Plug/IgniterSDR 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 COct 6, 1998 · N530QS · Braero BAE1251000 · Fuel Controlling SystemSDR 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 CAUOct 6, 1998 · N530QS · Braero BAE1251000A · Compressor Bleed ControlSDR 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.Aug 1, 1998 · N513QS · Braero BAE1251000 · Compressor Bleed ControlSDR AU971506O-Ring · failed(AUS) NO1 ENGINE HYDRAULIC PUMP HIGH PRESSURE FITTING `O' RING SEAL FAILED. LOSS OF HYDRAULIC FLUID.Nov 25, 1997 · Braero BAE1251000 · Hydraulic Pump (Electric/Engine), MainSDR 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 CONTAIOct 10, 1997 · N8271 · Lear 60LEAR · Fuel Controlling SystemSDR 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 Oct 10, 1997 · Fuel Control/Reciprocating EnginesSDR 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 AREAug 25, 1997 · Lear 60LEAR · Turbine SectionSDR 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 INDec 16, 1996 · N8271 · Lear 60LEAR · Fuel Controlling SystemSDR 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 Jul 30, 1996 · N65BL · Lear 60LEAR · Turbine Engine Oil SystemSDR 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 NORMFeb 28, 1996 · N799SC · Lear 60LEAR · Fuel Control/Turbine Engines
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