U/A Canada PT6A-60 series
Service difficulty reports · 31
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 = 'PT6A60' 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 = 'PT6A60' 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 CTYA2016040100000Engine · power lossPILOT REPORTED ENGINE RUNNING HOTTER THAN NORMAL, LACK OF POWER.SDR JVWA2016F00085Windshield · crackedRIGHT WINDSHIELD OUTER PANE CRACKED ABOUT 4" FROM THE INBD EDGE OF THE WINDSHIELD.SDR CA140630012Compressor · making metal(CAN) DURING APPROACH, PILOT FELT A STRONG VIBRATION AND AN EXCESSIVE TEMPERATURE RISE IN NR 1 ENGINE, REDUCED POWER. AFTER 2 MINUTES, THE TEMPERATURE INCREASED AGAIN AND THE PILOT PROCEEDED TO TURN OFF THE ENGINE. LANDED ACFT SAFELY. DURING ON GROUND TROUSDR CA140630020Compressor Wheel · seized(CAN) PILOTS EXPERIENCED STRONG VIBRATIONS ON ENGINE NR 1 FOLLOWED BY AN INCREASE IN INTER TURBINE TEMPERATURE (ITT). THEY ATTEMPTED TO REDUCE THE ITT TO NORMAL OPERATING LIMITS BY REDUCING POWER. HOWEVER, AFTER 2 MINUTES, ITT STARTED INCREASING WITHOUT ANY SDR CA140401013Filter · contaminated(CAN) DURING REVENUE FLIGHT, ON APPROACH FOR LANDING, THE PILOT DID NOT HAVE ANY POWER RESPONSE FROM ENG NR 2. THE ENGINE POWER WAS LEFT AT IDLE DURING APPROACH AND LANDED UNEVENTFULLY. DURING GROUND RUN, THE ENGINE POWER STAYED AT 48.5 PERCENT NG, WHICH IS CSDR CA140306001Engine · fire(CAN) REPORTED THAT WHEN BEGINNING DESCENT AN ORANGE GLOW WAS SEEN COMING FROM THE ENGINE. THE ENGINE FIRE LIGHT ILLUMINATED AND THE ENGINE WAS SHUTDOWN. THE FIRE LIGHT WENT OUT UPON SHUTDOWN AND THE FIRE BOTTLE WAS NOT DISCHARGED.SDR CA121119014Fuel Control · malfunctioned(CAN) REPORTING NO THROTTLE RESPONSE WHILE SPOOLING DOWN TO IDLE AT FL180. TROUBLESHOOTING IS ON-GOING AND FOCUSING ON THE FCU.SDR CA120905004Exhaust Duct · damaged(CAN) WHEN PERFORMING A SCHEDULED FUEL NOZZLE REPLACEMENT, A TECH NOTICED WITH THE BORESCOPE A PART OF THE INNER LINER OF THE EXHAUST DUCT PROTRUDING. THE POWER SECTION WAS THEN REMOVED FROM THE GAS GENERATOR AND FURTHER DAMAGE WAS NOTED.SDR 2010FA0000888Strap · crackedDURING A ROUTINE NR3 PHASE INSP, A CRACK WAS FOUND ON A CROSS TIE STRAP. THE STRAP LOCATION WAS ON THE RT SIDE OF THE CABIN INTERIOR AT SL 227.125. THE CRACK APPEARED TO BE A COMPRESSION RELIEF CRACK RUNNING IN A HORIZONTAL FASHION BETWEEN THE UPPER AND LOWER SDR S9BA20100003Bulkhead · corrodedLT BOTTOM SKIN ON AFT BULKHEAD HAS HOLE DUE TO CORROSION. REPAIRED HOLE IAW RD 53-387A AND RD53-387A 8110.SDR UVVR2010060700009Fitting · crackedRT ENGINE INBD ENGINE MOUNT FITTING WAS FOUND CRACKED APPROX .30 INCHES IN LENGTH DURING INSPECTION.SDR 2009FA0000710Bearing · failedFROM MFG: AN ELECTRICAL CURRENT FROM THE STARTER GEN OUT PUT SHAFT DISCHARGED INTO THE ENG ACCESSORY DRIVETRAIN CAUSE AN IN-FLIGHT SHUTDOWN. THE ELECTRICAL DISCHARGE PITTED THE DRIVE GEARS AND NR 1 BRG. THE PITTING OF THE BEARING LEF TO FATIGUE FAILURE OF TSDR 2008F00028Cowling · crackedPOSTFLIGHT RAMP INSP DISCLOSED THAT EACH ENG COWLING HAD SMALL CRACK FWD OF AND CONNECTING TO OTBD AFT LATCHING MECHANISM. CRACKS REPAIRED AND ACFT RETUNED TO SERVICE.SDR CA080618003Seal · leaking(CAN) DURING ENG COMPRESSOR RECOVERY WASH, ENGINE OIL LOSS FROM NR 1 BEARING SEAL. MULTIPLE ENGINE SPOOLS ARE REQUIRED TO COMPLETE AN ENG COMPRESSOR RECOVERY WASH IAW ENG MFG. MAINT FOUND IN CARRYING OUT MULTIPLE ENGINE SPOOLS, INTERNAL ENG SCAVANGE PUMPS LOCASDR UE5R02Gearbox · corrodedPT6A-60AG REDUCTION GEAR REAR HOUSING P/N 3106854-01 HAS SEVERE CORROSION ON OUTER SURFACE OF HOUSING. DEEP PITTING, SOME AREAS UP TO .125 INCH DEEP. CORRODED AREAS EXTEND THE ENTIRE CIRCUMFERENCE OF HOUSING, PRIMARILY NEXT TO MATING FLANGE FOR FWD HOUSING.SDR RU32005F00002Transducer · failedRT ENGINE OIL PRESSURE INDICATION WAS ABOVE 200 PSI. CREW NOTICED SLIGHT OIL SMELL IN AC. PRECAUTIONARY SHUTDOWN OF RT ENGINE IN FLIGHT. ALL OTHER INDICATIONS WERE NORMAL. REPLACED OIL PRESSURE TRANSDUCER. (K)SDR 2004FA0000805Blower · overheatedSMOKE COMING FROM UNDER PILOTS FLOORBOARDS. UPON INVESTIGATION FOUND ENVIRONMENTAL BLOWER MOTOR TOO HOT TO TOUCH. AIRCRAFT LANDED SAFE WITH FIRE DEPARTMENT FOLLOWING. INSPECTION FOUND NO TIME LIMIT ON BLOWER OR MOTOR. (EA23200410155)SDR AUS20040284Case · corroded(AUS) RT ENGINE AIR INLET CASE CORRODED.SDR I5W2003F00000Clevis · failedPILOT REPORTS DURING TAKE OFF LANDING GEAR RETRACTED HARD AND MADE LOUD NOISE, AFTER LANDING A VISUAL INSPECTION WAS PERFORMED. THE NOSE ACTUATOR CLEVIS PN 257063 WAS FOUND TO BE SHEARED OFF JUST ABOVE THE THREADED SECTION OF CLEVIS FITTING. ACTUATOR SHAFT WSDR ACE091103Pump · leakingPILOT NOTICED FUEL LEAKING FROM ENGINE DRAIN ON PRE-FLIGHT. MAINTENANCE REPLACED THE DEFECTIVE PUMP.SDR GMZ2003F00000Blower · failedBLOWER MOTOR WEARS OUT CAUSING BLOWER MOTOR TO START SMOKING FILLING THE AIRCRAFT WITH SMOKE. WHEN THE BLOWER MOTOR IS REMOVED AND INSPECTED. IT IS FOUND THAT THE BRUSHES ARE WORN OUT. RECOMMEND BLOWER ASSEMBLY BE CHANGED EVERY 1000 HOURS. IT WAS ALSO FOUNSDR AW42003F00000Windshield · crackedFOLLOWING DEPARTURE, PILOT`S WINDSHIELD INNER GLASS PANE CRACKED. AIRCRAFT RETURNED TO DEPARTURE WHERE WINDSHIELD WAS REPLACED.SDR 0020Torque Knee · crackedDURING COMPLIANCE OF SB 32-3134 AND AD 2002-01-10, RIGHT LANDING GEAR UPPER TORQUE KNEE WAS FOUND TO BE CRACKED AT PROTRUSION OF CENTER LUG. THIS UNIT HAD BEEN INSPECTED MULTI TIMES PRIOR TO THIS INSPECTION AND PASSED THOSE INSPECTIONS. UNITS EXACT TOTAL TIMSDR RU92003F00000Squat Switch · failedON NOV. 13, 2002 GEAR FAILED TO RETRACT, SQUAT SWITCH FAILED. REPLACED SQUAT SWITCH. OPS CHECK, OK.SDR CA020828006Motor · failed(CAN) ELECTRIC MOTOR ON HYDRAULIC PACK - DRAWS TOO MUCH AMPENAGE. THE SYSTEM IS PROTECTED BY A 60 AMP CIRCUIT BREAKER. THIS ASSY IS OPERATING AT BELOW OR AT THE CIRCUIT BREAKER CAPACITY. THE CB TRIPPED AND THE GEAR WOULD NOT EXTEND. GEAR HAD TO BE HAND PUMPED SDR AUS20020715Bolt · cracked(AUS) LT AND RT WING UPPER REAR AND LOWER REAR ATTACHMENT BOLTS EXHIBIT SIGNS OF CRACKING IN RADIUS. FOUND DURING INSPECTION IAW AD/BEECH 300/8 AND RAYTHEON S.I.R.M.SDR DBC2002F00002Pressure Switch · failedSHORTLY AFTER TAKEOFF, PILOT NOTED LOW PRESSURE FUEL LIGHT ILLUMINATED. PILOT LANDED WITHOUT INCIDENT. TROUBLESHOT TO FAILED FUEL PRESSURE SWITCH. REMOVED (PN 100-398018-23 SN 12948) AND REPLACED WITH NEW UNIT. OPERATIONS CHECKED, OK.SDR 2002FA0000364Window · crackedWINDOW, LOCATED IN UPPER CABIN DOOR, WAS FOUND TO HAVE 4 CONSECUTIVE MOUNTING HOLES BROKEN ALONG LOWER EDGE. A RETAINING RING, CALLED OUT IN PARTS BOOK, WAS NOT INSTALLED ON THIS WINDOW. THE INSTALLATION APPEARS TO HAVE BEEN DONE AT THE FACTORY, DUE TO DATESDR 20010425CW006Hose · burstIN FLIGHT THE LEFT ENGINE OIL COOLER HOSE BURST CAUSING A LOSS OF OIL AND A PRECAUTIONARY ENGINE SHUTDOWN. THE PILOT MADE AN UNEVENTFUL LANDING. BEIN THAT THIS WAS THE SECOND SUCH HOSE THAT HAS FAILED IN THIS METHOD ON THISAIRCRAFT PROBLEM IS SUSPECTED ING TSDR 97ZZZX4217Valve · brokenDISCOVERED ON POST-FLIGHT INSPECTION, NR 1 ENGINE BLEED AIR FLOW CONTROL VALVE HAS A BROKEN CONTROL LINKAGE ARM. APPEARS LIKE BALL SOCKET WORN OUT. REPLACED BLEED AIR CONTROL VALVE ASSEMBLY WITH NEW UNIT OBTAINED FROM BEECH.SDR AU961107Cowling · door failed(AUS) LH INBOARD ENGINE COWL DOOR SEPARATED ALONG HINGE LINE - DAMAGE TO ONE WINDOW AND MINOR SCRATCHES AND DENTS TO FUSELAGE
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