U/A Canada PT6A-15AG
Service difficulty reports · 23
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 = 'PT6A15AG' 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 = 'PT6A15AG' 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 CA160203003Engine · power loss(CAN) DURING CRUISE, THE ENGINE HAD A POWER ROLL BACK AND THE PILOT WAS NOT ABLE TO RECOVER POWER VIA POWER LEVER (PLA) COMMAND. ELECTED TO RETURN TO HIS DEPARTURE POINT WHERE AN UNEVENTFUL LANDING WAS MADE. AFTER THE EVENT THE ENGINE WAS STARTED AND IT TOOK SDR CA160203016Engine · power loss(CAN) WHILE THE ACFT WAS RETURNING FOR LANDING AFTER CROP-DUSTING FLIGHT, THE ENGINE POWER DROPPED AND REMAINED AT IDLE. THE PILOT PERFORMED A PRECAUTIONARY LANDING IN A PASTURE AREA. ACFT SUSTAINED NO DAMAGED AND THE PILOT WAS NOT INJURED.SDR CA150316007Pulley · loose(CAN) ON ENGINE SHUTDOWN A CLICKING SOUND WAS HERD UNDER ENGINE COWLING. UPON INVESTIGATION IT WAS NOTICED THAT THE AIR CONDITIONER COMPRESSOR DRIVE PULLEY ALLEN SCREW HAD LOOSENED OFF AND THE DRIVE PULLEY WAS SLIPPING. DRIVE PULLEY, DRIVE PAD ASSY AND BELT WSDR CA140120001Engine · stalled(CAN) DURING A TEST FLIGHT FOLLOWING PROPELLER GOVERNOR REPLACEMENT, AS THE ACFT WAS ON SHORT FINAL, THE PILOT REPORTED IT STALLED BEFORE CRASHING TO THE GROUND SOME 100 FT SHORT OF INTENDED LANDING STRIP. NO OTHER DETAILS ARE AVAILABLE ON THE CIRCUMSTANCESSDR CA120213009Engine · power loss(CAN) DURING CLIMB, THE ACFT LOSS ENGINE POWER AND THE PILOT MADE A FORCED LANDING INTO A FIELD. THE ACFT SUSTAINED SUBSTANTIAL DAMAGE. NO INVESTIGATION WAS REPORTEDLY UNDERTAKEN BY THE ATSB.SDR CA110929006Engine · fluctuates(CAN) AFTER T/O AT AN ALTITUDE OF 350-400 FT, THE ENGINE TORQUE AND SPEEDS BEGAN TO FLUCTUATE FOLLOWED BY AN UNCOMMANDED POWER LOSS. THE PILOT DUMPED THE CONTENTS OF THE HOPPER AND RETURNED TO THE DEPARTURE STRIP WHERE HE LANDED SAFELY. TROUBLESHOOTING IS ON-SDR CA110929003Engine · power loss(CAN) UPON REDUCING POWER FOR LANDING, THE ENGINE WOULD NOT DECREASE BELOW 75 PERCENT. THE PILOT ELECTED TO SHUTDOWN THE ENGINE DURING FINAL, HOWEVER HE MISJUDGED THE ALTITUDE REQUIRED TO GLIDE IN AND HE LANDED SHORT OF THE PRIVATE AIRSTRIP. THE ACFT WAS TOTASDR 2011FA0000424Engine · failedAG AIRCRAFT DUMPED A LOAD AND WAS RETURNING TO LAND WHEN THE PILOT LOST ENGINE POWER. EXECUTED A CRASH LANDING IN A WHEAT FIELD WITH SUBSTANTIAL DAMAGE TO THE AIRCRAFT. NO INJURIES TO THE SINGLE PILOT OCCUPANT.SDR CA100903006Engine · failedACCIDENT DURING TAKEOFF FROM AIRPORT, THE PILOT REPORTED SMOKE FROM THE EXHAUST DUCT. HE CLIMBED 10 TO 15 FEET AGL, AND REALIZED THE AIRPLANE WAS NOT ACCELERATING OR DECELERATING AND BEGAN TO MUSH. THE AIRPLANE TOUCHED DOWN ON GRASS BEYOND THE DEPARTURE END OSDR CA070914004Engine · power loss(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION DURING SPRAYING OPERATIONS RESULTING IN A FORCED LANDING AND SUBSTANTIAL AIRFRAME DAMAGE. MFG WILL MONITOR INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070914004)SDR CA060531008Engine · failed(CAN) THE ENGINE WAS REPORTED TO HAVE LOST POWER IN FLIGHT LEADING TO A FORCED LANDING AND RESULTANT AIRFRAME DAMAGE. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060531008)SDR 2005FA0001493Spar · separatedTHE MAIN SPARS (PN 4500-01 AND 4500-02, RT AND LT) WERE BROKEN AWAY FROM THE WINGLET. WINGLETS AND SPAR ARE PART OF STC INSTALLATION. SPAR IS ATTACHED TO INSIDE WINGLET WITH FIBERGLASS CLOTH. CLOTH WAS TORN AND DELAMINATED. SPAR WAS COMPLETELY SEPARATED FRSDR AU510001855Rod End · brokenLT HORIZONTAL STABILIZER ATTACHMENT BOLT BROKEN AT TOP OF THREADED AREA UNDER CLEVIS. FOUND WHEN STABILIZER REMOVED FOR PAINTING. INSPECTION FOUND ALL OTHER ATTACHMENT BOLTS RUSTED AND PITTED IN THE SAME AREA.SDR AUS20030470Longeron · cracked(AUS) FUSELAGE LONGERON CRACKED IN AREA INDICATED IN SL195.SDR AUS20021371Plate · cracked(AUS) VERTICAL FIN FRONT SPAR ATTACHMENT FITTING FAILED. REAR SPARCRACKED.SDR AU001115Spar Cap · cracked(AUS) LEFT SPAR CAP CRACKED IN AREA OF THE HOLE LOCATED 3 MM (0.118 INCHES) FORWARD ALONG THE BOTTOM FACE AND 8 MM (0.314 INCHES) UP THE HOLE. FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AT/20 SL 197. (X)SDR AU000355Tube · cracked(AUS) FUSELAGE VERTICAL TUBE CRACKED AT WING ANGLE ATTACHMENT POINT.SDR AU990949Turbine Disc · cracked(AUS) COMPRESSOR TURBINE DISC CRACKED ON THE TRAILING EDGE SIDE ADJACENT TO THE BALANCE RIM IN THE WEB AREA. ONE CONFIRMED CRACK AND ONE SUSPECT CRACK. FOUND DURING NDI.SDR AU990811Torque Tube · cracked(AUS) ELEVATOR TORQUE TUBE CRACKED.SDR AU990517Rib · cracked(AUS) HORIZONTAL STABILIZER NOSE RIBS CRACKED AT THE FORWARD EDGE ALONG THE FLANGE RADIUS.SDR AU990019Spar · cracked(AUS) WING FRONT SPAR SPLICE RIGHT OUTBOARD HOLE HAS A SMALL CRACK AT THE INBOARD LOWER CORNER OF THE SPAR SECTION RUNNING UP THE BOLT HOLE. CRACK LENGTH APPROXIMATELY 3.175 MM (0.125 INCH). FOUND DURING NDT INSPECTION IAW AD/ACSNOW/24 AMDT1.SDR AU971582Engine · failed(AUS) ENGINE SUFFERED COMPLETE FAILURE DURING CRUISE - CAUSE UNKNOWN AT THIS STAGE.SDR AU961085Bracket · broken(AUS) FORWARD FIN ATTACHMENT BRACKET BROKEN IN AREA DESCRIBED IN AIRTRACTOR SB 138 - AIRCRAFT IS FITTED WITH A 6.35MM (0.25IN)PLATE
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