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.

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 Jan 19, 2016 · Engine (Turbine/Turboprop)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.Jan 18, 2016 · Engine (Turbine/Turboprop)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 WMar 13, 2015 · Airtrc AT402B · Cabin Cooling SystemSDR 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 CIRCUMSTANCESJun 13, 2013 · Engine (Turbine/Turboprop)SDR 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.Jan 20, 2012 · Ayres S2RR1820 · Engine (Turbine/Turboprop)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-Sep 21, 2011 · Engine (Turbine/Turboprop)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 TOTAAug 10, 2011 · Airtrc AT400 · Engine (Turbine/Turboprop)SDR 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.Jun 28, 2011 · N1022N · Airtrc AT502 · Engine (Turbine/Turboprop)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 OAug 28, 2010 · Airtrc AT402B · Engine (Turbine/Turboprop)SDR 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)Jul 2, 2007 · Ayres S2RT15RESTD · Engine (Turbine/Turboprop)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)Apr 28, 2006 · Airtrc AT502 · Engine (Turbine/Turboprop)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 FROct 20, 2005 · Airtrc AT402 · Wing SparSDR 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.Jun 9, 2005 · Ayres S2RT15RESTD · Horizontal Stabilizer, Attach FittingsSDR AUS20030470Longeron · cracked(AUS) FUSELAGE LONGERON CRACKED IN AREA INDICATED IN SL195.May 2, 2003 · Airtrc AT502 · Fuselage Main, Longeron/StringerSDR AUS20021371Plate · cracked(AUS) VERTICAL FIN FRONT SPAR ATTACHMENT FITTING FAILED. REAR SPARCRACKED.Nov 25, 2002 · Airtrc AT502B · Vertical Stabilizer, Attach FittingsSDR 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)Nov 23, 2000 · Airtrc AT502 · Wing SparSDR AU000355Tube · cracked(AUS) FUSELAGE VERTICAL TUBE CRACKED AT WING ANGLE ATTACHMENT POINT.May 4, 2000 · Airtrc AT502B · Fuselage Main, FrameSDR 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.Sep 14, 1999 · Turbine SectionSDR AU990811Torque Tube · cracked(AUS) ELEVATOR TORQUE TUBE CRACKED.Aug 2, 1999 · Airtrc AT502 · Elevator StructureSDR AU990517Rib · cracked(AUS) HORIZONTAL STABILIZER NOSE RIBS CRACKED AT THE FORWARD EDGE ALONG THE FLANGE RADIUS.May 27, 1999 · Airtrc AT502 · Horizontal Stabilizer, Spar/RibSDR 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.Jan 13, 1999 · Ayres S2RT15NORMAL · Wing SparSDR AU971582Engine · failed(AUS) ENGINE SUFFERED COMPLETE FAILURE DURING CRUISE - CAUSE UNKNOWN AT THIS STAGE.Dec 30, 1997 · Ayres S2RT15NORMAL · Engine (Turbine/Turboprop)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)PLATEAug 7, 1996 · Airtrc AT502 · Fuselage, Stabilizer Attach Fittings
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