U/A Canada PT6A-42A
Service difficulty reports · 69
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 = 'PT6A42A' 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 = 'PT6A42A' 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 2CJA20150528001Solenoid · intermittentAT 0915 LOCAL TIME THEY WERE POSITIONED ON AIRPORT HOLDING, SHORT OF RUNWAY 19. NOTICED AIR CONDITIONING WAS NOT MAINTAINING & CABIN WAS GETTING WARM. AFTER CLEARANCE WAS GIVEN FOR TAKEOFF, POWER WAS APPLIED & THE ACFT BEGAN TO SHAKE, FELT LIKE A COMPRESSOR SDR G1IA20150311001Engine · malfunctionedWHILE ON FLIGHT, IN VMC CONDITIONS AT APPROX 0620 AST FL 270 & AT MOUNTAIN INTERSECTION, EXPERIENCED MECHANICAL IRREGULARITIES OF THE RT ENG. INITIALLY THERE WAS A SLOW FLUCTUATION OF TQ, N1 & FF, JUST SUBSEQUENT TO ENCOUNTERING SOME MILD MOUNTAIN WAVE TURBULSDR CA150306013Engine · making metal(CAN) PILOT REPORTED DURING FLIGHT THE NR 1 ENGINE OIL PRESS FLUCTUATED & STARTED DROPPING BELOW 100 PSI. THE CREW DIVERTED. MECHANIC REPORTED THAT HE PULLED THE OIL FILTER & WHEN HE PLACED THE OIL FILTER INTO SOME CLEANING FLUID, THE CLEAR FLUID WENT BLACK.SDR CA150224010Engine · malfunctioned(CAN) THE PLANE CRASHED SHORTLY AFTER TAKEOFF AS A RESULT OF A REPORTED TECHNICAL ISSUE. PRELIMINARY INFORMATION IS STATING ENGINE TROUBLE OCCURRED JUST AFTER TAKEOFF AND THE CRASH IS DESCRIBED AS A FORCED LANDING.SDR 5TNA2015F00027Warning Switch · reversedIN CRUISE, LT BLEED AIR FAIL LIGHT ILLUMINATED. CREW SWITCHED OFF LT BLEED PACK. SIMULTANEOUSLY, THE RT BLEED AIR OFF LIGHT ILLUMINATED. THE PLANE DESCENDED TO AN APPROPRIATE ALTITUDE AND LANDED AT THE DESTINATION. IT WAS DISCOVERED THAT THE RT EVA TUBE HADSDR G1IA20150107001Fire Detector · faultyWHILE ON A MEDEVAC FLIGHT LT ENG FIRE LIGHT CAME ON, THE INDICATIONS VARIED FROM FLICKERING RAPIDLY TO HOLDING STEADY FOR A BIT. LASTED NO MORE THAN 30 SECONDS, PROBABLY LESS, THEN WENT OUT. VISUALLY INSPECTED LT ENG, WHILE FLYING NOTICED NOTHING ABNORMAL, ALSDR MK9A20150102001Spline · wornWHILE ACCOMPLISHING SCHEDULED MX ON ACFT, NOTICED SLIGHT CHIPS OF METAL WERE FOUND ON THE AGB CHIP DETECTOR. THE AIR CONDITIONING COMPRESSOR WAS ABLE TO SPIN MORE FREELY THAN NORMAL WHEN HE CHECKED THE ROTATION UNIT. WHEN HE PULLED THE COMPRESSOR DRIVE UNIT SDR MGOR2014082759615Turbine Blades · separatedPILOT REPORTED 60 DEGREE TEMP SPLIT AT IDLE. BORESCOPE OF ENGINE REVEALED COMPRESSOR TURBINE BLADE SEPARATION.SDR CA140804011Seal · leaking(CAN) A FUEL LEAKAGE WAS FOUND FROM FMM SEAL DRAIN. SINCE THE FUEL LEAKAGE FROM SEAL DRAIN REACHED TO 50CC/HOUR, THEY DECIDED TO REPLACE THE UNIT. THE UNIT WILL BE REPLACED WITH A SERVICEABLE ONE AND THE REMOVED UNIT WILL BE SENT TO A SHOP FOR REPAIR/INVESTIGSDR F2PA20131126001Duct · unserviceableLEFT BLEED AIR FAIL WARNING LIGHT ILLUMINATED IN FLIGHT. RETURNED TO AIRPORT WITH LT BLEED AIR TURNED OFF IAW POH. NO BLEED LEAK WAS FOUND & THE WARNING SYS WAS RESTORED. ON A SECOND OCCASION, 1.5 FLIGHT HOURS LATER, WHILE ON THE GND DURING TAXI IN FROM A FLSDR 9PMA201304240001Resistor · burnedFOUND EMERGENCY LIGHTS ON BUT SWITCHES WERE OFF. PULLED CIRCUIT BREAKERS, LIGHT WENT OUT. SEVERAL HOURS LATER, ON PREFLIGHT, DISCOVERED BLACK SOOT COMING OUT OF ENGINE COWLING. DISCOVER WHAT APPEARS TO BE AN ELECTRICAL FIRE HAD OCCURRED. APPEARS THAT ASDR O9IA201212110001Fire Detector · false activationSHORTLY AFTER TAKEOFF THERE WAS A FIRE WARNING LIGHT ON THE LT ENGINE. CREW ELECTED TO RETURN TO DEPARTURE. ALL GAUGES WERE IN THE GREEN AND THERE WAS NO VISIBLE INDICATIONS OF SMOKE OR FIRE COMING FROM THE ENGINE. CREW ELECTED NOT TO SHUT THE ENGINE DOWN. SSDR O9IA201211161107Skin · corrodedDURING ROUTINE PHASE INSPECTION, TECH IDENTIFIED A BUBBLE IN THE PAINT ON LT SIDE OF FUSELAGE BELOW THE PILOTS DV WINDOW. UPON INVESTIGATING THE BLISTER, A HOLE THROUGH THE SKIN WAS IDENTIFIED UNDER THE PAINT. HOLE SIZE APPROX .7500" IN SIZE. APPEARANCE OF SDR 7EMA201214010512Fire Detector · false activationAT 17:36 ACFT LIFTED OFF FROM RUNWAY AND WAS CLIMBING IN THE RT TURN DIRECT HEADING OF 300. PROPS WERE AT 1900 AND ALL ENGINE INDICATIONS WERE NORMAL. THE SUN WAS JUST SETTING AT 10 O'CLOCK POSITION. AFTER LEVELING OFF AND BEGINNING TO ADJUST PROPS TO 1700,SDR 2010F00220Current Limiter · failedNR2 CURRENT LIMITER FAILED CAUSING THE NR2 GENERATOR TO DROP OFF LINE WHEN GEAR WAS SELECTED. THE PILOT SELECTED THE NR2 GENERATOR SWITCH TO OFF AND DONE A MANUAL EXTENSION FOR LANDING AT THE ORIGINAL DESTINATION. NO FURTHER DIFFICULTIES WERE REPORTED. THE BASSDR Q3EA924KCircuit Breaker · poppedNUMBER TWO BUS FEEDER BREAKERS POPPED CAUSING A LOSS OF GEAR STATUS INDICATION. PILOTS CHOSE TO EXTEND GEAR MANUALLY AND DECLARED AN EMERGENCY SINCE GEAR DOWN POSITION COULD NOT BE VERIFIED.SDR IFJA2010FA0000459Engine · leakingENGINE S/N 93901 WAS INSTALLED ON ACFT S/N BB-1219 AFTER OVERHAUL, DURING THE OPERATIONAL CHECK FLIGHT THE PILOT NOTICED SMOKE IN THE COCKPIT AND ABORTED THE CHECK FLIGHT RETURNING TO THE AIRPORT WITHOUT INCIDENT. AFTER TROUBLESHOOTING AND SPEAKING TO A TECH RSDR 35741Fire Detector · false activationDEPARTING TUCSON, DURING CLIMBOUT, NW BOUND, COPILOT ANNOUNCED "MASTER WARN - RT ENG FIRE". NO OBVIOUS INDICATION OF A FIRE. REQUESTED A CHANGE OF COURSE DUE TO THE FIRE DETECTION SYS DESIGN - PHOTO-SENSITIVE. AFTER FLYING THE NEW HEADING FOR APPROX 3 MIN, SDR SJ3R080124001Cam Follower · brokenREMOVED DUE TO SUSPECTED INTERNAL HUB COMPONENT FAILURE. BLADE S/N 4152 WAS FOUND TO ROTATE FREELY +/- 12.5 DEGREE POST FIRST GROUND RUN AFTER INSTALLATION. INSPECTION AFTER DISASSEMBLY REVEALED ONE BROKEN B-6545 PITCH CHANGE KNOB CAM FOLLOWER. THIS PART WAS
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