U/A Canada PT6A-65B
Service difficulty reports · 628
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 = 'PT6A65B' 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 = 'PT6A65B' 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 YADA2025051001Housing · erodedFLIGHT CREW REPORTED THE #1 ENGINE LEAKING OIL - MAINTENANCE LOCATED A PINHOLE ON THE ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED THE HOUSING DUE CAVITATION EROSION THROUGH THE PUMP BODY.SDR YADA2025012701Pump · erodedMAINTENANCE DISCOVERED A LEAKING ENGINE OIL SCAVENGE PUMP - A PINHOLE WAS VERIFIED IN THE PUMP HOUSING OUTER WALL FROM INTERNAL EROSION - REPLACED SAME.SDR YADA2025012201Housing · erodedMAINTENANCE NOTICED OIL LEAKING FROM #2 ENGINE COWLING. INSPECTION REVEALED OIL LEAKING FROM THE SCAVENGE OIL PUMP HOUSING PINHOLE AND REPLACED HOUSING. REMOVED UNIT WAS VERIFIED TO HAVE INTERNAL EROSION THROUGH BODY OF THE HOUSING. THIS HAS BECOME A COMMOSDR TIMA20240920012Engine · power lossON DESCENT TO RWY 27, ON ABOUT AN 8 MILE FINAL I REDUCED POWER TO SLOW DOWN. WHEN I WENT TO ADD POWER ONCE AGAIN THE LH SIDE PRODUCED NO ADDITIONAL THRUST. UPON LOOKING AT THE ENGINE INDICATIONS I NOTICED N1 WAS AT 35%, AUTO IGNITION WAS ACTIVATED, AND AUTO FESDR TIMA20240917011Engine · low torqueTAXIED FROM THE RAMP INTO THE RUN UP AREA, DID RUN UPS AS NORMAL NOTHING ABNORMAL DETECTED. TOOK OFF 16L REACHED V1 AND ROTATED AS I NOTICED THE PLANE WAS A LITTLE SLUGGISH TO LEAVE THE GROUND AS I GOT AIRBORNE I NOTICED THE TORQUE FOR THE LEFT ENGINE STARTINGSDR YADA2024060351101Housing · erodedPILOT REPORTED OIL LEAK ON #1 ENGINE AFTER FLIGHT - MAINTENANCE LOCATED LEAK AT #1 ENGINE SCAVENGE PUMP HOUSING AND REPLACED SAME.SDR YADA2024042401Housing · erodedMAINTENANCE DISCOVERED A LEAKING ENGINE OIL SCAVENGE PUMP - A PINHOLE WAS VERIFIED IN THE PUMP HOUSING OUTER WALL FROM INTERNAL EROSION - REPLACED SAME.SDR YADA2023110401Housing · erodedPILOT REPORTED SEEING OIL ON RH WING DURING PREFLIGHT. MAINTENANCE IDENTIFIED A LEAK FROM A HOLE IN THE RH ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED SAME. THIS IS A COMON ISSUE WITH THESE PUMP HOUSINGS.SDR TIMA20231031008Unknown · unknownNORMAL TAXI/RUN UP/TAKEOFF / CLIMB. AS I WAS LEVELING OFF FUEL PRESSURE LOW ON RH ENG ILLUMINATED, SWITCHED ON STANDBY PUMP AND LIGHT EXTINGUISHED LOOKED FOR AND FOUND NO SECONDARY INDICATIONS OF IMPENDING FAILURE. REDUCED POWER TO CRUISE SETTING AND SCANNED SDR YADA2023071301Housing · erodedPILOT REPORTED OIL LEAKING OUT OF RIGHT ENGINE. MAINTENANCE DISCOVER #2 ENGINE OIL SCAVENGE PUMP HAVING A PINHOLE LEAK AND THE HOUSING WAS REPLACED. INSPECTION DETERMINED THAT CAVITATION EROSION OF THE PUMP BODY IN A CORNER OF THE CAVITY HAD CREATED A HOLE. SDR JIKA20230116001Seal · leakingPILOT REPORTED THAT UPON APPROACH TO KRDM THE RT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED. PILOT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM TO A LEAK COMING FROM RH ENGINE OIL SCAVENGE PUMP. MAINTENANCE REMOVED AND RESDR YADA2022100301None · erodedDURING UNRELATED MAINTENANCE, AN OIL LEAK WAS DISCOVERED FROM THE LEFT ENGINE. MAINTENANCE IDENTIFIED THE ENGINE OIL SCAVENGE PUMP AS HAVING A PINHOLE LEAK AND THE PUMP HOUSING WAS REPLACED. INSPECTION DETERMINED THAT CAVITATION EROSION OF THE PUMP BODY IN ASDR YADA20211223201Control Panel · shortedSTRONG SMELL OF SOMETHING BURNING SUB PANEL LIGHTS FLICKERING THEN COMPLETELY SHUT OFF. FOUND EEL PANEL A321 114-384007-15 SHORTING INTERNALLY.SDR YADA2021081601Engine · failedINTERNAL ENGINE FAILURE OF RIGHT ENGINE WHILE AT CRUSIE 23000 FT.SDR YADA20210817201Housing · erodedPILOT REPORTED "OIL LEAKING FROM RIGHT ENGINE" - MAINTENANCE FOUND OIL LEAK TO BE COMING FROM THE ENGINE OIL SCAVENGE PUMP HOUSING. REPLACED HOUSING. FOUND CAVITATION EROSION THROUGH CASTING.SDR YADA20210510001Housing · erodedPILOT REPORTED "LEFT ENGINE OIL LEAK". MAINTENANCE OIL LEAK TO BE COMING FROM THE OIL SCAVENGE PUMP HOUSING. REPLACED SCAVENGE PUMP HOUSING. FOUND CAVITATION EROSION THROUGH CASTING.SDR JIKA2021020501Drain Line · leakingSMOKE IN COCKPIT. TURNED OFF BOTH BLEEDS. SMOKE FILTERED OUT. RIGHT BLEED CAUSED NO MORE SMOKE. LEFT BLEED BROUGHT SMOKE AGAIN. FINISHED WITH RIGHT BLEED ONLY. THE AIRCRAFT LANDED WITHOUT INCIDENT IN KOMA. OMA MX- CHECKED GAS GEN. BREATHER TUBE FOR OBSTRUCTIONSDR YADA2021062101Engine · failedINTERNAL ENGINE FAILURE OF RIGHT ENGINE WHILE ON DECENT FOR LANDING - ENGINE REPLACED - O/H FACILITY DID NOT DETERMINE ORIGINAL FAILURESDR YADA20210107001Scavenge Pump · cavitatesNR 2 ENGINE OIL LEAKING. MAINTENANCE FOUND OIL LEAK TO BE COMING FROM THE OIL SCAVENGE PUMP HOUSING. REMOVED AND REPLACED OIL SCAVENGE PUMP. UPON FURTHER INVESTIGATION OF REMOVED OIL SCAVENGE PUMP, THERE WAS CAVITATION INSIDE OF THE HOUSING ITSELF.SDR JIKA2020092801Fuel Control · brokenWHILE IN ROUTE TO KPDX, THE FLIGHT CREW REPORTED LEFT ENGINE TORQUE AND N1 INDICATIONS DROPPED. CHECKLIST ITEMS WERE FOLLOWED AND THE LEFT ENGINE WAS SHUT DOWN. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT DIVERTED TO KDLS AND LANDED WITHOUT INCIDENT. PDSDR YADA20200702001Fcu · power lossPILOT REPORT: LEFT ENGINE FAILURE IN FLIGHT. TORQUE ROLLED BACK SLOWLY TO 0 NG INDICATED APPROX 55 FUEL FLOW 100 PPH. ATTEMPTED STARTER ASSIST AIRSTART. PROP FEATHERED AND UNFEATHERED NORMALLY. SAME INDICATIONS FOR RESTART. SECURED ENGINE. 1300 LBS OF FUSDR TIMA20200613003Engine · malfunctionedAIRCRAFT DEPARTED DEN AND SHORTLY AFTER CLIMBOUT, LEVELING OUT AT 10K', THE PILOT BEGAN PULLING BACK POWER AND EXPERIENCED THE RIGHT ENGINE PROPELLER BECAME "JERKY" AND SPORADIC WITHOUT ANT PROPELLER LEVER INPUTS. SOON AFTER, THE RIGHT ENGINE ITT CLIMBED TO 11SDR JIKA2019112119Engine · oil consumptionENROUTE TO KSDF THE CABIN SHOWED SIGNS OF SMOKE WHEN THE RIGHT BLEED AIR WAS TURNED ON. THE SMOKE DISSIPATED WHEN THE RIGHT BLEED WAS TURNED OFF. MAINTENANCE INSPECTED THE RIGHT BLEED AIR SYSTEM AND FOUND RESIDUAL OIL IN THE RIGHT NACELLE BLEED AIR PRE COOLERSDR JIKA2019102301Oil System · leakingON APPROACH INTO KSDF THE PILOT REPORTED SMOKE COMING FROM THE BLEED AIR. THE PILOT TURNED OFF THE RIGHT BLEED AIR AND THE SMOKE DISSIPATED. THE PILOT LANDED AT KSDF WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. MAINTENANCE TROUBLE SHOT THE RIGHT ENGINE SDR JIKA2019101701Packing · leakingAPPROXIMATELY 1HR INTO FLIGHT, RIGHT ENGINE OIL PRESSURE DROPPED TO 40PSI ACCOMPANIED WITH LOW OIL PRESSURE WARNING ANNUNCIATOR LIGHT. CREW COMPLIED WITH CHECKLIST ACTION TO SECURE THE RIGHT ENGINE. THE FLIGHT WAS CONTINUED TO DESTINATION WITH SINGLE ENGINE ASDR YADA2019060600214Cable · draggingLEFT HAND CONDITION CABLE ASSEMBLY SUFFERED AN INCREASE IN FRICTION TO POINT OF ROD END FAILURE AT THE CONTROL LEVER WITH IN 30 DAYS OF INSTALL.SDR CA190219002Engine · shutdown(CAN) CUSTOMER REPORTED SHORTLY AFTER TAKEOFF, THE LEFT HAND ENGINE SHUT DOWN UNEXPECTEDLY. THE FIGHT CREW CONTINUED THE CLIMB TO 2000 FEET ASL IN VFR CONDITIONS, DECLARED AN EMERGENCY, AND RETURNED TO AIRPORT. THE SUBSEQUENT LANDING WAS UNEVENTFUL. PRATT ANDSDR TIMA201902081024Seal · leakingPILOT REDUCED RH ENGINE POWER AFTER THE OIL PSI LOW WARNING ANNUNCIATOR ALERTED. PILOT RETURNED TO DEPARTURE AIRPORT,
LANDED WITHOUT INCIDENT, AND SHUTDOWN ENGINE WHEN CLEAR OF THE RUNWAY.
MAINTENANCE FOUND FAULTY OIL SEAL AT PROP SHAFT AND REPLACED THE SESDR TIMA201902080004Seal · leakingPILOT REDUCED RH ENGINE POWER AFTER OIL PSI LOW WARNING ANNUNCIATOR ALERTED. PILOT RETURNED TO DEPARTURE AIRPORT,
LANDED WITHOUT INCIDENT, AND SHUTDOWN ENGINE WHEN CLEAR OF THE RUNWAY.
MAINTENANCE FOUND LEAKING OIL SEAL AT PROP SHAFT AND REPLACED THE SEAL.SDR YADA20180105001Scavenge Pump · leakingMAINTENANCE DISCOVERED THAT THE NR 1 ENGINE HAD AN OIL LEAK AT THE SCAVENGE PUMP HOUSING– THE PUMP WAS LEAKING THROUGH THE CASTING. THIS IS THE THIRD SUCH FAILURE OF THIS PART IN ONE YEAR FOR US.SDR YADA20190103001Scavenge Pump · leakingAFTER LANDING, CREW NOTICED ENGINE OIL ON LT WING. MAINTENANCE LOCATED OIL LEAK AT NR 1 ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED SAME. REMOVED HOUSING VERIFIED TO HAVE CAVITATION CAVITY THROUGH WALL OF SCAVENGE PUMP BODY THAT WAS ALLOWING OIL TO ESCAPE TSDR TIMA2018120400001Vernatherm · failedPILOT SHUTDOWN RT ENGINE AFTER NOTICING OIL TEMP HIGH, PRESSURE LOW, AND OIL STREAKS ON COWL. INVESTIGATION FOUND OIL TEMPERATURE VERNATHERM WAS NOT PASSING OIL THRU THE OIL COOLER.SDR TIMA2018103100001Hose · chafedENGINE WAS SHUTDOWN IN FLIGHT AFTER TORQUE AND OIL PRESSURE FLUCTUATIONS. INSPECTION REVEALED THAT THE OIL HOSE CONNECTED BETWEEN THE ENGINE AND OIL COOLER HAD CHAFED THROUGH THE INSULATION AND SHIELDING WHERE THE HOSE RESTED ON THE AFT NACELLE STRUCTURE TO TSDR YADA2018103000179Control Cable · corrodedRUDDER CABLE FOUND FRAYED AND SEVERELY CORRODED AT A ROUTINE INSPECTION.SDR YADA2018082017001Filter · contaminatedPILOT REPORTED THE RT ENGINE OIL PRESSURE WAS OBSERVED TO BE SHOWING 65 PSI AFTER TAKEOFF. NO EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE MAIN OIL FILTER AND THEN CLEANED CONTAMINATION OUT OF THE OIL PRESSURE TRANSMITTERSDR YADA20180518001Bellows · faultyPILOT REPORTED WHILE TAXIING THE RIGHT HAND ENGINE HAD A HUNG START WHILE USING BATTERY POWER TO START THE ENGINE AND THAT THE ENGINE FAILED DURING THE TAXI, PILOT RETURNED TO HOME STATION. MAINTENANCE IS CURRENTLY TROUBLESHOOTING THE ISSUE BUT HAS FOUND THAT SDR YADA20180426001Lens · detachedLEFT WING TIP NAV STROBE LENS COVER LOST INFLIGHT.SDR JDWA201804190001Fuel Control · malfunctionedDURING APPROACH, THE NR 1 POWER OUTPUT REDUCED AND WOULD NOT RESPOND TO INPUT. THE ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED NO DAMAGED P3 OR PY LINES. REPLACED FUEL CONTROL UNIT.SDR YADA2018022218001Gasket · failedRIGHT BLEED AIR ANNUNCIATOR ILLUMINATED INFLIGHT. RIGHT OVERTEMP SENSOR GASKET FAILED MELTING THE EVA TUBING.SDR TIMA20180214003Governor · openPROPELLER DID NOT COME OUT OF FEATHER AFTER A PROPELLER CYCLE CHECK DURING RUN-UP. REPLACING THE OVERSPEED GOVERNOR ELIMINATED THE PROBLEM. THE DUMP VALVE OF THE OVERSPEED GOVERNOR STUCK IN THE OPEN POSITION.SDR YADA20180118001Scavenge Pump · leakingMAINTENANCE DISCOVERED THAT THE NR 2 ENGINE OIL SCAVENGE PUMP HOUSING WAS LEAKING THROUGH THE CASTING. OIL SCAVENGE PUMP HOUSING WAS REMOVED AND REPLACED.SDR JIKA2018011601Tube · collapsedTHE PILOT REPORTED THAT THE LEFT ENGINE OIL PRESSURE BEGAN FLUCTUATING NEAR THE LOW REDLINE. THE PILOT PERFORMED A PRECAUTIONARY INFLIGHT SHUT DOWN OF THE LEFT ENGINE AND DIVERTED. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND OIL SDR TIMA20170811011Line · chafedAFTER A NORMAL TAKEOFF, THE PILOT WAS UNABLE TO MAINTAIN CLIMB POWER AND TORQUE ON THE LT ENGINE. AS POWER CONTINUED TO DECREASE, THE PILOT SHUT DOWN THE LT ENGINE AND RETURNED TO DEPARTURE FOR AN UNEVENTFUL LANDING. INSPECTION REVEALED THAT THE PRIMARY FUSDR YADA20170515001Fcu · unresponsivePILOT REPORTED THAT THE LEFT HAND ENGINE WAS UNRESPONSIVE TO POWER LEVER INPUT AND WOULD NOT COME OUT OF IDLE. MAINTENANCE PERSONAL REMOVED AND REPLACED THE LEFT HAND ENGINE FUEL CONTROL UNIT, PERFORMED RIGGING, OPERATIONAL AND LEAK CHECKS OF THE LEFT HAND ENGSDR JIKA2016050301Bleed Valve · stickingTHE TRAINING CAPTAIN REPORTED WHILE PERFORMING TRAINING STALL MANEUVERS, THE FIRST OFFICER REDUCED POWER, A MOMENTARY COMPRESSOR STALL OCCURRED, BETWEEN 500 - 1000 FT & LBS TORQUE ON THE LT ENG. TRAINING CAPTAIN REDUCED POWER, THIS RESULTED IN ANOTHER STALL. SDR CA160216023Motor · failed(CAN) FLIGHT CREW REPORTED ELECTRICAL SMOKE ODOR IN FLIGHT DECK. FLAP MOTOR FOUND U/S AND CIRCUIT BREAKER TRIPPED.SDR TIMA20160108001Pressure Switch · faultyIMMEDIATELY AFTER ROTATION THE LT PROPELLER AUTO FEATHERED. PILOT REDUCED POWER & IMMEDIATELY LANDED, ABORTING THE TAKEOFF. THE PROBLEM WAS DISCOVERED TO BE A FAULTY AUTO FEATHER LOW PRESS SWITCH.SDR CA160125006Fuel Control · failed(CAN) REJECTED TAKEOFF BY FLIGHT CREW WHO REPORTED NO POWER ON LT ENGINE. AS FLIGHT CREW TAXIED BACK POWER RETURNED AND ENGINE STABLE BUT SLOW RESPONSE TO POWER INPUT.SDR JIKA201512081501Fuel Control · low pressureEN-ROUTE, THE PILOT REPORTED THAT THE RT ENG TORQUE STARTED TO DROP OFF. THE PILOT WAS ABLE TO MATCH TOQUE BY ADVANCING THE RT POWER LEVER. DURING APPROACH, THE RT ENG BEGAN TO SURGE. THE PILOT PERFORMED A PRECAUTIONARY IN FLIGHT SHUTDOWN OF THE RT ENG. DESDR CA151204005Line · cracked(CAN) DURING INSTALLATION OF THE FUEL MOTIVE LINE IN THE RT WING ROOT IT WAS NOTICED THAT THE B-NUT TUBE SLEEVE WAS CRACKED.
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