U/A Canada PT6A-34
Service difficulty reports · 465
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 = 'PT6A34' 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 = 'PT6A34' 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 CA000928027Line · broken(CAN) DURING CLIMB LT BLEED AIR LIGHT ILLUMINTED INDICATING BLEED AIR FAILURE. THE AIRCRAFT RETURNED TO BASE AND LANDED UNEVENTFULLY. MAINTENANCE DISCOVERED THE SENSE LINE HAD BROKEN OFF A CONNECTION. THE SENSE LINE WAS RE-ATTACHED A GROUND RUN WAS CONDUCTED ASDR CA000829015Control Cable · frayed(CAN) WHILST CARRYING OUT AN 800 HOUR INSPECTION OF THE AIRCRAFT, SEVERAL CABLES WERE FOUND THAT HAD A QUANTITY OF BROKEN STRANDS BEYOND THE ALLOWABLE LIMITS. THIS IS ONE OF TH CABLES THAT WAS FOUND. IT SHOULD BE NOTED THAT THE AIRCRAFT MANUAL STATES THAT THE SDR CA000829016Control Cable · frayed(CAN) WHILST P/N C3CF195-7 AND P/N C3CF199-5. WHILST CARRYING OUT AN 800 HOUR INSPECTION OF THE AIRCRAFT, SEVERAL CABLES WERE FOUND THAT HAD A QUANTITY OF BROKEN STRANDS BEYOND THE ALLOWABLE LIMITS. THESE ARE TWO OF THE CABLES. IT SHOULD BE NOTED THAT THE AIRCSDR CA000829017Control Cable · frayed(CAN) WHILST CARRYING OUT AN 800 HOUR INSPECTION OF THE AIRCRAFT, SEVERAL CABLES WERE FOUND WHICH HAD A QUANTITY OF BROKEN STRANDS BEYOND THE ALLOWABLE LIMITS. THIS IS ONE OF THE CABLES THAT WAS FOUND. IT SHOULD BE NOTED THAT THE AIRCRAFT MANUAL STATES THAT THSDR CA000824031Hose · burned(CAN) ON TAKEOFF RUN SMOKE STARTED COMING FROM UNDER INSTRUMENT PANEL. THE TAKEOFF WAS ABORTED PRIOR TO LIFT-OFF THE WATER. MAINTENANCE FOUND THAT A SCAT HOSE IN THE HEATER SYSTEM FWD OF THE RT INSTRUMENT PANEL HAD MOVED REARWARD AND CONTACTED THE HOT BUS SIDESDR AU000556Bracket · cracked(AUS) NOSE LANDING GEAR ACTUATOR SUPPORT BRACKET CRACKED. CRACK LENGTH28.5MM (1.125IN). FOUND DURING INSPECTION IAW SB 110-53-0027. CRACK COULD BE SEEN VISUALLY.SDR CA000712014Rod End · loose(CAN) WHILST CARRYING OUT A 100 HOUR INSPECTION OF THE CONTROL SYSTEM, THE ENGINEER NOTICED THAT THE RT FLAP PUSH/PULL ROD END FITTING APPEARED TO BE LOOSE. THE ROD WAS REMOVED FROM THE AIRCRAFT FOR FURTHER INVESTIGATION. IT WAS FOUND THAT THE RIVETS WHICH SSDR CA000720003Valve Seat · failed(CAN) THE PILOT FLYING ALONG. WHEN REDUCED POWER FOR DESCENT, OIL PRESSURE DROPPED FROM 90 PSI TO 50 PSI. PILOT LANDED IMMEDIATELY AND SHUT DOWN ENGINE. ENGINE INSP, FOUND NON-MAGNETIC PARTICLES IN OIL FILTER. THE CHIP DETECTOR AND REDUCTION GEARBOX AREA WSDR CA000719029Bolt · sheared(CAN) A/C ON LANDING ROLLOUT PULLED TO R/H WHEN STOPPED. RT GEAR 90 DEGS TO DIRECTION OF FLT. MAINT HALF OF P/N 16469 CENTRE TORQUE LINK BOLT STILL IN PLACE. REPLACED BOLT FERRIED A/C TO MAINBASE. INSP CARRIED OUT USING MAINTENANCE MANUAL & 625 APPENDIX G. ABNSDR CA000614033Pedal · broken(CAN) WHILE TAXIING ON THE WATER IN STRONG WIND CONDITIONS, PILOT LOST RIGHT RUDDER CONTROL. PART WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE.SDR CA000621022Gear · failed(CAN) PILOT REPORTED A WOBBLY NOSE GEAR SHIMMY ON LANDING ROLL-OUT WITH LIMITED RT TURNING CAPACITY. MAINTENANCE FOUND TEETH MISSING OFF THE SECTOR GEAR JAMMING ON THE RACK FOR LIMITED TRAVEL WITH A GAP IN THE CENTER CAUSING THE SEVERE SHIMMY. THE GEAR WAS SDR 20000620SH029Seal · leakingGARLOCK SEAL FAILED CAUSING OIL TO DRAIN IN REAR OF ACCESSORY CASE. OIL THEN GOING FORWARD INTO COMPRESSOR AND DRAINING ON RAMP. (X)SDR CA000606023Bolt · cracked(CAN) INSPECTION OF CANOE RACK FOR LOOSENESS FOUND EYE BOLT HEAD SLIGHTLY BENT WITH CRACK ON FORWARD FACE. EYE BOLT REPLACED.SDR AU000318Hinge · corroded(AUS) CENTER RUDDER HINGE BRACKET CORRODED BEYOND REPAIR.SDR AU000319Hinge · corroded(AUS) RIGHT ELEVATOR CENTER HINGE CORRODED.SDR CA000331010Line · cracked(CAN) FUEL LINE CRACK AT B-NUT FOUND TO BE THE CAUSE OF FUEL ODOR, AT FCU. FEEDBACK.SDR AU000308Structure · misrepaired(AUS) STRUCTURE AT THE BASE OF THE COPILOT''S CONTROL COLUMN CUT AND GROUND AWAY IN THE AREA OF THE ELEVATOR PUSH-PULL ROD ATTACHMENT. UNAPPROVED MODIFICATION. .SDR AU000312Control Cable · worn(AUS) RIGHT WING FORWARD INBOARD AILERON CABLE AND LEFT WING AFT INBOARD AILERON CABLE SEVERELY ERODED IN THE AREA WHERE THEY EXIT THE FUSELAGE.SDR AU000313Fitting · corroded(AUS) LEFT INBOARD NACELLE TO FORWARD SPAR ATTACHMENT CASTING UPPER LUG CORRODED IN THE AREA AROUND HI-LOC FASTENER.SDR AU000314Fitting · worn(AUS) ELEVATOR TRIM FITTING AND HINGE HAD EXCESSIVE PLAY. FURTHER INVESTIGATION FOUND THE TRIM FITTING CRACKED.SDR AU000315Seat Track · corroded(AUS) ALL CABIN SEAT TRACKS SEVERELY CORRODED.SDR AU000316Seat · cracked(AUS) CABIN SEAT LEGS DEFORMED AND CRACKED IN THE AREA OF ATTACHMENT TO THE MAIN SEAT TUBE.SDR AU000317Control Cable · corroded(AUS) AFT ELEVATOR CABLES (4 OFF) AND AFT RUDDER CABLES CORRODED IN THE AREA LOCATED BETWEEN FRAME 19 AND FRAME 21.SDR AU000320Bellcrank · corroded(AUS) LEFT AND RIGHT ELEVATOR BELLCRANKS PN 4A-3224-02 (LT) AND PN 4A-3214-02 (RT) AND BELLCRANK STOPS PN 110-3010-26 AND PN 110-3010-27 CORRODED.SDR AU000321Hinge · corroded(AUS) RT AILERON INBOARD HINGE CORRODED.SDR AU000092Switch · intermittent(AUS) RIGHT MAIN LANDING GEAR DOWNLOCK MICROSWITCH INTERMITTENT IN OPERATION.SDR CA000218012Support Bracket · cracked(CAN) DURING CRUISE, CREW HEARD A KNOCKING SOUND ACCOMPANIED BY A NOISE THAT PULSATED LOUDER AS AIRSPEED INCREASED. AFTER LANDING, CREW NOTICED RT INBOARD MLG DOOR HAD PULLED FREE OF THE DOOR ROD. THE DOOR ROD RECEIVING BALL HAD PULLED THROUGH THE SUPPORT ASSSDR CA000120018Hinge · loose(CAN) WHILE CARRYING OUT A 100 HR INSP. ON THE LT WING, THE ENGINEER NOTICED THAT THE AILERON HINGE ON THE INBOARD AND OUTBOARD END OF THE AILERON HAD LOOSE RIVETS. THE END RIB AND HINGE FITTING WERE REMOVED FROM THE AILERON AND THE ARE INSPECTED. THE RIVET HOSDR CA991208086Bearing · corroded(CAN) CORROSION FOUND ON ALL THREE BLADE THRUST BEARINGS IN HUB AREA.SDR CA991209057Tire · failed(CAN) ON TAKEOFF, THE LEFT INBOARD MAIN WHEEL ASSEMBLY SHED ITS ENTIRE TREAD. ALTHOUGH THIS WAS A RECAPPED TIRE, THE TREAD DID NOT SEPARATE AT THE RECAP. IN THIS CASE, THE RETREAD LAYER AND THE LAYER OF THE RUBBER FROM THE RETREAD TO THE FIRST LAYER OF CORDSDR CA991116003Pump · failed(CAN) RIGHT HYDRAULIC PUMP FAILED AFTER TAKEOFF. PUMP REPLACED. LINES FLUSHED, FILTERS REPLACED.SDR CA991103048Contact · failed(CAN) AFTER TAKEOFF, THE CREW SELECTED GEAR UP BUT THE GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO BASE. TROUBLESHOOTING REVEALED THAT A SET OF POINTS IN THE LANDING GEAR CONTROLLER WELDED TOGETHER. THE MOTOR WAS REPLACED. THIS IS THE FOURTH PROBLEM WSDR CA991103069Bearing · failed(CAN) OIL FOUND CONTAMINATED, SUSPECT NR 1 BEARING.SDR CA991007069Wire · shorted(CAN) DURING FLIGHT, PILOT REPORTED SMOKE AROUND MASTER COMPASS AND LOSS OF OTHER LIGHTING IN THE COCKPIT. COMPASS LIGHT WIRES FOUND SHORTED AT CONNECTOR AND INSULATION BURNT. CIRCUIT BREAKER DID NOT TRIP.SDR CA991209087Switch · out of adjust(CAN) AFTER TAKEOFF WHEN GEAR SELECTED UP, CREW DIDN'T GET NOSE GEAR UP INDICATION THAT THE NOSE GEAR HAD MOVED. GEAR CYCLED WITH NO INDICATION. RETURNED HANDL E TO DOWN POSITION WITH 3 GREEN LIGHTS. NOSE GEAR CENTERING ACCUMULATOR WAS BELOW MINIMUM PRESSUSDR CA990915088Control Cable · frayed(CAN) DURING INSPECTION, AILERON CABLES WERE FOUND TO HAVE SEVERAL BROKEN STRANDS. CABLE REPLACED.SDR CA990915087Pushrod · worn(CAN) DURING INSPECTION, FOUND THAT THE PUSH/PULL ROD FOR THE ELEVATOR TRIM TAB WAS SEVERELY WORN. THE WEAR SPOT OCCURRED WHERE THE PUSH/PULL ROD RUNS THROUGH THE B/H AND CONTACTS TWO ROLLERS WHICH IT RIDES ON. THE PUSH/PULL ROD WAS REPLACED. THE ROLLERS HADSDR AU990721Rib · corroded(AUS) RIGHT WING INBOARD RIB CORRODED IN THE AREA BETWEEN THE FRONT AND REAR SPARS. FOLLOWING REMOVAL OF THE RIB A SMALL AMOUNT OF INTERGRANULAR/FILIFORM CORROSION WAS FOUND ON THE REAR SPAR WEB UNDER THE STAINLESS STEEL SHIMS LOCATED BETWEEN THE RIB REAR FLASDR AU990796Accumulator · faulty(AUS) NOSE LANDING GEAR CENTERING ACCUMULATOR FOUND TO HAVE NIL CHARGE.SDR CA990812012Bolt · striped(CAN) REMOVAL OF CT BOLT AT FIRST HSI DIFFICULT TO REMOVE. THREADS PULLED FROM END OF BOLT, WHICH WAS A POST SB 1439R2 BOLT.SDR AU990797Rod · broken(AUS) NOSE LANDING GEAR DOOR ROD BROKEN.SDR CA990728080Pin · broken(CAN) DURING THE WASH AND REGREASING OF THE RIGHT MAIN LANDING GEAR, THE PIN THAT ATTACHES THE DOWNLOCK HOOK TO THE DOWNLOCK LINK WAS FOUND PROTRUDING AND BROKEN. THE BREAK WAS LOCATED AT THE HOLE FOR THE ROLL PIN. THE ROLL PIN IS USED TO RETAIN THE HOOK PINSDR AU990704Fcu · faulty(AUS) FUEL CONTROL UNIT SUSPECT FAULTY.SDR CA990728032Downlock · blocked(CAN) PILOT COMPLAINED ABOUT NO GEAR DOWN INDICATION. CYCLED GEAR NUMEROUS TIMES WITH NO INDICATION. A MIRROR CHECK CONFIRMED THE GEAR WAS DOWN. DURING INSPECTION OF THE GEAR, FOUND THE FORWARD FLOAT ROPE STUCK INTO THE GEAR DOWNLOCK. THE END OF THE ROPE DSDR AU990372Fire Detector · broken(AUS) LEFT ENGINE FIRE DETECTOR LOCATED IN THE COMPRESSOR INLET AREA FOUND TO HAVE A FAULTY TERMINAL POST (POST BROKE WHEN THE WIRE WAS REMOVED). SUSPECT MOISTURE INGRESS CAUSED A SHORT CIRCUIT CAUSING THE FIRE WARNING TO ACTIVATE.SDR AU990363Fire Detector · contaminated(AUS) LEFT ENGINE FIRE WARNING DETECTORS CONTAMINATED WITH MOISTURE. AIRCRAFT FLEW THROUGH LIGHT RAIN.SDR AU990362Fire Detector · contaminated(AUS) LEFT ENGINE FIRE DETECTORS CONTAMINATED WITH MOISTURE.SDR CA990318073Window · leaking(CAN) GLYCOL PENATRATED CABIN WINDOW SOAKING INSULATION. WHEN HEATER APPLIED, VAPORS VISIBLE ON INTERIOR. WINDOW RESEALED AND INSULATION REPLACED.SDR CA990115012Accumulator · leaking(CAN) WHEN GEAR SELECTED UP AFTER TAKEOFF, ALL BUT THE NOSE GEAR INDICATED UP AND LOCKED. DOWN SELECTION MADE AND ALL GREENS. CREW RETURNED AND LANDING OK. THE NOSE LANDING GEAR CENTERING ACCUMULATOR FOUND LOW IN NITROGEN BECAUSE OF A LEAKING SCHRAEDER VALVSDR CA981230036Actuator · cracked(CAN) FLAP ACTUATOR DUST COVER FOUND DAMAGED. NO REPORTED FLAP OPERATION SNAGS. PART TC: 5,015.
Back to U/A Canada PT6A-34