U/A Canada PT6A-41

Service difficulty reports · 717

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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 = 'PT6A41'
  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 CA090421002Blades · damaged(CAN) EIR PT6A 2009-030 FIRST STAGE COMPRESSOR BLADE FAILURE.Apr 20, 2009 · Turbine Engine Compressor SectionSDR 2009FA0000291Solenoid Valve · corrodedACFT WOULD NOT MAKE MAX DIF IN FLIGHT, AND THE PASSENGER SAID THAT THEY COULD HEAR ALOT MORE WIND NOISE AROUND THE CABIN DOOR AREA THAN NORMAL. GROUND CHECKED THE SYS AND FOUND THAT THE CABIN DOOR PNEUMATIC VALVE WAS STUCK IN THE CLOSED POSITION. THIS VALVE Apr 6, 2009 · N911CM · Beech 200BEECH · Passenger/Crew DoorsSDR 2009FA0000269Bolt · failedWHILE REPLACING THE RT WING FWD WING BOLT AND BARREL NUT, HEARD A POP WHILE TIGHTENING THE NEW BOLT BEFORE REACHING FINAL TORQUE. REMOVED NEW BOLT/BARREL NUT AND FOUND THE THREADS DAMAGED AND PULLED-OUT OF BARREL NUT. THE BOLT WAS ALSO DAMAGED BUT APPEARED TO Apr 1, 2009 · N7074G · Beech A200 · Wing, Attach FittingsSDR CA090406004Torque Link · cracked(CAN) DURING PHASE INSP, THE RT UPPER TORQUE LINK WAS FOUND TO BE CRACKED AT THE CENTER JOINT. THE CRACK STARTED FROM THE GREASE HOLE AND SPREAD ABOUT 70 PERCENT ACROSS THE END.Apr 1, 2009 · Beech 200BEECH · Main Landing Gear Strut/Axle/TruckSDR CA090327004Ballast · shorted(CAN) UPON INSP FOUND BALLAST TO NR 4 WINDOW LIGHTING TO BE SHORTED. BALLAST REMOVED, WIRES CUT AND CAPPED, CONNECTOR TIED OFF. NR 4 WINDOW LIGHTING REMOVED FROM ACFT POWER, CIRCUIT RE-ACTIVATED, NO FURTHER FAULTS FOUND. CABIN LIGHTING SUFFICIENT FOR NORMAL OPMar 24, 2009 · Beech 200BEECH · Passenger Compartment LightingSDR CA090330002Duct · cracked(CAN) NR 2 PWR OUTPUT SECTION EXHAUST DUCT CRACKED AND DAMAGED, SUBSEQUENT PWR TURBINE BLADE DAMAGE. NO ENG PWR OR PERFORMANCE WAS EFFECTED DURING FLIGHT OPERATIONS. DAMAGE TO POWER OUTPUT SECTION EXHAUST DUCT WAS FOUND DURING ENG EXHAUST OUTLET REPLACEMENT. EMar 22, 2009 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR 2009FA0000239Bearing · wornTHE BUSHING PN 101-521046-5 THAT HOLDS THE BEARING PN4A INSIDE THE RT AILERON BELLCRANK PN 101-521046-3 WAS FOUND LOOSE IN THE BELLCRANK AND INDUCED A LOSS MOTION OF APPROX .75 INCH AT THE T/E WITH THE RIG PINS INSTALLED.Mar 20, 2009 · N6507B · Beech 200BEECH · Aileron Control SystemSDR CA090326009Skin · cracked(CAN) CRACK FOUND ON EMERGENCY EXIT EXTERNAL SKIN, LOWER REAR CORNER DURING REGULAR DOOR AND ESCAPE HATCH INSP IAW MM 52-20-00 PG. 204.Mar 19, 2009 · Beech 200BEECH · Emergency ExitsSDR CA090319002Flex Drive · failed(CAN) LT OTBD FLAP FLEXIBLE DRIVE SHAFT FAILURE ON APPROACH.Mar 17, 2009 · Beech 200BEECH · Trailing Edge Flap Control SystemSDR CA090304012Engine · fire(CAN) DURING CRUISE, AT FL250, FLAMES AND DEBRIS WERE OBSERVED COMING OUT OF LT EXHAUST STACK. THE ENGINE WAS SHUTDOWN AND SECURED BEFORE A SINGLE ENGINE LANDING WAS ACCOMPLISHED. THE ENGINE HAS BEEN REMOVED AND RETURNED TO MFG FOR INVESTIGATION.Feb 22, 2009 · Beech 200BEECH · Engine (Turbine/Turboprop)SDR CA090210003Rheostat · unserviceableTHE SIDE PANEL LIGHTING WOULD NOT WORK UNTIL THE RHEOSTAT KNOB WAS PULLED. WHEN THE KNOB WAS WIGGLED A CRACKLING SOUND COULD BE HEARD. THE RHEOSTAT WAS REPLACED AND OPERATED NORMALLY. THE OLD RHEOSTAT HAD BEEN REPLACED FEB 2/09.Feb 4, 2009 · Beech 200BEECH · Flight Compartment LightingSDR CA090205006Thrust Bearing · improper partMAIN GEAR ACTUATOR WAS REMOVED TO COMPLETE AN INSP, END PLAY AND RELUBE. WHEN ACTUATOR WAS DISASSEMBLED IT WAS DISCOVERED THAT THRUST BEARING (REF I.P.C. PAGE 32-30-40 ITEM 20) WAS NOT CORRECT. COMPONENT MM REQUIRES THAT THIS BEARING BE INSTALLED A CERTAIN WAFeb 4, 2009 · Beech 200BEECH · Landing Gear ActuatorSDR CA081231003Windshield · cracked(CAN) WINDSHIELD CRACKED AS AIRCRAFT CLIMBED OUT OF YYC. AIRCRAFT RETURNED TO YYC. MAINTENANCE REPLACED WINDSHIELD AND RETURNED AIRCRAFT TO SERVICE.Dec 21, 2008 · Beech 200BEECH · Flight Compartment WindowsSDR CA081231004Windshield · cracked(CAN) AFTER START PILOT NOTED THAT THE WINDSHEILD WAS CRACKED. ENGINES WERE SHUT DOWN AND MAINTENANCE REPLACED THE WINDSHEILD AND RETURNED THE AIRCRAFT TO SERVICE.Dec 21, 2008 · Beech 200BEECH · Flight Compartment WindowsSDR CA081216003Engine · making metal(CAN) PILOTS HEARD A GRINDING SOUND FROM THE EXHAUST STACK WHEN PUTTING ON THE PROP TIE`S AFTER A FLIGHT. MAINTENANCE CONFIRMED THE SOUND AND UPON REMOVING A EXHAUST STACK TO INVESTIGATE THEY VISUALLY CONFIRMED THAT THERE APPEARED TO BE A PIECE OF METAL CONTADec 11, 2008 · Beech 200BEECH · Engine (Turbine/Turboprop)SDR CA081118008Panel · smoke(CAN) ACFT RETURNED SHORTLY AFTER DEPARTURE DUE TO AN ELECTRICAL ODOR AND A WISP OF SMOKE AT THE CO-PILOTS CONTROL WHEEL. IT LASTED FOR A FEW SECONDS AND THEN DISAPPEARED. MX INSPECTED THE ACFT UPON ARRIVAL AND FOUND THAT THE EDGE-LIGHTED PANEL AT THE CO-PILOTNov 15, 2008 · Beech 200BEECH · Flight Compartment LightingSDR HDNA200811030001Cowling · departedDURING CRUISE FLIGHT, THE AIRCRAFT SHUDDERED LIGHTLY AND THE PILOT SAW A FLASH OF WHITE. THE NR 1 ENGINE TOP FORWARD COWLING DISENGAGED FROM THE AIRPLANE. INITIAL THOUGHT WAS A BIRD STRIKE, BUT THERE WAS NO VISIBLE EVIDENCE. THE ENGINE INSTRUMENTS WERE MONINov 1, 2008 · N315MS · Beech B200 · Engine Cowling SystemSDR CA081027005Fork · broken(CAN) AFTER TAKEOFF THE PILOT SELECTED GEAR UP, RT MLG FAILED TO RETRACT. GEAR WAS CYCLED WITH NO SUCCESS. GEAR WAS RETURNED TO DOWN POSITION AND THERE WERE 3 GREEN LIGHTS. DISPATCH AND MX WERE CONTACTED AND IT WAS DECIDED TO RETURN TO BASE. LANDING WAS UNEOct 22, 2008 · Beech 200BEECH · Landing Gear ActuatorSDR CA081030001Controller · smoke(CAN) THE FLIGHT CREW REPORTED SMOKE IN THE CABIN, THE ACFT LANDED SAFELY. MX INSPECTED AND SMOKE WAS THOUGHT TO BE COMING FROM THE VENT BLOWER, THE BLOWER WAS REPLACED, GROUND RUN-UP CHECK WAS CARRIED OUT AND NO SMOKE WAS EVIDENT COMING FROM AIR CONDITIONING Oct 12, 2008 · Beech 200BEECH · Cabin Temperature Control SystemSDR CA080828006Wire · out of position(CAN) WHEN DESCENDING THROUGH FL 180, CREW NOTICED RT ENG WOULD NOT GO BELOW 1600 FT/LBS TORQUE WITH PWR LEVER AT FLIGHT IDLE. CREW CHECKED REMAINING RT INSTRUMENTS AND CONFIRMED IT WAS NOT AN INDICATION ISSUE. RT PROP LEVER WAS OPERATED WITH TORQUE INCREASE Aug 27, 2008 · Beech 200BEECH · Powerplant System WiringSDR VGR2008F00000Landing Gear · collapsedFLIGHT CREW REPORTED NOT GETTING NOSE GEAR GREEN "DOWN AND LOCKED" LIGHT AFTER EXTENDING LANDING GEAR. FLY BY THE TOWER CONFIRMED THE NOSE GEAR NOT LOCKED DOWN. THE AC WAS DIVERTED, WHERE IT MADE AN EMERGENCY LANDING WITH THE NOSE GEAR NOT DOWN AND LOCKED. Jul 29, 2008 · N44US · Beech 200BEECH · Nose/Tail Landing GearSDR CIE2008F00003Fcu · malfunctionedWHILE PERFORMING ENGINE RUN UP AT RUNWAY 36R RUN UP, LT ENGINE WAS FOUND TO BE UNRESPONSIVE AFTER LT ENGINE PROP GOVERNOR CHECK WAS COMPLETE. N1 DROPPED BELOW 50 PERCENT AND CONTINUED TO DROP. FUEL FLOW ALSO DROPPED AND CONTINUED TO DROP. ENG WAS THEN SHUTDJul 17, 2008 · N60PD · Beech 200BEECH · Fuel Controlling SystemSDR CA080718005Pump · leaking(CAN) AFTER REPLACING THE ENGINE, A LEAK CHECK WAS COMPLETED AND IT WAS FOUND THAT THE LP FUEL PUMP WAS LOOSING FUEL OUT THE VENT LINE. THE PUMP WAS REPLACED WITH NO FURTHER PROBLEMS.Jul 14, 2008 · Beech 200BEECH · Engine Fuel PumpSDR DVI2008F00000Landing Gear · failedCREW EXTENDED THE LANDING GEAR IN PREP FOR LANDING. AFTER EXTENDING THE GEAR, RT MAIN GEAR STUCK IN A POSITION APPROX 12 INCHES FWD OF "DOWN AND LOCKED" POSITION. WHEN THE LANDING GEAR WAS RECYCLED, RT MAIN GEAR DID NOT MOVE, IT REMAINTED IN THE SAME POSITIOJun 25, 2008 · N311AV · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR K5LA050908001Bellcrank · twistedDRUING A ROUTINE PHASE 3 INSPECTION, IT WAS FOUND THAT THE MAIN CABIN DOOR AFT UPLOCK BELLCRANK WAS TWISTED ABOUT 10 DEGREES FROM WHAT A NEW ONE IS.. ALSO THE BOLT PN NAS110321D THAT THE UPLOCK BRACKET PIVOTS ON WAS DEFORMED SLIGHTLY. THIS WAS PROBABLY CAUSED May 5, 2008 · N636B · Beech A200 · Passenger/Crew DoorsSDR MV1R200808136Blower · burned outDURING FLIGHT, SMOKE INITIATED FROM BEHIND INSTRUMENT PANEL CENTER BELOW. PROJECT POWER TERMINATED. ALL ELECTRICAL POWER NOT NECESSARY FOR FLIGHT, OFF. EMERGENCY LANDING, ON GROUND MAINT FOUND VENT BLOWER ASSY INOP AND BURNED. BLOWER MEL'D AND FLOWN WITHOUT FApr 29, 2008 · N35 · Beech 200BEECH · Air Distribution FanSDR 2008FA0000262Hinge · brokenENGINE ICE VANE HINGE ASSY, BROKEN. HINGE ASSY BREAKS AND FRAGMENTS INTO SMALL PIECES THAT TEND TO BE INGESTED INTO ENGINE, CAUSING FOD. (K)Apr 1, 2008 · Beech 200BEECH · Nacelle/Pylon, Main FrameSDR CTU2008F00000Windshield · crackedAFTER DEPARTURE CLIMBING THRU 8000 FT MSL CREW HEARD A POPPING NOISE, NOTICED CO-PILOTS WINDSHIELD HAD CRACKED. NO EMERGENCY DECLARED, AC RETURNED TO AIRPORT. NO OTHER AIRCRAFT DAMAGE. TYPICAL WINDSHIELD FAILURE TOLAMINATED HEATED WINDSHIELD. (K)Jan 28, 2008 · N911ND · Beech 200BEECH · Flight Compartment WindowsSDR K5L2007F00001Actuator · inoperativeDESCENDING, PILOT SELECTED ICE VANES EXTENDED AND ONLY THE LT ONE EXTENDED. PULLED CIRCUIT BREAKER AND SLOWED AIRCRAFT AND EXTENDED RT ICE VANE WITH THE MANUAL EXTENSION HANDLE. REPLACED RT ICE VANE ACTUATOR MOTOR. (K)Nov 25, 2007 · N636B · Beech A200 · Airfoil Anti/De-ice SystemSDR K5L2007F00002Power Supply · failedAWAITING TAKEOFF, PILOT TURNED ON CABIN LIGHTS AND NOTICED SMOKE FUMES IN COCKPIT AND CABIN. TURNED OFF VENT BLOWED AND CABIN LIGHTS AND RETURNED TO RAMP. IT WAS DETERMINED THAT THE POWER SUPPLY (BALLAST) HAD FAILED AND CAUSED THE SMOKE. POWER SUPPLY WAS RENov 25, 2007 · N636B · Beech A200 · Passenger Compartment LightingSDR CA071107002Blades · failed(CAN) PILOTS OBSERVED SPARKS COMING OUT RT ENGINE EXHAUST ON LANDING. MAINTENANCE INSPECTION FOUND COMPRESSOR BLADES LAYING IN THE ENGINE BAY. (TC NR 20071107002)Nov 5, 2007 · Beech 200BEECH · Turbine Engine Compressor SectionSDR CA071029011Control Cable · chafed(CAN) GRINDING NOISE UNDER PILOT FLOOR WHEN AILERONS ARE MOVED. CONTROL CABLE FOUND CHAFING ON STEEL BRAIDED NITROGEN LINE. APPROX 3 INCH DEFLECTION OF CONTROL CABLE CAUSED, DUE TO INCORRECT ROUTING OF NITROGEN LINE. NITROGEN PRESSURE LINE REROUTED. AILERON COct 27, 2007 · Beech 200BEECH · Aileron Control SystemSDR 2007FA0000850Exhaust Duct · crackedWHILE PERFORMING SCHEDULED MAINTENANCE, REMOVED RT EXHAUST STACKS TO FACILITATE INSPECTING THE EXHAUST DUCT. FOUND A 1 INCH CRACK IN THE SKI SLOPE. SB 3380 WAS COMPLIED WITH 711 HOURS EARLIER. POWER SECTION WAS PULLED AND SENT OFF FOR REPAIR.Sep 27, 2007 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR CA070918001Circuit Board · shorted(CAN) A SHORT ON THE NR 2 ENGINE FUEL COLLECTOR DRAIN PUMP CIRCUIT (TC NR 20070918001)Sep 14, 2007 · Beech 200BEECH · Engine Fuel System WiringSDR CA070913008Engine · overheated(CAN) SHORTLY AFTER LANDING, THE PILOT NOTICED AN UNUSUALLY HIGH ITT INDICATION FOLLOWED BY SPARKS EXITING THE RT ENGINE. THE PILOT SHUTDOWN THE ENGINE AND CONTINUED TAXING WITHOUT FURTHER INCIDENT. FURTHER REPORT TO FOLLOW PENDING TEARDOWN REPORT. (TC NR 2007Sep 11, 2007 · Beech 200BEECH · Engine (Turbine/Turboprop)SDR CIEA200700008Packing · deformedAFTER LANDING AND SLOWING TO TAXI SPEED, THE FLIGHT CREW WERE UNABLE TO MAKE A RT TURN TO EXIT THE RUNWAY DUE TO THE LOSS OF BRAKING ACTION OF THE RT BRAKE. THE AIRCRAFT WAS STOPPED AND THEN REMOVED FROM THE RUNWAY USING A TOW TRACTOR. MAINTENANCE INSPECTED Aug 30, 2007 · N428P · Beech 200BEECH · Landing Gear Brake SystemSDR CIEA200700007Bracket · bentDURING CRUISE FLT, CREW HEARD A NOISE & NOTICED THAT THE LT WING LOCKER HAD COME OPEN AND DOOR WAS TRAILING A FEW INCHES OPEN IN FLIGHT. ACFT APPROXIMATELY 25 MILES FORM A SUITABLE AIRPORT & CREW LANDED WITHOUT FURTHER INCIDENT. BAGGAGE FROM WING LOCKERS REMAug 28, 2007 · N520MC · Beech 200BEECH · Cargo/Baggage DoorsSDR CIEA200700006Wire · pinchedSHORTLY AFTER TAKEOFF THE PASSENGER NOTIFIED THE FLIGHT CREW THAT THEY HAD OBSERVED SMOKE FROM THE AREA OF THE NO SMOKING FASTEN SEAT BELT SIGN. THE FLIGHT CREW THAN OBSERVED THAT THE NO SMOKING FASTEN SEAT BELT SIGN CIRCUIT BREAKER HAD IN FACT POPPED. THE FAug 25, 2007 · N520MC · Beech 200BEECH · Light System WiringSDR CA070821006Intake · cracked(CAN) COWL ASSY LOWER FWD P/N 101-910024-1 WAS ONCE MODIFIED. (TC NR 20070821006)Aug 20, 2007 · Beech 200BEECH · Engine Cowling SystemSDR CA070814007Exhaust Duct · cracked(CAN) DURING ROUTINE MAINTENANCE ON THE ENGINE, AN INSPECTION OF THE POWER TURBINE BLADES INDICATED LARGE CRACKS AND MISSING SECTIONS OF THE EXHAUST DUCT. THIS ENGINE WAS INSTALLED ON APRIL 02, 2007 AFTER OVERHAUL. THE CAUSE OF THE CRACKS ARE UNDER INVESTIGATIAug 13, 2007 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR 2007AP081001Torque Tube · wornWHILE UNDERGOING A SCHEDULED INSPECTION, FOUND THE RT ELEVATOR HAD DEVELOPED VERTICAL PLAY WHEN GRASPED FROM THE TRAILING EDGE. FOUND THE ELEVATOR TORQUE TUBE HAD ROTATIONAL WHERE THE 6 EACH OB BLIND RIVETS ATTACH THE TORQUE TUBE TO THE MOUNT PLATE.Aug 10, 2007 · N7166P · Beech 200BEECH · Elevator Control SystemSDR 2007FA0000785Sensor · faultyAT APPROXIMATELY 1635 LOCAL, IN CLOUDY CONDITIONS, ON A MAINTENANCE TEST FLIGHT, THE NR 1 ENGINE FIRE LIGHT BRIEFLY ILLUMINATED, THEN EXTINGUISHED. ALL ENGINE GAUGES INDICATED NORMALLY. ALREADY IN DESCENT, THROUGH 4,500 FT, AND CONTINUED TO A SAFE LANDING. Aug 7, 2007 · N636B · Beech A200 · Fire DetectionSDR CA070725005Blade · cracked(CAN) DURING A ROUTINE COMPRESSOR TURBINE BLADE (STRETCH) INSP, ONE CT BLADE WAS FOUND CRACKED DURING THE NDT PROCESS. THE CRACK WAS ACROSS THE BLADE FACE AND BACK. THIS TYPE OF CRACK SCRAPS THE BLADE AND THE SET IT WAS INSTALLED WITH. THIS SET OF BLADES HAD AJul 11, 2007 · Beech 200BEECH · Turbine Engine Compressor SectionSDR CA070528011Windshield · cracked(CAN) CO-PILOTS WINDSCREEN CRACKED UNDER PRESSURIZED CONDITION. AIRCRAFT RETURNED TO BASE FOR WINSHEILD REPLACEMENT. UNABLE TO INDICATE CORRECT MFG. (NOT IN LIST) (TC NR 20070528011)May 28, 2007 · Beech 200BEECH · Flight Compartment WindowsSDR CA070509002Control Valve · inoperative(CAN) WORK WAS DONE TO THE AC THAT OPENED THE PRESSURE VESSEL. WHEN THIS WORK WAS STARTED THE AC WOULD HOLD MAX DIFF. THE WORK DONE LED TO A PRESSURIZATION PROBLEM, WHICH, WHILE TROUBLESHOOTING, LED TO THE DISCOVERY OF FLOW CONTROL VALVE THAT WAS WORKING INCORMay 9, 2007 · Beech 200BEECH · Pressure Regulator/Outflow ValveSDR CA070618005Power Lever · worn(CAN) FLIGHT SNAG REPORTED - (LT ENGINE REMAINS AT HIGH IDLE AT LOW IDLE SETTINGS). MAINTENANCE FOUND THE AIRFRAME POWER LEVER ARM AT THE REVERSING CAM GROUND PIN HEAD JUMPED THE SPLINE, CAUSING THE SHOULDERED PIN TO HOLD THE FCU INTERCONNECT ARM FROM RESETTIMay 4, 2007 · Beech 200BEECH · Power LeverSDR CA070504009Computer · malfunctioned(CAN) FLIGHT DIRECTOR CB TRIPPED AND WILL NOT RESET. (TC NR 20070504009)May 3, 2007 · Beech 200BEECH · Autopilot SystemSDR CA070504008Pump · malfunctioned(CAN) RT FUEL PUMP RUNNING EVEN AFTER MASTER SWITCH OFF. (TC NR 20070504008)May 3, 2007 · Beech 200BEECH · Fuel Boost PumpSDR CA070504003Turbine Wheel · cracked(CAN) DURING A HOT SECTION INSPECTION, A CRACK WAS DISCOVERED ON THE CT HUB FROM ONE UNUSED BALANCE HOLE, AROUND THE FLANGE AND BACK TO THE SAME BALANCE HOLE.THE CRACK WAS ADJACENT TO (1) OF THE (3) PROTRUDING LOCK LUGS. (TC NR 20070504003)May 2, 2007 · Beech 200BEECH · Turbine SectionSDR 2007FA0000419Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.THE EXHAUST DUCT SB 3380 HAD BEEN COMPLIED WITH 365 HOURS PRIOR.POWER SECTION WAS REMOVED FOR REPAIR.Apr 10, 2007 · Beech 200BEECH · Engine Collector/Tailpipe/Nozzle
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