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 CA991230001Spring · cracked(CAN) RT BRAKE CITED AS ''SOFT''. AME REMOVED RT SHUTTLE VALVE AND DISSASSEMBLED IT. CUT O-RING REPLACED. FAULT STILL APPEARED. AME REMOVED RT MASTER CYLINDER (P/N90-380001-11(VI-15-1000)) AND DISASSEMBLED.SPRING WASHER FOUND TO BE SPLIT IN HALF.SPRING REPLANov 29, 1999 · Beech 200BEECH · Master Cylinder/Brake ValveSDR CA991208073Actuator · burnt(CAN) AIRCRAFT FLAPS WERE LOWERED FOR PRE-FLIGHT WALK AROUND INSPECTION. DURING THE COCKPIT PRE-FLIGHT INSPECTION, THE FLAP MOTOR CIRCUIT BREAKER POPPED OUT. THE C/B WAS RESET AND APPEARED OK. THE STDB ENGINE WAS STARTED AND THEN THE PORT ENGINE. SMOKE WASNov 8, 1999 · Beech 200BEECH · Trailing Edge Flap ActuatorSDR CA991103029Windshield · shattered(CAN) BEFORE WINDSHILED CRACKED IN-FLIGHT, THE GLASS WAS DELAMINATING AT APPROXIMATELY 4 SQUARE INCHES IN THE LEFT BOTTOM CORNER. DELAMINATION AND LACK OF SEAL IN WINDOW FRAME MAY HAVE CONTRIBUTED TO OVERSTRESS IN TIME. SUBMITTER SUGGESTED FACTS TO REDUCE POOct 24, 1999 · Beech 200BEECH · Flight Compartment WindowsSDR 99ZZZX4398Fcu · leakingFOUND FUEL LEAKING OUT OF IDLE CUT-OFF SHAFT OF FCU.Oct 13, 1999 · N703KH · Beech 200BEECH · Fuel Control/Turbine EnginesSDR AU991023Windshield · broken(AUS) INNER PANEL ON PILOT'S WINDSHIELD SHATTERED.Oct 8, 1999 · Beech B200C · Flight Compartment WindowsSDR AU991105Bearing · failed(AUS) NOSE LANDING GEAR ACTUATOR DRIVE SHAFT SUPPORT BEARING DISINTEGRATED.Oct 5, 1999 · Beech 200BEECH · Landing Gear ActuatorSDR 99ZZZX3927Case · crackedFLOW DIVIDERS WERE BEING SWAPPED TO TROUBLESHOOT STARTING PROBLEM AND A CRACK WAS NOTICED AT THE WELD AREA OF THE FLOW DIVIDER/FUEL NOZZLE MOUNTING BOSS. WHEN THE BOSS WAS SLIGHTLY SIDE LOADED WITH A ROD, CRACK OPENED UP VERIFYING THE CASE IS CRACKED NOT JUSTSep 29, 1999 · N7074G · Beech C12C · Turbine Engine Combustion SectionSDR AU990853Filter · contaminated(AUS) ENGINE CHIP DETECTOR AND OIL FILTER METAL CONTAMINATION. SUBMITTER SUSPECTED THE ENGINE HAD BEEN DROPPED FOLLOWING OVERHAUL.Aug 26, 1999 · Beech 200BEECH · Turbine Engine Oil SystemSDR CA990907037Ballast · overheated(CAN) CABIN LIGHTING WAS TURNED ON RESULTING IN AN ELECTRICAL BURNING ODOR AND SMOKE. LIGHTING AND ALL ELECTRICS WERE TURNED OFF. MAINTENEANCE FOUND A BURNED LIGHTING BALLAST UNIT.Aug 18, 1999 · Beech 200BEECH · Passenger Compartment LightingSDR AU990826Diode · faulty(AUS) RIGHT POWER SUPPLY DIODE FAULTY.Aug 11, 1999 · Beech 200BEECH · Power Indicating SystemSDR AU990762Nut · failed(AUS) LEFT MAIN LANDING GEAR NUT ASSEMBLY FAILED. THE FAILURE WAS CAUSED BY A CRACK LOCATED APPROXIMATELY 31.75 (1.25 INCHES) FROM THE END OF THE NUT HOUSING EXTENDING FOR 360 DEGREES CIRCUMFERENTIALLY WITH 100 PERCENT PENETRATION. FURTHER INVESTIGATION FOUNJul 23, 1999 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR AU990763Nut · cracked(AUS) NOSE LANDING GEAR NUT ASSEMBLY CRACKED. CRACK LOCATED APPROXIMATELY 25.4 MM (1 INCHES) FROM THE END OF THE NUT HOUSING AND EXTENDING FOR APPROXIMATELY 100 DEGREES CIRCUMFERENTIALLY. SEE OPER CONTROL NR AU990762 FOR FURTHER INFORMATION.Jul 23, 1999 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR AU990766Nut · cracked(AUS) RIGHT MAIN LANDING GEAR NUT ASSEMBLY CRACKED APPROXIMATELY 38.1 MM (1.5 INCHES) FROM THE END OF THE NUT HOUSING EXTENDING FOR APPROXIMATELY 180 DEGREES CIRCUMFERENTIALLY. SEE OPER CONTROL NR AU990762 FOR FURTHER INFORMATION.Jul 23, 1999 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR AU990717Fitting · cracked(AUS) RIGHT AFT SPAR FITTING CRACKED. FOUND DURING FLUORESCENT DYE PENETRANT INSPECTION.Jul 20, 1999 · Beech 200BEECH · Wing SparSDR AU990718Cap · corroded(AUS) LEFT FORWARD UPPER SPAR CAP CORRODED. FOUND DURING VISUAL INSPECTION.Jul 20, 1999 · Beech 200BEECH · Wing SparSDR AU990767Fitting · corroded(AUS) RIGHT WING AFT SPAR FITTING CORRODED.Jul 20, 1999 · Beech 200BEECH · Wing SparSDR CA990707080Fcu · failed(CAN) WHILE TAXIING, THERE WAS NO POWER CONTROL ON NR 1 ENGINE. UNABLE TO GO ABOVE IDLE. FUEL CONTROL UNIT WAS REPLACED.Jun 23, 1999 · Beech 200BEECH · Fuel Control/Turbine EnginesSDR CA990521022Exhaust Tube · cracked(CAN) ORIGINAL SNAG WAS CHAFING AT TUBE WHERE IT ATTACHES TO EXHAUST STACK. A WEEK LATER FOLLOWING INSTALLATION OF NEW PART, TUBES WERE FOUND TO BE CRACKED INBETWEEN PLEATS OF FLEX TUBE. ON ONE TUBE, MATERIAL WAS MISSING AND SIGNIFICANT AMOUNT OF EXHAUST WASMay 7, 1999 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR 99ZZZX2313Detector · corrodedFALSE FIRE WARNING, RT ENGINE. POSSIBLY CAUSED BY AGE OF THE UNIT, OR MOISTURE AND SOAP CREEPING INSIDE. SUBMITTER SUGGESTED BETTER SEALING OF DETECTOR.Apr 9, 1999 · N2883 · Beech 200BEECH · Fire DetectionSDR CA990412005Windshield · shattered(CAN) COPILOT WINDSHIELD INNER PLY SHATTERED. AIRCRAFT WAS IN CRUISE AT 27,000 FEET AT MAXIMUM CABIN DIFFERENTIAL (6.0 PSI). FLIGHT CREW DEPRESSURIZED AIRCRAFT AND DESCENDED TO 12,000 FEET.Mar 27, 1999 · Beech B200 · Flight Compartment WindowsSDR CA990318004Line · bent(CAN) ON A COLD START (APPROX -37 CELSIUS), HIGH OIL PRESSURE (>200 PSI) WAS OBSERVED ON RIGHT ENGINE. ENGINE START WAS ABORTED. COPILOT OBSERVED OIL FLOWING FROM ENGINE. FURTHER INVESTIGATION FOUND THIS TUBE HAD (WAS) BENT SEVERELY AT BOTH BEND RADII AND HFeb 18, 1999 · Beech 200BEECH · Engine Oil Distribution (Airframe Furnished)SDR AU990093Warning System · contaminated(AUS) FIRE WARNING SYSTEM CONTAMINATED WITH MOISTURE CAUSING FALSE FIRE WARNING.Feb 5, 1999 · Beech B200C · Fire DetectionSDR CA990219007Windshield · cracked(CAN) WINDSHIELD CRACKED AND DELAMINATED ON LOWER INSIDE CORNER.Feb 3, 1999 · Beech 200BEECH · Flight Compartment WindowsSDR CA990129010Cylinder · leaking(CAN) OIL LEAK OBSERVED RUNNING DOWN NR 3 PROPELLER BLADE. INVESTIGATION DISASSEMBLY FOUND PROPELLER CYLINDER TO BE WORN BELOW MANUFACTURER'S LIMITS.Jan 20, 1999 · Beech 200BEECH · Propeller Hub SectionSDR 99ZZZX488Engine · failedCATASTROPHIC FAILURE OF LEFT ENGINE. AIRCRAFT WAS EN ROUTE TO DESTINATION WHEN AN IN-FLIGHT FAILURE OF LEFT ENGINE OCCURRED. DESTRUCTION AND SEPARATION OF TURBINE BLADES AFT OF HOT SECTION OCCURRED. PIECES OF BLADES WENT THROUGH AND DESTROYED BOTH EXHAUST SJan 14, 1999 · N5PA · Piper PA42 · Engine (Turbine/Turboprop)SDR 99ZZZX456Fcu · out of adjustINVESTIGATED LEFT ENGINE CONTROL LINKAGE AND FOUND POWER CONTROL LEVER WOULD NOT RETARD WITH POWER CONTROL CABLE MOVEMENT. LUBRICATED PIVOT POINTS, CHECKED ADJUSTMENTS AND RIGGING, PERFORMED ENGINE RUN CHECKS, NO DEFECTS NOTED.Jan 4, 1999 · N777XS · Beech 200BEECH · Fuel Control/Turbine EnginesSDR CA990111010Hose · deteriorated(CAN) NR 1 AND NR 2 TIRES BLEW ON LANDING DUE TO BEING FROZEN. THE LEFT BRAKE DE-ICE HOSE HAD DETERIORATED FROM THE HEAT AND BROKE INTO SMALL PIECES, PLUGGING THE LINE TO THE HEAT MANIFOLDS AND LETTING BRAKE DE-ICE PRESSURE ESCAPE.Dec 26, 1998 · Beech 200BEECH · Landing Gear Brake SystemSDR 99ZZZX384Housing · damagedDURING RE-ASSEMBLY OF THE REDUCTION GEARBOX AFTER LIGHTNING STRIKE INSPECTION, FOUND THE PROPELLER OIL TRANSFER HOUSING WAS DAMAGED. THE CHIP DETECT LIGHT CAME ON DURING FIRST FLIGHT. REMOVED GEARBOX, INSTALLED NEW HOUSING. PEFORMED IAW MM AND SUBMITTER STADec 21, 1998 · N22071 · Beech 200BEECH · Turbine Engine Reduction GearSDR 99ZZZX383Engine · making metalWHILE THE AIRCRAFT WAS FLYING OVER LAX ON RETURN TO VAN NUYS, THE LEFT HAND ENGINE CHIP DETECTOR LIGHT CAME ON. THE PILOT SHUT THE ENGINE DOWN IAW EMERGENCY PROCEDURES AND PROCEEDED TO VAN NUYS ON ONE ENGINE. INSPECTION REVEALED CHIPS ON THE CHIP DETECTOR, IDec 1, 1998 · N110G · Beech 200BEECH · Engine (Turbine/Turboprop)SDR CA990129003Bearing · corroded(CAN) INSPECTION FOUND MAJOR CORROSION, IN THE COMMON AREA, BETWEEN THE O- RING AND THE BEARING.Nov 12, 1998 · Beech 200BEECH · Propeller AssemblySDR CA981116004Warning System · failed(CAN) NO SOUND OUTPUT WITH ACTIVATION OF CABIN WARNING SIGNS.Nov 9, 1998 · Beech 200BEECH · Flight Management Computing Hardware SystemSDR 98ZZZX4612Engine · malfunctionedSHORTLY AFTER TAKEOFF, PILOT REPORTED 'SMALL EXPLOSION' WITH SPARKS AND 'SMOKE' FROM THE RT ENGINE. SECURED SAME AND RETURNED TO AIRPORT AND MADE UNEVENTFUL SINGLE ENGINE LANDING. MAINTENANCE FOUND N1 SECTION OF ENGINE LOCKED UP. NII SECTION FREE TO ROTATE.Nov 3, 1998 · N500PH · Beech 200BEECH · Engine (Turbine/Turboprop)SDR AU981439Structure · damaged(AUS) RUDDER DAMAGED BY COLLISION WITH ANOTHER AIRCRAFT. PART TC: 14,326.Oct 29, 1998 · Beech 200BEECH · Rudder StructureSDR 98ZZZX4194Fuel Control · malfunctionedFUEL CONTROL UNIT WOULD NOT LET THE ENGINE GO BELOW 1,400 POUNDS OF TORQUE ON DESCENT FROM ALTITUDE. ENGINE WAS SHUT DOWN. PROPELLER SECURED TO ALLOW FOR A SAFE LANDING. SUBMITTER STATED CAUSE OF MALFUNCTION UNKNOWN.Oct 22, 1998 · N210SU · Beech 200BEECH · Fuel Control/Turbine EnginesSDR AU981357Nut · cracked(AUS) LEFT MAIN LANDING GEAR ACTUATOR NUT CRACKED CIRCUMFERENTIALLY FOR APPROXIMATELY 25 PERCENT OF THE CIRCUMFERENCE 31.75 MM (1.25 INCH FROM THE TOP OF THE NUT.Oct 19, 1998 · Beech B200C · Landing Gear ActuatorSDR CA981019012Detector · sheared(CAN) ON APPROACH, THE RIGHT HAND ENGINE EXPERIENCED TORQUE FLUCTUATIONS. POWER WAS REDUCED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. ON SHUTDOWN, OIL WAS OBSERVED LEAKING FROM THE RIGHT HAND ENGINE. ON INVESTIGATION, IT WAS FOUND THAT THE MAGNETIC CHIP DETOct 3, 1998 · Beech 200BEECH · Turbine Engine Oil SystemSDR AU981231Bleed Air Duct · failed(AUS) BLEED AIR DUCT LOCATED IN LEFT WING LEADING EDGE FAILED AT JOIN.Sep 24, 1998 · Beech 200BEECH · Pneumatic Distribution SystemSDR CA981022010Switch · out of adjust(CAN) WHEN LANDING GEAR SELECTED UP, THE GEAR UNSAFE LIGHT REMAINED ON. DURING MAINTENANCE RETRACTION TESTS, THE LEFT GEAR UP SWITCH WAS FOUND TO BE OUT OF ADJUSTMENT. SWITCH ADJUSTMENTS CARRIED OUT AND SYSTEM CHECKED OKAY.Sep 23, 1998 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR CA981109009Transponder · failed(CAN) TRANSPONDER SNAGGED FOR NO LIGHTS. FURTHER INVESTIGATION REVEALED BOARD NEAR TRANSISTOR WAS BURNT. THIS PROBLEM ADDRESSED UNDER MOD NR 6 FOR THIS TRANSPONDER. NEW TRANSPONDER INSTALLED AND IT WAS DISCOVERED THIS ONE HAD NOT BEEN MODIFIED. IT ALSO WASSep 20, 1998 · Beech 200BEECH · ATC Transponder SystemSDR CA980928020Wire · chafed(CAN) OVER A SHORT PERIOD OF TIME, CREW REPORTED A PECULIAR ODOR DURING TAKEOFF IN PERFORMING MAINTENANCE BEHIND PILOTS INSTRUMENT PANEL, SOOT TRAILS AND ELECTRICAL ARC MARKS WERE FOUND ON LOWER INBOARD EDGE OF WINDSHIELD WIPER MOTOR MOUNTING PLATE. IT APPEARSep 18, 1998 · Beech 200BEECH · Instrument System WiringSDR AU981113Control Cable · worn(AUS) RIGHT OUTBOARD FLAP DRIVE CABLE WORN AT THE MOTOR END. PART TC: 9,693.Sep 4, 1998 · Beech B200C · Trailing Edge Flap Control SystemSDR AU981009Windshield · bird strike(AUS) LEFT WINDSHIELD OUTER PANE EXTENSIVELY CRACKED DUE TO BIRDSTRIKE.Aug 13, 1998 · Beech B200C · Flight Compartment WindowsSDR AU980964Circuit Breaker · failed(AUS) LANDING GEAR CONTROL CIRCUIT BREAKER FAULTY.Aug 4, 1998 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR AU980786Nut · separated(AUS) RIGHT MAIN LANDING GEAR ACTUATOR WORM DRIVE ASSEMBLY SEPARATED FROM INNER BORE OF SHAFT. SIGNS OF RUST ON SHAFT INNER BORE.Jul 2, 1998 · Beech 200BEECH · Landing Gear ActuatorSDR AU980805Actuator · failed(AUS) RIGHT MAIN LANDING GEAR ACTUATOR FAILED DURING LANDING GEAR RETRACTION CAUSING DAMAGE TO THE GEARBOX.Jul 2, 1998 · Beech 200BEECH · Landing Gear ActuatorSDR AU980646Ignitor Lead · broken(AUS) RT ENGINE IGNITOR LEAD BROKEN. THE FOLLOWING DEFECTS IN THE IGNITION SYSTEM WERE ALSO FOUND: 1. RELAY P/N 50-380048-1. 2. FUEL INDICATION CB PANEL CONNECTOR J108 CONTAMINATED WITH MOISTURE AND CORROSION. 3. IGNITOR BOX P/N 10-381550.Jun 11, 1998 · Beech 200BEECH · Ignition Harness (Distribution)SDR AU980878Circuit Breaker · failed(AUS) NR 1 AVIONICS MASTER CIRCUIT BREAKER FAULTY.Jun 10, 1998 · Beech 200BEECH · AC Power Distribution SystemSDR CA980707030Blade · shifted(CAN) STARTER WOULD ENGAGE ON START, BUT ENGINE WOULD NOT ROTATE. STARTER WAS REMOVED AND IT WAS FOUND THE NG WOULD NOT ROTATE. ENGINE WAS SPLIT AT THE C-FLANGE AND THE N1 WHEEL WOULD NOT ROTATE AND A LOUD GRINDING SOUND WAS HEARD COMING FROM THE COMPRESSOR Jun 6, 1998 · Beech 200BEECH · Turbine Engine Compressor SectionSDR HEEA0014570Bleed Valve · faultyBLEED VALVE POPPING AT HIGH TORQUE.Jun 4, 1998 · N789DS · Beech 200BEECH · Compressor Bleed ValveSDR AU980564Arm · loose(AUS) LT ENGINE POWER LEVER INPUT ARM MOVING ON THE INPUT SHAFT.May 11, 1998 · Beech 200BEECH · Power Lever
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