U/A Canada PT6A-42

Service difficulty reports · 396

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 = 'PT6A42'
  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 CA020226005Pump · leaking(CAN) DURING SCHEDULED MAINTENANCE, NOTICED A DRIP OF FUEL COMING OFF OF THE ENGINE DRIVEN FUEL PUMP TO ENGINE FLANGE. WITH A CLOSER LOOK FOUND A BROWN STAIN AS WELL. REMOVED ENGINE DRIVEN FUEL PUMP ASSEMBLY AND INSPECTED. FOUND SPLINE DRIVE COUPLING WHICH ENTFeb 7, 2002 · Beech B200 · Engine Fuel PumpSDR AUS20020091Stringer · cracked(AUS) STRINGER NR 9 LT LOCATED BEHIND FRONT PRESSURE BULKHEAD CRACKED AT THE END OF THE ATTACHMENT GUSSETT.Feb 3, 2002 · Beech B200C · Fuselage Main, Longeron/StringerSDR AUS20020098Ignition Lead · mismanufactured(AUS) ENGINE IGNITER LEADS CAUSING IGNITER PIN EROSION. LEADS ARE A NEW ITEM WITH SHORTER INSULATORS.Jan 22, 2002 · Beech B200C · Ignition Harness (Distribution)SDR AUS20020028Door · separated(AUS) RT MAIN LANDING GEAR DOOR SEPARATED FROM AIRCRAFT DUE TO FAILURE OF THE HINGE PIN.Jan 14, 2002 · Beech B200C · Landing Gear DoorsSDR 2002FA0000444Flow Divider · leakingRECEIVED NEW FLOW DIVIDER TO REPLACE FLOW DIVIDER WITH SUSPECTED LEAKING DUMP VALVE. AT MFG REQUEST, A LEAK CHECK WAS PERFORMED ON THE NEW FLOW DIVIDER. IT WAS FOUND THAT THE NEW FLOW DIVIDER LEAKED AT THE DUMP VALVE AND IS NOT SERVICEABLE. THIS IS SECOND FJan 4, 2002 · N520DG · Beech B200 · Engine Fuel DistributionSDR AUS20011340Diode · failed(AUS) NR 2 BUS SYSTEM FEED DIODES FAILED.Dec 11, 2001 · Beech B200C · AC Power Distribution SystemSDR AUS20011320Ignition Lead · shorted(AUS) IGNITER LEAD INSULATION SHORT.Dec 9, 2001 · Beech B200C · Ignition Harness (Distribution)SDR AUS20011226Engine · malfunctioned(AUS) NEWLY INSTALLED ENGINE FAILED TO CORRECTLY CONTROL PROPELLER.Nov 13, 2001 · Beech B200C · Engine (Turbine/Turboprop)SDR AUS20011112Compressor · fod(AUS) ENGINE FIRST STAGE COMPRESSOR DAMAGE. FOD.Oct 19, 2001 · Beech B200C · Turbine Engine Compressor SectionSDR AUS20011079Amplifier · faulty(AUS) LH ENGINE FIRE WARNING SYSTEM CONTROL AMPLIFIER SUSPECT FAULTY.Oct 11, 2001 · Beech 200BEECH · Fire DetectionSDR AUS20010972Gearbox · disconnected(AUS) ENGINE ACCESSORY GEARBOX DECOUPLED PREVENTING ACCESSORIES FROM OPERATING.Aug 29, 2001 · Beech B200C · Turbine Engine Accessory DriveSDR AUS20010944Circuit Breaker · faulty(AUS) LANDING GEAR INDICATION SYSTEM CIRCUIT BREAKER HAD HIGH RESISTANCE.Aug 24, 2001 · Beech B200C · Landing Gear Position and WarningSDR AUS20010955Detector · unserviceable(AUS) FIRE DETECTOR FAULTY.Aug 23, 2001 · Beech B200C · Fire DetectionSDR AUS20010971Windshield · failed(AUS) LH WINDSHIELD SHATTERED.Aug 22, 2001 · Beech 200BEECH · Flight Compartment WindowsSDR AUS20010892Fcu · unserviceable(AUS) LH ENGINE FUEL CONTROL UNIT FAULTY.Aug 17, 2001 · Beech 200BEECH · Fuel Control/Turbine EnginesSDR 2001FA0000329Bolt · backed outAN5-4A BOLT IN BOTTOM PIVOT POINT ROD ATTACHMENT BACKED OUT CAUSING LOSS OF ENGINE CONTROL. AN936B516 LOCK WASHER WAS PRESENT.Aug 1, 2001 · N424RA · Beech B200 · Power LeverSDR AUS20010800Rod End · out of adj(AUS) LT ENGINE POWER LEVER CABLE TO POWER INPUT LEVER ROD END OUT OF ADJUSTMENT AND THE LOCKNUT WAS LOOSE. THE ROD END AND LOCKNUT HAD NOT BEEN CORRECTLY INSTALLED FOLLOWING FCU CHANGE.PERSONNEL/MAINTENANCE ERROR.Jul 26, 2001 · Beech 200BEECH · Power LeverSDR AUS20010921Compressor · fod(AUS) ENGINE COMPRESSOR EXTENSIVELY DAMAGED BY FOD. INVESTIGATION FOUND A DAMAGED WASHER IN THE COWL. SUSPECT CAME FROM BOLT SECURING COMPRESSOR SCREEN REMOVED DURING MAINTENANCE PRIOR TO THISFLIGHT. PERSONNEL/MAINTENANCE ERROR.Jun 28, 2001 · Beech 200BEECH · Turbine Engine Compressor SectionSDR AUS20010678Windshield · cracked(AUS) RH WINDSHIELD INNER PANE CRACKED.Jun 26, 2001 · Beech 200BEECH · Flight Compartment WindowsSDR CA010627055Switch · intermittent(CAN) WHEN LANDING GEAR SELECTED UP AFTER TAKE OFF, GEAR DID NOT RETRACT. GEAR SELECTED BACK DOWN WITH NORMAL DOWN AND LOCKED INDICATION ON ALL GEAR. NORMAL LANDING CARRIED OUT WITHOUT INCIDENT. TROUBLESHOOTING FOUND INTERMITTENT MIRCOSWITCH CONTACTS IN LANDINJun 15, 2001 · Beech B200 · Landing Gear SelectorSDR AUS20010620Motor · burned out(AUS) TRAILING EDGE FLAP ELECTRIC MOTOR WINDINGS BURNT OUT. SUSPECT CAUSED BY FAILURE OF DYNAMIC BRAKE.Jun 12, 2001 · Beech 200BEECH · Trailing Edge Flap ActuatorSDR CA010523014Connector · damaged(CAN) AFTER TAKEOFF FLT CREW REPORTED THEY WERE UNABLE TO GET L/G TO RETRACT FULLY, OR EXTEND TO DOWN POSITION. ALL C/BS WERE CHECKED TO NO AVAIL. THE GEAR WAS EXTENDED BY USING THE EMERGENCY BLOW DOWN PROCEDURE. THREE GREEN INDICATORS WERE ATTAINED AND VISUALApr 28, 2001 · Beech B200C · Landing Gear Retraction/Extension SystemSDR CA010406009Downlock Switch · intermittent(CAN) ON FINAL APPROACH WHEN GEAR WAS SELECTED DOWN, RT GEAR LIGHT WOULD NOT COME ON. GEAR WAS SELECTED SEVERAL TIMES WITH SOME RESULT. GO AROUND WAS UNDERTAKEN. RT GEAR WAS VISUALLY CHECKED IN THE DOWN POSITION AND ON THE NEXT APPROACH AIRCRAFT LANDED WITHOUTMar 21, 2001 · Beech B200C · Landing Gear Position and WarningSDR AU010233Exhaust Pipe · failed(AUS) ENGINE EXHAUST DUCT FAILED IN AREA AROUND NR 3 BEARING COVER SUPPORT.Mar 19, 2001 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR CA010322004Tire · imbalanced(CAN) SEVERE VIBRATION WAS FELT ON TAKEOFF. AIRCRAFT RETURNED TO BASE. NOSE WHEEL REMOVED AND UNABLE TO BALANCE. UPON TIRE REMOVAL AN INTERNAL BALANCE PATCH WAS FOUND UNATTACHED. THIS TIRE WAS PURCHASED NEW IS A GOODYEAR P/N 301-392-641, S/N 91851436 WAS INSTAMar 11, 2001 · Beech B200 · TireSDR AU010138Hose · split(AUS) COPILOTS OXYGEN HOSE FAILED. HOSE HAD BEEN INCORRECTLY FITTED WITH A TIGHT RADIUS.Feb 20, 2001 · Beech 200BEECH · Crew Oxygen SystemSDR AU010120Engine · making metal(AUS) ENGINE CHIP DETECTOR CONTAMINATED BY METAL CHIP. SUSPECT CHIP WAS A PART OF A TAB WASHER.Feb 16, 2001 · Beech 200BEECH · Engine (Turbine/Turboprop)SDR AU010110Skin · debonded(AUS) TOP SKIN DISBONDED.Feb 14, 2001 · Beech 200BEECH · Fuselage Main, Plate/SkinSDR 20010416CW009Fuel Control · inoperativeDURING TRAINING FLIGHT IN AN EMERGENCY DECENT SIMILATION, THE LEFT ENGINE FLAMED OUT AND COULD NOT BE RESTARTED. REPLACED THE FUEL CONTROL AND OPERATION IS NORMAL.Jan 10, 2001 · N63791 · Beech B200 · Fuel Control/Turbine EnginesSDR AU010006Fitting · corroded(AUS) RUDDER CENTER HINGE ASSEMBLY ATTACHMENT FITTING CORRODED.Jan 3, 2001 · Beech 200BEECH · Rudder StructureSDR AU010021Pin · sheared(AUS) DOOR HOOK CLEVIS PIN SHEARED. DOOR DIFFICULT TO OPEN.Jan 3, 2001 · Beech 200BEECH · Passenger/Crew DoorsSDR AU001195Compressor · damaged(AUS) ENGINE SURGING ABOVE 1400 FTLBS OF TORQUE. BLEED VALVE CHECKEDOK. FIRST STAGE COMPRESSOR BLADES HAD SOME LEADING EDGE ROUGHNESS. RECOVERY WASH CARRIED OUT. STALL/SURGE AT 900 FT LBS ACCOMPANIED BY A LOUD SQUEAL FROM THE ENGINE. SUSPECT COMPRESSOR SECTIONDec 13, 2000 · Beech 200BEECH · Turbine Engine Compressor SectionSDR 20001214SH001Harness · burnedWIRE BUNDLE SPIRAL WRAP MELTED AND CHAFING AGAINST THE BRAKE DE-ICE HEAT LINE WHERE IT MAKES THE TURN TO COME INTO THE FORWARD INBOARD PART OF WHEELWELL AT WS 85, ACCESS PANEL NR 13 AS SEEN ON CHAP 12-20-00 PAGE 249, FIG. 205 OF MM. (X)Dec 12, 2000 · N773TP · Beech B200 · Electrical Power SystemSDR AU001138Cover · separated(AUS) STARTER COVER CAME OFF AND JAMMED BETWEEN THE COWL AND THE ENGINE FCU CONTROL ROD.Nov 30, 2000 · Beech B200C · Starter-GeneratorSDR AU001132Bulkhead · cracked(AUS) REAR PRESSURE BULKHEAD CRACKED. FOUND DURING INSPECTION IAW AD/200/67.Nov 25, 2000 · Beech B200C · Fuselage Main, BulkheadSDR CA001205023Skin · cracked(CAN) CRACKED SPAR PART NR 35-165050-229. (X)Nov 20, 2000 · Beech B200 · Trailing Edge FlapsSDR CA001128006Circuit Breaker · tripped(CAN) LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE FOUND THE CIRCUIT BREAKER FOR THE LANDING GEAR MOTOR POPPED. THE GEAR WAS SWUNG SEVERAL TIME AND THE FAULT COULD NOT BE DUPLICATED. THE GEAR WAS INSPECTED AND THE RIGGING CHECKEDAND ALL WAS FOUNDNov 12, 2000 · Beech 200BEECH · Landing Gear ActuatorSDR AU001036Stringer · cracked(AUS) STRINGER NR 10 RT LOCATED AT FRAME 207 CRACKED. NEW FRAME 207 AND SKIN HAD BEEN FITTED. (X)Oct 24, 2000 · Beech B200C · Fuselage Main, Longeron/StringerSDR AU001247Windshield · cracked(AUS) LT WINDSHIELD OUTER PANE CRACKED.Oct 3, 2000 · Beech 200BEECH · Flight Compartment WindowsSDR CA001030002Compressor · failed(CAN) SHORTLY AFTER TAKEOFF, THE CABIN FILLED WITH FUMES AND LIGHT SMOKE. THE AIRCRAFT RETURNED TO THE POINT OF DEPARTURE. ENGINE WAS SPLIT AT THE C-FLANGE. NO OBVIOUS DAMAGE OR ABNORMALITIES WERE FOUND. A NEW NR 2 BEARING COVER AND GASKET WERE INSTALLED.Sep 19, 2000 · Beech B200 · Turbine Engine Compressor SectionSDR AU000895Switch · misinstalled(AUS) CABIN ALTITUDE SENSE SWITCH INCORRECTLY WIRED. CABIN OXYGEN MASKS FAILED TO CORRECTLY DEPLOY. (X)Sep 17, 2000 · Beech B200C · Passenger Oxygen SystemSDR AU000966Pressure Switch · faulty(AUS) HYDRAULIC PRESSURE SWITCH FAULTY. (X)Sep 5, 2000 · Beech B200C · Hydraulic Pressure SensorSDR AU000661Frame · cracked(AUS) FUSELAGE FRAME 207 LEFT, CRACKED. (X)Sep 1, 2000 · Beech B200C · Fuselage Main, FrameSDR CA000927004Fuel Control · failed(CAN) UPON APPROACH TO YRT, PILOTS DISCOVERED NR 1 ENGINE WOULD NOT RESPOND TO POWER LEVER COMMANDS. AS A RESULT, THE PILOTS HAD TO SHUT DOWN NR 1 ENGINE TO LAND. FCU WAS REPLACED. ENGINE GROUND TESTED SERVICEABLE. (X)Aug 28, 2000 · Beech B200 · Fuel Control/Turbine EnginesSDR AU000761Switch · out of adj(AUS) RT MAIN LANDING GEAR UP LIMIT MICROSWITCH OUT OF ADJUSTMENT. ABURNING SMELL IN THE CABIN WAS ATTRIBUTED TO A RECENT COMPRESSOR WASH.Aug 28, 2000 · Beech 200BEECH · Landing Gear Position and WarningSDR CA000906006Windshield · failed(CAN) WHILE IN CRUISE AT 28,000 FEET, THE R/H WINDSHIELD FAILED. THE INNER LAMINATION SUSTAINED A FAILURE RESULTING IN A LATTICE LIKE SERIES OF CRACKS. (INSTALLED MAY 1997.)Aug 17, 2000 · Beech B200 · Flight Compartment WindowsSDR CA001018002Fire Detector · contaminated(CAN) AFTER STARTING BOTH ENGINES, THE FIRE INDICATION FOR THE RT ENGINE WENT OFF. MAINTENANCE INSPECTED ALL FIRE DETECTORS AND TESTED THEM AND FOUND THEM TO BE SERVICEABLE. AN ENGINE RUN WAS ALSO CARRIED OUT AND WAS SUCCESSFUL. THE AIRCRAFT WAS RETURNED TO SEJul 31, 2000 · Beech 200BEECH · Fire DetectionSDR CA000809012Tube · split(CAN) DURING CLIMB CREW OBSERVED A RT BLEED AIR LIGHT. WHEN RT BLEED AIR SWITCHED OFF, LT BLEED WOULD NOT HOLD CABIN PRESSURE. AN EMERGENCY DESCENT WAS CARRIED OUT. AT 7,000 THE AIRCRAFT LEVELED OFF AND RETURNED TO BASE. THE DAMAGED PIECE OF TUBING WAS REPLACEJul 24, 2000 · Beech B200C · Cabin Pressure SensorSDR AU000532Frame · cracked(AUS) LEFT FUSELAGE FRAME NR 207 CRACKED. LEFT AND RIGHT STIFFENER PN 101-120021-17 AND PN 101-120021-18 ALSO CRACKED. (X)Jul 11, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000530Frame · cracked(AUS) FUSELAGE FRAME NR 207 CRACKED ON LEFT SIDE. (X)Jul 9, 2000 · Beech B200C · Fuselage Main, Frame
Back to U/A Canada PT6A-42