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 CA000621008Bearing · seized(CAN) DURING CRUISE RT ENGINE FLUXUATES ALL PARAMETERS THAN DROPS TO GROUND IDLE. UNEVENTFUL LANDING. T/S P3,PY ALL SYSTEM FOR LEAKS AND OR BLOCKAGE - NONE FOUND. PULLED FCU AND FOUND DRIVE BEARING SEIZED AND DRIVE COUPLER BROKEN.Jun 7, 2000 · Beech B200 · Fuel Control/Turbine EnginesSDR AU000117Nozzle · improper part(AUS) NR 13 FUEL NOZZLE TIP INCORRECT PART. PART FITTED IS PN 3017957. CORRECT PN 3019424. UNAPPROVED PART.Apr 11, 2000 · Beech 200BEECH · Fuel Injector NozzleSDR CA000322019Probe · leaking(CAN) PILOT NOTICED FUEL TRAILING FROM AIRCRAFT DURING FLIGHT. DISCOVERED FUEL PROBE WAS LEAKING OUT THROUGH CENTER OF PROBE. PROBE REPLACED.Mar 13, 2000 · Beech B200 · Fuel Quantity SensorSDR AU000236Flap · faulty(AUS) FLAPS WOULD NOT EXTEND. INVESTIGATION COULD FIND NO FAULT AND THE FLAPS HAVE OPERATED CORRECTLY SINCE.Mar 11, 2000 · Beech 200CBEECH · Trailing Edge Flap Control SystemSDR CA000313008Nut · stripped(CAN) AIRCRAFT WAS ON TRAINING FLIGHT, LANDING CONFIGURATION. WHEN GEAR WAS SELECTED UP A LOUD SNAPPING SOUND WAS HEARD AND THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. GEAR SELECTED DOWN & L/H GREEN LOCK LIGHT FAILED TO ILLUMINATE. THE GEAR UNSAFE LIGHT ILLUMMar 2, 2000 · Beech 200BEECH · Landing Gear ActuatorSDR AU000157Bulkhead · cracked(AUS) REAR PRESSURE BULKHEAD LOCATED AT BS 346.75 CRACKED IN TWO PLACES.Feb 28, 2000 · Beech B200C · Fuselage Main, BulkheadSDR AU000167Bulkhead · cracked(AUS) REAR PRESSURE BULKHEAD TOP WEB CRACKED IN SEVERAL PLACES.Feb 28, 2000 · Beech B200C · Fuselage Main, BulkheadSDR AU000158Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Feb 22, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000159Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Feb 22, 2000 · Beech B200T · Fuselage Main, FrameSDR AU000160Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Feb 22, 2000 · Beech B200C · Fuselage Main, FrameSDR CA000128026Shaft · fractured(CAN) POWER TURBINE SHAFT BROKEN. RESEARCH OF DETAILS ONGOING.Jan 28, 2000 · Turbine SectionSDR AU000049Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Jan 22, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000050Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Jan 22, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000045Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Jan 22, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000048Frame · cracked(AUS) FUSELAGE FRAME LOCATED AT BS 207 RT CRACKED. CRACKS ALSO FOUND ON FUSELAGE FRAMES AT BS 197.5 AND BS 227.Jan 20, 2000 · Beech B200C · Fuselage Main, FrameSDR CA000118002Squat Switch · out of adjust(CAN) AFTER TAKEOFF, THE GEAR FAILED TO RETRACT WHEN SELECTED UP. RETRACTION CHECKED CARRIED OUT IN HANGAR. FAILURE FOUND TO BE RIGHT SQUAT SWITCH OUT OF ADJUSTMENT.Dec 31, 1999 · Beech B200 · Landing Gear Position and WarningSDR CA991229043Lever · slipped(CAN) CAMBOX INPUT LEVER SLIPPING ON SHAFT, DUE TO INTERFERENCE FROM IMPROPERLY RIGGED FUEL SHUTOFF LINKAGE. OPERATOR REQUESTS TORQUE VALUE FOR IMPUT LEVERFROM MANUFACTURER, NOTE SHAFT IS SERRATED STANDARD MAINTENANCE PRACTICES CAN BE IMPLOYED.Dec 21, 1999 · Beech B200 · Power LeverSDR CA991229044Attach Fitting · damaged(CAN) DAMAGE FOUND ON COUNTERBORE FITTINGS FACE OF UPPER AND LOWER AFT WING ATTACH POINTS.FOUND INCORRECT PART NUMBER WASHER, USED ON BOLT STACK-UP FOR AFT FITTINGS.Dec 17, 1999 · Beech B200 · Wing, Attach FittingsSDR CA991229042Windshield · cracked(CAN) WINDSHIELD CRACKED IN FLIGHT BELIEVED TO HAVE BEEN CAUSED BY HAILSTONE STRIKING WINDSCREEN AND PREVIOUS DELAMINATION. UPON REMOVAL OF WINDSCREEN IT WAS DISCOVERED THAT THE MINIMUM ALLOWABLE CLEARANCE BETWEEN THE WINDSCREEN FLANGEAND THE AIRFRAME WAS BELODec 10, 1999 · Beech B200 · Flight Compartment WindowsSDR CA991229041Probe · worn(CAN) MAINTENANCE LOCATED FUEL QUANTITY ERRATIC READINGS TO BE FROM THE LT CENTRE AUX TANK PROBE.UPON EXAMINATION IT WAS DISCOVERED THAT THE FUEL PROBE SOUTER SHEATH OF THE CAPACITOR WAS LOOSE AT THE UPPER ATTACH RIVETS. THIS MOVEMENT WOULD HAVE VARIED THE ELEDec 8, 1999 · Beech B200 · Fuel Quantity SensorSDR 2000ZZZX173Exciter Box · failedDURING ROUTINE START-UP, THE LEFT ENGINE FAILED TO LIGHT OFF. THE IGNITION SYSTEM WAS IMMEDIATELY SUSPECT DUE TO LACK OF 'POPPING' THAT ACCOMPANIES THE FIRING OF THE IGNITERS. THE EXCITER BOX WAS REPLACED AND THE ENGINE STARTED NORMALLY.Nov 24, 1999 · N430MC · Beech 200BEECH · ExciterSDR 99ZZZX4397Fcu · leakingFOUND FUEL LEAKING OUT OF IDLE CUT-OFF SHAFT OF FUEL CONTROL UNIT.Nov 3, 1999 · N500LP · Beech B200 · Fuel Control/Turbine EnginesSDR AU991026Actuator · faulty(AUS) LANDING GEAR MOTOR FAULTY.Oct 16, 1999 · Beech B200C · Landing Gear ActuatorSDR AU990943Switch · faulty(AUS) UPLIMIT MICROSWITCH ACTUATOR HEAD LOOSE ON SWITCH BODY. MICROSWITCH WAS A NEW ITEM.Sep 7, 1999 · Beech 200BEECH · Landing Gear Position and WarningSDR AU990948Switch · faulty(AUS) LANDING GEAR DOWN LIMIT MICROSWITCH FAULTY. DOWEL PINS HOLDING THE SWITCH BODY AND THE ACTUATOR HEAD TOGETHER HAD PARTIALLY WORKED ITS WAY OUT.Sep 7, 1999 · Beech 200BEECH · Landing Gear Position and WarningSDR AU990951Switch · faulty(AUS) LANDING GEAR UPLIMIT MICROSWITCH FAULTY. INSPECTION FOUND THAT THE DOWEL PINS HOLDING THE MICROSWITCH BODY TO THE ACTUATOR HEAD HAD COME OUT. THE LANDING GEAR MOTOR CONTROL CIRCUIT BREAKER BLEW WHEN THE GEAR OVERRAN.Sep 7, 1999 · Beech 200BEECH · Landing Gear Position and WarningSDR AU990820Wire · worn(AUS) WIRE BUNDLE CHAFING ON PITOT/STATIC LINE IN AREA BELOW THE CIRCUIT BREAKER PANEL.Aug 12, 1999 · Beech B200C · Electrical Power System WiringSDR AU990810Circlip · separated(AUS) EMERGENCY UNDERCARRIAGE HAND PUMP PISTON RETAINING CIRCLIP DISLODGED ALLOWING LOSS OF HYDRAULIC FLUID.Aug 6, 1999 · Beech B200C · Landing Gear Retraction/Extension SystemSDR 99ZZZX3001Cooler · failedWHILE PERFORMING RUN-UP CHECKS, NR 1 ENGINE WOULD NOT ACCELERATE. TROUBLESHOT TO BAD FUEL/OIL HEAT EXCHANGE P/N 3039259, S/N WA11014. INSTALLED NEW FUEL OIL HEAT EXCHANGE P/N 3039259, S/N W11769. OPERATIONS CHECKED OK.Jul 30, 1999 · N670DF · Beech B200 · Engine Fuel/Oil CoolerSDR AU990799Disc · broken(AUS) BRAKE ROTATING DISC BROKEN. SUSPECT CAUSED BY OVERHEATING.Jul 30, 1999 · Beech B200C · BrakeSDR AU990725Propeller Assy · fod(AUS) PROPELLER CONTAINED FOD LEFT OVER FROM THE LAST ASSEMBLY. A BRIDGING TOOL USED TO PREVENT CUTTING OF THE PISTON O-RING DURING ASSEMBLY WAS FOUND ON THE PRESSURE SIDE OF THE PISTON. THE PISTON SKIRT HAD BEEN DAMAGED AND THE CYLINDER SCORED. FOD.Jul 16, 1999 · Beech B200C · Propeller AssemblySDR AU990711Hub · fod(AUS) PROPELLER FOD. A SMALL BRIDING TOOL WAS FOUND INSIDE THE PROPELLER CAUSING DAMAGE TO PARTS. METAL CONTAMINATION OF OIL SYSTEM.Jul 14, 1999 · Beech B200C · Propeller Hub SectionSDR AU990712Door · misrepaired(AUS) BAGGAGE DOOR MODIFICATION POOR WORKMANSHIP PREVENTED CORRECT CLOSURE OF BAGGAGE DOOR. DOOR TOP HINGES HITTING DOOR FRAME WHEN FULLY OPEN CAUSING DEFORMATION AND TWISTING OF TOP OF FRAME. DOOR ALSO SIDE LOADED BY GUIDE BLOCK.Jul 12, 1999 · Beech 200BEECH · Cargo/Baggage DoorsSDR AU990713Control Cable · corroded(AUS) CONTROL CABLES, WIRING AND COAXIAL CABLES LOCATED BEHIND THE INSTRUMENT PANEL AND CENTER CONSOLE CORRODED. CORROSION AND SURFACE CORROSION ON MOST EXPOSED STEEL AND CADMIUM PLATED SURFACES. THE AIRCRAFT HAD BEEN TAXIED WITH THE NLG BAY AFT ACCESS PANELJul 12, 1999 · Beech 200BEECH · Flight Control SystemSDR AU990571Shock Absorber · cracked(AUS) NOSE LANDING GEAR SHOCK ABSORBER CRACKED. FOUND DURING INSPECTION IAW AD/BEECH200/45 AMDT2 (BEECH SB 2102 REV III).Jun 8, 1999 · Beech 200BEECH · Nose/Tail Landing Gear Strut/AxleSDR AU990417Hinge · corroded(AUS) ELEVATOR HINGES CONTAINED EXFOLIATION CORROSION. THE CORROSION WAS MAINLY IN BUT NOT CONFINED TO THE HINGE ATTACHMENT AREA.Apr 21, 1999 · Beech 200BEECH · Elevator StructureSDR AU990519Light · overheat(AUS) WINDOW FLUORESCENT LIGHT TRANSFORMER OVERHEATED CAUSING THE VELCRO ATTACHMENT TOUCHING THE TRANSFORMER TO MELT. SUSPECT VELCRO INCORRECTLY FITTED.Apr 13, 1999 · Beech 200BEECH · Passenger Compartment LightingSDR 99ZZZX3298Compressor · seizedCOMPRESSOR LOCKED UP. REF: MCN NR 4.Jan 31, 1999 · N75LV · Beech B200 · Turbine Engine Compressor SectionSDR 99ZZZX1136Turbine · damagedPROPELLER STRIKE. DUE INSPECTION DUE TO SUDDEN STOPPAGE. PART CYCLES: 3192.Jan 8, 1999 · N301HC · Beech B200 · Turbine SectionSDR 99ZZZX1137Blade · damagedPROPELLER DAMAGED DUE TO PROPELLER STRIKE. THREE EACH BLADES REMOVED, P/N 100LA-2. S/N'S EJ-015, EJ-023, EJ-046. TIME SINCE NEW: 1,008.2 HOURS.Jan 8, 1999 · N301HC · Beech B200 · Propeller Blade SectionSDR CA990119006Guard · missing(CAN) AIRCRAFT IN-FLIGHT WHEN ELEVATOR TRIM JAMMED. NO DIFFICULTIES ENCOUNTERED. INVESTIGATION REVEALED THAT THE ELEVATOR TRIM CABLE HAD JUMPED OFF THE DRUM OF THE COCKPIT CONTROL QUADRANT. ICE MAY HAVE BEEN A FACTOR CAUSING TRIM TO BE STIFF. WHEN OPERATEDJan 1, 1999 · Beech B200C · Elevator Tab Control SystemSDR AU981471Gear · corroded(AUS) PROPELLER REDUCTION GEARBOX GEAR CORRODED. PART TC: 1,710.Nov 9, 1998 · Beech 200BEECH · Turbine Engine Reduction GearSDR AU981498Seal · failed(AUS) LOSS OF TORQUE AND ENGINE OIL PRESSURE. SUSPECT CAUSED BY FAILURE OF NR 3 OR NR 4 BEARING OIL SEAL DUE TO CORROSION OF THE HOUSING.Nov 9, 1998 · Beech 200BEECH · Turbine SectionSDR CA980819011Fire Detector · failed(CAN) DURING FLIGHT, MASTER CAUTION AND RIGHT FIRE LIGHT ILLUMINATED. ENGINE SHUT DOWN AND AIRCRAFT RETURNED TO BASE. MAINTENANCE CHECK FOUND FAULTY FIRE DETECTOR SENSOR AND THERE WAS NO EVIDENCE OF FIRE.Aug 11, 1998 · Beech B200C · Fire DetectionSDR AU981026Lever · loose(AUS) ENGINE POWER LEVER ARM SLIPPING ON THE GROOVED PIN OF THE REVERSING MECHANISM. SUSPECT LEVER ARM CLAMPING BOLT AND NUT INSUFFICIENTLY TORQUED DURING INSTALLATION 47.2 HOURS PREVIOUSLY.Aug 5, 1998 · Beech B200C · Power LeverSDR AU981027Pin · defective(AUS) POWER LEVER GROOVED PIN IS IMPRESSING GROOVES INTO LIGHT ALLOY OF POWER LEVER ARM.Aug 5, 1998 · Beech B200C · Power LeverSDR AU981025Battery · overtemp(AUS) BATTERY OVERHEATED. SUSPECT CAUSED BY NUMEROUS STARTS.Aug 1, 1998 · Beech 200BEECH · Battery/Charger SystemSDR AU981232Regulator · failed(AUS) LKH VOLTAGE REGULATOR FAULTY.Jul 28, 1998 · Beech B200C · DC RegulatorSDR AU981233Regulator · failed(AUS) LEFT VOLTAGE REGULATOR FAILED.Jul 27, 1998 · Beech B200C · DC RegulatorSDR AU981024Spar · delaminated(AUS) CENTER WING SPAR LOWER SPAR CAP DELAMINATED FOR APPROXIMATELY 609.6MM (24 INCHES). PART TC: 1,710.Jul 26, 1998 · Beech 200BEECH · Wing Spar
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