U/A Canada PT6A-41

Service difficulty reports · 717

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 = '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 CA020523008Frame · cracked(CAN) FUSELAGE LT FRAME AT STATION 158.00 STINGER 9 CRACKED. TO BE REPAIRED PRIOR TO FURTHER FLIGHT.May 22, 2002 · Beech 200BEECH · Fuselage Main, FrameSDR CA020521010Frame · cracked(CAN) DURING STRUCTURAL INSPECTION FOUND FLIGHT DECK UPPER FUSELAGE LEFT HAND FORMER CRACKING IN TWO LOCATIONS. FORMER TO BE REPLACED PRIOR TO FURTHER FLIGHT.May 21, 2002 · Beech 200BEECH · Fuselage Main, FrameSDR CA020516009Frame · cracked(CAN) FUSELAGE RIGHT HAND FRAME AT STA 158.00, STRINGER 10 CRACKED. SHEET METAL REPAIR TO BE DONE PRIOR TO FURTHER FLIGHT.May 16, 2002 · Beech 200BEECH · Fuselage Main, FrameSDR CA020516010Frame · cracked(CAN) FUSELAGE RIGHT HAND FRAME STA 167.625, STRINGER 10 CRACKED. SHEET METAL REPAIR TO BE DONE PRIOR TO FLIGHT.May 16, 2002 · Beech 200BEECH · Fuselage Main, FrameSDR CA020516011Frame · cracked(CAN) FUSELAGE RIGHT HAND FRAME AT STA 177.50, STRINGER 8 CRACKED. SHEET METAL REPAIR TO BE DONE PRIOR TO FURTHER FLIGHT.May 16, 2002 · Beech 200BEECH · Fuselage Main, FrameSDR CA020517009Bulkhead · cracked(CAN) BULKHEAD CRACKED BELOW FLOOR AT STATION 227.125 CENTER SECTION. SHEET METAL REPAIRS TO BE CARRIED OUT PRIOR TO FURTHER FLIGHT.May 16, 2002 · Beech 200BEECH · Fuselage Main, BulkheadSDR CA030102005Skin · damaged(CAN) BEFORE INSTALLING BAGGAGE PAD, MAINTENANCE NOTICED THAT BELLY SKIN AFT OF REAR SPAR AT STA 226.5 WAS SLIGHTLY WRINKLED, AND LOWER FLAP/FUSELAGE FAIRING SLIGHTLY WRINKLED. HARD LANDING/TURBULENT AIR INSPECTION AS PER 5-50-00 CARRIED OUT. SLIGHT WRINKLE ONMay 11, 2002 · Beech 200BEECH · Fuselage Main, Plate/SkinSDR AUS20020465Engine · making metal(AUS) LT AND RT ENGINE CHIP DETECTORS ILLUMINATED IN FLIGHT. CHIP DETECTORS ON BOTH ENGINES CONTAMINATED WITH METAL FLAKES. FLAKES APPEAR TO BE A MIXTURE OF BRONZE, FERROUS AND NON FERROUS PARTICLES.May 10, 2002 · Beech 200BEECH · Engine (Turbine/Turboprop)SDR AUS20020407Fork · unserviceable(AUS) NLG ASSEMBLY TUBE UNCHROMED PORTION EXCEEDED 1.27MM (0.050IN) AND LENGTH OF THE TUBE EXCEEDED 91MMM (23.10IN). FOUND DURING INSPECTION IAW AD/BEECH200/45 AND SB2102 REV5.May 2, 2002 · Beech 200BEECH · Nose/Tail Landing Gear Strut/AxleSDR S8A2002F00000Impeller · brokenAIRCRAFT DEPARTED FOR RETURN TRIP HOME. APPROXIMATELY 80 MILES FROM DEPARTURE POINT, THE ENGINE STARTED HAVING COMPRESSOR STALLS AND FLAMES COULD BE SEEN IN THE EXHAUST STACKS. ENGINE WAS SHUT DOWN AND PROPELLER FEATHERED. PRELIMINARY INVESTIGATION BY FIELDApr 9, 2002 · N266EB · Beech 200BEECH · Turbine Engine Compressor SectionSDR S8A2002F00001Fire Detector · false activationAIRCRAFT DEPARTED FOR RETURN TRIP HOME. APPROX 80 MILES FROM DEPARTURE POINT ENGINE STARTED HAVING COMPRESSOR STALLS AND FLAMES COULD BE SEEN IN EXHAUST STACKS. ENGINE WAS SHUT DOWN AND PROPELLER FEATHERED. PRELIMINARY INVESTIGATION FIELD SERVICE REPRESENTAApr 9, 2002 · N266EB · Beech 200BEECH · Fire DetectionSDR CA020405005Bolt · cracked(CAN) DURING MAIN WHEEL ASSEMBLY TIRE REPLACEMENT, THREE TIE BOLTS OUT OF EIGHT SHEARED WHEN RECOMMENDED TORQUE WAS APPLIED. PRIOR TO ASSEMBLY ALL BOLTS WERE VISUALLY INSPETED AND NO EVIDENCE OF CRACKS WERE NOTED. ALL EIGHT BOLTS WERE REPLACED.Mar 26, 2002 · Piper PA42 · Wheel/Ski/FloatSDR CA020403006Latch · failed(CAN) AFTER TAKEOFF CALGARY (CYYC), CLIMBING THROUGH 14,000 FEET, THE CREW AND PASSENGERS HEARD A LOUD BANG, THEN THE CABIN AIRSTAIR DOOR DROPPED OPEN. THE CREW DECLARED AN EMERGENCY TO ATC, INSTITUTED AN EMERGENCY DESCENT AND TURNED BACK FOR CALGARY WHERE THEMar 20, 2002 · Beech 200BEECH · Passenger/Crew DoorsSDR CA020314001Pressure Switch · sticks(CAN) AFTER TAKEOFF THE HYDRAULIC PUMP CYCLED ON FOR AN ABNORMAL LENGTH OF TIME WITH THE GEAR SELECTED TO THE UP POSITION. THE LANDING GEAR WAS SELECTED TO DOWN AND THE CIRCUIT BREAKER POPPED. THE CREW CARRIED OUT THE LANDING GEAR EMERGENCY EXTENSION PROCEDUREMar 12, 2002 · Beech 200BEECH · Hydraulic Pressure Regulator, MainSDR CA020417004Spacer · damaged(CAN) AT ROUTINE ENGINE INSPECTION OF COMPRESSOR FIRST STAGE, FIRST STAGE DISK MADE SCRAPING NOISE AND JAMMED WHEN ROTATED. VISUAL INSPECTION FOUND FIRST STAGE SPACER HEAVILY RUBBED WITH LEADING EDGE METAL PIECES CURLED OUTWARD FROM INERTIAL FORCE. ENGINE REMMar 12, 2002 · Beech 200BEECH · Turbine Engine Compressor SectionSDR CA020307008Bracket · bent(CAN) PROP SYNCROPHASER TARGET CONTACTED THE SYNCROPHASER MONOPOLE DAMAGING THE MONOPOLE, MONOPOLE BRACKET AND PROP DE-ICE BRUSH BLOCK BRACKET. THE PROP DE-ICE BRUSH BLOCK BRACKET WAS BENT ENOUGH TO DISPLACE THE PROP DE-ICE BRUSHES ENOUGH TO SHORT ACROSS DE-ICFeb 28, 2002 · Beech 200BEECH · Propeller/Rotor Anti-Ice/De-Ice SystemSDR CA020306001Compressor · failed(CAN) THE AIRCRAFT WAS IN CRUISE FLIGHT AT FL20000. THERE WAS A LOUD BANG THAT SHUCK THE AIRCRAFT AND FLAMES APPEARED COMING OUT OF THE EXHAUST STACKS. THE ENGINE WAS SHUT DOWN AND FEATHERED. FLAMES EXTINGUISHED RIGHT AWAY IN THE STAKES. THERE WAS A SMALL AMFeb 23, 2002 · Beech 200BEECH · Engine (Turbine/Turboprop)SDR R2J2002F00000Antenna · misinstalledDURING AAIP PHASE INSPECTION, FOUND UN-DOCUMENTED GPS INSTALLATION. FOUND ANTENNA MOUNTED IN PRESSURE VESSEL AREA WITH NO SEALING OR DOUBLER, COULD CAUSE VESSEL FAILURE. REPAIR OF FUSELAGE AND ALTERATION, INSTALLING ANTENNA, MADE USING APPROVED DATA. ALWAYSFeb 13, 2002 · N574GS · Beech 200BEECH · Global Positioning SystemSDR R2J2002F00004Splice Plate · improper partDURING AAIP PHASE INSPECTION DISCOVERED IMPROPER PARTS HAD BEEN INSTALLED WHILE INSTALLING AVIADESIGN WING SPAR STRAP PER STC SA 1602CE. STC HOLEDER WAS CONTACTED AND APPROVED PART, WHICH IS A SPECIAL ALLOY, WAS INSTALLED. FAA-PMA PART. SUGGEST CALLING THE Feb 13, 2002 · N574GS · Beech 200BEECH · Wing Miscellaneous StructureSDR AUS20020144Windshield · cracked(AUS) WINDSHIELD CRACKED WHEN HEAT TURNED ON.Feb 12, 2002 · Beech 200BEECH · Flight Compartment WindowsSDR VXW2002F00000Bearing · failedPOST FLIGHT INSPECTION FOUND BOTH PIVOT BEARINGS ON LEFT MAIN LANDING GEAR ACTUATOR SHATTERED. UPON REMOVAL, BOTH BEARING OUTER RACES HAD BEEN BROKEN IN HALF AND BALLS FALLING DOWN TO WING SPAR. MISC PIECES ALSO LAYING ON SPAR, CONSIDERING THE FORCE REQUIREDFeb 6, 2002 · N12CF · Beech 200BEECH · Landing Gear Door ActuatorSDR CA020207002Blade · cracked(CAN) TWO (2) CT BLADES CRACKED.Feb 3, 2002 · Beech B200 · Turbine SectionSDR AUS20020083Blade · cracked(AUS) LT PROPELLER NR 2 BLADE CRACKED. CRACK LENGTH APPROXIMATELY 40MM (1.57IN) RUNNING CHORDWISE ACROSS THE BLADE FROM THE TRAILING EDGE. CRACK IS LOCATED APPROXIMATELY 150MM (5.9IN) FROM THE BLADE TIP.Feb 1, 2002 · Beech B200C · Propeller Blade SectionSDR CA020208001Windshield · failed(CAN) APPROX 15 MINS AFTER LEVELLING OFF AT CRUISE ALTITUDE OF 29,000 FEET, SMALL CRACK FORMED ON RIGHT WINDSHIELD. FEW SECONDS LATER, ENTIRE INNER PLY SHATTERED & CABIN PRESSURIZATION LOST AT RATE OF APPROX 2500 FT/MIN . EMERGENCY OXYGEN DEPLOYED & MASKS DOJan 25, 2002 · Beech 200BEECH · Flight Compartment WindowsSDR CA020108003Pump · stripped(CAN) ENGINE SHUT DOWN IN CRUISE FLIGHT. AIRCRAFT MADE AN UNSCHEDULED LANDING TROUBLESHOOTING REVEALED NO FUEL FLOW TO DIVIDER. HIGH PRESSURE FUEL PUMP REMOVED. FUEL PUMP SPLINES FUND TO BE STRIPPED. PUMP REPLACED.Dec 14, 2001 · Piper PA42 · Engine Fuel PumpSDR T4O2001F00001Torque Tube · looseTHE RIVETS ON THE RIGHT ELEVATOR TORQUE TUBE TO INBOARD CASTING (FOR PUSHROD) WERE LOOSE AND SMOKING. PROBABLE CAUSE UNKNOWN. INSTALLED A NEW TORQUE TUBE ASSEMBLY FOR THE RT ELEVATOR.Dec 6, 2001 · N266RH · Beech 200BEECH · Elevator StructureSDR T4O2001F00002Torque Tube · looseTHE RIVETS ON THE RIGHT ELEVATOR TORQUE TUBE TO OUTBOARD CASTING (WHERE IT BOLTS TO ELEVATOR) WERE LOOSE AND SMOKING. PROBABLE CAUSE UNKNOWN. INSTALLED A NEW TORQUE TUBE ASSEMBLY FOR THE RIGHT ELEVATOR.Dec 6, 2001 · N5PX · Beech 200BEECH · Elevator StructureSDR CA020114009Engine · failed(CAN) ENGINE WAS SENT TO ATI FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED THAT ENGINE HAD BEEN SHUT DOWN IN FLIGHT. THE OPERATOR REPORTED THAT DURING THE APPROACH THE PILOT HAD NOTICED THE TURBINE INTERSTAGE TEMPERATURE HAD INCREASED TO 950 DEGREESNov 30, 2001 · Engine (Turbine/Turboprop)SDR CA011116018Windshield · cracked(CAN) THE AIRCRAFT WAS IN CRUISE AT FLIGHT LEVEL 290, APPROXIMATELY 50 MILES NW OF SUDBURY, ONTARIO, ENROUTE FROM THUNDER BAY TO THETFORD MINES, QUEBEC, WHEN THE LT WINDSHIELD INNER PANE SHATTERED. THE CREW REDUCED PRESSURIZATION TO 4 PSI DIFFERENTIAL PRESSURENov 8, 2001 · Beech 200BEECH · Flight Compartment WindowsSDR CA011116020Windshield · failed(CAN) ON APPROACH INTO CIGAR LAKE, SASKATCHEWAN (JWY) THE RIGHT HAND WINDSHIELD INNER PANE SHATTERED IN A LATTICE LIKE MODE. THE NETWORK OF CRACKS EXTENDED OVER THE ENTIRE INNER SURFACE OF THE SHIELD AND AN ORIGINATING POINT OR CAUSE COULD NOT BE DETERMINED.Nov 6, 2001 · Beech 200BEECH · Flight Compartment WindowsSDR AUS20011184Cowling · separated(AUS) LH ENGINE FORWARD UPPER COWL ASSEMBLY SEPARATED IN FLIGHT. PILOTHAD RECENTLY PERFORMED MAINTENANCE ON THE COWL. MINOR DAMAGE TO COWLS AND LEADING EDGE CAUSED BY COWL SEPARATION. PERSONNEL/MAINTENANCE ERROR.Nov 2, 2001 · Beech 200BEECH · Engine Cowling SystemSDR WD42001F00000Valve · mismanufacturedNEW REPLACEMENT PARTS FOR THE ANTI-SIPHON VALVE ASSEMBLY ARE BEING MFG INCORRECTLY. PROBLEM IS THE FLAPPER ASSEMBLY GASKET AND BACKUP PLATE WERE TRIMMED INCORRECTLY AND HINGE IS EXPOSED LEAVING A GAP WHERE FUEL CAN BE SIPHONED OUT DURING FLIGHT IF THE FUEL CANov 1, 2001 · N638B · Beech A200 · Fuel StorageSDR 2001FA0000227Engine · failedLEFT ENGINE SHUT DOWN DUE TO CHIP DETECTOR LIGHT ON ENGINE SURGING AND OIL PRESSURE FALLING OFF. ON INITIAL INSPECTION SUSPECTS COMPRESSOR, NR1 OR NR 2 MAIN LINE BEARING FAILURE.Jul 30, 2001 · N2025M · Beech 200BEECH · Engine (Turbine/Turboprop)SDR CA010809018Outflow Valve · dirty(CAN) AT FLIGHT LEVEL 22000, CABIN LOST PRESSURE. AN EMERGENCY DESCENT WAS CARRIED OUT AND THE REMAINDER OF THE FLIGHT WAS NORMAL. UPON INSPECTION THE OUTFLOW VALVE WAS FOUND TO BE LOOSE AND DIRTY. THE VALVE WAS CLEANED & TIGHTENED, THEN A SATISFACTORY TEST FLJul 26, 2001 · Piper PA42 · Pressure Regulator/Outflow ValveSDR Z4MR601462Relief Valve · leakingA RANDOM INSPECTION OF THE FUEL PUMP REVEALED FUEL LEAKING FROM THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP RELIEF VALVE GASKET.Jul 14, 2001 · N726CB · Beech B200 · Engine Fuel PumpSDR AUS20010755Fitting · corroded(AUS) HORIZONTAL STABILISER AFT UPPER FITTING CONTAINED SEVEREINTERGRANNULAR CORROSION. NDI CARRIED OUT ON FITTING FOLLOWINGREMOVAL FOUND THREE CRACKS BETWEEN THE BOLT HOLES.Jul 5, 2001 · Beech 200BEECH · Horizontal Stabilizer, Attach FittingsSDR CA010627056Windshield · failed(CAN) AIRCRAFT WAS IN LEVEL FLIGHT AT 24000 FEET ON AUTOPILOT WHEN LT WINDSHIELD SHATTERED. FLIGHT CREW DEPRESSURIZED AND DESCENDED. AIRCRAFT RETURNED WITHOUR FURTHER INCIDENT.Jun 26, 2001 · Beech 200BEECH · Flight Compartment WindowsSDR AUS20010695Indicator · out of adj(AUS) AIRSPEED INDICATOR READING 5 KNOTS OUT OVER THE ENTIRE RANGE. FOUND DURING INSPECTION IAW AD/INST/9 AMDT5.Jun 24, 2001 · Beech 200BEECH · Airspeed/Mach IndicatorSDR CA010625005Control Cable · broken(CAN) WHILE OPERATING IN CRUISE FLIGHT, A SELECTION OF THE PROPELLOR LEVER CONTROL FOR THE RIGHT ENGINE WAS MADE WITH NO CHANGE IN PROP RPM. ANOTHER SETTING WAS TRIED WITH NO RESPONSE. THE RPM REAMINED AT 1900. THE FLIGHT ROUTIG WAS CANCELLED AND TH AIRCRAFT RJun 16, 2001 · Beech 200BEECH · Propeller Controlling SystemSDR CA010703006Pump · misinstalled(CAN) RECEIVED MOTOR P/N 115-380002-5 S/N 1783 FROM TRANSPORT CANADA STICK INSTALLED THE O/H MOTOR ON THE AIRCRAFT AS PER WIRING DIAGRAM IN WESTERN AIRCRAFT MAINTENANCE MANUAL. FOUND THAT THE HYDRAULIC PUMP ROTATION WAS INCORRECT. THE WIRING DIAGRAM WAS REVERJun 1, 2001 · Beech 200BEECH · Hydraulic Pump (Electric/Engine), MainSDR CA010625024Engine · failed(CAN) ABOUT 1 HR INTO FLT CREW NOTED A SLIGHT FLUNCTUATION IN RT ENGINE TORQUE ALONG WITH A REDUCTION IN ENGINE NG SPEED. ITT ALSO INCREASED 50 DEGS HIGHER THAN NORMAL FOR CRUISE POWER.THE CREW MONITORE ENGINE PARAMETERS & NOTED A FURTHER DECREASE IN NG TO BELMay 9, 2001 · Beech 200BEECH · Engine (Turbine/Turboprop)SDR CA010523003Light · shorted(CAN) SHORTLY AFTER GEAR DOWN SELECTED ON FINAL, PUFF OF SMOKE NOTICED BY PASSENGER IN AREA OF LT NR 1 & 2 WINDOWS. LDG CARRIED OUT NORMLLY AS NO FURTHER SMOKE. AS PRECAUTION A/C STOPPED & SHUTDOWN AT THE 1ST AVAILABLE RWY TURNOFF & PASSENGER UNLOADED. FAULT CMay 8, 2001 · Beech 200BEECH · Passenger Compartment LightingSDR CA010411008Pump · leaking(CAN) CARRYING OUT A DAILY INSPECTION ON MARCH 16, AFTER RETURNING FROM A TRAINING FLIGHT. FOUND THAT THE ENGINE DRIVEN FUEL BOOST PUMP P/N 91-38003 THAT IS MOUNTED ON THE REAR OF ENGINE S/N PCE-81053 WAS LEAKING FUEL AROUND THE BASE OF THE VALVE THAT IS INSTAMar 16, 2001 · Beech 200BEECH · Fuel Boost PumpSDR CA010302010Current Limiter · failed(CAN) AIR NUNAVUT KING AIR WAS ON APPROACH TO IGALUIT AT NIGHT. FLIGHT CREW SELECTED GEAR, THEY RECEIVED AN UNSAFE GEAR INDICATION AND HAD TO USE GEAR EMERGENCY EXTENSION METHOD, AFTER WHICH GAVE 3 GREEN GEAR DOWN AND LOCKED INDICATION. THE AIRCRAFT LANDED WITJan 31, 2001 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR 20001229SH006Compressor · failedJUST AFTER TAKEOFF, COPILOT REPORTED SPARKS COMING FROM RT ENGINE INBOARD AND OUTBOARD EXHAUST STACKS. POWER WAS REDUCED AND AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. INSPECTION THROUGH THE HIGH AND LOW BLEED VALVE OPENINGS REVEALED MASSIVE COMPRESSOR FDec 20, 2000 · N366EA · Beech 200BEECH · Turbine Engine Compressor SectionSDR 20010125CW001Compressor · failedJUST AFTER T/O COPILOT REPORTED SPARKS COMING FROM RIGHT ENGINE, INBOARD AND OUTBOARD EXHAUST STACKS. POWER WAS REDUCED AND AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. INSPECTION THROUGH HIGH AND LOW BLEED VALVE OPENINGS REVEALED MASSIVE COMPRESSOR FAILURDec 8, 2000 · N366EA · Beech 200BEECH · Turbine Engine Compressor SectionSDR 20010207CW005Vane · brokenS/D TEARDOWN REPORT REVEALED ONE EACH VANE BROKEN IN STAGE ONE VANE AND SHROUD CAUSING INTERNAL DAMAGE. STAGE 2 COMPRESSOR AND VANE & SHROUD SUSTAINED HEAVY FOD, STAGE 3 COMPRESSOR AND VANE AND SHROUD SUSTAINED HEAVY FOD.Dec 8, 2000 · N366EA · Beech 200BEECH · Turbine Engine Compressor SectionSDR AU001263Regulator · leaking(AUS) PRESSURE REGULATOR LEAKING P3 AIR INTO CABIN. INTERNAL INSPECTION FOUND ALL SEALS WORN AND THE REGULATOR WORN AND LEAKING.Dec 2, 2000 · Beech B200C · Pressure Regulator/Outflow ValveSDR 20010129CW021Hose · chafedHOSE IS RUBBING AGAINST ENGINE COWLING. RT ENGINE OUTBOARD STACK RELOCATE PICK UP TUBE LOCATION, ANGLE TOWARDS ENGINE CASE.Dec 1, 2000 · N280SC · Beech 200BEECH · Heating SystemSDR 20010129CW022Hose · chafedHOSE IS RUBBING AGAINST ENGINE COWLING. RT ENGINE INBOARD STACK. RELOCATE PICK UP TUBE LOCATION ANGLE TOWARDS ENGINE CASE.Dec 1, 2000 · N280SC · Beech 200BEECH · Heating System
Back to U/A Canada PT6A-41