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 20010129CW023Hose · chafedHOSE IS RUBBING AGAINST ENGINE COWLING. LEFT ENGINE INBOARD STACK. RELOCATE PICK UP TUBE LOCATION, ANGLE TOWARDS ENGINE CASE.Dec 1, 2000 · N280SC · Beech 200BEECH · Heating SystemSDR 20010129CW024Hose · chafedHOSE IS RUBBING AGAINST ENGINE COWLING. LEFT ENGINE OUTBOARD STACK. RELOCATE PICK UP TUBE LOCATION. ANGLE TOWARDS ENGINE CASE.Dec 1, 2000 · N280SC · Beech 200BEECH · Heating SystemSDR CA001219010Tire · separated(CAN) PILOT REPORT THAT SHORTLY AFTER TAKEOFF THEY EXPERIENCED A VIBRATION. THEY COMPLETED CCT & RETURNED TO AN A.M.O. FACILITY. NOSE OF A/C WAS RAISED & NOSE WHEEL WAS MANUAL SPUN. MAINT FOUND NOSE WHEEL BEARING WAS NOT CORRECTLY PRELOADED CAUSING TIRE TO SPINov 30, 2000 · Beech 200BEECH · TireSDR CA001229010Bearing · failed(CAN) ON FINAL LEG OF DAY, PILOTS RPT THAT WHEN LDG GEAR SELECTED UP, INTRANSIT LIGHT NEVER EXTINGUISHED. VISUAL CHECK CONFIRMED THAT LDG GEAR INDEED RETRACTED. LDG GEAR EXTENDED AS USUAL&SAFELDG MADE. AT HOME BASE, MAINT PERSONNEL PERFORMED RETRACTION TEST&DINov 29, 2000 · Beech 200BEECH · Landing Gear ActuatorSDR CA001218014Lever · worn(CAN) LEVER THAT ATTACHES POWER LEVER CONTROL ROD TO FCU ON ENGINE SLIPPPED WHEN L/H POWER LEVER WAS BROUGHT FROM REVERSE INTO IDLE, CAUSING N1 TO READ 3% HIGHER THAN NORMAL.INSPECTION OF LEVER SHOWED NO ABNORMALITIES, ONLY THING NOTED IS INSIDE BORE OF LEVER Nov 27, 2000 · Beech 200BEECH · Power LeverSDR 20001214SH028Pump · leakingDURING FLIGHT, THE FUEL FLOW DROPPED OFF UNTIL THE ENGINE TORQUE DROPPED ENOUGH TO FEATHER THE PROPELLER. THE CREW THEN SHUT THE ENGINE OFF WITH THE FUEL CONDITION LEVER. MAINTENANCE FOUND THE 4 SCREWS (THAT WERE SAFTIED) HOLDING THE PRESSURE RELIEF ADJUSTMENov 25, 2000 · N847BA · Beech 200BEECH · Aircraft Fuel Distribution SystemSDR CA001212023Windshield · cracked(CAN) THE FLIGHT CREW HEARD A NOISE IN THE FRONT OF THE AIRCRAFT AND UPON INVESTIGATION, DETERMINED THAT THE CAPTAINS WINDSCREEN HAD CRACKED IN THE OUTER PANE OF GLASS. THE AIRCRAFT RETURNED TO BASE AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE WINDSHIELNov 21, 2000 · Beech 200BEECH · Flight Compartment WindowsSDR CA001123003Windshield · cracked(CAN) DURING PRE-FLIGHT INSPECTION, THE FLIGHT CREW NOTICED A CRACK IN THE LT WINDSHIELD. MAINTENANCE ADVISED. AIRCRAFT REMOVED FROM SERVICE WINDSHIELD REPLACED. (X)Nov 8, 2000 · Beech 200BEECH · Flight Compartment WindowsSDR B3OR200000005Tube · crackedPILOTS COMPLETED PRE-TAKEOFF ENGINE RUNS AND RETURNED ENGINES TO IDLE. WHEN POWER LEVERS WERE ADVANCED FOR TAXI TO ACTIVE, NR 1 ENGINE DID NOT RESPOND TO INPUT. AIRCRAFT WAS RETURNED TO RAMP WHERE IT WAS DISCOVERED THAT P3 SENSE LINE TO FCU WAS CRACKED NEAR Nov 2, 2000 · N7074G · Beech A200 · Engine Fuel and ControlSDR AU001024Switch · stuck(AUS) FLAP WARNING SYSTEM MICROSWITCH STUCK. (X)Oct 25, 2000 · Beech B200C · Trailing Flap Position Indicating SystemSDR 001020Motor · slowUPON INSTALLATION OF THIS NEWLY OVERHAULED LANDING GEAR RETACT MOTOR THE LANDING GEAR WOULD CYCLE AT ABOUT HALF NORMAL SPEED. ALL MECHANICAL AND ELECTRICAL SYSTEMS CHECKED GOOD. INSTALLED A NEW RETRACT MOTOR AND ALL SYSTEMS OPERATED NORMALLY.Oct 20, 2000 · N7166P · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR AU001003Valve · faulty(AUS) CABIN PRESSURIZATION SYSTEM FAULTY RESULTING IN AUTO DEPLOYMENT OF THE OXYGEN MASKS. INVESTIGATION FOUND THE RIGHT FLOW PACK PN 101-380013-19 UNSERVICEABLE AND THE LEFT PNEUMOSTAT PN 101-380013-3 STICKING. (X)Oct 19, 2000 · Beech B200C · Cabin Pressure Control SystemSDR AU001058Valve · faulty(AUS) RIGHT FLOW PACK PN 101-380013-19 FAULTY AND LT PNEUMOSTAT PN 101-380013-3 STICKING. (X)Oct 19, 2000 · Beech B200C · Cabin Pressure Control SystemSDR AU001030Link · separated(AUS) NOSE LANDING GEAR DRIVE CHAIN LINK ASSEMBLY SEPARATED DUE TO FAILURE OF THE RETAINING CLIP. INSPECTION OF THE RETAINING CLIP UNDER A 10X MAGNIFYING GLASS FOUND INDICATIONS OF FATIGUE AND CORROSION. (X)Oct 18, 2000 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR 20001101SH022Pump · brokenLEFT ENGINE FLAMED OUT IN-FLIGHT, RESTART PROCEDURES TRIED, BUT ENGINE WOULD NOT START. EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND DRIVESHAFT FOR HIGH PRESSURE FUEL PUMP BROKEN. ENGINE OIL FILTER CHECKED FOR METAL CONTAMINATOct 17, 2000 · N561SS · Beech 200BEECH · Engine Fuel PumpSDR CA001212019Harness · broken(CAN) WHEN GEAR SELECTED DOWN - R/H GEAR DID NOT INDICATE DOWN AND LOCKED.MAINTENANCE FOUND BROKEN WIRE IN HARNESS OF DOWN LOCK SWITCH.Oct 4, 2000 · Beech B200 · Landing Gear Position and WarningSDR AU000879Diode · shorted(AUS) CABIN OXYGEN CONTROL SOLENOID TRANSIENT VOLTAGE SUPPRESSION DIODE SHORT CIRCUITED. FAILURE OF PASSENGER OXYGEN MASK AUTOMATIC DEPLOYMENT. (X)Sep 15, 2000 · Beech B300C · Passenger Oxygen SystemSDR AU000848Solenoid · open(AUS) PASSENGER OXYGEN MASKS DID NOT DEPLOY DURING TEST FLIGHT. INVESTIGATION FOUND SOLENOID OPEN CIRCUIT. (X)Sep 7, 2000 · Beech 200BEECH · Passenger Oxygen SystemSDR AU000665Fitting · scored(AUS) LEFT UPPER FORWARD WING ATTACHMENT FITTING SCORED IN THE BORE OFTHE BARREL NUT RECESS IN THE BATHTUB FITTING. CAUSED BY THE BARREL NUT INSERT BEING INSERTED 90 DEGREES OUT FROM ITS CORRECT POSITION. SUBMITTER SUSPECTED OCCURRED DURING THE PREVIOUS INSPSep 1, 2000 · Beech 200BEECH · Wing, Attach FittingsSDR AU000777Fitting · loose(AUS) RIGHT AILERON FOULING ON UPPER WING SKIN PREVENTING FULL AILERON MOVEMENT. FURTHER INVESTIGATION FOUND THAT THE INBOARD HINGE ATTACHMENT BRACKET WAS NOT SECURED. THE TWO LOWER ATTACHMENT SCREWS WERE INSTALLED BUT NOT SECURED TO THE ANCHOR NUTS. (X)Aug 27, 2000 · Beech 200BEECH · Wing, Control Surface Attach FittingsSDR CA000828006Skin · cracked(CAN) FUSELAGE SKIN CRACK IN PRESSURE VESSEL LOCATED AT WING TO FUSELAGE FILLET MOUNTING SCREW HOLE (ANCHOR NUT) AT LEFT HAND WING LEADING EDGE (APPROX 1.25 INCHES LONG).Aug 15, 2000 · Beech 200BEECH · Fuselage Structure (General)SDR 20000814SH014Shaft · shearedFAR 135 OPERATOR HAD TO CONDUCT AN EMERGENCY LANDING DUE TO A LEFT ENGINE FAILURE. THE ENGINE WAS BEING MAINTAINED UNDER THE MORE PROGRAM STC SE0000EN. THE ENGINE FAILED. TEAR-DOWN REPORT SHOWED THE ACCESSORY GEARBOX INPUT DRIVSHAFT AND DRIVESHAFT BEARINGS Aug 7, 2000 · N79GA · Beech 200BEECH · Turbine Engine Accessory DriveSDR 20000814SH015Bearing · shearedFAR 135 OPERATOR HAD TO CONDUCT AN EMERGENCY LANDING DUE TO A LEFT ENGINE FAILURE. THE ENGINE WAS BEING MAINTAINED UNDER THE MORE PROGRAM STC SE0000EN. THE ENGINE FAILED. TEAR-DOWN REPORT SHOWED THE ACCESSORY GEARBOX INPUT DRIVSHAFT AND DRIVESHAFT BEARINGS Aug 7, 2000 · N79GA · Beech 200BEECH · Turbine Engine Accessory DriveSDR CA000925005Motor · stuck(CAN) LANDING GEAR WOULD NOT RETRACT WHEN SELECTED. (X)Jul 31, 2000 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR CA000802019Motor · failed(CAN) - AIRPLANE HAD SMOKE IN COCKPIT / CABIN. AFTER TROUBLESHOOTING FOUND THAT FORWARD BLOWER MOTOR MAKING GRINDING NOISE AND SMOKE. REPLACED FORWARD BLOWER ASSEMBLY GROUND CHECK SERVICE.Jul 13, 2000 · Beech 200BEECH · Air Distribution FanSDR CA000719026Shaft · twisted(CAN) FLAP JUMPED FLAP LIMIT & SWITCH, WHILE GOING IN TO THE UP POSITION AND CAUSING A FAILURE OF THE FLAP SHAFT LT OUTBOARD TELEFLEX ASSY. RECTIFICATION: REPLACED THE FLAP MOTOR. INSPECTED THE 90 DEGREES DRIVE. INSPECTED THE FLAP TRANSMISSION AND REPLACED THJul 9, 2000 · Beech 200BEECH · Trailing Edge Flap Control SystemSDR CA000719010Frame · cracked(CAN) 0.75 INCH CRACK AT TOP OF SIDE FRAME INSIDE BEND RADIUS.Jun 28, 2000 · Beech 200BEECH · Fuselage Main, FrameSDR 20000721SH036Engine · making metalPILOT EXPERIENCED OIL PRESSURE AND TORQUE FLUCTUATION. THIS ENGINE SHUT DOWN IN-FLIGHT. INSPECTION OF OIL FILTER SHOWED METAL CONTAMINATION. THIS ENGINE HAS BEEN OPERATED FOR 714.9 HOURS ON THE MORE PROGRAM. THE EXACT REASON FOR THIS FAILURE IS NOT KNOWN AJun 26, 2000 · N79GA · Beech 200BEECH · Engine (Turbine/Turboprop)SDR AU000466Gearbox · contaminated(AUS) PROPELLER REDUCTION GEARBOX METAL CONTAMINATION.Jun 16, 2000 · Beech 200BEECH · Turbine Engine Reduction GearSDR AU000460Gearbox · contaminated(AUS) PROPELLER REDUCTION GEARBOX METAL CONTAMINATION.May 29, 2000 · Beech B200C · Turbine Engine Reduction GearSDR CA000606035Tube · cracked(CAN) AFTER TAKEOFF, FUEL VAPOR SMELL IN CABIN, SHUT OFF BLEED AIR, SMELL WENT DOWN. AIRCRAFT RETURNED TO YQB. FOUND FUEL PRESSURE TUBE ASSY CRACKED JUST AFT OF B-NUT.May 15, 2000 · Beech 200BEECH · Engine Fuel DistributionSDR CA000516024Valve · failed(CAN) PILOTS CHECKED FOR BRAKE PRESSURE DURING CRUISE FLIGHT AT 33,000 FEET. BRAKES WERE VERY SOFT. PARKING BRAKE VALVE FOUND TO HAVE LEAKING O-RINGS. SEALS REPLACED.May 8, 2000 · Piper PA42 · Master Cylinder/Brake ValveSDR AU000361Bearing · failed(AUS) ENGINE POWER SECTION FAILED. SUSPECT CAUSED BY NR 3 BEARING FAILURE.May 1, 2000 · Beech B200C · Turbine SectionSDR AU000229Motor · faulty(AUS) LANDING GEAR MOTOR FAILED TO OPERATE.Apr 26, 2000 · Beech 200BEECH · Landing Gear ActuatorSDR CA000410009Windshield · cracked(CAN) WINDSHIELD DELAMINATED 2 MONTHS PRIOR TO CRACK. DELAMINATION WAS WITHIN THE BEECH SERVICE MANUAL LIMITS. WINDSHIELD CRACKED IN AREA OF DELAMINATION.Mar 31, 2000 · Beech 200BEECH · Flight Compartment WindowsSDR CA000329014Controller · faulty(CAN) ON PREPARATION FOR DESCENT, CABIN PRESSURIZATION CONTROLLER RATE WAS ADJUSTED. AFTER ADJUSTMENT WAS MADE CABIN PRESSURE INCREASED TO MAXIMUM DIFERENTIAL AND WAS UNCONTROLLABLE AND NONRESPONSIVE TO ANY FURTHER ADJUSTMENTS TO THE CONTROLLER. CONTROLLER RMar 21, 2000 · Beech 200BEECH · Cabin Pressure ControllerSDR AU000210Panel · missing(AUS) RIGHT NACELLE FUEL DRAIN PANEL NOT REINSTALLED FOLLOWING MAINTENANCE. SAFETY PLUG AND LOCKWIRE ALSO MISSING.Mar 17, 2000 · Beech B200C · Nacelle/Pylon, Plate/SkinSDR CA000404006Restrictor Valve · sheared(CAN) RESTRICTOR VALVE SHEARED OFF FROM THE LEFT MAIN LANDING GEAR RETRACT/EXTEND ACTUATOR (UP LINE) CAUSING HYDRAULIC FLUID TO BE LOST DURING FLIGHT. RESTRICTOR VALVE REPLACED.Mar 15, 2000 · Beech 200BEECH · Landing Gear ActuatorSDR AU000174Circuit Breaker · corroded(AUS) CIRCUIT BREAKER PANEL CORRODED DUE TO WATER INGRESS THROUGH THE COPILOT''S DV WINDOW.Feb 29, 2000 · Beech 200BEECH · DC Power Distribution SystemSDR CA000404005Fire Detector · shorted(CAN) THE CREW REPORTED THAT DURING FLIGHT THE LEFT ENGINE FIRE WARNING CAME ON INTERMITTENTLY. THE LIGHT INDICATION OCCURS ONLY AFTER PRECIPITATION OR AIRCRAFT WASHING. FOUND FIRE DETECTOR TRIGGER VOLTAGE LEAKING THROUGH WIRE INSULATION WHEN IT IS WET.Feb 29, 2000 · Beech B200C · Fire DetectionSDR CA000307005Door Frame · cracked(CAN) DOOR WAS REMOVED FOR MAIN HINGE REPLACEMENT AND UPON FURTHER DISASSEMBLY THE FOLLOWING PARTS WERE FOUND CRACKED: MAIN REAR DOOR MEMBER (P/N 50-430043-373; INTERCOSTALS (P/N 50-430043-1291 AND 101-43178-1); UPPER STRUCTURAL MEMBER (P/N 50-430043-1273).Feb 24, 2000 · Beech 200BEECH · Entrance StairsSDR CA000307020Windshield · failed(CAN) DURING CRUISE, THE COPILOTS WINDSCREEN SHATTERED. WINDSCREEN REPLACED.Feb 21, 2000 · Beech 200BEECH · Flight Compartment WindowsSDR CA000218008Switch · damaged(CAN) RUDDER BOOST SYSTEM - INOPERATIVE ON RIGHT SIDE.Feb 8, 2000 · Beech 200BEECH · Flight Control SystemSDR CA000330003Motor · weak(CAN) DURING CLIMB WHEN THE GEAR WAS SELECTED UP, THE GEAR RETRACTED ONLY HALF WAY AND THE GEAR HANDLE RED LIGHT REMAINED ILLUMINATED. THE GEAR WAS LEFT IN ITS PARTIALLY RETRACTED POSITION. WHEN ON APPROACH AND THE GEAR SELECTED TO EXTEND, THE GEAR WOULD NOTJan 31, 2000 · Beech 200BEECH · Landing Gear ActuatorSDR AU000128016Switch · failed(AU) PILOTS REPORTED THAT THE NOSE LANDING GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN ON 2 OCCASSIONS. NOSE GEAR DOWNLOCK MICROSWITCH WAS REPLACED.Jan 28, 2000 · Beech 200BEECH · Landing Gear Door ActuatorSDR CA000128016Switch · failed(CAN) PILOTS REPORTED THAT THE NOSE LANDING GEAR DOWN & LOCKED LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN ON 2 OCCASSIONS. NOSEGEAR DOWNLOCK MICROSWITCH WAS REPLACED.Jan 28, 2000 · Beech 200BEECH · Landing Gear Position and WarningSDR CA000218001Bearing · broken(CAN) OUTER WHEEL HALF BEARING WAS FOUND LOOSE. THIS ALLOWED WHEEL TO MOVE AND LOCK BRAKE DISC IN CALIPERS. IT APPEARS THAT THE OUTER BEARING SEIZED OR JAMMED AND THE OUTER RACE SPUN IN THE ALUMINIUM WHEEL HALF WEARING THE WHEEL HALF AND DEFORMING IT. GREASJan 17, 2000 · Piper PA42 · Wheel/Ski/FloatSDR CA000120017Windshield · failed(CAN) WHILE CRUISING AT 27,000 FT. THE RT WINDSHIELD INNER PANE SUDDENLY SHATTERED INTO A LATTICE LIKE PATTERN OF NUMEROUS CRACKS.Jan 12, 2000 · Beech 200BEECH · Flight Compartment WindowsSDR CA991229059Valve · worn(CAN) BLEED AIR DETECT LIGHT CAME ON. DUCT UNDER CABIN FLOOR FOUND WITH HOLES WORN IN SIDE WALL DUE TO INTERNAL CHAFING OF CHECK VALVE.Dec 7, 1999 · Beech 200BEECH · Air Distribution SystemSDR CA991229058Drain Valve · missing(CAN) ON APPROACH THE RT ENGINE LOST PARTIAL POWER AND THEN FLAMED OUT COMPLETELY. PILOT NOTICED FLUCTUATING FUEL FLOW AND SELECTED STANDBY PUMP ON. AT THIS POINT THE PILOT NOTICED MINIMUM FUEL IN RT MAINTANK.INSPECTION FOUNDTHAT THE VALVE ASSEMBLY IS SWAGED Dec 4, 1999 · Beech 200BEECH · Aircraft Fuel Filter/Strainer
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