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 CA980529017Cam · broken(CAN) WHILE CARRYING OUT LANDING GEAR RETRACTION TESTS WITH THE NOSE GEAR DOORS DISCONNECTED AS PER THE MAINTENANCE MANUAL, THE CLEVIS FOR THE GEAR DOORS WAS ACCIDENTALLY ROTATED TO THE HORIZONTAL POSITION. WHEN THE LANDI NG GEAR WAS RETRACTED IT CAUGHT THE CMay 11, 1998 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR CA980519021Valve · failed(CAN) NACELLE FUEL CELL OVERPRESSURIZED DUE TO FAILURE OF CHECK VALVE CAUSING STRUCTURAL DAMAGE TO THE WHEEL WELL. CHECK VALVE REPLACED AND A/C FLOWN FOR 60 HOURS WITH NO SIGNS OF FURTHER DAMAGE.May 3, 1998 · Beech 200BEECH · Fuel StorageSDR CA980504005Valve · loose(CAN) PILOT REPORTED THE NR 1 ENGINE OIL AND TORQUE PRESSURE DROPPED TO ZERO. NR 1 ENGINE PROP RPM FROM 1900 TO 1500. N1 AND ITT WERE NORMAL. THE ENGINE WAS SHUTDOWN WITHIN MINUTES. POST- FLIGHT INSPECTION FOUND NR 1 ENGINE OIL PRESSURE RELIEF VALVE TO BE Apr 27, 1998 · Beech 200BEECH · Engine Oil PressureSDR 98ZZZX2245Pump Housing · erodedOIL WAS FOUND ON COWL. INVESTIGATION FOUND THE AFT EXTERNAL SCAVENGE PUMP HOUSING WAS LEAKING OIL. PUMP WAS DISASSEMBLED AND FOUND CAVITATION EROSION WHICH CAUSED A PIN HOLE THROUGH THE HOUSING.Apr 23, 1998 · N5UN · Beech 200BEECH · Turbine Engine Oil SystemSDR AU980424Switch · out of adjust(AUS) RIGHT MAIN LANDING GEAR `UP' POSITION MICROSWITCH OUT OF ADJUSTMENT.Apr 17, 1998 · Beech 200BEECH · Landing Gear Position and WarningSDR AU980425Switch · out of adjust(AUS) FLAP UPLIMIT MICROSWITCH OUT OF ADJUSTMENT CAUSING THE FLAP MOTOR TO FAIL.Apr 16, 1998 · Beech 200BEECH · Trailing Edge Flap Control SystemSDR CA980406049Connector · corroded(CAN) DURING ROUTINE MAINTENANCE, THE LEFT HAND (LT) WINDSHIELD HEAT DID NOT WORK. TROUBLESHOOTING OF SYSTEM REVEALED WIRES H15B8 AND H23B8 AT CANNON PLUG J195 WERE CORRODED. WIRES REPAIRED AND TESTED SERVICEABLE.Apr 2, 1998 · Beech 200BEECH · Windshield/Door Rain/Ice RemovalSDR CA971104007Piston Rod · leaking(CAN) MAIN LANDING GEAR ACTUATOR LEAKING FLUID BETWEEN PISTON ROD AND ACTUATOR HOUSING. DISASSEMBLY OF THE ACTUATOR REVEALED CORROSION ON ROD AFFECTED THE"O" RING CAUSING THE HYDRAULIC LEAK. NEW ACTUATOR INSTALLED.Mar 31, 1998 · Beech 200BEECH · Landing Gear ActuatorSDR CA980325053Valve · damaged(CAN) DURING MAINTENANCE, LEFT WING TIP FUEL CAP WAS REMOVED AND IT WAS NOTICED THE ANTI-SYPHON VALVE WAS DAMAGED. IT APPEARS THE NOZZLE FROM THE FUEL TRUCK SOME HOW TIPPED BACK, IN TURN, BENDING AND SPLITTING THE BODY OF THE ANTI-SYPHON VALVE. THE VALVE WASMar 17, 1998 · Beech 200BEECH · Fuel StorageSDR AU980289Screw · defective(AUS) FUEL PUMP SCREWS FAILED TORQUE CHECK IAW ROMEC SB 101SB018.Mar 12, 1998 · Beech 200BEECH · Engine Fuel PumpSDR CA980406046Engine · failed(CAN) DURING CLIMB, THE AIRCRAFT YAWED TO THE LEFT. THE NR 1 ENGINE OVERTEMPED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO BASE. POST-FLIGHT INSPECTION FOUND THE ENGINE HAD AN INTERNAL FAILURE RESULTING IN ENGINE PARTS EXITING THE ENGINE THROUGH TMar 7, 1998 · Beech 200BEECH · Engine (Turbine/Turboprop)SDR CA980521002Socket · failed(CAN) PILOT HEAT REPORTED AS INTERMITTENT. MAINTENANCE CHECK CONFIRMED WHEN WINDSHIELD HEAT SELECTED TO NORMAL OR HIGH, VOLTAGE DROPPED OFF TO ZERO VOLTS. FURTHER INVESTIGATION REVEALED THAT CONTACT SOCKET P/N 66259-1, 1C, IN J195 DC. POWER CONNECTOR WAS OVMar 4, 1998 · Beech 200BEECH · Windshield/Door Rain/Ice RemovalSDR AU980205Circuit Breaker · open(AUS) FLAP MOTOR CIRCUIT BREAKER INTERMITTENT OPEN CIRCUIT.Feb 16, 1998 · Beech 200BEECH · DC Power Distribution SystemSDR AU980220Gear · failed(AUS) RT ENGINE REDUCTION GEARBOX PLANETARY GEAR FAILURE. METAL CONTAMINATION OF GEARBOX. GEARBOX DECOUPLED FROM POWER TURBINE. SECOND STAGE TURBINE SHED ALL BLADES CAUSING INTERNAL DAMAGE.Feb 11, 1998 · Piper PA42 · Turbine Engine Reduction GearSDR AU980283Engine · failed(AUS) ENGINE POWER SECTION FAILED.Feb 11, 1998 · Piper PA42 · Turbine SectionSDR CA980330020Valve · malfunctioned(CAN) AFTER TAKEOFF IN MINUS 42 DEGREES CENTIGRADE AND BLOWING SNOW, THE LANDING GEAR TOOK 3 CYCLE ATTEMPTS TO RETRACT. SUBSEQUENT RETRACTIONS WERE NORMAL AS THE AIRCRAFT APPROACHED WARMER CLIMATES. BEFORE LANDING AT HOME BASE, AND GEAR EXTENSION, A NOISE SIFeb 11, 1998 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR CA980330019Bleed Valve · faulty(CAN) DURING CLIMB THE NR 1 ENGINE WAS TEMPERATURE LIMITED. THE NR 1 ENGINE POWER LEVER WAS STAGGERED 1 INCH BEHIND ITS NORMAL POSITION. FLIGHT CONTINUED AT REDUCED POWER TO NEXT AVAILABLE AIRPORT. NO FAULT FOUND ON GROUND RUN, BOTH BLEED VALVES (P/NS 3100922Feb 8, 1998 · Beech 200BEECH · Compressor Bleed ValveSDR CA980330018Intake · cracked(CAN) DURING DAILY INSPECTION, IT WAS FOUND THAT THE RAM AIR RECOVERY VANE P/N 81-3103-109 WAS LOOSE AND THE NACELLE AREA WHICH SUPPORTS THE VANE WAS CRACKED. NACELLE CRACKS WERE REPAIRED PER STANDARD REPAIR PRACTICES AND NEW VANE INSTALLED.Jan 29, 1998 · Beech 200BEECH · Nacelle/Pylon, Main FrameSDR AU980064Battery · leaking(AUS) ELT BATTERIES LEAKING. FOUND DURING BATTERY CHANGE.Jan 22, 1998 · Beech 200BEECH · Emergency Locator BeaconSDR 99ZZZX390Stator · failedRIGHT ENGINE FAILED SHORTLY AFTER TAKEOFF. LABRATORY REPORT FROM P & W CONTRIBUTED ENGINE FAILURE TO 1ST STAGE COMPRESSOR STATOR FAILURE. STATOR AIRFOIL FAILED DUE TO HIGH CYCLE FATIGUE.Jan 7, 1998 · N500PH · Beech 200BEECH · Turbine Engine Compressor SectionSDR 98ZZZX453Ct Vane Ring · crackedON 12-31-97, REPAIR STA (RUHR840H) PERFORMED AN HSI FOR IFL GROUP INC., ON ENGINE, SN 81488, REPLACING CT VANE WITH AN OVERHAULED ONE. 10.8 HOURS LATER, HAD A 40 DEGREE INCREASE IN ITT. IFL SPLIT THE ENGINE AND FOUND SOME TIP RUB AND THAT THE CT VANE HAD DEVDec 31, 1997 · N36CP · Beech 200BEECH · Turbine SectionSDR CA980113018Chain Keeper · missing(CAN) NOSE GEAR AFT CHAIN MASTER LINK MISSING AND ADJACENT LINK BENT, ONLY HELD ON BY ONE HOLE. REPAIRED/REPLACED.Dec 22, 1997 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR AU971578Tachometer · defective(AUS) DURING AN INSPECTION OF A TURBINE TACHOMETER PRIOR TO TESTING,THE FRONT LENS WAS FOUND TO SHOW EVIDENCE OF MOISTURE CONTAMINATION (FOGGING). FURTHER INVESTIGATION FOUND THAT THE CASE HAD BEEN SEALED WITH RTV TYPE SEALANT AND NOT HERMETICALLY SOLDER SEALEDec 18, 1997 · Beech 200BEECH · Engine RPM Indicating SystemSDR AU971614Tach Generator · failed(AUS) RH ENGINE N1 TACH GENERATOR DRIVE SHAFT SHEAREDDec 18, 1997 · Beech 200BEECH · Engine RPM Indicating SystemSDR AU971573Transmitter · failed(AUS) DURING FLIGHT THE LT ENGINE FUEL FLOW GAUGE REDUCED INDICATION FROM 550 PPH TO 100 PPH AND DIDN'T ALTER WITH POWER CHANGES. GROUND INVESTIGATION FOUND THE LT FUEL TRANSMITTER WAS FAULTY.Dec 15, 1997 · Beech 200BEECH · Fuel Flow SensorSDR 98ZZZX1372Filter Housing · crackedPILOT NOTICED OIL PRESSURE DROPPED AFTER 1:30 HOURS INTO FILIGHT. FOUND OIL FILTER HOUSING CRACKED.Dec 14, 1997 · N90PB · Beech 200BEECH · Turbine Engine Oil SystemSDR AU971513Spring · faulty(AUS) RUDDER BOOST CABLE TENSION SPRING STRETCHED. INCORRECT TENSION ON THE CABLE ALLOWED THE RUDDER BOOST ACTUATOR ARM TO JAM UNDER THE LIP OF THE BULKHEAD. THE BULKHEAD WAS ALSO DAMAGED.Nov 26, 1997 · Beech 200BEECH · Rudder Control SystemSDR CA971015062Engine · failed(CAN) DURING CLIMB OUT THE PILOT SAW FLAMES PULSING FROM NR2 ENGINE, ALL ENGINE PARAMETERS WERE NORMAL. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT BORESCOPE INSPECTION FOUND NO ABNORMALITIES. FUEL NOZZELS AND THE OIL FILTERS Oct 3, 1997 · Beech 200BEECH · Engine (Turbine/Turboprop)SDR AU971550Bearing · seized(AUS) AIRCONDITIONER BELT SNAPPED. INVESTIGATION FOUND THAT THE AIRCONDITIONING COMPRESSOR WAS TIGHT TO TURN AND BINDING. THE ASSEMBLY WAS STRIPPED AND ONE THRUST BEARING WAS FOUND WELDED AND SEIZED.Sep 24, 1997 · Beech 200BEECH · Cabin Compressor SystemSDR CA970909003Connector · failed(CAN) DURING TROUBLESHOOTING A FAULTY RADAR, IT WAS FOUND THAT THE FORWARD PRESSURE BULKHEAD CONNECTOR HAD HEATED AND MELTED THE CONNECTOR MATERIAL (PLASTIC) THEREBY ALLOWING SOME CONNECTOR PINS TO MAKE CONTACT AND CAUSE A SHORT.Aug 24, 1997 · Beech 200BEECH · Electrical Power SystemSDR 97ZZZX3995Coupling Shaft · shearedRIGHT HAND ENGINE SHUT DOWN IN-FLIGHT DURING DESCENT INTO 1B1 AS A RESULT OF A SHEARED DRIVE SHAFT (ACCESSORY GEARBOX).Jul 22, 1997 · N689BV · Beech 200BEECH · Turbine Engine Accessory DriveSDR CA970715015Windshield · cracked(CAN) THE LEFT HAND WINDSHIELD OUTER LAMINATION CRACKED IN CRUISE FLIGHT. AIRCRAFT RETURNED TO BASE. NO CAUSE OF CRACKING ESTABLISHED.Jul 2, 1997 · Beech 200BEECH · Flight Compartment WindowsSDR CA970916003Planetary Gear · separated(CAN) DURING FLIGHT A CHIP DETECTOR LIGHT CAME ON NR2 ENGINE. THE ENGINE WAS SHUTDOWN AND THE FLIGHT CONTINUED TO DESTINATION. POST FLIGHT INSPECTION FOUND METAL IN THE OIL FILTER. THE ENGINE WAS SENT FOR INVESTIGATION AND DISASSEMBLY OF THE REDUCTION GEARBOX Jun 29, 1997 · Beech 200BEECH · Turbine Engine Reduction GearSDR CA970710002Exhaust Stack · cracked(CAN) LEFT HAND EXHAUST STACK WAS FOUND CRACKED AT THE WELD BETWEEN THE DEICE TUBE AND THE MAIN BODY OF THE STACK. SUBMITTER RECOMMENDS INSPECTING THIS AREA.Jun 26, 1997 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR 97ZZZX2905Clamp · missingFUEL FLOW TRANSMITTER IS MOUNTED TO ENGINE WITH 2 STAINLESS LINES PN 3032010 AND PN 3026779 B1; AND, IF SUPPORT CLAMP PN 30006614 IS NOT INSTALLED, LINES WILL CRACK AT WELDS CREATING A HEAVY FUEL LEAKING ENGINE COMPARTMENT AND ONTO WING.Jun 8, 1997 · N242RA · Piper PA42 · Fuel Flow SensorSDR AU970694Bearing · failed(AUS) RH ENGINE FUEL CONTROL UNIT (FCU) FAULTY - BEARING FAILED - FCU TO FUEL PUMP DRIVE COUPLING SHEAREDJun 3, 1997 · Beech 200BEECH · Fuel Control/Reciprocating EnginesSDR AU970552Battery · failed(AUS) MAIN BATTERY LOW VOLTAGEMay 22, 1997 · Beech 200BEECH · Battery/Charger SystemSDR CA970527006Uplock Switch · malfunctioned(CAN) PILOTS REPORTED THE LANDING GEAR HANDLE LIGHTS REMAIN ON IN THE UP POSITION. INVESTIGATION FOUND A DEFECTIVE RIGHT LANDING GEAR UPLOCK SWITCH. A CONTINUITY CHECK FOUND HIGH RESISTANCE. SWITCH REPLACED.May 21, 1997 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR AU970503Fire Detector · faulty(AUS) RH ENGINE FIRE WARNING SYSTEM FIRE DETECTOR FAULTY - SUSPECT MOISTURE INGRESS AS RAIN FELL DURING THE PREVIOUS NIGHTMay 19, 1997 · Beech 200BEECH · Fire DetectionSDR AU971458Transceiver · faulty(AUS) HF RADIO SCRATCHY AND WEAK ON TRANSMIT.May 1, 1997 · Beech 200BEECH · HF Communications SystemSDR CA970513024Connector · corroded(CAN) AFTER TAKEOFF, THE PILOTS SELECTED GEAR UP, BUT THE LANDING GEAR WOULD NOT CYCLE UP, TWO MORE SELECTIONS, BUT THE GEAR WOULD NOT CYCLE UP AND THE HYD PUMP RED LIGHT WOULD NOT COME ON. STILL HAD THREE GREEN GEAR SAFE LIGHTS. FLY-BY TOWER CONFIRMED GEAR Apr 28, 1997 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR HAIHEEA9582Engine · noisyENGINE MAKING NOISE. TIME SINCE REPAIR 0:00.Apr 24, 1997 · Engine (Turbine/Turboprop)SDR CA970505001Transducer · failed(CAN) DURING CRUISE FLIGHT THE PILOT NOTICED THE #1 ENGINE OIL PRESSURE READING ZERO, NO CAUTION LIGHT ILLUMINATION AND ALL OTHER PARAMETERS READING NORMAL. AIRCRAFT RETURNED TO BASE. POST FLIGHT INVESTIGATION FOUND THE OIL PRESSURE TRANSDUCER TO BE FAULTY. THApr 17, 1997 · Beech B200 · Engine Oil PressureSDR 97ZZZX1745Pump · shaft failedENGINE WENT TO IDLE CUT OFF IN-FLIGHT. (FLAME OUT.) MAIN ENGINE PUMP SEIZED. ENGINE SHAFT BECAME WORN AND ROUNDED OFF SPLINES.Apr 8, 1997 · N942CE · Beech B200 · Engine Fuel PumpSDR CA970408007Bleed Air Detect · failed(CAN) DURING CLIMBOUT THE BLEED AIR DETECT ANNUNCIATOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BASE. MAINTENANCE FOUND A PREVIOUS REPAIR HAD FAILED. THE TUBING WAS REPAIRED IN ACCORDANCE WITH THE MANUFACTURER'S RECOMMENDATIONS AND THE AIRCRAFT RETURNED TO Mar 26, 1997 · Beech 200BEECH · Bleed Air Indicating SystemSDR CA970523004Selector Valve · failed(CAN) GEAR WOULD NOT DROP WHEN SELECTED. GEAR DROPPED WITH EMERGENCY PROCEDURE. WITH AIRCRAFT ON JACKS, THE GEAR WOULD CYCLE UP, BUT HYDRAULIC PRESSURE HAD TO BE RELEASED MANUALLY TO GET THE GEAR TO DROP. POWER WAS FOUND GOING INTO THE VALVE BUT WAS NOT SHIFMar 11, 1997 · Beech 200BEECH · Landing Gear SelectorSDR 97ZZZX1328Pump · seizedLEFT ENGINE ROLLED BACK TO IDLE CUT-OFF IN FLIGHT. (FLAME OUT.) MAIN ENGINE FUEL PUMP SEIZED CAUSING ROUNDING OFF OF SPLINE ON PUMP AND DRIVE COUPLING. SUBMITTER SUGGESTED TO INCREASE FREQUENCY OF INSPECTION FOR THIS COMPONENT.Mar 10, 1997 · N942CE · Beech 200BEECH · Engine Fuel PumpSDR AU970210Detector · faulty(AUS) RH ENGINE FIRE DETECTORS (3OFF) FAULTY - DETECTOR AMPLIFIER ALSO REPLACEDMar 5, 1997 · Beech 200BEECH · Fire DetectionSDR AU970216Windshield · cracked(AUS) PILOTS WINDSHIELD CRACKED IN SEVERAL PLACES - WINDSHIELD HEAT WAS OPERATING AT THE TIMEMar 5, 1997 · Beech 200BEECH · Flight Compartment WindowsSDR AU970161Battery · malfunction(AUS) BATTERY CHARGE LIGHT ILLUMINATED - BATTERY REMOVED TO BATTERY SHOP - INVESTIGATION COULD FIND NO FAULTS WITH THE BATTERYFeb 19, 1997 · Beech 200BEECH · Battery/Charger System
Back to U/A Canada PT6A-41