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 AU981015Bearing · failed(AUS) LEFT ENGINE NR 4 BEARING CAGE FAILED. METAL CONTAMINATION OF OIL SYSTEM.May 21, 1998 · Beech B200C · Turbine SectionSDR 98ZZZX2190Fuel Pump · failedDURING CRUISE FLIGHT, THE RT ENGINE FLAMED OUT AND WOULD NOT RESTART IN-FLIGHT. AFTER A SAFE LANDING, THE ENGINE STARTED NORMALLY. HOWEVER, WHEN POWERED UP TO 100 PERCENT, THE ENGINE WOULD IMMEDIATELY FLAME OUT. INSPECTION REVEALED THE HIGH PRESSURE, ENGINEApr 28, 1998 · N430MC · Beech 200BEECH · Engine Fuel PumpSDR AU980751Windshield · cracked(AUS) PILOT'S WINDSCREEN OUTER PLY CRACKED. PART TOTAL CYCLES: 1,967.Apr 23, 1998 · Beech B200C · Flight Compartment WindowsSDR AU980157Brake Disc · worn(AUS) RH OUTBOARD BRAKE ROTOR CRACKED. RH OUTBOARD WHEEL CRACKED AT BRAKE DRIVE LUG.Feb 2, 1998 · Beech B200C · BrakeSDR AU980043Wire · broken(AUS) LH MAIN LANDING GEAR DOWNLOCK SWITCH WIRE BROKEN.Jan 1, 1998 · Beech 200BEECH · Landing Gear System WiringSDR AU971653Switch · mis installed(AUS) LH AND RH BLEED AIR SENSE LINES TRANSPOSED. LH LINE CONNECTED TO RH SWITCH AND VICE VERSA. A HOLE IN THE RH SENSE LINE ACTIVATED THE LH BLEED AIR WARNING. SEE MDR 97/1609 FOR MORE INFORMATION.Dec 25, 1997 · Beech 200BEECH · Bleed Air Indicating SystemSDR AU971609Switch · mis wired(AUS) LH BLEED AIR WARNING SWITCH PRESSURE LINE TRANSPOSED WITH RH SWITCH. RH BLEED AIR SENSE LINE CONTAINED A SMALL HOLE WHICH HAD ACTIVATED THE (INCORRECT) WARNING LIGHT. PERSONNEL/MAINTENANCE ERROR.Dec 15, 1997 · Beech 200BEECH · Bleed Air Indicating SystemSDR AU971563Hose · failed(AUS) OXYGEN SYSTEM ON/OFF CONTROL CABLE FAILED. OXYGEN SYSTEM REMAINED ON FOR AN EXTENDED TIME CAUSING THE SUPPLY HOSE TO THE CASUALTY OXYGEN MASK TO RUPTURE AND ALLOWING THE OXYGEN SYSTEM TO DISCHARGE TO 0PSI.Dec 3, 1997 · Beech B200C · Passenger Oxygen SystemSDR AU971528Diode · shorted(AUS) FIRE AUDIO BOX DIODE SHORT CIRCUITED.Dec 2, 1997 · Beech 200BEECH · Fire DetectionSDR AU971516Switch · intermittent(AUS) LANDING GEAR DOWNLOCK MICROSWITCH INTERMITTENT OPERATION.Nov 13, 1997 · Beech B200C · Landing Gear Position and WarningSDR AU971515Windshield · bird strike(AUS) BIRDSTRIKE ON RH WINDSCREEN. NIL DAMAGE.Nov 8, 1997 · Beech B200C · Flight Compartment WindowsSDR AU971439Blade · fod(AUS) LH PROPELLER BLADE TIP BENT. BLOOD ON THE BLADE LEADS TO THE ASSUMPTION OF AND ANIMAL STRIKE.Oct 21, 1997 · Beech B200C · Propeller Blade SectionSDR AU970834Trim System · malfunction(AUS) ELEVATOR TRIM FAULTY - MAINTENANCE CHECKS COULD FIND NO FAULTSWITH THE TRIM SYSTEM - SUSPECT CAUSED BY ICINGJun 26, 1997 · Beech B200C · Elevator Tab Control SystemSDR AU970833Rudder System · malfunction(AUS) RUDDER BOOST SYSTEM FAULTY - MAINTENANCE CHECKS OF SYSTEM COULD FIND NO FAULTSJun 12, 1997 · Beech B200C · Rudder Control SystemSDR AU970666Landing Gear · faulty(AUS) LANDING GEAR EXTENSION SYSTEM FAULTY - UNABLE TO MOVE EMERGENCY EXTENSION LEVER - LANDING GEAR 60AMP CIRCUIT BREAKER POPPED - CIRCUIT BREAKER RESET, EMERGENCY SYSTEM DISENGAGED AND LANDING GEAR EXTENDED NORMALLY - INSPECTION COULD FIND NO APPARENT DEFECTMay 31, 1997 · Beech B200C · Landing Gear Retraction/Extension SystemSDR AU970387Motor · shorted(AUS) HYDRAULIC POWER PACK ELECTRIC MOTOR COMMUTATOR SHORT CIRCUITEDApr 9, 1997 · Beech 200BEECH · Hydraulic Pump (Electric/Engine), MainSDR CA970528029Windshield · cracked(CAN) WHILE CLIMBING THROUGH 15,000 FEET THE RIGHT HAND WINDSHIELD WAS SEEN TO CRACK AND DELAMINATE OVER A 2 X 3 SQUARE INCH AREA. THE FAILURE OCCURRED IN THE LOWER LEFT HAND CORNER OF THE WINDSHIELD, ADJACENT TO THE WINDSHIELD HEAT INPUT TERMINAL.Mar 20, 1997 · Beech B200 · Flight Compartment WindowsSDR CA970401009Windshield · failed(CAN) AIRCRAFT HAD CLIMBED TO FL 230 WITH THE WINDSHIELD HEAT ON. SHORTLY AFTER THE HEAT WAS TURNED OFF A LOUD BANG WAS HEARD AND THE LT WINDSHIELD SHATTERED INTO A RIVER OF LATTICE-LIKE CRACKS ON THE INNER LAMINATIONS. WINDSHIELD HAD BEEN INSTALLED 18 MONTMar 20, 1997 · Beech B200 · Flight Compartment WindowsSDR AU970370Clip · cracked(AUS) CLIPS ATTACHING CHANNEL TO STRINGERS AT REAR PRESSURE BULKHEAD CRACKED ON LH SIDE - CLIP PNO 8050-30, PNO 8050-31, PNO 8050-32,PNO 8050-33 AND PN0 8050-36Mar 15, 1997 · Beech B200C · Fuselage Miscellaneous StructureSDR CA970319002Actuator · failed(CAN) THE PILOT SELECTED GEAR UP. THE NOSE GEAR UNLOCKED BUT DID NOT GO UP. THE MAINS REMAINED DOWN AND LOCKED. THIS AIRCRAFT HAD THE AVIA DESIGN LANDING GEAR STC SA4378WP ALTHOUGH THE MOTOR IS AN ORIGINAL BEECH PART NUMBER.Mar 7, 1997 · Beech B200C · Landing Gear ActuatorSDR AU970192Hose · contaminated(AUS) RH AIRCONDITION SYSTEM ENGINE DRIVEN FREON COMPRESSOR SUCTION AND PRESSURE HOSES CONTAMINATED WITH RUBBER PARTICLES - SUSPECT DEBRIS FROM INCORRECT MANUFACTURING TECHNIQUE - FORWARD AND REAR EVAPORATOR TRANSFER VALVES ALSO CONTAMINATEDMar 5, 1997 · Beech 200BEECH · Cabin Compressor SystemSDR CA970318005Fuel Contrl Unit · faulty(CAN) ENGINE TORQUE AND TEMPERATURE CONTINUED TO INCREASE AS THROTTLE WAS RETARDED. PILOT SELECTED THROTTLE TO OFF POSITION, TEMPERATURE STILL INCREASED. ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION FOUND FUEL CONTROL UNIT FAULTY. FCU WAS REPLACED.Mar 3, 1997 · Piper PA42 · Fuel Control/Reciprocating EnginesSDR AU970198Flap · damaged(AUS) LH OUTBOARD WING FLAP DAMAGED - SPAR BENT AND SKIN CREASED -INVESTIGATION FOUND A DEAD HARE ON THE RUNWAYFeb 26, 1997 · Beech B200C · Trailing Edge FlapsSDR CA970228007Hp Bleed Valve · faulty(CAN) ON DESCENT THERE WERE TWO LOUD BANGS FROM #1 ENGINE AND A FLASH OF FLAME FROM THE ENGINE EXHAUST DUCT. AFTER FIVE SECONDS THIS EVENT REPEATED ITSELF. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS CARRIED OUT. POST FLIGHT INVESTIGATION FOUND THEFeb 19, 1997 · Beech B200C · Compressor Bleed ValveSDR AU970128Windshield · cracked(AUS) CO-PILOTS WINDSHIELD OUTER LAMINATION CRACKED IN TOP RH CORNER -WINDSHIELD WAS DELAMINATING PRIOR TO CRACKING (THE DELAMINATION WAS WITHIN MANUFACTURERS LIMITS)Feb 5, 1997 · Beech B200C · Flight Compartment WindowsSDR AU970122Brake Disc · failed(AUS) RH OUTBOARD BRAKE DISC BROKEN - BROKEN PIECE OF DISC DAMAGED WHEEL ASSEMBLY AND BRAKE BACKPLATE - WHEEL JAMMEDJan 28, 1997 · Beech B200C · BrakeSDR AU970103Wire · faulty(AUS) HF INSTALLATION SUSPECT FAULTY - INSUFFICIENT PROTECTION OF 22GAWIRE CONNECTING THE LAMP TO THE 15AMP CIRCUIT BREAKER - IF THE22GA WIRE SHORT CIRCUITS TO THE AIRFRAME IT IS SUSPECTED THAT THE 15AMP CIRCUIT BREAKER WOULD NOT TRIP ALLOWING THE WIRE TO THENJan 23, 1997 · Beech 200BEECH · Communications System WiringSDR AU970121Brake Disc · failed(AUS) LH OUTBOARD BRAKE ROTATING DISC BROKEN - ONE SEGMENT CRACKED AND FELL OUT CAUSING MINOR DAMAGE TO WHEELJan 17, 1997 · Beech B200C · BrakeSDR 97ZZZX1889Idler Gear · failedPILOT REPORTED AIR COND INOP. MAINT SUSPECTED 'QUILL SHAFT' HAD SHEARED. REMOVED AND FOUND SHAFT IN SERVICEABLE CONDITION. REMOVAL OF ACCESSORY CASE FOUND IDLER GEAR HAD FAILED RESULTING IN LOSS OF DRIVE FOR AIR/COND COMP. NO REASON FOR FAILURE HAS BEEN DEJan 9, 1997 · N6606R · Beech B200 · Turbine Engine Accessory DriveSDR CA970110004Lighting Panel · shorted(CAN) WHILE IN CRUISE FLIGHT SMOKE WAS NOTED COMING FROM THE RIGHT HAND SAT/COMM AUDIO PANEL LOCATED IN THE CABIN. CIRCUIT BREAKERS PULLED AND THE PANEL WAS REPLACED AFTER A SAFE LANDING.Dec 31, 1996 · Beech B200C · Audio Integrating SystemSDR 97ZZZX864Fuel Filter · froze upPRECAUTIONARY SHUT DOWN FOR FLUCTUATING TORQUE AND WP. UPON INSPECTION, DETERMINED THE RIGHT FUEL SEDIMENT BOWL (FIREWALL FILTER) CONTAINED A SUFFICIENT AMOUNT OF ICE CRYSTALS TO RESTRICT FUEL FLOW. DISASSEMBLED, CLEANED, AND REINSTALLED FILTER ELEMENTS/ASSEDec 20, 1996 · N4277C · Beech B200 · Engine Fuel DistributionSDR CA961223006Engine · making metal(CAN) DURING FLIGHT #2 ENGINE CHIP DETECTOR ILLUMINATED. ENGINE WAS SHUTDOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. ENGINE WAS REMOVED FOR INVESTIGATION. REPORT TO FOLLOW.Dec 16, 1996 · Beech B200C · Engine (Turbine/Turboprop)SDR CA961218005Switch · failed(CAN) THIS AIRCRAFT'S ELECTRICAL LANDING GEAR SYSTEM HAD BEEN REPLACED WITH A HYDRAULIC SYSTEM. THE NOSE GEAR GREEN LIGHT DID NOT COME ON WHEN THE GEAR WAS DOWN AND LOCKED. THUS, THE PILOT HAD TO DO SEVERAL GEAR CYCLES AND A FLY-BY. HE LANDED OK. THE NOSE Nov 26, 1996 · Beech B200C · Landing Gear Position and WarningSDR CA961016007Exhaust Stack · cracked(CAN) EXHAUST STACK FOUND CRACKED ALONG THE OUTBOARD WELD SEAM, APPROXIMATELY 5, 1/4" LONG. THIS STACK HAD BEEN REPLACED IN MAY 1995.Sep 18, 1996 · Beech B200 · Engine Collector/Tailpipe/NozzleSDR AU961168Compressor Blade · fod(AUS) RH ENGINE COMPRESSOR FIRST STAGE BLADES DAMAGED BY FOD - AIRCRAFTHAD PREVIOUSLY OPERATED FROM GRAVEL STRIPSAug 13, 1996 · Beech B200C · Turbine Engine Compressor SectionSDR AU961187Skin · delaminated(AUS) WING SKIN DELAMINATED - FOUND DURING INSPECTION IAW AD/BEECH200/43 AMDT5 (BEECH SB 2040 REV 3)May 23, 1996 · Beech 200BEECH · Wing, Plate/SkinSDR AU960591Fire Detector · contam-water(AUS) RH ENGINE FIRE DETECTOR ACTIVATED DUE TO MOISTURE ON THE SENSORS - FIRE BOTTLE DISCHARGEDMay 9, 1996 · Beech 200BEECH · Fire DetectionSDR AU960625Switch · failed(AUS) LH MAIN LANDING GEAR DOWNLOCK MICROSWITCH INTERNAL FAILUREMay 2, 1996 · Beech B200C · Landing Gear Position and WarningSDR AU960328Valve · faulty(AUS) PRESSURISATION SYSTEM LH FLOW PACK LOW ON FLOW - RH FLOW PACK SOLENOID STICKING CAUSING INTERMITTENT OPERATION - BLEED AIR DUCTFAIL LIGHT WIRE LOOSEMar 5, 1996 · Beech 200BEECH · Air Distribution FanSDR 97ZZZX1014Control Rod · hung upLEFT ENGINE CRUISE POWER REMAINED STEADY AFTER PILOT PULLED BACK POWER LEVER TO BEGIN DESCENT. ENGINE REACHED HIGH TORQUE LIMIT AND HAD TO BE SHUT DOWN IN-FLIGHT. MAINTENANCE INSPECTED ENGINE AND FOUND THE COTTER PIN ON THE CASTELLATED NUT RETAINING THE FCU Feb 29, 1996 · N107Z · Beech B200C · Fuel Control/Reciprocating EnginesSDR 96ZZZX1377Gearshaft · shearedPILOT REPORTED A LOW FUEL PRESSURE LIGHT FOLLOWED BY AN AUTOFEATHER ON LEFT ENGINE. PILOT SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENCE. UPON INVESTIGATION, NOTED THE OIL LEVEL LOW, THERE WAS OIL IN THE EXHAUST CASE, AND METAL PARTICLES AND FLAKES PRESENT INFeb 10, 1996 · N18260 · Turbine Engine Oil SystemSDR AU960688Ring · missing(AUS) ENGINE POWER TURBINE DISC NO3 BEARING COVER PNO 3103204-01 MOVED REARWARDS CONTACTING THE 2ND STAGE POWER TURBINE DISC RIM PNO3029313 - SUSPECT RETAINING RING PNO AS3218-173 NOT FITTED AT LAST ASSEMBLY - PERSONNEL/MAINTENANCE ERRORJan 8, 1996 · Turbine SectionSDR 96ZZZX28Bearing · spalledDURING PRE-FLIGHT WHILE TURNING RIGHT PROPELLER, HEARD AN UNUSUAL NOISE COMING FROM POWER SECTION. INSPECTED CHIP DETECTOR AND MAIN OIL SCREEN AND FOUND SMALL QUANTITIES OF METAL. REMOVED POWER SECTION FOR REPAIR. FOUND NR 4 BEARING RACE STARTING TO SPALL. Dec 13, 1995 · N887T · Beech B200 · Turbine SectionSDR CA951116025Blades · fractured(CAN)DURING CRUISE AT 13,000 FEET THE PILOT HEARD A LOUD BANG FOLLOWED BY TORQUE DROPPING TO "0". AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. POST FLIGHT INSPECTION REVEALED THE CAUSE OF THE INFLIGHT SHUTDOWN (IFSD) WAS DUE TO THE RELEASE OF 2 COMPRESSOR TURAug 27, 1995 · Turbine SectionSDR 95ZZZX5256Engine · failedENGINE FAILED DURING LEVEL CRUISE FLIGHT AT 13,000 FEET MSL. NO WARNING OR INDICATION OF A PROBLEM PRIOR TO SUDDEN POWER LOSS. SECURED ENGINE AND LANDED. CAUSE OF FAILURE IS UNKNOWN AT THIS TIME. ENGINE IS TO BE RETURNED TO MANUFACTURER FOR INSPECTION AND Aug 26, 1995 · N1PD · Beech B200 · Engine (Turbine/Turboprop)SDR 95ZZZM222Vane Ring · failedON CLIMB-OUT AT 16,000 FEET, A LOUD BANG WAS HEARD. AFTER THE LOUD BANG, THE LEFT ENGINE TEMPERATURE STARTED TO RISE AND THE ENGINE STARTED LOOSING POWER. THE ENGINE WAS THEN SHUTDOWN AND THE AIRCRAFT RETURNED FOR AN EMERGENCY LANDING WITHOUT FURTHER INCIDENMar 1, 1995 · N32SV · Beech 200BEECH · Turbine Engine Combustion Section
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