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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2007FA0000431Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.THE EXHAUST DUCT SB 3380 HAD NOT BEEN COMPLIED WITH.POWER SECTION WAS REMOVED FOR REPAIR.SDR CA050531007Windshield · cracked(CAN) DURING A/C CLIMB THROUGH 10,000, RT WINDSHIELD OUTERPANE CRACKED ACROSS ENTIRE WINDOW, (WINDSHIELD HEAT ON). NO OTHER PROBLEMS OCCURED (DEPRESSURIZATION ETC) AIRCRAFT RETURNED TO BASE AND COMPLETED A NORMAL LANDING. MAINTENANCE CHANGED WINDOW AND A/CSDR CA050607007Exhaust Duct · cracked(CAN) WHILE CONDUCTING A PHASE 4 INSPECTION, THE EXHAUST STACKS WERE REMOVED FROM THE RT ENGINE. A VISUAL INSPECTION HAD INDICATED A CRACKED EXHAUST DUCT. POWER SECTION WAS REMOVED FOR INVESTIGATION AND REPAIRS. THE EXHAUST DUCT HAD CRACKING IN THE AFT END OF SDR CA050517008Potentiometer · failed(CAN) DURING LANDING PHASE OF FLT, MLG SELECTED DOWN & 3 GREEN LIGHTS DID NOT APPEAR TO BE ON. AFTER ALL PROPER PROCEDURES, ACFT LANDED WITHOUT FURTHER INCIDENT. ONCE GENERATORS SELECTED OFF LINE, GREEN LIGHT ILLUMINATED. BEING A LATER S/N AIRCRAFT THESE LIGHTSDR 2007FA0000422Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.POWER SECTION WAS REMOVED FOR REPAIR.SDR CA050517007Arm · wornAFTER AN UNEVENTFUL FLT, CREW UNABLE TO GET THE RT ENGINE TO DROP BELOW 78 PERCENT NG AND IT HAD INSUFFICIENT REVERSE. MAINTENANCE INVESTIGATED AND FOUND THAT THE PIVOT ARM (50-944076-3) ON THE CAM CLUSTER HAD WORN ALLOWING IT TO SLIP ON THE CAM, CHANGING THESDR CA050510005Bracket · torn(CAN) ON TUESDAY, APRIL 26, 2005 THIS AIRCRAFT SUFFERED A RIGHT HAND OUTBOARD FLAP FAILURE WHILE APPROACHING CYWG. THE CREW WERE ABLE TO MAINTAIN CONTROL OF THE AIRCRAFT AND LANDED WITHOUT FURTHER INCIDENT.ON EXIT FROM THE AIRCRAFT, THE CREW OBSERVED NR 1, 2 ASDR 2007FA0000438Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.THE EXHAUST HAD NOT HED SB 3380 COMPLIED WITH.POWER SECTION WAS REMOVED FOR REPAIR.SDR 2007FA0000408Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.POWER SECTION WAS REMOVED FOR REPAIR.SDR CA050302002Heater · failed(CAN) ELECT SMELL/SMOKE WAS CAUSED BY FAILED GROUND POINT FOR WINDSHIELD HEAT ON LT WINDSHIELD. CREW FOLLOWED EMERG CKLIST, WHICH CALLS FOR TURNING OFF ELEC PWR. THIS AC HAS HYDR LANDING GEAR RETRACT SYS INSTALLED (STC), ELECTRICALLY DRIVEN HYDR PUMP PROVIDESSDR CA050221004Valve · missing(CAN) PILOT REPORTED RAPID FUEL LOSS IN FLIGHT. INNER ASSY OF FUEL QUICK DRAIN FOUND TO BE MISSING FROM RT NACELLE FUEL FILTER QUICK DRAIN ASSY. FUEL VALVE IS COMPRIZED OF 2 MAIN PARTS. MAIN HOUSING, AND DRAIN ASSY. MOVEABLE PART OF DRAIN IS INSTALLED IN SDR G1I2005F00000Landing Gear · malfunctionedDURING TRAINING FLIGHT, THE LANDING GEAR WOULD NOT EXTEND NOR THE HANDLE LIGHT ILLUMINATE WHEN GEAR DOWN WAS SELECTED. GEAR WAS EXTENDED MANUALLY AND THE AIRCRAFT MADE A NORMAL LANDING. THIS CONDITION WAS ENCOUNTERED AFTER REPEATED GEAR EXTENSION/ RETRACTIONSDR CA050112004Tube · chafed(CAN) UPON INSPECTION OF THE FUEL TRANSFER PRESSURE SWITCH, IT WAS NOTICED THAT ONE OF THE ENGINE CONTROLS WAS RUBBING AGAINST THE MAIN FEED LINE TO THE RT NAC TANK. REPLACED TUBE ASSY AND TIED BACK TELEFLEX CABLES TO PREVENT FURTHER RUBBING.SDR K5L2005F00000Uplock Switch · failedON TAKEOFF, RETRACTED GEAR AND IN TURBULENCE, GEAR HANDLE LIGHTS FLICKERED ON AND OFF. PULLED BACK ON YOKE AND LIGHTS STAY ON, PUSH FWD AND LIGHTS GO OFF. REMOVED GEAR UP LIMIT SWITCH AND FOUND IT WAS GOING OFF BEHIND AUDIAL CLICK OFF SWITCH. REPLACED SWITCSDR CA050110008Engine · failed(CAN) AFTER TAKE-OFF, THE NR 1 ENGINE REPORTEDLY LOST POWER. THE AIRCRAFT SETTLED TO THE GROUND, DEPARTED THE RUNWAY AND WAS CONSUMED BY FIRE. PWC WILL INVESTIGATED THE ENGINE AND WILL SUPPLIMENT THIS REPORT TO PROVIDE ROOT CAUSE, AS AND WHEN DETERMINED.SDR CA041213002Master Link · disconnected(CAN) WHEN THE FLT CREW EXTENDED LANDING GEAR FOR LANDING , THEY HEARD STRANGE SOUNDS AND THEY ONLY RECIEVED TWO MAIN LANDING GEAR LIGHTS. THE NOSE GEAR LIGHT WAS NOT GREEN AND THEY HAD A RED LIGHT ON IN THE HANDLE. THEY LOOKED IN THE NACELLE MIRROR AND WERE ASDR CA041206008Spar · cracked(CAN) DURING LANDING PHASE AIRCRAFT ROLLED TO LT WHEN APPROACH FLAPS WERE SELECTED. ROLL RESPONSE WAS CORRECTED WITH AILERON TRIM INPUT. FURTHER FLAP DEPLOYMENT DID NOT CREATE ANY FURTHER CONTROL DIFFICULTY. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED THAT SDR CA041112004Pump · failed(CAN) ON TAKE OFF, GEAR WOULD NOT RETRACT. NOSE GEAR GREE LIGHT WENT OUT, AND RED INTRANSIT LIGHT REMAINED ON. GEAR WOULD NOT RETRACT OR EXTEND.PRIOR TO LANDING THE BACKUP EXTENSION SYSTEM WAS USED, AND ALLGEAR INDICATIONS WERE THAT THE GEAR WAS DOWN AND LOCKESDR CA041107001Switch · intermittent(CAN) AFTER TAKE-OFF THE CABIN DOOR WARNING LIGHT ILLUMINATED, WITH THE DOOR REMAININGIN THE CLOSED POSITION. THE AIRCRAFT RETURNED TO BASE FOR LANDING WITHOUT INCID ENT. UPON LANDING AND TAXI TO THE RAMP THE CREW CONFIRMED THAT THE DOOR WAS INDEED IN THE CLOSSDR CA041022001Retaining Ring · missing(CAN) AIRCRAFT WAS ON APPROACH AND SELECTED LANDING GEAR DOWN. LANDING GEAR FAILED TO EXTEND. THE FLIGHT CREW THEN SELECTED THE EMERGENCY LANDING GEAR EXTENSION SYSTEM. THE LANDING GEAR LOCKED DOWN AND THE AIRCRAFT LANDED SAFELY. UPON INSPECTION OF THE LANSDR CA041021005Indicator · failed(CAN) AFTER START-UP AND SELECTION OF THE AVIONICS MASTER ON, THE CREW NOTED THAT THE INSIDE OF THE FLIGHT DIRECTOR INDICATOR, BEHIND THE GLASS FACE, APPEARED TO HAVE SMOKE INSIDE OF THE INSTRUMENT. THE AVIONICS MASTER WAS SELECTED TO OFF AND THE ENGINES SHUT SDR CA041001013Fitting · chafed(CAN) DURING THE WING BOLT INSPECTION, THE LT LOWER AFT BATHTUB FITTING WAS FOUND TO HAVE CHAFE MARK FROM CONTACT WITH THE CLIP ON THE WING FITTING COVER. ONE MARK EXTENDED INTO THE FITTING RADIUS. MFG WAS CONSULTED AND SENT OUT A FIELD REPAIR TO REMOVE THE DASDR CA040927002Cross Tie · cracked(CAN) DURING MAINTENANCE, A CRACK WAS DISCOVERED IN A FUSELAGE CROSS TIE FOR THE UPPER RT FUSELAGE, IMMEDIATELY AFT OF THE EMERGENCY EXIT WINDOW. NEW PART HAS BEEN ORDERED AND WILL BE INSTALLED TO RECTIFY THIS DEFECT.SDR CA040921008Windshield · broken(CAN) IN FLIGHT WINDSHIELD INNER PANE SHATTERED, PLANE RETURNED TO BASE.SDR CA040901009Motor · failed(CAN) SHORTLY AFTER AIRCRAFT DEPARTURE, THE AIRCRAFT RETURNED DUE TO FLAP PROBLEMS. THE FLAP MOTOR WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 2004FA0000738Turbine · shiftedNEW STYLE PN SEGMENT INSTALLED AT HSI 258 HOURS PRIOR. THIS NEW STYLE SEGMENT SHIFTS AFT RESULTING IN HOT SECTION FAILURE. VERY COMMON WITH THIS PN SEGMENT, MFG NEEDS TO CHANGE DESIGN.SDR 2004FA0000889Turbine · shiftedNEW STYLE, PN SEGMENT INSTALLED AT HSI 258 HRS PRIOR. THIS NEW STYLE SEGMENT SHIFTS AFT RESULTING IN HOT SECTION FAILURE. VERY COMMON WITH THIS PN SEGMENT 3053094/ MFG NEEDS TO CHANGE DESIGN.SDR CA040902011Windshield · cracked(CAN) ON DECENT, THE CREW NOTICED A CRACK IN THE PILOTS WINDSHIELD. THE CREW CONTINUEDAND LANDED NORMALLY.SDR CA040902010Bearing · failedWHEN MLG EXTENDED ON ARRIVAL, GEAR CAME OUT OF WW & STOPPED. CREW EXTENDED MLG WITH THE EMERGENCY EXTENTION SYSTEM. CREW FOUND IT VERY HARD TO MOVE HANDLE FOR 1ST FEW STROKES. WERE ABLE TO KEEP GOING UNTIL 3 GREEN LIGHTS. LANDED A/C NORMALLY. A/C PUT ON JACSDR SWIA200413676Flap Track · wornAFTER TAKEOFF SELECTED FLAPS UP AND RECEIVED FLAP DISAGREEMENT. REMOVED AND REPLACED RT IB FLAP OB TRACK AND ALL ROLLERS ON RT IB FLAP IAW 27-50-02, OPERATIONAL CHECKS GOOD.SDR CA040819004Screw · bent(CAN) WHILE IN CRUISE OF FL270 THE PILOT HEARD A BANG AND EXPERIENCED A PARTIAL LOSS OF PRESSURIZATION. HE INITIATED AN EMERGENCY DESCENT AND LANDED AT DESTINATION WITHOUT INCIDENT. UPON INVESTIGATION IT WAS NOTED THAT THE FORWARD UPPER LATCH PLATE HAD SHIFTEDSDR CA040902009Windshield · cracked(CAN) ON DECENT, THE CREW HEARD A BANG AND THE PILOTS SIDE WINDSHIELD WAS CRACKED. THE CREW CONTINUED THE DECENT AND LANDED NORMALLY.SDR 2004FA0000709Panel · crackedCLOSE OUT PANEL ON AFT SIDE OF REAR SPAR CARRY THROUGH. TWO CRACKS IN LOWER BEND RADIUS. FIRST CRACK AT END OF CENTER STRINGER AND LOWER END OF ANGLE STRIP ATTACHED TO PANEL SKIN. SECOND CRACK IS FORWARD OF LEFT OF CENTER STRINGER IN BEND RADIUS OF PANEL. SDR AUS20040490Windshield · cracked(AUS) PILOTS WINDSHIELD CRACKED ON INSIDE LAMINATE. OUTER LAMINATE WAS INTACT.SDR CA040526007Motor · failed(CAN) ON APPROACH, CREW SELECTED LANDING TO EXTEND. LANDING GEAR WOULD NOT EXTEND. GEAR HANDLE CYCLED. STILL NO GEAR EXTENSION. CREW CARRIED OUT LANDING GEAR EMERGENCY EXTENSION. NO FURTHER FAULTS. MAINTENANCE FOUND LANDING GEAR ELECTRIC MOTOR PREMATURELY FASDR JAC006RRWire Harness · failedRT ENGINE ITT INDICATION FAILED IN FLIGHT, PROBLEM WAS DETERMINED BY MAINT TO BE AN ENGINE HARNESS FAILURE. AC FERRIED HOME, WHERE THE T5 HARNESS ASSY WAS REPLACED. CORRECTING DISCREPANCY. THE FAULT WAS NOT DETECTABLE THROUGH NORMAL INSPECTION PROCEDURES, SSDR AUS20040373Spar Cap · corroded(AUS) RT HORIZONTAL STABILISER UPPER REAR SPAR CAP CONTAINED SEVERE INTERGRANNULAR CORROSION.SDR CA040506004Rivet · broken(CAN) DURING INSPECTION IT WAS NOTICED THAT ONE OF THE RIVETS THAT RETAIN THE BRAKE PAD ON TO THE BRAKE ASSEMBLY WAS BROKEN, THE BRAKE ASSEMBLY WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THIS IS THE THIRD OCCURRENCE IN THE LAST FEW MONTHS, (SDR 2003092SDR LKL2004F00000Engine · failedAIRCRAFT WAS IN CRUISE FLIGHT AT 26,000 FT WHEN PILOT HEARD A BANG FROM THE LT ENGINE. THE LT ENGINE CAME TO A STOP AND THE PILOT PERFORMED A SINGLE ENGINE LANDING WITH OUT INCIDENT. INITIAL OBSERVATION BY THE PILOT SHOWED METAL FLAKES IN THE EXHAUST AND OILSDR CA040422007Receptacle · burned(CAN) WHEN THE CABIN CENTER HEADLINER WAS REMOVED DURING ROUTINE MX, RADIANT HEAT RECEPTACLES/SOCKETS WERE FOUND CHARRED AND MELTED WITH THE WIRE CONNECTERS INSIDE THE SOCKET LOOSE AND BURNT, PROBABLY FROM THE AMOUNT OF CURRENT BEING DRAWN THROUGH THE WIRES WHSDR CA040503002Actuator · failed(CAN) DURING TROUBLESHOOTING OF A LANDING GEAR PROBLEM WE NOTICED THAT THE NUT ASSEMBLY IN THE NOSE GEAR ACTUATOR COULD MOVE A SMALL AMOUNT FROM SIDE TO SIDE PLAY IN THE HOUSING. THE ACTUATOR WAS REMOVED AND WE NOTICED THAT THE MECHANISM WAS A LITTLE ROUGH WHESDR G1IA2004001Warning System · activatedLT BLEED AIR FAIL LIGHT ILLUMINATED DURING FLIGHT. SECURED BLEED AIR FOR AFFECTED SIDE AND LANDED AT SCHEDULED DESTINATION. MAINTENANCE DEPT INSPECTED ALL BLEED DUCTS AND EVA TUBING, WITH NO DEFECTS NOTED. PURGED SYSTEM WITH COMPRESSED AIR CLEARING POSSIBLESDR AUS20040222Shaft · failed(AUS) LT MAIN LANDING GEAR RETRACTION DRIVE TUBE FAILED DUE TO INTERFERENCE WITH PNEUMATIC DUCTING CLAMP.SDR CA040330005Wire · loose(CAN) AFTER TAKE OFF THE CREW SELECTED THE LANDING GEAR UP. THE LANDING GEAR DID NOT MOVE AND STAYED EXTENDED. THE CREW PUT THE GEAR HANDLE BACK DOWN AND RETURNED TO THE HANGER. AIRCRAFT PUT ON JACKS AND GEAR RETRACTION TRIED AGAIN WITH NO MOVEMENT OF THE GEARSDR AUS20040197Blade · lightning strike(AUS) LT PROPELLER BLADE EXHIBITED LIGHTNING EXIT MARKS. FURTHER INVESTIGATION FOUND BOTH LT AND RT PROPELLERS MAGNETISED BEYOND LIMITS. LT ENGINE POWER SECTION MAGNETISM BEYOND LIMITS. LIGHTNING EXIT MARKS FOUND ON LT ELEVATOR OB TRAILING EDGE.SDR 2004FA0000402Actuator · separatedCREW RETRACTED FLAPS, FLAPS STOPPED .5000 WAY UP. SPLIT FLAP SAFETY CIRCUIT STOPPED FLAP RETRACTION. REVEALED THAT LT IB FLAP ACTUATOR HAD FAILED. 90 DEGREE DRIVE (P/N 50-380153-3) HAD COMPLETELY SEPARATED FROM MAIN BODY (SCREW DRIVE) OF ACTUATOR. FAILURE SDR CA040308007Gearbox · inoperative(CAN) DURING FLIGHT THE LANDING GEAR TOOK LONGER THAN NORMAL TO RETRACT. COULD NOT DUPLICATE THE PROBLEM IN THE HANGAR EVEN WHEN SWINGING THE GEAR WITH EXTRA LOADS. SUSPECTED THAT THE CLUTCH WAS SLIPPING DURING RETRACTION WITH THE INCREASED LOADS DURING FLIGHSDR CA040607003Landing Gear · malfunctioned(CAN) DURING FLIGHT, THE LANDING GEAR TOOK LONGER THAN NORMAL TO RETRACT. COULD NOT DUPLICATE THE PROBLEM IN THE HANGAR EVEN WHEN SWINGING THE GEAR.SDR CA040311011Channel · cracked(CAN) DURING INSPECTION A CRACK WAS DISCOVERED ALONG THE TRAILING EDGE OF THE CABIN DOOR CHANNEL P/N 50430043619. THE CRACK PROPAGATED APPROXIMATELY 6 IN, JUST ABOVE THE DOOR HINGE. THE DOOR WAS REMOVED AND SENT TO AN APPROVED OVERHAUL SHOP, REPAIRED AND REINSSDR AUS20040145Link · misinstalled(AUS) NOSE WHEEL RETRACTION CHAIN CONNECTING LINK INCORRECTLY FITTED. PERSONNEL/MAINTENANCE ERROR.
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