U/A Canada PT6A-60A
Service difficulty reports · 596
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 = 'PT6A60A' 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 = 'PT6A60A' 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 CA070404008Cross Tie · cracked(CAN) THE STRUCTURAL PIECE CALLED A CROSSTIE P/N 97-430000-150 WAS FOUND CRACKED DURING INSPECTION. IPC / REF: 53-10-20 FIG. 20 ITEM NR 26. THE CRACK IS LOCATED LT SIDE OF AIRCRAFT AT FS 187.383 AND WL 119 ( LOWER LONGERON ). REPLACED WITH NEW. (TC NR 20070404SDR CA070322001Panel · cracked(CAN) PANEL IS INSTALLED ON RT IB SIDE OF NACELLE. IT COVERS THE FUEL FIREWALL SHUTOFF VALVE. THE PANEL IS MANUFACTURED WITH A BULGE TO ACCOMMODATE THE VALVE. IN THIS INSTALLATION THE VALVE CONNECTOR PLUG CHAFFED AGAINST THE PANEL CAUSING A STRESS RISER RESULSDR 2007FA0000284Attach Fitting · looseMANY OF THE BLIND RIVETS, PN NAS1738B6, ATTACHING THE WING SKIN TO THE LOWER FORWARD WING ATTACHMENT FITTING WERE FOUND TO BE LOOSE. CONDITION EXISTED ON BOTH WINGS. CONDITION ALSO FOUND ON AC SN FL59 (8100 HRS). (K)SDR 2007FA0000237Windshield · crackedAT AN ALTITUDE OF 17,000 FT OAT -6 DEGREES C, THE RT WINDSHIELD CRACKED FROM THE CENTER OB FROM THE TOP TO THE BOTTOM ABOUT 2 INCHES OB ON THE OUTER PANE. RETURNED TO THE DEPARTING AIRPORT WITHOUT ANY PROBLEMS. WINDSHIELD WAS REPLACED AND NO KNOWN CAUSE FOR SDR EAS21907Windshield · brokenAIRCRAFT WAS ENROUTE, AT FL27000 THE RT WINDSHIELD INNER PANE SHATTERED. CREW DESCENDED TO FL18000 AND MAINTAINED CABIN PRESSURE OF 3 PSI. AIRCRAFT RETURNED TO DEPARTURE WITHOUT INCIDENT.SDR CA070226005Plate · failed(CAN) DISCOVERED DOOR MAKING NOISE WHEN RAISING OR LOWERING DOOR. INVESTIGATED FOR LOOSE HARDWARE INSIDE DOOR AND DETERMINED PIN AND ROLLER ASSY MIGRATED OUT OF LOWER AFT LATCH ASSY. THE DEFECTIVE PART IN QUESTION IS THE PLATE P/N 101-430032-7. THE PLATE IS THSDR 2007FA0000086Downlock Switch · failedNOSE LANDING GEAR DID NOT HAVE A DOWN AND LOCKED INDICATION GEAR WARNING SYSTEMS ACTIVATED (LIGHT IN SELECTOR HANDLE AND GEAR HORN). AN UNEVENTFUL LANDING HAS MADE VISUAL CHECK OF NOSE GEAR SHOWED TO BE IN THE DOWN AND LOCKED POSITION. SWITCH REMOVED AND REPLASDR CA061216002Valve · false indication(CAN) NEW VALVE WAS INSTALLED. LANDING GEAR VALVE FAILS TO INDICATE THAT IT IS OPEN WHEN SELECTED. VALVE WORKS CORRECTLY, BUT FAILS TO INDICATE TO CREW THAT IT IS WORKING. SEEMS TO BE JUST AN ISSUE WITH THE INDICATION SIDE OF THE VALVE AND NOT THE ACTUAL MECHASDR LX5R200600002Wire Harness · shortedUPON TAKEOFF ROLL THE CREW GOT THE AUTOFEATHER OFF LIGHT AND THE MASTER CAUTION LIGHT. THE CREW THEN OPTED TO ABORT TAKEOFF ROLL AND RETURN TO RAMP WITHOUT INCIDENT. UPON RETURNING TO RAMP THE CREW NOTICED THAT THE AUTOFEATHER CIRCUIT BREAKER HAD POPPED, IT WASDR LX5R200600003Wire Harness · shortedUPON TAKEOFF ROLL, THE CREW GOT THE AUTO FEATHER OFF LIGHT AND THE MASTER CAUTION LIGHT. THE CREW THEN OPTED TO ABORT TAKEOFF ROLL AND RETURN TO RAMP WITHOUT INCIDENT. UPON RETURNING TO RAMP, THE CREW NOTICED THAT THE AUTO FEATHER CRICUIT BREAKER HAD POPPED,SDR 2006FA0000968Starter Gen · wornIN FLIGHT THE LT SIDE STARTER/GEN AFT BEARING AT THE COOLING FAN FAILED AND THE GENERATOR FAILED. THE AC RETURNED TO ITS DEPARTURE TERMINAL WITHOUT INCIDENT. THE STARTER/GEN WAS REPLACED AND THE CHARGING AND ELECTRICAL SYSTEM OPS, CHECKED GOOD. NO KNOWN CAUSDR 2006FA0001003Starter Gen · wornIN FLIGHT THE LT SIDE STARTER/GENERATOR AFT BEARING AT THE COOLING FAN FAILED AND THE GENERATOR FAILED. THE AC RETURNED TO ITS DEPARTURE TERMINAL WITHOUT INCIDENT. THE STARTER/GENERATOR WAS REPLACED AND THE CARGING AND ELECTRICAL SYSTEM OPS CHECKED GOOD. NOSDR RU3A0612Governor · malfunctionedON FINAL, RWY23 AT KBTL, WHEN POWER LEVERS BROUGHT TO IDLE, AIRCRAFT YAWED LEFT. SUSPECT RIGHT PROP STAYED IN FLIGHT IDLE AND LEFT PROP WENT TO GROUND IDLE. GO-AROUND ACCOMPLISHED. PULLED PROP GOV TEST CB, LANDED UNEVENTFULLY. CLEANED REVERSING CABLE AND RSDR SUPRU3A0612Governor · malfunctionedON FINAL, RWY 23 AT KBTL. WHEN POWER LEVERS BROUGHT TO IDLE, AIRCRAFT YAWED LEFT. SUSPECT RIGHT PROP STAYED IN FLIGHT IDLE AND LEFT PROP WENT TO GROUND IDLE. GO-AROUND ACCOMPLISHED. PULLED PROP GOV TEST CB, LANDED UNEVENTFULLY.SDR CA060821005Bypass Valve · failed(CAN) RT OIL TEMPERATURE REACHED THE REDLINE WHEN CLIMBING THROUGH 25000 FT. POWER REDUCED AND A/C DESENDED TO 20000 FT. OIL TEMP RETURNED TO NORMAL. ENG POWER SETTING RETURNED TO NORMAL, NO FURTHER FAULT. NR 2 ENGINE OIL COOLER THRMOSTATIC BYPASS VALVE REPSDR RU3A0610Unknown · unknownON SHORT FINAL HEARD SOUND OF PROPS GOING INTO GROUND FINE. FELT YAWING MOTION. APPLIED POWER, WENT AROUND.SDR RU3A0608Control Handle · failedDESCENT CHECKLIST WAS COMPLETED. PILOT LOWERED GEAR HANDLE BELOW 184 KNOTS. SIC COMMENCED CHECKLIST AND NOTED THE GEAR POSITION INDICATOR LIGHTS WERE NOT ILLUMINATED NOR WERE THE 2 RED INDICATOR LIGHTS IN THE LANDING GEAR CONTROL HANDLE. PILOT COMMENCED A GO-ASDR CA060705008Motor · malfunctioned(CAN) DURING APPROACH LANDING GEAR WOULD NOT EXTEND NORMALLY AND 2 AMP CONTROL CIRCUIT BREAKER HAD OPENED. LANDING GEAR WAS LOWERED USING MANUAL SYSTEM AND UNEVENTFUL LANDING CARRIED OUT. MAINTENANCE FOUND 60 AMP LANDING GEAR CIRCUIT BREAKER OPEN (IN LH WING).SDR 2006FA0000649Switch · out of limitsDURING SCHEDULED 12 MONTH TEST OF CABIN ALTITUDE WARNING SYSTEM FOUND BAROMETRIC SWITCH OPERATING OUT OF SPECIFIED MM. REPLACED PN 1013384028-3 SWITCH ASSY. CABIN ALTITUDE WARNING TESTS WITHIN SPECIFIED SERVICE LIMITS ON RETEST. SUGGEST A SB BE ISSUED TO RESDR 2006F00025Canister · openSMOKING ON SHUT DOWN. OPENED RIGHT SIDE COWLING AND FOUND THE END OF THE EPA/JOHN'S CAN COMPLETELY OPEN. END PLATE FOUND IN BOTTOM OF COWLING. TT PRESUMED TO BE ORIGINAL.SDR CA060301007Nut Plate · damagedAIRCRAFT WAS ON APPROACH. POSITIVE NOSE GEAR DOWN LOCK WAS NOT INDICATING USING THE NORMAL SYSTEM. EMERGENCY GEAR DOWN WAS REQUIRED TO HAVE POSITIVE DOWN AND LOCK INDICATION. NOSE LANDING GEAR INSPECTION WAS CARRIED OUT OF THE GREEN LIGHT INDICATOR SWITCHESSDR 2006FA0000205Cover · chafedCOVER IS CHAFING LOWER FWD LT AND RT WING ATTACH POINT, SPAR CAP AND WING SKIN. THE COVER HAS NO ANTI-CHAFE PROTECTION. RECOMMEND RUBBER EDGE SEAL OR FAY SEALED EDGE TO AVOID METAL TO METAL CONTACT WITH SPAR AND WING SKIN. (K)SDR 2006FA0000206Cover · chafedCOVER IS CHAFING LOWER FWD LT AND RT WING ATTACH POINT, SPAR CAP AND WING SKIN. THE COVER HAS NO ANTI-CHAFE PROTECTION. RECOMMEND RUBBER EDGE SEAL OR FAY SEAL EDGE TO AVOID METAL TO METAL CONTACT WITH SPAR AND WING SKIN. (K)SDR 2006FA0000207Cover · chafedCOVER IS CHAFING LOWER FWD LT AND RT WING ATTACH POINT SPAR CAP AND WING SKIN. THE COVER HAS NO ANTI-CHAFE PROTECTION. RECOMMEND RUBBER EDGE SEAL OR FAY SEAL EDGE TO AVOID METAL TO METAL CONTACT WITH SPAR AND WING SKIN. (K)SDR IPM2006F00000Jackscrew · jammedPILOT REPORTED ASYMMETRICAL FLAP CONDITION ON LANDING. FOUND RT FLAP EXTENDED APPROX 10 DEGREES, AND JACKSCREW TO FLAP ATTACH BRACKET TORN FROM FLAP. THE TRANSMISSION AND FLAP SYSTEM WAS INSPECTED IAW AD AND FOUND TO MEET SPECS (MEASUREMENTS HAD NOT CHANGED SDR DAT2006F00001Radar · smokeCLIMBING THROUGH APPROX 4000 FT THE WEATHER RADAR SCREEN STARTED TO FLICKER THEN WENT BLANK. IT WAS ON THE (40 MILE) SETTING. AS I WAS TURNING IT TOWARDS (OFF) THE SCREEN CAME ON AGAIN. IT FLICKERED SOME MORE THEN THERE WAS A SMELL OF SOMETHING BURNING. IMSDR 2006FA0000102Trunnion · crackedDURING 100 HOUR INSPECTION FOUND CRACK IN WEB OF AFT MLG TRUNNION ASSY AIRCRAFT. (K)SDR 2006FA0000204Cover · chafedCOVER IS CHAFING LOWER FWD LT AND RT WING ATTACH PORT SPART CAP AND WING SKIN. THE COVER HAS NO ANTI-CHAFE PROTECTION. RECOMMEND RUBBER EDGE SEAL OR FAY SEALED EDGE TO AVOID METAL TO METAL CONTACT WITH SPAR AND WING SKIN. (K)SDR TIM2006F00000Relay · failedLANDING GEAR DID NOT EXTEND WHEN SELECTED. PILOT EXTENDED GEAR MANUALLY AND LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THAT THE HYDRAULIC POWER PACK MOTOR RELAY HAD WELDED IN THE CLOSED POSITION RESULTING IN THE MOTOR RUNNING CONTINOUSLY UNTIL IT FAILEDSDR DAT2006F00000Line · chafedON INITIAL TAKEOFF AT APPROXIMATELY 200 FEET AGL BOTH HYDRAULIC LIGHTS CAME ON AND TOTAL SYSTEM PRESSURE WAS ZERO PSI. THE FLIGHT CREW EXECUTED THE CHECKLIST. EVENTUALLY THE RT SIDE PUMP BEGAN WORKING AGAIN. RETURNED AND MADE AN UNEVENTFUL LANDING. SENT RESDR 2006FA0000020Conduit · leakingLT NACELLE TANK SENDER WAS LEAKING OUT OF TOP OF NACELLE. SENDER SCREWS HAD BEEN TIGHTENED AND GASKETS REPLACED BUT STILL LEAKED. TECH FOUND ALUMINUM CONDUIT THAT SENDER WIRING IS ROUTED THROUGH IN TANK TO HAVE APPROX 10-15 PINHOLES IN IT FROM CORRODING FROM TSDR 2005FA0001649Brake · draggingON TAKEOFF ROLL, BRAKES APPEARED TO BE DRAGGING. CREW DECIDED TO ABORT TAKEOFF W/O INCIDENT AND TAXIED BACK TO GATE. MAINT JACKED AC AND CHECKED BRAKES. BRAKES APPEARED TO BE DRAGGING AND NOT RELEASING ALL THE WAY. THESE ARE UNMODIFIED BRAKES (W/O STAINLESS SDR CA051213006Hose · burstDURING DAILY INSPECTION, THE AME FOUND THE LT BRAKE DEICE HOSE (P/N 101-380015-9) BURST NEAR UNION (P/N 832-12D).SDR AU510001884Screw · looseOUTER WING FORWARD UPPER BATHTUB FITTING TO UPPER SKIN PANEL ATTACHMENT SCREWS LOOSE. SUSPECT SCREWS INCORRECTLY TORQUED DURING MANUFACTURE.SDR AU510001890Screw · looseOUTER WING FORWARD UPPER BATHTUB FITTING TO UPPER SKIN PANEL ATTACHMENT SCREWS LOOSE. SUSPECT SCREWS INCORRECTLY TORQUED DURING MANUFACTURE.SDR AU510001930Lock Nut · missing(AUS) RUDDER PEDAL INTERCONNECT TUBE DISCONNECTED AT PILOT`S RUDDER PEDAL BELLCRANK. INVESTIGATION FOUND THE ATTACHING BOLT PNO 130909B81 AND WASHER ON THE FLOOR AND THE NUT ON TOP OF THE BELLCRANK. NIL EVIDENCE OF A SPLIT PIN WAS FOUND. THE NYLOC NUT WAS INSPSDR CA051222004Spar · corrodedA/C IN FOR 5 YR WING BOLT REPLACEMENT AND MAIN SPAR LWR FITTING VISUAL INSPECT. LWR FWD LT WING BOLT DIFFICULT TO REMOVE AND UPON REMOVAL MODERATE CORROSION WAS OBSERVED IN BOLT BORES. LOOKING AT BOLT BORES FROM FRONT, GREATEST CORROSION APPEARED TO BE AFT ASDR POS2006F00000Uplock Switch · out of adjustON FLIGHT, ON RETRACTING THE LANDING GEAR THE FLIGHT CREW NOTICED THAT THE LANDING GEAR HANDLE STAYED (RED) INDICATING THE LANDING GEAR WAS NOT UP AND STOWED. THE FLIGHT CREW LOWERED THE LANDING GEAR. THE LANDING GEAR WENT DOWN AND GAVE A SAFE DOWN AND LOCKESDR TIM2005F00014Skin · damagedTHE FASTENERS WERE DISCOVERED TO BE WORKING INTO THE LOWER SKIN WHILE DOING AN INSPECTION OF THE WING. IT APPEARS THAT THIS WAS CAUSED BY NORMAL WING FLEX IN THIS AREA. (K)SDR CA051202008Angle · crackedWHEN COMPLYING WITH SPECIAL INSPECTION ON CABIN DOOR, DISCOVERED CRACKED CABIN DOOR SILL ANGLE AT TOP OF DOOR. ADVISED TO HAVE A SPARE PART ON HAND BEFORE DOING INSPECTION. PART WAS CRACKED ALONG WIDTH OF THE ANGLE RUNNING FORE AND AFT FROM AFT END OF THE DSDR 2005FA0001349Spar Cap · crackedDURING COMPLIANCE WITH AD 89-25-10, 1,000 HOUR INTERVAL EDDY CURRENT INSPECTION, THE SPAR CAP WAS FOUND TO BE CRACKED 3 INCHES OB OF BATHTUB AT RT WING LOWER FORWARD SPAR ATTACH POINT.SDR CA051009001Windshield · broken(CAN) ON CLIMB OUT, THE CREW HEARD A LOUD BANG AND THE PILOTS WINDSHIELD INNER PANE HAD BROKEN. THE CREW RETURNED WITHOUT A PROBLEM.SDR CA051003002Windshield · fractured(CAN) WHILE ON ROUTE, AT 23,000 FEET AT 12 NOON, OAT -25 C, WINDSHIELD HEAT ON. THE PILOTS (LT) INNER LAYER OF WINDSHIELD FRACTURED WITHOUT WARNING DURING FLIGHT. NO LOSS OF CABIN PRESSURE OR OTHER EFFECTS FROM WINDSHIELD DELAMINATING. EMERGENCY WAS DECLARED ASDR CA050815001Blower · failed(CAN) THE AIRCRAFT WAS ON THE RETURN LEG OF A TRIP WHEN THE FORWARD VENT MOTOR P/N 101-384176-1 MODEL EM640-1 FAILED ON SHORT FINAL LANDING. THE TBO ON THIS UNIT IS 1500 HRS IAW COMPONENT OVERHAUL MANUAL. OUR UNIT FAILED PRIOR TO THIS LIMIT AND HAVE HAD OTHER SDR FCPR200500020Barrel · brokenSHARP TAXI TURN, NOSE WHEEL STEERING BARREL BROKE AT RETAINER AREA. C/W SB 220 TO PREVENT RECURRENCE. (K)SDR CIEA200500014Fire Detector · shortedAFTER THE PILOT GOT INTO THE AIRCRAFT TO PERFORM A TRIP AND TURNED ON THE MASTER SWITCH, THE ENGINE FIRE WARNING CIRCUIT BREAKER POPPED AND WOULD NOT RESET. THE TRIP WAS CANCELED AND THE AIRCRAFT WAS TURNED OVER TO MAINTENANCE. MAINTENANCE TROUBLESHOT AND FOSDR CA050720001Display · malfunctionedAFTER DEPARTURE AT ABOUT 30NM, CLIMBING THROUGH FL240 THE CO-PILOT EHSI STARTED FLASHING WITH NUMEROUS FLAGS. REQUESTED A RETURN TO BASE AND LANDED NORMALLY. MAINTENANCE REPLACED U/S EHSI AND RESUMED TRIP.SDR 2005FA0000939Support Tube · fracturedTHE RT LANDING GEAR COLLAPSED DURING TAKEOFF FROM A ROUGH DIRT STRIP. A LANDING GEAR SUPPORT TUBE BROKE NEAR ONE ATTACH POINT. CORROSION WAS PRESENT.SDR TXH2005F00000Skin · crackedDEFECT WAS NOTED DURING INSPECTION OF HORIZONTAL AND VERTICAL STABILIZERS. SKIN AND RIB, TOP SIDE OF RUDDER BALANCE WEIGHT ATTACHMENT AND STRUCTURAL AREA CRACKED AND CORRODED. (WP13200509006) (K)SDR 2005FA0001000Skin · delaminatedDURING A POST FLIGHT CHECK, A MECHANIC NOTICED A BULGE ON THE UNDERSIDE OF THE IB LEADING EDGE OF THE LT WING. UPON FURTHER INVESTIGATION, A DELAMINATION AREA OF APPROXIMATELY 22 INCHES X 10 INCHES WAS FOUND. AFTER REMOVAL OF THE LEADING EDGE AND CLOSER EXA
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