Pilatus PC-12/47
Service difficulty reports · 273
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 aircraft_model_key = 'PC1247' 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 aircraft_model_key = 'PC1247' 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 6CBA2016070716152Indicator · odorCREW REPORTED A BURNING ODOR COMING FROM LOWER EFIS TUBE AFTER BLANKING OUT. PERFORMED VISUAL INSPECTION OF EHSI WIRING IAW WDM 34-26-00, NO DEFECTS NOTED. IDENTIFIED BURNING ODOR WITHIN PILOTS EHSI. PERFORMED REPLACEMENT OF PILOT EHSI IAW AMM 12-A-34-26-02SDR 2016F00122Adapter · failedPILOTS WERE DIRECT SMO AT THE END OF THE FLIGHT AT 5,000 FT. AUTOPILOT WAS ENGAGED IN ALTITUDE HOLD NAV MODE. WE RECEIVED A CAS WARNING OF PITCH TRIM RUNAWAY ALONG WITH VOICE CALLOUT TRIM RUNAWAY. WE PUSHED THE TRIM INTERRUPT SWITCH & RAN THE QRH CHECKLIST.SDR 6CBA20160505150Master Cylinder · faultyBRAKE PEDALS GO TO THE FLOOR WITH MINIMAL BRAKING AUTHORITY. SYS WILL NOT HOLD PRESS. THE BRAKE SYS WAS INSPECTED & THE PILOTS LT BRAKE MASTER CYLINDER, PN 959.47.51.131, WAS FOUND TO BE FAULTY. IT WAS R & R IAW AMM 12-A-32-40-04-00A-920A-A. THE BRAKE SYS SDR K5SR2016050927516Contactor · stuckPILOT REPORTED THAT THE UNDER FLOOR HEATER TRIPS THE CIRCUIT BREAKER AND WILL NOT RESET. PERFORMED TROUBLESHOOTING OF UNDER FLOOR HEATER SYS. FOUND UNDER FLOOR HEATER K665 CONTACTOR HAD STUCK IN ENERGIZED CLOSED POSITION CAUSING 28 VOLTS TO CONSTANTLY FEED HESDR CA160120013Engine · power loss(CAN) DURING TAKEOFF, THAT ACFT IS REPORTED TO HAVE SUFFERED A POWER LOSS BEFORE IT CRASHED IN A DITCH JUST OFF THE RUNWAY. A POST-CRASH FIRE OCCURRED. BOTH CREW MEMBERS WERE INJURED AND TRANSPORTED TO THE HOSPITAL. NO FURTHER DETAILS ARE AVAILABLE AT THIS TISDR CA160120002Engine · power loss(CAN) DURING TAKEOFF, THAT ACFT IS REPORTED TO HAVE SUFFERED A POWER LOSS BEFORE IT CRASHED IN A DITCH JUST OFF THE RUNWAY. A POST-CRASH FIRE OCCURRED. BOTH CREW MEMBERS WERE INJURED AND TRANSPORTED TO THE HOSPITAL. NO FURTHER DETAILS ARE AVAILABLE AT THIS SDR 6CBA20151116145Mount · damagedTHIS ACFT WAS UNDERGOING REPAINT & SOME DAMAGE OCCURRED TO THE LT ELEVATOR AT THE INBD STATIC WICK MOUNT. THE DAMAGE WAS REPAIRED USING ENGINEERING REPAIR RM-12-000844 WITH ASSOCIATED STATEMENT OF APPROVED DESIGN DATA, SADD-12-0761. A FORM 337 WAS SUBMITTED SDR ESMA2015102801Shaft Seal · galled1.5 HOURS INTO THE FLIGHT, THE THROTTLE WAS RETARDED, IMMEDIATELY OIL SPRAYED ONTO THE WINDSCREEN. UPON DESCENT THE OIL DID NOT CONTINUE TO SPRAY ON THE WINDSCREEN. AN EMER WAS DECLARED & THE ACFT LANDED WITHOUT INCIDENT. A NEW PROP SHAFT SEAL THAT HAD JUST SDR 2015FA0000469Ahrs · failedLOSS OF BOTH AHRS CHANNELS A+B DURING FLIGHT. PILOTS RETURNED TO ORIGIN.SDR 6CBA20150918144Skin Panel · damagedTHE ACFT SUFFERED A LIGHTNING STRIKE WHICH RESULTED IN DAMAGE TO THE LT WING, LOWER INBD SKIN PANEL, BETWEEN RIBS 6 - 8. MFG ISSUED A REPAIR MEMO RM-12-000817 & ASSOCIATED SADD-12-0737 THAT COVERED A REPAIR BY REPLACEMENT OF THE LT LOWER WING SKIN PANEL BETWESDR CA150923009Bleed Valve · cracked(CAN) DURING BRAKE REPLACEMENT IT WAS NOTICED THAT THE BRAKE BLEEDER VALVE SEAT ON THE NEWLY O/H ASSY WAS CRACKED. IT WAS ALSO NOTICED THAT THE O-RING ON THE FLUID SUPPLY FITTING, ELBOW, WAS ASSEMBLED ON THE THREADED PORTION NOT THE SMOOTH GLAD AREA AND THAT SDR 6CBA20150830143Wire · brokenTHE FLIGHT CREW REPORTED ON APPROACH, LT LG INDICATION, GEAR UNSAFE, INTERMITTENTLY FLASHES WHILE IN FLIGHT. THE ACFT ABORTED APPROACH, HAD TOWER VISUALLY CONFIRM ALL GEAR DOWN & LOCKED. THE ACFT LANDED SAFELY. THE ACFT WAS THEN FERRIED FOR REPAIRS. DURINGSDR 2015FA0000386Relay · stickingDURING TAKEOFF, RUDDER TRIM RAN FULL DEFLECTION IN 1 DIRECTION. PILOT ATTEMPTED TO MANUALLY NEUTRALIZE THE TRIM BUT IT WOULD NOT RUN TOWARDS NEUTRAL. IT IS ELECTRIC. PILOT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. WERE ABLE TO DUPLICATE THE DISCRESDR CA150806005Brake Disc · cracked(CAN) DEFECT OF RT BRAKE LOCKING UP WHEN ACFT IS PUSHED OUT OF HANGAR REPORT BY AIRCREW. RT BRAKE FOUND TO HAVE A CRACKED OTBD ROTOR. RT BRAKE ASSY REPLACED AND RT MAIN WHEEL ASSY. REPLACED DUE WORN DRIVE KEYS, P/N 205-05201. NO OTHER FAULTS FOUND WITH MAISDR 6CBA20150709142Wire · damagedAFTER DEPARTURE, GEAR HANDLE IN UP POSITION. LT MAIN GEAR DOWN, NOSE GEAR UP. INDICATION 3 DOWN & LOCKED. EMERGENCY GEAR EXTENSION UNSUCCESSFUL. SPEED TURNS REQUIRED TO EXTEND & LOCK LT MLG. THE ACFT LANDED SAFELY. WIRING TRANSPORTING DRIVE & ENABLE COSDR CA150624001Bearing · stiff(CAN) PILOT DEPARTED & DID A NORMAL CLIMB TO FL280. AROUND 1425Z HE HAD CAS CAUTION MSG AP HOLD LT WING DN. DISENGAGED THE AUTOPILOT & FOUND THAT THE AILERONS WERE BLOCKED IN NEUTRAL POSITION. REQUESTED A LOWER ALTITUDE & A RETURN STARTED DESCENT 1429Z GOINSDR 3S4A2015F00063Relay · shortedDURING DESCENT A PITCH TRIM RUNAWAY OCCURRED AND THE SYSTEM WAS REVERTED TO MANUAL CONTROL FOR THE REMAINING PORTION OF THE FLIGHT.SDR CA150504006Windshield · cracked(CAN) LEFT WINDSHIELD CRACKED.SDR 2015FA0000151Trim System · faultyAN EMERGENCY WAS DECLARED FOR A RUDDER TRIM SYSTEM MALFUNCTION.SDR U5OA20150427001Wire Harness · shortedFOUND CONNECTOR WIRE SHIELDING SHORTING AT BACK OF CONNECTOR FOR ENGINE OIL TEMPERATURE SENSOR.SDR 6CBA20150403141Light · inoperativeRIGHT MLG GREEN LIGHTS INOPERATIVE. R & R RT LANDING GEAR INDICATOR LIGHT BULBS WITH NEW PN CM6839 IAW AMM 12-A-31-11-01-00A-920A-A. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.SDR CA150708005Hose · leaking(CAN) NEW FUEL HOSE INSTALLED AT ENGINE REPLACEMENT FOUND TO BE SEEPING AFTER 4.7 HRS OF FLIGHT. APPEARED TO BE LEAKING FROM THE SWAGE AREA.SDR CA150323009Idler Gear · damaged(CAN) DURING O/H OF 2 PROPELLER GOVERNORS THE IDLER GEAR, P/N 5337-050, WAS FOUND WITH THE BUSHING INSERT MISSING. THESE 2 PROPELLER GOVERNORS WERE RECEIVED WITH BEARINGS INSTALLED IN THE PLACE OF THE BUSHING, HOWEVER WERE INADVERTENTLY DISCARDED AT DISMANTLESDR 2015FA0000077Display · failedREPEATED, 4 CONSECUTIVE AFT AND 3 CONSECUTIVE REPAIRED UNITS, FAILURE OF EIS, ENGINE INSTRUMENT SYSTEM, DISPLAYS DURING SELF TEST FOUND AT ANNUAL/150 HOUR INSPECTIONS. FAILURES ARE A CODE 25, FAILURE OF RS232 RECEIVER, INTERNAL OR APU A OR B MONITOR TEST FAILUSDR CA150225001Proximity Sensor · failed(CAN) DURING LANDING GEAR FUNCTION TEST, GEAR HANDLE SOLONOID STAYED LATCHED WHEN AIRCRAFT WAS ON JACKS NOT ALLOWING GEAR TO RETRACT. AFTER TROUBLESHOOTING IT WAS FOUND THAT BOTH LEFT AND RIGHT PROXIMITY SENSORS HAD FAILED IN THE GEAR DOWN WOW POSITION.SDR 6CBA20150116140Circuit Breaker · poppedUPON GEAR RETRACTION HYD CTL CB POPPED, HYD CAS & GEAR REMAINED UNSAFE. THE ACFT MADE AN UNSCHEDULED LANDING. THE HYD CTL CB WAS RESET, THE HYD SYS WAS CHECKED FOR PROPER SERVICING IAW AMM 12-B-29-00-00-00A-902A-A. CHECKED SECURITY OF HYD PUMP MOTOR LEADS SDR CA150130001Fuel Control · faulty(CAN) AFTER LANDING DURING REVERSING OF PROPELLER, GROUND IDLE POWER WENT LOW CAUTION LIGHTS CAME ON. PROPELLER RPM REDUCED THE PROPELLER GOT INTO FEATHER POSITION. ITT INCREASED TO 880 C FOR 1 SECOND. PILOT TRIED TO REDUCE ITT BUT ENGINE SHUT DOWN AT ITT OFSDR LF1R2015011200001Turbine Blades · separatedON TAKEOFF ROLL AT ABOUT 25 KTS AND AS POWER WAS BEING APPLIED, PILOT HEARD LOUD BANG FOLLOWED BY CHIP DETECTOR LIGHT AND SEVERAL CAS MESSAGES. PILOT ABORTED TAKEOFF, REDUCED POWER, AND TAXIED OFF RUNWAY. THE PROPELLER HAD STOPPED BUT THE GAS GENERATOR SECTIOSDR CA141208008Display · malfunctioned(CAN) DURING CRUISE FLIGHT, THE FLIGHT CREW WENT TO SELECT A DIRECT TO WAYPOINT, THE APEX FMS SYS DID NOT ACCEPT THE SELECTION, NOTHING HAPPENED, A SECOND ATTEMPT WAS MADE TO SELECT THE WAYPOINT AND AT OR ABOUT THE SAME TIME AS WHEN THE SELECTION WAS MADE THE SDR CA141202028Clamp · broken(CAN) THERE ARE 4 V BAND SEGMENTS SPOT WELDED ON CLAMP. ONE V BAND SEGMENT BROKE OFF DUE TO SPOT WELD FAILURE FROM V BAND SEGMENT TO CLAMP STRAP.SDR 6CBA20141123139Relay · stickingACS LOW INFLOW INFLIGHT BURNING ODOR COMING FROM VENTS. THE ACS SYS & COMPONENTS WERE INSPECTED WITH NO DEFECTS FOUND. A FUNCTIONAL & OPERATIONAL TEST OF THE TEMPERATURE CONDITIONING & ACS & AUXILIARY HEATING SYSTEMS WAS PERFORMED IAW 12-B-71-00-00-00A-903S-SDR CA141124003Throttle · frozen(CAN) POWER CONTROL LEVER STUCK AT CRUISE POWER WHILE AT CRUISE ALTITUDE. A FLIGHT REPORT REVEALED THAT WHEN THE CREW TRIED TO REDUCE POWER, THE LEVEL COULD NOT BE MOVED. FLIGHT CREW APPLIED MORE FORCE, THE POWER LEVER BECOME UNSTUCK AND COULD BE OPERATED NORMSDR 6CBA20141118138Powerpack · malfunctionedLANDING GEAR FAILED TO EXTEND, HYDR CAWS ILLUMINATED, PERFORMED QRH, GEAR EXTENDED. THE ACFT MADE AN UNSCHEDULED LANDING. THE HYD POWER PACK MOTOR PN 960.30.02.104 & HYD POWER RELAY PN 974.09.26.112 WERE FOUND FAULTY, R & R. THE HYD SYS WAS FOUND TO FUNCTIOSDR CA141208001Light · contaminated(CAN) LED TAIL NAVIGATION LIGHT ASSEMBLY ILLUMINATION VERY DIM. UNIT RELACED WITH SERVICEABLE UNIT. FOUND MOISTURE INSIDE SEALED NAVIGATION LIGHT ASSY.SDR CA141118004Acm · leaking(CAN) DURING WALK AROUND, FOUND OIL WEEPING FROM COLD AIR UNIT FAN OUTLET VENT ON SIDE OF AIRCRAFT. FURTHER INSPECTION FOUND OIL LEAKING ON FAN SIDE OF COLD AIR UNIT TURBINE. REFRIGERATION PACK REPLACED. ENVIROMENTAL CONTROL SYSTEM FUNCTION CHECK CARRIED OUT. SDR CA141106001Engine · malfunctioned(CAN) APPROXIMATELY 40 MINUTES CRUISING AT 16000` THERE WAS A THUD SOUND FROM THE FRONT OF THE PLANE FOLLOWED BY A SUSTAINED HIGH PITCH SQUEAL FOR THE DURATION OF THE FLIGHT. NO CAS MESSAGES APPEARED AND ALL ENGINE PARAMETERS REMAINED THE SAME. THE ENGINE PARASDR CA141107005Actuator · failed(CAN) WHEN PILOT DISENGAGED AUTO PILOT ON APPROACH, CONTROLS WERE HEAVY COULD NOT MANUAL TRIM TO LIGHTEN. ALTERNATE TRIM USED TO LIGHTEN FLIGHT LOADS. ON GROUND, MANUAL TRIM ACTIVATION HAD NO RESPONSE. PITCH TRIM ACTUATOR REPLACED, REQUIRED FUNCTION TEST CASDR 6CBA20140920137Fitting · looseTHE FLIGHT CREW REPORTED LT SIDE AIRSPEED INDICATION FAILURE. THE NR 1 PITOT FITTING WAS FOUND LOOSE. THE FITTING WAS TIGHTENED IAW SB34-039. THE PITOT STATIC AIRSPEED SYS OPERATIONALLY CHECKED GOOD IAW THE AMM 12-B-34-11-00-00A-903A-A & 12-B-34-16-00-00A-9SDR CA140917019Computer · failed(CAN) PILOT REPORT OF CAS, PUSHER, INDICATION IN FLIGHT AND SYSTEM WOULD NOT TEST/RESET. AIRCRAFT RETURNED TO BASE. ON TROUBLESHOOTING, FOUND STICK PUSHER COMPUTER WOULD NOT CLEAR AND RESET. STICK PUSHER COMPUTER REPLACED WITH SERVICEABLE UNIT. STICK PUSHESDR 6CBA201409121136Fitting · separatedTHE PITOT LINE FITTING IN LT WING AT RIB 14A WAS FOUND TO BE SEPARATED. THE POLY FLOW TUBING PITOT LINE IN LT WING, FROM WING ROOT TO BULLHEAD FITTING AT RIB 14A & FITTING PN 946.01.17.101 WAS REPLACED IAW 12-B-20-50-02-00A-901A-A & SB34-039. A PITOT & STATSDR 6CBA20140912136Unknown · malfunctionedPILOT AIRSPEED MIS-COMPARE BY 15 KTS, PILOTS IAS INDICATOR CONTINUED TO DROP TO 0 KTS. A SUPPLEMENTAL SDR WILL NEED TO BE FILED. MAINTENANCE IS STILL BEING COMPLETED, THE FINAL FIX IS NOT DETERMINED AT THIS TIME.SDR CA140917018Shim · migrated(CAN) INSPECTION OF FLAP SHIMS PREVIOUSLY C/O IAW SB 57-006 ON 2013-01-22. NO DEFECTS FOUND AT TIME. AT ANNUAL INSPECTION FOUND SHIMS HAD STARTED TO MIGRATE. SHIMS REPLACED IAW MFG INSTRUCTIONS AND FASTENERS TORQUED.SDR 6CBA20140901135Unknown · odorPILOT REPORTED AFTER DEPARTURE STRONG ELEC BURNING SMELL OBSERVED AFTER TAKEOFF. THE ACFT RETURNED & LANDED SAFELY FOR REPAIRS. INSPECTED UNDER INSTRUMENT PANELS, FLOORBOARDS, ENG COMPARTMENT & VCCS COMPARTMENT TRYING TO LOCATE SOURCE OF ELEC SMELL, NONE FOUSDR CA140910008Control System · frozen(CAN) FLIGHT LEVEL 27,000 FT ,OAT -45 .THE AUTO PILOT DIS- ENGAGED AT THIS TIME THE PILOT TOOK CONTROL OF THE AIRCRAFT AND FOUND THE AILERON CONTROLS WERE FROZEN. THE PILOT DESENDED TO 15,000 FEET AT THIS POINT THE CONTROLS STARTED TO FREE UP AND AS THE AIRCRASDR 6CBA20140825134Motor · burned outCRUISE FLIGHT, ODD ELEC NOISE, BUS TIE CAWS, NON-ESSENTIAL CAWS & FLICKERING BATTERY CAWS, BUS TIE & GEN 2 TIE RELAYS POPPED. BATTERY 1 AMPS DISCHARGING. STRONG ELEC ODOR INSIDE TAIL SECTION NOTED UPON LANDING. THE VCCS SYS DRIVE MOTOR PN 1134104-1, SN 992SDR 6CBA20140814133Motor · faultyAFTER DEPARTURE HYD CAWS IN FLIGHT, GEAR EXTENDED MANUALLY IAW QRH. THE ACFT DIVERTED & LANDED SAFELY. A FERRY PERMIT WAS OBTAINED FOR ACFT RELOCATION WHERE REPAIRS WERE MADE. THE HYD POWER PACK MOTOR PN 960.30.02.104 & RELAY 974.09.26.112 FOUND TO BE FAULTYSDR 6CBA20140806132Circuit Breaker · poppedAFTER DEPARTING, THE FLIGHT CREW REPORTED HYD CAWS IN FLIGHT. HYD CB POPPED SHORTLY AFTER GEAR SELECTED UP. THE LG WAS VISUALLY INSPECTED, FUNCTIONAL TEST COMPLETED OF NORMAL & EMERGENCY EXTENSION & RETRACTION SYSTEMS IAW AMM 12-A-32-30-00-00A-903A-A. NO DESDR 6CBA20140728131Bolt · brokenAFTER DEPARTURE RT GEAR UNSAFE LIGHT ILLUMINATED ON GEAR RETRACTION. THE ACFT DIVERTED & LANDED SAFELY. INSPECTION OF THE RT LG REVEALED THE LOWER RT LG ACTUATOR BOLT BROKEN AT THE NUT ATTACHMENT & WAS WORKING OUT OF THE GEAR MOUNTING HOLE. THE INNER BORE OSDR HZYR20140717001Motor · failedJUST AFTER START UP THERE WAS A ODOR OF "OZONE" IN THE CABIN. THE ENGINE WAS SHUTDOWN AND THE PILOT DETERMINED THE ODOR WAS COMING OUT OF THE SERVICE AREA IN THE TAIL. OPENED THE DOOR TO THIS AREA SMOKE WAS OBSERVED AND IT WAS DISCOVERED THAT THE AIR CONDITISDR 2014FA0000511Adapter · malfunctionedDURING CLIMB OUT, YAW DAMPENER DISENGAGED. DISENGAGED AUTOPILOT AND MANUALLY FLEW THE AIRCRAFT. NOTICED THE ACFT WAS STARTING TO YAW ABNORMALLY AND CONTROL WAS BECOMING INCREASINGLY DIFFICULT. DURING FURTHER INVESTIGATION, FOUND THE RUDDER HAD BEEN TRIMMED A
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