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 = 'B200' 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 = 'B200' 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 CA140619009Light · overheated(CAN) ON FINAL APPROACH, AN ARCID SMELL WAS NOTED, AND THOUGHT TO BE DUE TO CROP SPRAYING IN THE AREA. AFTER TOUCHDOWN DURING ROLL OUT, AN ORANGE GLOW AND SMOKE COMING UP FROM THE UPPER AFT CORNER OF THE PILOT SIDE CIRCUIT BREAKER PANEL WAS NOTED IN THE AREA OSDR CA140612007Cap · unsecure(CAN) AFTER RUNNING-UP THE ENGINES BY MAINTENANCE ACAS, IT WAS NOTICED SOME SMOKE COMING FROM THE NR 1 ENGINE EXHAUST AFTER SHUTDOWN. INVESTIGATING LEAD TO CHECKING THE PURGE TANK AND VALVE SYS. UPON OPENING THE SIDE COWLING IT WAS FOUND THAT 1 END-CAP OF THESDR CA140521010Seat Track · cracked(CAN) DURING PHASE 3 INSPECTIONS, CABIN FLOOR SEAT TRACK SUPPORT BULKHEADS WERE FOUND CRACKED AT LT & RT FS 246.75 AND FS 265.75. SIRM CH 53-00-11-201 STATES STANDARD REPAIRS FOR CRACKS FOUND IN THESE FLOOR STRUCTURES. HOWEVER, RT FS 246.75 INITIAL CRACK FOUNSDR CA140506003Trunnion · cracked(CAN) DURING CLEANING OF THE LANDING GEAR, AME NOTICED WHAT LOOKED TO BE A CRACK AT THE UPPER TORQUE LINK ATTACH ON THE RT GEAR TRUNNION. PAINT WAS REMOVED, PART WAS INSPECTED AND A CRACK WAS FOUND. THE RT GEAR WAS INSPECTED AND A CRACK WAS FOUND IN THE SAMESDR CA140430007Hinge · cracked(CAN) THE PILOTS WERE PUSHING THE ACFT IN THE HANGER WITH THE CABIN DOOR CLOSED AFTER A FLIGHT WHEN THEY NOTICE THE DOOR HINGE WAS CRACKED. THEY REPORTED IT TO THE MAINTENANCE WHICH REMOVED THE DOOR AND FOUND 10 INCHES OF DOOR HINGE CRACKED ONLY ON THE DOOR HISDR HSRR201404150001Crossbeam · crackedDURING ROUTINE INSPECTION DISCOVERED A CRACK IN THE CROSS TIE RADIUS AT THE LOWER AFT SIDE OF THE RT EMERGENCY EXIT.SDR CA140402008Roller · worn(CAN) AFTER FINDING A FAILED ROLLER AND WORN INSIDE FLAP WALL, CHECKED ALL ACFT AND RT OTBD FLAP WAS FOUND OF THIS ACFT WAS ALSO FOUND WORE AND READY TO FAIL. BECAUSE OF HIGH CYCLES AND HOURS ON OUR ACFT EACH YEAR. WE WILL REMOVE ALL FLAPS AND REPLACE ROLLESDR CA140402004Arm · cracked(CAN) WHEN DISASSEMBLING THE RT ENGINE POWER LEVER ASSY FOR FRICTION BRAKE REPAIR A CRACK WAS OBSERVED IN THE ARM ASSEMBLY BUSHING, AROUND WHICH THE POWER LEVER AND THE FRICTION BRAKE PIVOT.SDR CA140326025Motor · failed(CAN) THE PILOTS SELECTED GEAR DOWN AND THE LANDING GEAR MOTOR CB POPPED. THEY MANUALLY EXTENDED THE GEAR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CAME TO TROUBLESHOOT THE PROBLEM AND FOUND POWER TO THE MOTOR. WHEN GEAR WAS SELECTED DOWN THEY HIT THESDR CA140401009Pump · failed(CAN) WHILE IN CRUISE, THE CREW OBSERVED TORQUE AND FUEL FLOW FLUCTUATIONS ON THE LT ENGINE. THIS WAS SHORTLY FOLLOWED BY THE ENGINE FAILURE. THE CREW SECURED THE LT ENGINE, DECLARED AN EMERGENCY. THE CREW DECIDED TO DIVERT. THE ACFT LANDED SAFELY. THE CUSTOMESDR CA140331010Pump · failed(CAN) IN CRUISE FLIGHT, THE LT ENGINE BEGAN TO SURGE AND THEN FLAMED OUT APPROXIMATELY 80NM FROM AIRPORT. THE LT ENGINE DRIVEN HP FUEL PUMP WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA140602012Engine · unknown(CAN) PILOT REPORTED A CHIP DETECTOR LIGHT ILLUMINATED FOLLOWED BY RISE IN ITT AND AN ENGINE WAS SHUTDOWN IN FLIGHT. THE ON GROUND TROUBLESHOOTING REVEALED A MAJOR QUANTITY OF FERROUS METAL DEBRIS ADHERED TO CHIP DETECTOR MAGNETS. THE ENGINE WAS SENT FOR INVESSDR CA140402007Bearing · worn(CAN) THE ACFT WAS COMING IN TO LAND AND WHEN APPROACH FLAPS WERE SELECTED, THE ACFT ROLLED SLIGHTLY. THE PILOT LANDED THE ACFT WITHOUT NO OTHER PROBLEMS. THE PILOT CHECKED THE FLAPS AND FOUND THE RT OTBD INNER ROLLER HAD FAIL AND RUBBED THOUGH THE INSIDE WALSDR CA140318015Fcu · surges(CAN) CLIMBING THROUGH 18000` THE LT ENGINE SURGED WITH THE TORQUE NEEDLE GOING JUST OVER THE REDLINE. THE PILOTS RETARDED THE POWER AND THE TORQUE DROPPED. THE ENGINE SURGED A SECOND TIME AND THE TORQUE HIT AND STAYED AT 2450 FT/LBS WITH NO THROTTLE RESPONSSDR CA140318013Hub · damaged(CAN) DURING A ROUTINE 200HR PHASE INSPECTION, 1 OF THE LOW PITCH STOP ROD COLLARS WAS FOUND TO BE CRACKED THROUGH ON THE NR 2 PROPELLER. THE PROPELLER WAS CHANGED OUT WITH AN O/H PROPELLER AND SENT TO A REPAIR FACILITY.SDR HSRR2014021200070Windscreen · crackedDURING CRUISE AT 26000 FT, RT WINDSCREEN INNER PANE SHATTERED. HEAT WAS ON SINCE TAKEOFF. NO LOSS OF PRESSURE AS OUTER PANE HELD.SDR CA140127012Skin · cracked(CAN) A 3.5" CRACK WAS FOUND ON A REGULAR SCHEDULED PHASE INSPECTION. ON INVESTIGATION IT WAS DISCOVERED THAT THE EMERGENCY EXIT DOOR WAS OUT OF ALIGNMENT WHICH MAY HAVE PUT PRESSURE ON THE EXIT DOOR.SDR ENHA20140103Autopilot Sys · malfunctionedAFTER REACHING A CRUISE ALTITUDE OF 4000 ON AN IFR FLT THE AUTOPILOT BEGAN TO MALFUNCTION. THE PILOT OBSERVED THE COMMAND BARS ON THE FLIGHT DIRECTOR GOING OUT OF VIEW & ALTITUDE STARTING TO GRADUALLY DESCEND. AT THIS POINT THE PILOT ATTEMPTED TO CORRECT THESDR CA131219023Clevis · cracked(CAN) DURING PHASE 1 INSPECTIONS, LDG CLEVISES REMOVED FOR REQUIRED DVI. CLEVISES ALSO SENT FOR NDT INSPECTION, IAW ADDITIONAL INSPECTION PROGRAM. CLEVISES SENT FOR NDT MAGNETIC PARTICLE INSPECTION. 1 MLG CLEVIS FAILED THIS NDT INSPECTION, AS IT WAS FOUND CRASDR CA131216011Engine · power loss(CAN) DURING SHORT FINAL APPROACH, THE CO-PILOT OBSERVED FIRE/SPARKS COMING FROM THE EXHAUST STACK ON THE R/H ENGINE, AND HEARD TWO SHORT SERIES OF BANGS. A BRIEF LOSS OF POWER WAS ALSO EXPERIENCED. THE ALTITUDE WAS 500FT AT THIS POINT, SO THE CREW SAFELY LANDSDR MFG2013F00000Amplifier · malfunctionedWITH NO PASSENGERS THE PILOTS EXPERIENCED A LOUD SQUEALING IN THEIR HEADSETS SO THEY TURNED OFF ALL ENVIRONMENTALS & THE NOISE WENT AWAY. THEY TURNED AROUND & WERE COMING BACK TO DEPARTURE, WHEN THEY SMELLED WHAT THEY THOUGHT WAS SMOKE. THEY DECLARED AN EMERSDR CA131201002Engine · power loss(CAN) DURING CLIMB THROUGH FL150, THE ENGINE TORQUE DROPPED FROM 1800 TO 600 FT-LB FOR APPROXIMATELY 3 TO 4 SECONDS. POWER RESTORED WITHOUT PILOT INTERVENTION. THIS OCCURRED APPROX 4 OR 5 TIMES WITH FUEL FLOW, COMPRESSOR SPEED AND TORQUE FLUCTUATING TOGETHER.SDR 2013FA0000773Skin · damagedLEFT CENTER WING, JUST FWD OF SPAR CAP, AND JUST INBD OF NACELLE. THE SKIN HAS MULTIPLE PULLED THROUGH RIVETS THAT ATTACH THE SKIN TO THE SPAR, MOSTLY ON OTBD AFT AREA, INSTALLED NEW RIVETS. HAVE HAD THIS PROBLEM ON MULTIPLE MILITARY SERIES ACFT. IN THE LASSDR VQMA20131108001Engine · malfunctionedINFLIGHT , RT ENGINE TORQUE GAGE BEGAN TO FLUCTUATE ON THE RETURN LEG BACK TO DEPARTURE. WITHIN TWO MINUTES, RT ENGINE OIL PRESSURE GAGE STARTED TO FLUCTUATE AS WELL. FLUCTUATED BETWEEN 100PSI, AND 50PSI RAPIDLY. A MINUTE OR TWO LATER THE RT OIL PRESSURE GSDR F2PA20131126001Duct · unserviceableLEFT BLEED AIR FAIL WARNING LIGHT ILLUMINATED IN FLIGHT. RETURNED TO AIRPORT WITH LT BLEED AIR TURNED OFF IAW POH. NO BLEED LEAK WAS FOUND & THE WARNING SYS WAS RESTORED. ON A SECOND OCCASION, 1.5 FLIGHT HOURS LATER, WHILE ON THE GND DURING TAXI IN FROM A FLSDR CA131103002Gyro · failed(CAN) ON A ROUTINE DESCENT, THE CREW NOTED THAT THE RT ATTITUDE GYRO TOPPLED AND BECAME UNSERVICEABLE. MAINTENANCE REPLACED THE UNIT AND THE SYS WAS GROUND FUNCTION CHECKED SERVICEABLE.SDR CA131018012Propeller · overserviced(CAN) WHEN CONDUCTING DE-ICE SYSTEM FUNCTION TESTS HIGHER THEN NORMAL AMP READINGS OR INTERMITTENT AMP READING HAD BEEN NOTED. UPON FURTHER INVESTIGATION THE DE-ICE BRUSH BLOCK AND SLIP RING WAS CONTAMINATED WITH FLUID FROM PROPELLER. SEE PHOTO ATTACHED 1 AND SDR CA131103005Window · failed(CAN) ON CLIMBOUT THE CREW SELECTED WINDSHIELD HEAT ON IN ANTICIPATION OF ICE. IMMEDIATELY THE RT WINDSCREEN SHATTERED, CREW RETURNED TO POINT OF DEPARTURE. MAINTENANCE REPLACED THE WINDSCREEN AND THE SYSTEM FUNCTION CHECKED SERVICEABLE.SDR CA130925008Balance Weight · separated(CAN) ON TAKEOFF THE PILOT NOTICED SUBSTANTIAL AIRFRAME VIBRATION THAT DISSIPATED WHEN CLIMBING THROUGH 1000 AGL. SUSPECTED NOSE WHEEL/TIRE ASSY DISTRESS. THE FLIGHT WAS DIVERTED TO HOME BASE FOR PRECAUTIONARY MEASURES WHERE AN UNEVENTFUL LANDING OCCURRED. SDR CA131103004Gyro · failed(CAN) ON CLIMB OUT THE CREW NOTICED THE RT ATTITUDE GYRO HAD BECOME UNSERVICEABLE. THE FLIGHT CONTINUED WITH OUT INCIDENT TO DESTINATION. MAINTENANCE REPLACED THE GYRO AND THE SYSTEM WAS GROUND FUNCTION CHECKED SERVICEABLE.SDR CA131104004Receiver · failed(CAN) ON A ROUTINE FLIGHT THE CREW NOTED THE NAV 2 SYSTEM FLAGGED UNSERVICEABLE. THE NAV RECEIVER WAS REPLACED WITH NEW AND THE SYS GROUND FUNCTION CHECKED SERVICEABLE.SDR CA130830016Actuator · cracked(CAN) DURING INSPECTION MAINTENANCE NOTICE END CAP ON NOSE ACTUATOR WAS CRACKED. ACTUATOR WAS R & R WITH A NEW ACTUATOR, GEAR SWUNG.SDR CA131104003Bladder · leaking(CAN) AFTER SERVICING THE ACFT WITH FUEL THE CREW NOTICED A SMALL FUEL LEAK DEVELOPED ON THE RT WING. MAINTENANCE REPLACED THE FUEL BLADDER AND THE SYS WAS FUNCTION CHECKED SERVICEABLE. NOTE THE FUEL BLADDER WAS ORIGINAL 1988 AND LAST INSTALLED AT THE FACTORSDR CA130809006Amplifier · misinstalled(CAN) THE AIRCRAFT EXPERIENCED AUDIO CONTROL ISSUES ON A ROUTINE FLIGHT FROM YEG TO YMM, MAINTENANCE WAS CALLED OUT AND VERIFIED THE AUDIO AMP HAD FAILED. THE AMP WAS REPLACED AND THE AUDIO SYSTEM WAS GROUND FUNCTION CHECKED SERVICEABLE. ON AUG 6, 2013 THE AISDR CA130820002Display · inoperative(CAN) PILOT`S PFD FAILED TO INITIALIZE ON START-UP. TROUBLESHOOTING FAILED TO INITIALIZE SCREEN. SCREEN EXCHANGED WITH O/H UNIT. NEW SCREEN INSTALLED AND SYS FOUND SERVICEABLE. NO SIGNS OF ANY CONTAMINATION ON THE EXTERIOR OF THE OLD SCREEN. UPON RECEIPT SDR CA131103003Gyro · failed(CAN) ON CLIMBOUT THE CREW NOTICED THE RT ATTITUDE GYRO HAD BECOME UNSERVICEABLE. THE FLIGHT CONTINUED WITH OUT INCIDENT TO DESTINATION. MAINTENANCE REPLACED THE GYRO AND THE SYSTEM WAS GROUND FUNCTION CHECKED SERVICEABLE.SDR CA130805012Engine · fluctuates(CAN) PRIOR LANDING THE PILOT OBSERVED ENGINE PARAMETERS FLUCTUATION THEN THE ENGINE SHUTDOWN ITSELF. THIS IS A RECURRENT ISSUE. ENG REP WILL INVESTIGATE THE IFSD. AT INITIAL OCCURRENCE AN FCU REPLACEMENT WAS CONDUCTED.SDR WAIA2013F00148Lamp · inoperativeFLIGHT CREW NOTED ON LONG FINAL APPROACH, MLG EXTENDED AND LT MAIN GREEN LIGHT DID NOT ILLUMINATE. OPTED TO CYCLE MLG ONE TIME WITH SAME RESULT. LOW APPROACH & VIEWING FROM TOWER. TOWER REPORTED ALL THREE GEARS APPEARED DOWN. AFTER REACHING 3000 AGL, LT MAISDR CA130709012Engine · contaminated(CAN) ON APPROACH FLIGHT, CREW NOTICED A CHIP DETECTOR WARNING LIGHT ON THE RT ENGINE. ACFT LANDED WITHOUT A PROBLEM, MAINTENANCE WAS NOTIFIED. COWLS WERE REMOVED, CHIP PLUG PULLED, METAL WAS FOUND ATTACHED TO MAGNETIC PINS ON PLUG. ENGINE WAS REMOVED AND O/SDR 2013FA0000347Pump · failedLEVEL CRUISE ENROUTE AT 25K FEET WHEN THE LT ENGINE LOST POWER. LT FUEL FLOW DROPPED TO ZERO. PILOT FEATHERED LT PROP AND FOLLOWED EMERGENCY PROCEDURES. ATTEMPTS TO RELIGHT FAILED. DIVERTED. MX PERSONNEL REPORTED THAT THE LT ENGINE FUEL PUMP SHAFT FAILED.SDR CA130612007Drive Shaft · worn(CAN) DURING ENGINE UPGRADE, COMPLETED AT ELLIOTT AVIATION CRS KX5R005N, IAW BLACKHAWK STC SA10737SE THE COMPRESSOR QUILL DRIVE SHAFT WAS NOT REPLACED BY SHAFT PN 117-910058-5 AS DETAILED IN BLACKHAWK DWG 06010001 REV B AND SB21-3303 R1. THE SHORTER -3 SHAFT ESDR CA130605010Circuit Breaker · tripped(CAN) ON TAXI CHECKS THE CREW NOTICED THE CVR SYSTEM DID NOT TEST AND THE CIRCUIT BREAKER HAD POPPED. MAINTENANCE REPLACED THE CVR WITH A SERVICEABLE UNIT AND GROUND FUNCTION CHECKED THE SYSTEM SERVICEABLE. (TC# 20130605010)SDR CA130604011Relay · tripped(CAN) THE PILOTS WASHED THE AIRCRAFT AND THEN GOT A DISPATCH (THE FLAPS WHERE DOWN FOR WASHING). ON THE TAXI OUT THEY SELECTED FLAPS UP BUT DID NOT NOTICE THE FLAPS HAD ONLY CAME UP TO APPROACH BEFORE THE CIRCUIT BREAKER POPPED FROM THE FLAP SYSTEM. THEY TOOK SDR CA130530002Control Lever · malfunctioned(CAN) DURING T/O AND INITIAL CLIMB, THE PROPELLER WAS NOT MAINTAINING STEADY RPM. THE PROP. LEVER WAS SET TO FEATHER BUT THE PROPELLER DID NOT FEATHER UNTIL LATER ON FINAL APPROACH, DURING THE RETURN TO THE AIRPORT. AN UNEVENTFUL LANDING FOLLOWED. TROUBLESHOOTSDR CA130522004Actuator · cracked(CAN) DURING WALK AROUND, FLIGHT CREW NOTICED THAT THERE WAS HYDRAULIC FLUID ON NOSE GEAR ACTUATOR. MAINTENANCE WAS NOTIFIED, ACFT WAS JACKED, GEAR WAS SWUNG, ACTUATOR INSPECTED FOR LEAKS. AFTER SEVERAL GEAR SWINGS FLUID WAS FOUND TO BE LEAKING FROM END CAP.SDR 2013FA0000276Windshield · failedIN LEVEL CRUISE FLIGHT, WITH WINDSHIELD HEAT ON. THE CO PILOT WINDSHIELD INNER PLY CRACKED/SHATTERED. A NORMAL LANDING WAS MADE FOLLOWING THE ABNORMAL CHECKLIST FOR A FAILED WINDSHIELD. NO INJURIES AND NO OTHER DAMAGE OR PRESSURIZATION LOSS WAS EXPERIENCED.SDR CA130503005Beta Ring · cracked(CAN) DURING INSTALL OF HOT SECTION INSPECTION, AME NOTICED THAT THE PROP BETA RING HAD A CRACK ON THE AFT FACE, ON FURTHER INSPECTION ANOTHER CRACK WAS FOUND. BETA RING WAS REMOVED AND A SERVICEABLE RING INSTALLED. AT THIS TIME IT WAS NOTED THAT THE INSTALL PSDR CA130507007Spring · weak(CAN) WHILE TAXING IT WAS NOTICED THAT IT WAS HARD TO TURN. WE REMOVED THE STEERING SPRING AND NOTICED IT WAS SHORTER THAN THE NEW ONE, MAKING IT WEAKER. WE INSTALLED A NEW SPRING AND TESTED THE STEERING AND FOUND IT WAS GOOD.SDR CA130430009Engine · power loss(CAN) THE FLIGHT CREW REPORTED NG DROP DURING CRUISE WITH THE PROP RPM AT 1700 AND PULLING BACK ON THE POWER LEVERS TO APPROXIMATELY 1100 ON BOTH ENGINES. THE RIGHT ENGINE DROPPED TO 300 LBS OF TORQUE AND THE FUEL FLOWS DID FOLLOW. THE AIRCRAFT DID YAW AND THESDR CA130604010Hsi · failed(CAN) ON THE CLIMB OUT ON A ROUTINE FLIGHT, THE CO-PILOT REPORTED THE RH HSI IMAGE BECAME DISTORTED AND UNREADABLE. THE CAPTAIN FLEW THE AIRCRAFT FOR THE REMAINED OF THE FLIGHT HOME FROM THE LH SIDE WITH OUT INCIDENT. MAINTENANCE REPLACED THE HPU UNIT AND THE
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