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 CA120726010Inverter · failed(CAN) ON A ROUTINE FLIGHT, THE CREW NOTED THAT NR 1 INVERTER BECAME UNSERVICEABLE. THE INVERTER WAS REPLACED WITH AN O/H UNIT AND THE SYS WAS FUNCTION CHECKED SERVICEABLE.SDR CA120726008Transducer · malfunctioned(CAN) DURING CLIMB POWER FLIGHT, CREW REPORTED THAT THE RT TORQUE GAUGE WOULD INTERMITTENTLY FLUCTUATE. MAINTENANCE REPLACED THE TORQUE TRANSDUCER WITH A NEW UNIT AND THE PROBLEM WAS RECTIFIED.SDR CA120717014Bladder · failed(CAN) ONCE THE ACFT WAS SERVICED WITH FUEL, THE CREW NOTED FUEL LEAKING FROM THE WHEEL WELL AREA, MAINTENANCE WAS CALLED, THEY TIGHTENED A FEW FITTINGS THAT WERE FOUND TO HAVE BEEN WEEPING AND THE LEAK APPEARED TO HAVE BEEN STOPPED. THE CREW FLEW THE ACFT TO DSDR CA120717013A/C Pack · malfunctioned(CAN) ON A ROUTINE FLIGHT, THE CREW NOTICED THE ACFT WAS ONLY MAINTAINING 3.2 PSI CABIN DIFFERENTIAL. THE CREW REQUESTED LOWER TO 15,000 FT AND CONTINUED TO DESTINATION WITHOUT INCIDENT. MAINTENANCE DISCOVER A WEAK FLOW PAC, THE FLOW PAC WAS REPLACED AND SEVESDR 2012FA0000481Blade · looseDURING SECOND ENGINE START OF THE DAY, THE RT PROP STARTED VIBRATING. START WAS ABORTED AT APPROX 40 PERCENT N1. ON INSPECTION OF PROPELLER, FOUND 3 BLADES FEATHERED AND IN LOW PITCH. NR 1 BLADE COULD BE REPOSITIONED BY HAND. REMOVED PROPELLER AND SENT FORSDR CA120702004Engine · warning light(CAN) PASSING THROUGH 18,000 FT THE PILOT REPORTED A MOMENTARY INDICATION OF THE CHIP DETECTOR LIGHT, WHICH THEN EXTINGUISHED ITSELF. A SHORT TIME AFTER THIS THE PILOT NOTICED TORQUE FLUCTUATIONS FROM THE ENGINE. THE PILOT INITIATED AN ENGINE SHUTDOWN, HOWEVSDR CA120628010Altimeter · failed(CAN) ON A ROUTINE FLIGHT, THE PILOT NOTED THAT THROUGH ROTATION THE NR 1 ALTIMETER FAILED IN THE CLIMBOUT. THE CREW DID NOT REALIZE THAT THERE WAS A SWITCH LOCATED IN THE COCKPIT TO SELECT WITCH ENCODING ALTIMETER THAT PROVIDES THE MODE C. THEREFORE THE ACFSDR M20A2012F00112Hydraulic Line · leakingLEAK IN LANDING GEAR HYD LINE COMING FROM THE HYD POWER PACK IN LT WING CENTER SECTION GOING TO THE RT LG BEFORE THE SPLIT TO THE NLG. THE LEAK OCCURED UNDER THE INTERIOR FLOORBOARD CAUSING THE LANDING GEAR RELAY TO POP. LEVELED THE AIRCRAFT AT 12,000 FEET ASDR CA120604017Fuel Control · malfunctioned(CAN) ON CLIMBOUT, THE PILOTS REPORTED THAT THROUGH 18,000 FT THE POWER LEVERS WOULD DEVELOPED A 3 KNOB SPLIT AND THE RT ENGINE WOULD HAVE A ITT, TEMPERTURE INCREASE OF 35 DEGREES. ONCE THE ACFT REACHED DESIRED ALTITUDE, THE POWER LEVERS WOULD MATCH UP OVER TSDR CA120627016Indicator · malfunctioned(CAN) ON A ROUTINE FLIGHT, THE CO-PILOT ATTITUDE INDICATOR BECAME UNSERVICEABLE DURING THE DECENT, APPROACH. THE CAPTAIN TOOK CONTROL OF THE ACFT AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED AND FUNCTION CHECKED THE SYS SERVICEABLE.SDR CA120524010Angle · cracked(CAN) FATIGUE CRACK FOUND VISUALLY DURING PHASE INSPECTION IN ANGLE,. INBD ANGLE ATTACHING RT-MLG ACTUATOR SUPPORT HSG TO FWD SIDE OF WING SPAR.SDR CA120601008Armature · shorted(CAN) AFTER LANDING, CREW STARTED BOTH ENGINES FOR DEPARTURE BUT COULD NOT GET THE LT GENERATOR TO COME ONLINE. CREW SHUTDOWN TO ADVISE THE MAINTENANCE DEPT. THEY WENT BACK TO THE ACFT TO DO SOME TROUBLESHOOTING, STARTED THE RT ENGINE THEN TRIED TO START THE SDR 2012FA0000316Sun Gear · wornPOWER SECTION SUN GEAR FAILED AS ALL TEETH WORE OFF CAUSING FAILURE OF THE POWER SECTION AND BOTH POWER TURBINE DISKS TO BREAK LOOSE CAUSING ADDITIONAL COLLATERAL DAMAGE TO THE POWER SECTION, EXHAUST DUCT AND COMPRESSOR TURBINE DISK ASSY. INCIDENT HAPPENED ONSDR CA120417016Cross Tie · cracked(CAN) WHILE DOING A STRUCTURE INSPECTION, IT WAS NOTICED THAT THE CROSS TIE WAS CRACKED HALF WAY UP INBD AFT. THIS IS A HIGH TIME ACFT.SDR CA120417015Cross Tie · cracked(CAN) WHILE DOING A STRUCTURE INSPECTION, WE NOTICED THAT THE CROSS TIE WAS CRACKED HALF WAY UP ON THE AFT INSIDE OF THE EMERGERCY WINDOW ON THE RT SIDE ON THE FUSELAGE.SDR CA120417014Latch · cracked(CAN) WHILE DOING A MAJOR INTERNAL INSPECTION, IT WAS NOTICED THAT 1 UPPER WELDED LATCH WAS CRACKED. WE INSPECTED THE OTHER UPPER LATCH AND FOUND IT WAS CRACKED ALSO.SDR CA120417013Channel · worn(CAN) WHILE DOING AN INSPECTION, IT WAS NOTICED THAT THE CHANNEL WAS WORN THOUGH AT THE AFT TOP OF THE DOOR FRAME.SDR CA120417010Heater · cracked(CAN) DURING INSPECTION IT WAS NOTICED THAT THE BACK OF THE HEATED LIP WAS CRACKED ARCOSS FROM TOP TO BOTTOM . THE OTHER SIDE WAS INSPECTED AND ALSO FOUND CRACKED 2 TIMES IN THE SAME LOCATION.SDR CA120331001Wire · damaged(CAN) THE ACFT WAS RELEASED GROUND FUNCTION CHECKED SERVICEABLE FROM A PHASE INSPECTION AND A FEW UNSCHEDULED MAINTENANCE TASKS. IN TOTAL,THE ACFT WAS IN MAINTENANCE FOR SEVEN DAYS. ONCE RELEASED BACK TO THE FLIGHT LINE, ON THE ACFT`S FIRST FLIGHT THE CREW NOTSDR CA120328005Powerpack · failed(CAN) WHEN LANDING GEAR WAS SELECTED FOR LANDING, THE 2 AMP LANDING GEAR CONTROL C/B POPPED. CREW TRIED TO RESET IT BUT COULD NOT. GEAR WAS MANUALLY EXTENDED AND AIRCRAFT LANDED WITHOUT INCIDENT. ACFT WAS JACKED, SYS WAS CHECKED BY MAINTENANCE AND FOUND THATSDR CA120326010Indicator · failed(CAN) ON A ROUTINE FLIGHT, ELECTRICAL SMOKE FUMES WHERE NOTICED IN THE CABIN, PILOT INSPECTION REVEALED THE TURN CO-ORDINATOR WAS FLAGGED UNSERVICEABLE. THE CREW PULLED THE CIRCUIT BREAKER FOR THE TURN CO-ORDINATOR AND CONTINUED ON THE FLIGHT AS PLANNED, THESDR CA120326007Indicator · malfunctioned(CAN) ON APPROCH, THE FLIGHT DIRECTOR WAS "LAZY" THE VERTICIAL GYRO WAS REPLACED, SYSTEM WAS FUNCTION CHECKED SERVICABLE. (TC# 20120326007)SDR CA120326009Impeller · damaged(CAN) ACFT WAS BROUGHT IN FOR A PHASE INSPECTION, PILOTS REPORTED IMMEDIATELY THAT THE BRAKES WHERE SOFT. AS THE AME`S GOT DEEPER INTO THE INSPECTION IT WAS REVEALED THAT THE INTAKES WHERE SEVERELY SAND BLASTED AND THE NOSE WHEEL BEARINGS WHERE GRINDING, FULLSDR CA120309005Bearing · worn(CAN) DISCOVERED FLEETWIDE PROBLEM WITH THE OTBD FLAPS, INBD AFT HINGE, OTBD RIB BRACKET. THE FLAP ROLLER BEARING, PN BC56985, CAN WEAR, ALLOWING THE BEARING FLANGE TO CONTACT AND WEAR THE FLAP RIB, CALLED A BRACKET, PN 35-165050-30 AND -31. ALL 5 COMPANY ACSDR CA120307004Bearing · rough(CAN) BEARING ROUGH. CENTER PORTION MIGRATED TO OR WAS MFG BELOW THE SURFACE OF FLANGE CAUSING DAMAGE TO ADJACENT BRACKET. DISCOVERED WHEN FLAP WAS REMOVED FOR UNRELATED REASON.SDR CA120222007Actuator · inoperative(CAN) LT MAIN ENGINE ANTI-ICE CIRCUIT BREAKER POPPED. AFTER RESET ON THE GROUND, IT POPPED WITHIN 2 SECONDS AGAIN". STANDBY MODE SERVICEABLE. ACTUATOR FUNCTION CHECKED AND FOUND INOPERABLE IN "MAIN ANTI ICE OFF" SELECTION, ALL OTHER 3 SELECTIONS SERVICEABLESDR CA120220010Gyro · stuck(CAN) AFTER LANDING AND AFTER TURNING OFF THE TAXI WAY, THE CO-PILOT NOTICED HIS DG WAS STUCK IN ONE POSITION. THE DG WAS R & R AND THE SYS WAS GROUND FUNCTION CHECKED SERVICEABLE.SDR WAIA2012F00057Cap · leakingFLIGHT CREW REPORTED AN ANOMALY WITH THE RT BRAKE ON LANDING. MX FOUND NO OBVOIUS DAMAGE TO THE BRAKES, BUT DURING BLEEDING OF THE BRAKE SYS, AIR WAS DISCOVERED TO BE PRESENT IN THE SYS. BRAKES PROPERLY BLED AND BRAKE SYS WAS TESTED ON GROUND, NO DEFECTS NOTESDR CA120125017Switch · failed(CAN) FLIGHT CREW HAD A BLEED AIR WARNING LIGHT DURING FLIGHT. SYSTEM WAS TROUBLESHOT AND PROBLEM WAS FOUND TO BE THE BLEED AIR WARNING SWITCH HAD AN INTERNAL FAILURE. SWITCH, PN 90-380002-3 WAS REPLACED WITH NEW AND SYS GROUND TESTED SERVICEABLE.SDR 7EMA201214010512Fire Detector · false activationAT 17:36 ACFT LIFTED OFF FROM RUNWAY AND WAS CLIMBING IN THE RT TURN DIRECT HEADING OF 300. PROPS WERE AT 1900 AND ALL ENGINE INDICATIONS WERE NORMAL. THE SUN WAS JUST SETTING AT 10 O'CLOCK POSITION. AFTER LEVELING OFF AND BEGINNING TO ADJUST PROPS TO 1700,SDR CA120106007Hinge · cracked(CAN) DURING AN INSPECTION, MAINTENANCE FOUND CRACKS IN THE SKIN COMING OUT OF THE RADIUS OF THE NLG FORWARD HINGE CUTOUTS ON BOTH THE LH & RH SIDE. WE BELIEVE THIS HAS HAPPENED OVER TIME WITH THE OPERATION OF THE NLG DOORS.SDR HSRR2011122800001Structure · crackedCRACKS INSIDE DOOR STRUCTURE FOUND.SDR CA111228009Brush Block · failed(CAN) ON DESCENT, IT WAS NOTICED THAT CYCLE WAS READING ZERO FOR THE PROP DE-ICE SYSTEM. THE DECENT AND LANDING CONTINUED WITHOUT INCIDENT. UPON FURTHER INSPECTION MAINTENANCE FOUND THE BRUSH HAD FAILED FOR THE PROP HEAT ON THE LT SIDE. THE BRUSH WAS REPLACESDR CA111219019Skin · damaged(CAN) WHILE DOING A 10,000 CYCLE INSPECTION, IT WAS NOTED THAT THE RT UPPER WING INBD SKIN HAD SEVERAL COUNTER SUNK RIVETS PULL THROUGH OR ABOUT TO PULL THROUGH. IT IS DISCOVERED THAT THE MFG DID NOT USE ANYTHING TO BOND THE SKINS AT ASSY. THIS CAUSED THE RISDR CA111219014Gyro · used(CAN) ON A ROUTINE FLIGHT, PILOT REPORTED THAT THE FLIGHT DIRECTOR SHOWS 15-20 DEGREE BANK IN LEVEL FLIGHT. MAINTENANCE FAULTED THE VERTICIAL GYRO, SN 461. REPLACED WITH SERVICABLE UNIT SN 2379, SYS GROUND FUNCTION CHECKED SERVICABLE.SDR CA111219007Igniter · failed(CAN) NEW IGNITORS WERE INSTALLED AT PHASE INSPECTION, 26 HRS PRIOR AND FAILED ON A ROUTINE START. PILOT REPORTED DURING RT ENGINE START TO ENGINE WOULD STABLIZE AT 16 PERCENT THEN NOT LIGHT OFF. HE REPORTED TO HAVE TRIED THE START SEQUANCE 3 TIMES BEFORE DESDR CA111219013Gyro · malfunctioned(CAN) ON A ROUTINE FLIGHT PILOT REPORTED LT EADI INDICATING A 5 DEGREE AND THEN DRIFTED TO A 10 DEGREE BANK ANGLE IN FLIGHT, WHEN ACFT WAS CONFIRMED LEVEL. AN AVIONICS SHOP LTD WAS CONTRACTED VIA PURCHASE ORDER TO TROUBLESHOOT AND REPAIR AS NESSECARRY. SHOP FSDR K5LA2012F00000Starter Gen · inoperativeTHE LEFT STARTER WOULD NOT ROTATE ENGINE, MX TROUBLESHOT AND FOUND STARTER/GENERATOR INOPERATIVE. REPLACED WITH O/H UNIT AND ENGINE STARTED ON NEXT ATTEMPT.SDR CA111118011Stator Vane · cracked(CAN) DURING HOT SECTION INSPECTION THE FIRST STAGE PT STATOR HAD VANE AND INNER RING CRACKS THAT EXCEEDED MM LIMITS. PART WAS REPLACED WITH O/H LIKE PART.SDR CA111118010Liner · cracked(CAN) 400 HR FUEL NOZZLE CHECK BOROSCOPE INSPECTION OF HOT SECTION COMPONENTS REVEALED CRACKS IN OUTER COMBUSTION LINER THAT EXCEEDED MM LIMITS. LINER REPLACED WITH O/H PART.SDR CA111118009Gyro · malfunctioned(CAN) DURING A ROUTINE FLIGHT IT WAS NOTED DURING THE DESCENT AND APPROACH THE CO-PILOT DIRECTIONAL GYRO BECAME UNSERVICEABLE INDICATED BY A FLAG ON THE INSTRUMENT HEAD AND AN INCORRECT HEADING, THE FLIGHT AND LANDING CONTINUED WITHOUT COMPLICATIONS WHEN THE CSDR CA111117026Control Box · faulted(CAN) DURING A ROUTINE FLIGHT, IT WAS NOTED THE PROPELLERS WOULD NOT SYNCHRONIZE, THE PROPS WHERE SYNCHRONIZED MANUALLY AND THE FLIGHT CONTINUED WITHOUT COMPLICATIONS. MAINTENANCE FOUND A FAULTY PROPELLER SYNC CONTROL BOX, IT WAS R & R, THE SYSTEM GROUND FUNCSDR CA111117019Governor · failed(CAN) AIRCRAFT DEPARTED AND PILOTS NOTICED RT PROPELLER WOULD NOT INCREASE PAST 1900 RPM. TAKE-OFF RPM IS 2000 RPM. IN THE CLIMB IT WAS DECIDED THEY RETURN THE ACFT BACK TO DEPARTURE. TROUBLESHOT AND FOUND THAT THE RT ENGINE OVERSPEED GOVERNER, AIRFRAME COMSDR CA111026004Check Valve · unserviceable(CAN) DURING SCHEDULED PHASE 3 INSP, DECISION WAS MADE TO REMOVE AND INSPECT THE 2 PNEUMATIC SYS CHECK VALVES FOR CONDITION. FOUND TO BE UNSERVICEABLE DUE TO THE FLAPPER VALVE HINGE PIN WORKING LATERALLY UNTIL THE HINGE BECAME DISCONNECTED ON 1 PIVOT POINT. SDR CA111117006Windshield · delaminated(CAN) CO-PILOT WINDSHIELD DELAMINATED DURING CRUISE FL230.SDR CA111117008Windshield · cracked(CAN) PILOT SIDE WINDSHIELD CRACKED SHORTLY AFTER TAKEOFF, IN THE CLIMB.SDR CA111003013Hose · burned(CAN) AS THE AIRCRAFT CLIMBED THROUGH 14,000 FT, CABIN WOULD START CLIMBING AT THE RATE OF 1000 FT PER MIN AT 20,500 FEET, IT WOULD START WORKING PROPERLY. ON INSPECTING THE VENTURI, IT WAS NOTED THAT BOTH LINES THAT GO FROM THE VENTURI TO THE TEST PORTS IN SDR 2011F00205Wire · brokenCREW NOTICED NOSE GEAR LIGHT DID NOT INDICATE GREEN. CREW CHECKED BULB IT WAS GOOD. DID NOT HAVE A "RED" UNSAFE LIGHT AND WHEN FLAPS PUT TO "FULL" DOWN, NO GEAR WARNING HORN. TOWER SAID GEAR APPEARED DOWN BUT COULD NOT VERIFY IF IT WAS LOCKED. DIVERTED WHERESDR CA110907005Tube · leaking(CAN) THE SNAG WAS THE LOW BLEED LIGHT WARNING WAS COMING ON SOMETIMES IN FLIGHT. AFTER PRESSURIZING THE HOSE IT WAS NOTED THAT THE HOSE HAD A LEAK IN IT CAUSING THE PRE-SET SWITCH TO KICK ON.SDR 2011FA0000573Fuel Cell · leakingFOUND INBOARD LEADING EDGE FUEL CELL IN RT WING LEAKING AT RUBBER NIPPLE REINFORCEMENT FLANGE. THIS PMA FUEL CELL WAS INSTALLED 3 MONTHS AGO.
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