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 2018FA0000458Circuit Breaker · malfunctionedCOCKPIT SIDE PANEL LIGHT CIRCUIT BREAKER EMITTED SMOKE. FOUND MECHANICAL PRODUCTS 4200-002-5 BREAKER AT FAULT. AD 87-06-09 ADDRESSES THIS ISSUE. THE DATE CODE OF THIS BREAKER R8639 AND A PAINT MARKED T ON THE BREAKER END IS NOT APPLICABLE TO THIS AD.SDR O9IA201804190001Sensor · damagedDURING CRUISE FLIGHT, PILOT NOTED AN FAINT ELECTRICAL SMOKE ODOR. DETECTED IN THE CABIN AS WELL. TURNED BACK TO BASE. THE CREW IN THE BACK TRACED THE ODOR TO THE OVERHEAD PANEL THAT HOUSES THE AUTO TEMP SENSOR. THE PILOT THEN TURNED OFF THE AUTO TEMP MODE SDR G1IA201803100001Downlock Switch · loosePILOT REPORTED THAT WHILE ON FINAL APPROACH, PLACED THE GEAR HANDLE DOWN. IT FELT VERY MUCH LIKE A NORMAL EXTENSION. ON PERFORMING THE LANDING CHECKLIST, NOTICED THAT OF THE GREEN LIGHTS WERE ON. THE LNDG LIGHTS WERE REFLECTING OFF THE CLOUDS BACK INTO THE CSDR CA180314002Filler · leaking(CAN) AFTER STARTING THE RIGHT HAND ENGINE, THE PILOT OBSERVED THE ENGINE OIL PRESSURE WAS LOW (80PSI) AND FLUCTUATING +/- 5 PSI. THE PILOT PROCEEDED TO SHUT DOWN THE ENGINE AND OBSERVED THE OIL LEVEL WAS VERY LOW AND APPEARED TO HAVE LEAKED OUT THROUGH THE OSDR CA180207023Solenoid Valve · failed(CAN) AIRCRAFT REQUIRED LEFT RUDDER INPUT IN FLIGHT AND ON GROUND. MORE THAN NORMAL RUDDER TRIM REQUIRED IN FLIGHT. CORRESPONDING RUDDER BOOST SOLENOID VALVE FOUND FAILED IN OPEN POSITION CAUSING RUDDER BOOST TO ACTUATE SLIGHTLY DURING ALL PHASES OF OPERATIOSDR M9TR2018011001Gasket · leakingDURING THE REQUIRED PITOT STATIC SYSTEM TEST, THE STATIC SYSTEM WAS FOUND TO BE LEAKING BEYOND LIMITS. TROUBLESHOOTING FOUND THE PILOT AIRSPEED INDICATOR HAD A CASE LEAK. FOUND THE GASKET FOR THE FRONT GLASS WAS EXTRUDED. THE INDICATOR WAS JUST INSTALLED DURSDR GYWA20171213001Control Switch · bentAIRCRAFT FAILED TO PRESSURIZE. PILOT DESCENDED, CONTACTED ATC AND RETURNED TO DEPARTURE POINT (KMDD). AIRCRAFT PRESSURIZATION SYSTEM WAS GROUND TESTED AND OBSERVED TO OPERATE NORMALLY. THE PRESSURIZATION CONTROL SWITCH WAS OBSERVED TO BE DEFORMED PRESUMABLY BYSDR G1IA201711230001Filter · not reportedATTEMPTED TO PUT THE GEAR DOWN AND ONLY RECEIVED A NOSE GEAR GREEN LIGHT AND GEAR HANDLE RED LIGHT. CYCLED THE GEAR BUT HAD THE SAME RESULTS. EXECUTED THE EMERGENCY GEAR EXTENSION CHECK LIST. CONFIRMED 3 GREEN LIGHTS, HANDLE EXTINGUISHED. LANDED WITHOUT INCSDR 7EMA201708010001Bulb · burned outNO RIGHT MAIN LANDING GEAR DOWN AND LOCK INDICATION. FOUND BURNED OUT LIGHT BULB.SDR HSRR201706260001Unknown · odorPILOT REPORTED AN ODOR FROM THE AIR CONDITIONING VENTS UPON LANDING. THE AIRCRAFT WAS INSPECTED AND NO FAULTS WERE FOUND. THEY THEN TOOK IT ON A TEST FLIGHT AND COULD NOT DUPLICATE THE REPORTED ODOR.SDR 2017FA0000294Transducer · shortedAFTER DEPARTURE, THE FLIGHT CREW RECOGNIZED A LOW OIL PRESSURE INDICATION ON THE LEFT ENGINE. WHILE ABORTING THE FLIGHT AND RETURNING TO DEPARTURE, THE CAPTAIN ASKED FOR THE ABNORMAL CHECKLIST AND COPILOT RETRIEVED THE APPROPRIATE CHECKLIST AND COMPLETED THE CSDR 15MA2017060500001Skin · crackedDURING A VISUAL INSPECTION, LOWER FUSELAGE SKIN FOUND CRACKED AT RBL 11, BS 368.75 TO 389.75.SDR QMLA2017050117049Ahrs · malfunctionedWHILE FLYING IN IMC ENROUTE FROM JVY TO OWB, THE ATTITUDE, HEADING, REFERENCE SYSTEM AND AUTOPILOT FAILED IN FLIGHT. AT THE TIME OF THE FAILURE, THE AIRCRAFT WAS LEVEL AT 6,000 FT, AT 220 KIAS AND COUPLED TO THE AUTOPILOT IN NAV MODE AND ALTITUDE HOLD. PILOTSDR 2017FA0000354Diode · failedSELECTED THE GEAR DOWN AND ALL THE INDICATING AND TRANSIT LIGHTS FOR THE GEAR WENT OUT. RAN THE APPROPRIATE CHECKLIST AND PUMPED THE GEAR DOWN. DECLARED AN EMERGENCY AND RECEIVED VISUAL CONFIRMATION FROM THE TOWER THAT THE GEAR APPEARED DOWN AND LANDED WITHOSDR GAYA20170331001Service difficultyLANDING GEAR FAILED TO EXTEND AFTER GEAR WAS SELECTED TO THE DOWN POSITION.SDR HDNA2017030515Line · meltedPLASTIC TUBING "SENSE" LINE FOR BLEED AIR INDICATING ANNUNCIATION MELTED DUE TO IMPROPER ROUTING CAUSING THE BLEED AIR FAIL CAUTION TO ILLUMINATE.SDR 2016FA0000607Angle · corrodedINTERGRANULAR CORROSION FOUND IN AFT VERTICAL STABILIZER SPAR, LEFT AND RIGHT AFT SPAR CAP ANGLES, AT LOWER RUDDER HINGE BRACKET ATTACH LOCATIONS. LEFT AFT CHORD ANGLE ALSO CORRODED INTERGRANULAR APPROX. 5 INCHES BELOW UPPER HINGE FITTING LOCATION IN AFT FACE SDR DBCA2016112600007Pressure Switch · failed5 MINUTES AFTER TAKEOFF RIGHT SIDE BLEED AIR ANNUNCIATOR CAME ON DURING FLIGHT. CREW RETURNED TO DEPARTURE. LANDING WAS UNEVENTFUL. TROUBLESHOT AND FOUND BLEED AIR PRESSURE SWITCH FAILED. REPLACED THE SWITCH, OPS CHECKED GOOD.SDR G1IA20161112983C1Downlock Switch · faultyPILOT REPORTS, THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS SELECTED TO THE DOWN POSITION. WE CYCLED THE GEAR THREE TIMES TO NO AVAIL. PROCEEDED TO EMERGENCY GEAR DOWN PROCEDURES VIA CHECKLIST AND GOT A GREEN NOSE GEAR LIGHT. LANDED UNEVENTFULLY.SDR 2016FA0000384O-Ring · leakingLEFT ENGINE OIL LEAK. FOUND INBOARD OIL PRESSURE SCAVENGE LINE LEAKING AT O-RINGS. REPLACED THE O-RINGS, RAN ENGINE FOUND OIL LEAKING AT COUPLING. INSTALLED NEW COUPLING. INSTALLED IAW MM 79-20-01. SERVICED ENGINE WITH 5 QTS OF OIL. RAN ENGINE AND LEAK CHECKEDSDR G1IA2016080260701Wire · separatedCAPTAIN AND CO-PILOT HAD FLOWN UNEVENTFULLY AND JOINED THE DOWNWIND WITH THE INTENTION OF LANDING AT APPROXIMATELY 22:15, WHEN SELECTED THE DOWN POSITION WITH THE LANDING GEAR HANDLE AND THE LANDING GEAR REMAINED UP. NO GEAR HANDLE LIGHTS OR GEAR POSITION LIGSDR O9IA20060727001Gps · malfunctionedDURING FLIGHT, THE COPILOTS GPS LOST ALL OF ITS PRIMARY FLIGHT DATA AND DISPLAYED ALL RED X'S. THIS LASTED FOR JUST UNDER 2 MINUTES AND THEN RETURNED TO NORMAL ON ITS OWN. ON APPROACH, THE PILOTS GPS, AUDIO SELECTOR, AUTOPILOT, AND INVERTER ALL TRIPPED OFF LSDR G1IA2016071210742Switch · wornTHE MAIN LANDING GEAR DID NOT EXTEND NORMALLY ON APPROACH. HAD TO USE EMERGENCY GEAR EXTENSION PROCEDURE. AFTER GETTING 3 GREEN, GEAR DOWN INDICATION, LANDED NORMALLY. DID NOT DECLARE AN EMERGENCY. MAINTENANCE TROUBLESHOT CAUSE OF GEAR EXTENSION FAILURE AND SDR 3FFA2016060800001Relay · failedTROUBLESHOT AND FOUND FLAP MOTOR RELAY FAILED CLOSED WHERE IT WAS CONTINUOUSLY MAINTAINING POWER TO THE FLAP MOTOR. AFTER APPROXIMATELY 2.3 HOUR, PART 91 FLIGHT PILOT AND DOM STARTED ENGINE FOR RETURN FLIGHT HOME. APPROXIMATELY 45 SECONDS LATER THE CABIN STASDR VE7A2016060300001Rheostat · shortedFLIGHT CREW REPORTED "STRONG ODOR OF ELECTRICAL OVERHEATING FILLED CABIN ABOUT 10 MINUTES PRIOR TO LANDING. TUNRED OFF BLOWER. TURNED UP CABIN PRESSURE. ODOR DISSIPATED. MAINTENANCE NOTIFIED." UPON EXAMINATION OF THE ACFT, MAINTENANCE SMELLED RESIDUAL ODOR SDR CA160302013Bearing · seized(CAN) BEARINGS FOUND TO BE NON OPERATIONAL. GREASE DRIED OUT, BEARING BEGINNING TO BORE INTO ADJACENT BRACKET. SEE ALSO SDR 20120307004- SINCE 2012 HAVE CARRIED OUT FLAP REMOVAL AND INSPECTION OF BEARINGS AND BRACKETS EVERY 800 HOURS TO COINCIDE WITH PHASE 1 ISDR O9IA20160223001Fire Detector · failedLOG PAGE WRITE UP IS AS FOLLOWS, RT ENG FIRE LIGHT ON APPROACH & LANDING, STAYED ON AFTER ENG SHUTDOWN. INSPECTED THE ENG FOR ANY SIGNS OF FIRE & FOUND NONE. THE FIRE WARNING LIGHT REMAINED LIT DURING INSPECTION. FOLLOWING THE TROUBLESHOOTING GUIDE IN THE ASDR 2016FA0000091Landing Gear · malfunctionedLANDING GEAR FAILED TO EXTEND NORMALLY ON APPROACH. EMERGENCY GEAR EXTENSION ACCOMPLISHED. LANDED NORMALLY. FERRY PERMIT RECEIVED AND ACFT FLOWN TO REPAIR BS. REPAIR BS CYCLED GEAR 7 TIMES WITH NO FAULTS FOUND. REPAIR STATION VACUUMED AROUND LANDING GEARSDR CA160301012Engine · power loss(CAN) IN CRUISE, THE PILOT NOTICED THE LEFT ENGINE PARAMETERS DROP TO IDLE. POWER LEVER WAS BROUGHT TO IDLE DETENT THEN PUSHED BACK WITH NO RESPONSE. ENGINE KEPT IN IDLE WHILE AIRCRAFT WAS DIVERTED. IT LANDED WITHOUT INCIDENT.SDR CA160310004Panel · corroded(CAN) THE AIRCRAFT WAS ON DESCENT THE R/H DC GENERATOR FAILED THERE WAS ALSO A FAINT ODOR IN THE AIRCRAFT. MAINTENANCE PERSONAL DISCOVERED THE NR 6 RELAY PANEL HAD SHORTED DUE TO CORROSION . ALSO THE CONNECTOR FAILED DUE TO HEAT . ALL OTHER AIRCRAFT IN THE OPESDR J21R2016FA0000007Mount · brokenON INSPECTION, FOUND PIVOT MOUNT AFT MOUNT TO COMPRESSOR BROKEN. PILOT HAD FELT SOME VIBRATION PREVIOUS TO THE PIVOT MOUNT REPLACEMENT. NO OTHER COMPONENT DAMAGE FROM THE BROKEN PIVOT MOUNT BREAKAGE. REPLACED PIVOT MOUNT, NO FURTHER INCIDENT.SDR CA151218004Pivot · cracked(CAN) DURING PHASE INSPECTION THE AIR-CONDITIONER COMPRESSOR PIVOT PLATE WAS FOUND TO BE CRACKED NEAR THE MOUNTING LUG. THIS IS THE IMPROVED PIVOT PLATE MADE OF STEEL AS REFERENCED IN MFG COMMUNIQUE 97-002.SDR CA151217002Hinge · cracked(CAN) SEVERAL LOBES ON THE HINGE HAD CRACKED. WHEN THE DOOR WAS REMOVED IT WAS FOUND THE BRACKET 101-910022-22, BRACKET 101-910022021 AND THE ANGLE 101-910022-27 WERE ALSO CRACKED. THE DOOR ASSY WAS REPLACED AND THE SYS RIGGED IAW THE AMM. THESE CRACKS WERE SDR CA151204001Display · failed(CAN) DISPLAY FAILS WHEN DARK, SUSPECT PHOTO CELL.SDR HSRR2015120400620Skin · corrodedSEVERE CORROSION ON THE CENTER WING UPPER FUEL PROBE DISH AND THE UPPER SKIN AUXILIARY TANK DISH FLANGE.SDR CA151201006Engine · power loss(CAN) ON APPROACH, WITH POWER SET AT 400-500 FT/LBS, THE RT ENGINE TORQUE DROPS AWAY AND RETURNS MULTIPLE TIMES. TORQUE IS DROPPING AS LOW AS 150 LBS.SDR CA151110007Wheel · out of balance(CAN) PILOT REPORTED AIRFRAME VIBRATION AFTER TAKEOFF, THAT DISSIPATED SHORTLY THEREAFTER. NOSE WHEEL REMOVED AND DISASSEMBLED. FOUND 1.75 OUNCE RUBBER BALANCE WEIGHT HAD COME LOOSE FROM INSIDE THE TIRE. THESE BALANCE WEIGHTS ARE INSTALLED AT TIME OF TIRE MFGSDR CA160302008Oil System · leaking(CAN) PILOT REPORT THAT HE HAD JUST LEVELED OFF WHEN, THE COCKPIT FILLED WITH SMOKE. THERE WAS NO INDICATOR THAT ANYTHING WAS WRONG. PILOT RETURNED TO AIRPORT. UPON ARRIVAL IT WAS NOTICED THAT THERE WAS EXCESSIVE OIL LEAKING FROM THE ENGINE. THE COWLING WAS RESDR CA151022005Chip Detector · broken(CAN) PILOT REPORT THAT HE HAD JUST LEVELED OFF AFTER DEPARTURE FROM AIRPORT WHEN THE COCKPIT FILLED WITH SMOKE. THERE WAS NO INDICATOR THAT ANYTHING WAS WRONG. PILOT RETURNED TO AIRPORT. UPON ARRIVAL IT WAS NOTICED THAT THERE WAS EXCESSIVE OIL LEAKING FROM SDR CA151016011Screw · loose(CAN) MAINTENANCE WAS COMPLETING ROUTINE GEAR SWINGS ON KING AIR AND DISCOVERED THAT THE RT MAIN GEAR DOWN LOCK HOOKS WERE NOT FULLY ENGAGING ON THE DOWN LOCK PIN. UPON FURTHER INVESTIGATION THEY FOUND THE SET SCREW, WHICH SECURES THE PIN IN PLACE WAS LOOSE. WSDR CA151015016Blade · separated(CAN) IN FLIGHT SEPARATION OF APPROXIMATELY 1.3" OF BLADE TIP. CREW DID NOT NOTE ANY ABNORMAL PARAMETERS OR VIBRATION. LOSS WAS FOUND AFTER SHUTDOWN. THERE WAS NO EVIDENCE OF A PROP STRIKE. CRACK MAY HAVE ORIGINATED FROM A SMALL STONE SCUFF NEAR THE TIP. MSDR CA150925014Tube · corroded(CAN) THE TUBE FAILED DUE TO CORROSION. THIS TUBE IS A FREON CARRYING TUBE. THE CORROSION OCCURRED AT THE POINT WHERE THE EXPANSION VALVE SENSING COIL, COPPER, WAS IN CONTACT WITH THE TUBE ASSY, ALUMINUM. CAUSED LOSS OF ALL FREON FROM THE SYSTEM. OIL FROM THSDR CA150922012Engine · unknown(CAN) ACFT ENCOUNTERED A NR 2 ENGINE PROBLEM DURING A MISSED APPROACH. FLAMES APPEARED TO BE COMING FROM EXHAUST.SDR CA151006008Engine · power loss(CAN) CUSTOMER REPORTED THAT DURING THE MISSED APPROACH, THE NR 2 ENGINE DID NOT GENERATE FULL POWER DURING THE GO-AROUND MANEUVER. THE PILOTS NOTED LARGE FLAMES COMING-OUT FROM THE EXHAUST AND A SPIKE IN THE ITT OF THENR 2 ENGINE. THE FLIGHT CREW SECURED THESDR CA150814010Bleed Valve · faulty(CAN) THE AIRCRAFT COMMENCED TAKEOFF RUN AT ABOUT 1100 POUNDS OF TORQUE (ABOUT HALF OF TAKEOFF POWER) THE CREW NOTICED THAT THE RIGHT RUDDER BOOST HAD ACTIVATED AND REJECTED TAKEOFF AND EXITED THE RUNWAY AT TAXIWAY (LESS THAN HALF OF THE TOTAL RUNWAY AVAILABLESDR 2015FA0000449Fuel Tank · leakingSEVERAL HUNDRED LITERS OF FUEL LEAKED FROM SEVERAL RUBBER BLADDER FUEL TANKS, INBD BOX SECTION FUEL CELL, LOCATED IN THE ACFT'S RT WING ON AUGUST 8, 2015 WHILE IT WAS PARKED. 2 TANKS WERE REPLACED AND ALL OTHERS INSPECTED. ON SEPTEMBER 11, 2015, MORE FUEL LESDR CA150903004Actuator · stiff(CAN) THE CREW REPORTED A PAUSE ON GEAR RETRACTION AFTER TAKEOFF, HOWEVER, NO ABNORMALITIES OCCURRED DURING EXTENSION. LANDING GEAR SWINGS WERE COMPLETED IN THE HANGAR TO TROUBLESHOOT THE DEFECT AND IT WAS FOUND THAT THE DEFECT WAS RECREATED 2 TIMES OUT OF 8 SDR CA150731007Transistor · burned(CAN) ON APPROACH , FLIGHT CREW NOTICED THE ODOR OF ELECTRICAL SMOKE AND INFORMED THE TOWER OF THE SITUATION. THE ACFT LANDED, TAXIED TO HANGAR AND SHUTDOWN. AFTER CREW AND PASSENGER HAD LEFT THE AIRCRAFT, THE AIRPORT FIRE CREWS CHECKED FOR HOT SPOTS AND NONSDR CA150730017Tire · out of balance(CAN) DURING TAKEOFF, AFTER ROTATION A STRONG VIBRATION WAS FELT. THE VIBRATION CEASED AS THE LANDING GEAR FINISHED RETRACTING AND THE WHEEL SPIN UP HAD STOPPED. SUSPECTED WHEEL OUT OF BALANCE CONDITION. ACFT COMPLETED A CIRCUIT AND LANDED WITH NO INCIDENT. SDR 2015FA0000326Blower · burned outAFTER TAKE OFF, PASSING THROUGH 16,000 FEET, OBSERVED AND SMELLED SMOKE IN THE AIRCRAFT. IT APPEARED TO ME TO BE VERY LIGHT GREY SMOKE, AND HAD AN ACRID SMELL AND WAS SLIGHTLY IRRITATING TO THE EYES AND THROAT. THE MED CREW IN THE REAR SAID THEY COULD ALSO SEE
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