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 = 'B300C' 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 = 'B300C' 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 2026FA0000072Sensor · faultedDURING PREFLIGHT CHECKS, THE TEST FEATURE OF THE LIQUID LEVEL SENSOR WAS ACTIVATED & TESTED IAW THE BEFORE START CHECKLIST RESULTING IN A GOOD ACTIVATION TEST WITH A CAS MESSAGE ON THE MFD REPORTING HYD LOW LEVEL AS IT SHOULD. THE TEST FUNCTION WAS DEACTIVATEDSDR NOZR72024BBleed Valve · failedTHE FLIGHT CREW REPORTED THE NO:1 ENGINE BEGAN POPPING AND LOST 50% OF ITS POWER 11 MINUTES AFTER TAKEOFF. AN UNSCHEDULED LANDING WAS PERFORMED AT THE DEPARTURE AIRPORT - NO INJURIES OR EQUIPMENT DAMAGED RESULTED FROM EPISODE. UPON FURTHER INVESTIGATION, THE DSDR 2022F00134Oxygen Bottle · faultyOVER THE COURSE OF 24 HOURS LIQUID OXYGEN CONVERTOR EXPELLED ALL LIQUID OXYGEN DUE TO A FAULTY VENT RELIEF VALVE.SDR 2021FA0000013Relay · failedFUEL SYSTEM INDICATION FOR MAIN/AUX/ER GOES THRU K1 RELAY PN M5757/1-021 BEHIND FUEL PANEL. NEW RELAY SAME PART NUMBER ARE BEING SOLD WITH AN INCORRECT DRAWING OF CONTACTS, POSSIBLY INTERNALLY MISWIRED OR BOTH. UPON INSTALLING NEW CIRCUIT BREAKERS IMMEDIATELSDR 2020FA0000561Actuator · corrodedLT MAIN GEAR RETRACT ACTUATOR FOUND CORRODED THRU CHROME COATING NEAR ATTACH END WERE EXPOSED WITH GEAR IN THE RETRACTED POSITION. NEW VERSION OF ACTUATOR HAS CHROME ALL THE WAY TO THE END OF THE SHAFT INSTEAD OF LEAVING A PARTIAL METAL TO CHROME EDGE WHICH WSDR 15MA202012070001Heater · failedWHILE DOING A PATIENT FLIGHT AT APPROXIMATELY 16:45 CENTRAL TIME, AIRCRAFT TOTAL TIME OF 2872.2 ONE OF OUR FLIGHT NURSES STARTED MENTIONING HOW OUR MEDICAL BED FELT RATHER WARM. AS I LOOKED BACK INTO THE CABIN I NOTICED A FAINT HAZE. THE FLIGHT NURSE STARTESDR CA190807002Heater · malfunctioned(CAN) FOLLOWING RETURN FROM A MISSION THE PILOTS OF B300C AIRCRAFT, REPORTED THAT THE RIGHT SIDE PITOT HEAT WAS INOPERATIVE. MAINTENANCE CARRIED OUT TROUBLESHOOTING AND DISCOVERED THAT THE PITOT HEAT POWER WIRE H3B20 LOCATED FORWARD OF THE NOSE PRESSURE BULKHSDR 2018FA0000320Wire Harness · out of positionWIRE CABLE BUNDLE ON LEFT SIDE OF CENTER PEDESTAL INTERFERING WITH ENGINE CONTROLS BY ABRAIDING ON PUSH-PULL TUBES. INCORRECT ROUTING?SDR CA180808025Compressor · failed(CAN) AIR CONDITIONING COMPRESSOR P/N 201-0450-3 FAILURE, 73.5 HRS FROM INSTALLATION. DEFECT REPORTED: `AIR CONDITIONING NOT COOLING` AIR CONDITIONING COMPRESSOR FOUND TO HAVE A FREEWHEELING CLUTCH, SUSPECTED THAT THE COMPRESSOR SEIZED. THE AIR CONDITIONING SDR CA180808024Compressor · failed(CAN) AIR CONDITIONING COMPRESSOR P/N 201-0450-3 FAILURE, 15.7 HRS FROM INSTALLATION. DEFECT REPORTED: `AIR CONDITIONING NOT WORKING` AIR CONDITIONING COMPRESSOR FOUND TO HAVE FAILED. THE AIR CONDITIONING COMPRESSOR WAS REMOVED AND THE SYSTEM FLUSHED IN ACCOSDR CA180808020Display · failed(CAN) ROCKWELL COLLINS PROLINE FUSION EQUIPPED AIRCRAFT, ADAPTIVE FLIGHT DISPLAY AFD-3700. DEFECT REPORTED AS `NUMEROUS ERRONEOUS CAS MESSAGES SHOWING UP ON RETURN TO YEG, UNCOMMANDED FLL CHANGE FROM 160 TO 99 IN CLIMB OUT OF YQU`. AFD 2 DETERMINED TO HAVE FSDR CA180808023Compressor · failed(CAN) AIR CONDITIONING COMPRESSOR P/N 201-0450-3 FAILURE ON AN AIRCRAFT WITH UNDER 400 HRS FROM NEW. DEFECT REPORTED: `AIR CONDITIONING FOUND TO NOT BE BLOWING COOL AIR` AIR CONDITIONING COMPRESSOR FOUND TO HAVE FAILED. A NEW COMPRESSOR WAS INSTALLED, SAME PSDR Q5QA2016060300001Skin · crackedWITH ONLY 240.4 HRS TT ON ACFT, CRACKS WERE DISCOVERED ON THE RT T/E OF THE WING. THE UPPER SKIN WAS CRACKED IN 2 PLACES AT THE OTBD END. THE LOWER SKIN WAS CRACKED AT THE OTBD END. AFTER THE SKINS WERE REMOVED A CRACK WAS DISCOVERED IN THE OTBD RIB AND THESDR J8UR20151228001Pin · out of positionPULLEY GUARD PIN, PN NAS427K-20, MIGRATED OUT OF THE LOCKING POSITION OF THE PULLEY ASSY FOR THE RUDDER TRIM CABLE, CAUSING A CONDITION THROUGH THE VIBRATION OF FLIGHT AND GROUND OPERATION OF THE CABLES COMING OFF OF THE PULLEYS AND CROSSING FROM ONE PULLEY TOSDR 2015FA0000472Placard · inaccurateAUXILIARY FUEL TANK PLACARDS FROM OEM REFLECT STANDARD CONFIGURATION WHEN ACFT ARE EQUIPPED WITH EXTENDED RANGE TANKS. ALSO, MLG PLACARDS FROM OEM REFLECT STANDARD LANDING GEAR HEIGHT RANGE WHEN HIGH FLOTATION GEAR ARE INSTALLED, 4.5"-5.0" STANDARD GEAR VS 5.SDR 2014FA0000256Warning Light · illuminatedAFTER ENGINE START, PILOT NOTICED CHIP LIGHT ON NR 2 ENGINE, SHUTDOWN.SDR CA140115002Downlock Switch · failed(CAN) DURING A ROUTINE FLIGHT THE PILOTS REPORTED THAT THE LANDING GEAR INDICATION CIRCUIT BREAKER TRIPPED. UPON INSPECTION BY MAINTENANCE PERSONNEL IT WAS DISCOVERED THAT THE WIRING HARNESS OF THE LT LANDING GEAR DOWNLOCK MICROSWITCH, PN 101-364628-1 WAS WORSDR CA131212001Switch · out of adjust(CAN) THE ACFT DEPARTED FOR A ROUTINE MEDI-VAC AND UPON LEVELING AT 240, THE DOOR UNLOCK ANNUNCIATOR ILLUMINATED. THE CREW ELECTED TO RETURN TO MAIN BASE AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION AND DISCOVERED THE CARGO DOOR SDR CA131009003Hose · chafed(CAN) WHILE CONDUCTING THE PHASE 3, 600 HR INSPECTION MAINTENANCE DESCOVERED THAT THE AIR CONDITIONING PLUMBING HOSES, PART NR 300-0872-1 AND 300-0873-1, IPC REF 21-52-00-02 ITEM VIEW D FOUND TO BE TO CHAFING ON THE AIR CONDITIONING BLOWER UNIT.SDR CA130501001Skin · cracked(CAN) DURING MAINTENANCE, A CRACK WAS FOUND IN THE T/E OF THE LT WING AT WS 148 APPROXMATE 6" AFT OF THE REAR SPAR. THE CRACK IS JUST OVER 2.5" LONG IN SKIN, PN 50-110028-16. ALSO STIFFENER PN 50-11028-12 IS CRACKED ON THE INSIDE OF THE WING IN THIS SAME AREASDR CA130211002Strut · damaged(CAN) DURING INSPECTION, MAINTENANCE FOUND THAT THE RT MLG STRUT PISTON HAD DAMAGE TO THE CHROME AREA , WITH SCORING AND CHROME MISSING FROM THE PISTON. PISTON WAS R & R USING HBC KIT PN 130-8001-003 AND PN 60-38-4016-50 PISTON RING, AND PN 8-335N300-90, BACSDR CA121017013Engine · shutdown(CAN) AIRCRAFT EXPERIENCED AN IFSD.SDR CA120621001Hinge · cracked(CAN) DURING AN AFTER FLIGHT WALK AROUND, NOTICED THAT THE LT NLG REAR DOOR HINGE WAS BEGINNING TO SEPARATE FROM THE DOOR SKIN. UPON CLOSER INSPECTION, THE HINGE WAS CRACKED ON ONE OF THE UPPER HOLES. THE DOOR WAS REMOVED AS WELL AS THE HINGE ASSEMBLY. A NESDR J8UR20120326002Handpump · malfunctionedDURING EMERGENCY LANDING GEAR OPERATIONAL AND FUNCTIONAL (GROUND) CHECK, EMERGENCY HANDPUMP HANDLE SEPERATED FROM PUMP HOUSING. (SNAP-RING THAT HOLDS PISTON ASSEMBLY INTO THE HAND PUMP ASSEMBLY DISENGAGED, CAUSING HAND PUMP ASSY TO COME APART DURING OPERATION)SDR J8UR20120118001Pressure Switch · failedPROPELLER AUTO-FEATHER DOES NOT TEST DURING GROUND AND PRE-FLIGHT ENGINE RUNS. GROUND IDLE SOLENOID FAILS TO OPERATE PROPERLY.SDR J8UR20111219001Connector · chafedRT FUEL SHUT-OFF VALVE ELECTRICAL CONNECTOR IS COMING IN CONTACT WITH ACCESS PANEL NUTPLATE ON RT NACELLE (PANEL NR 5RH). THE CLOSE PROXIMITY OF THE FIREWALL ELECTRICAL CONNECTOR AND THE ACCESS PANEL NUTPLATE CAUSED WIRING TO BECOME CHAFED. NUTPLATE PROTRUDESDR 2011FA0000209Bulkhead · chafedDURING THE FIRST PHASE INSPECTION OF BUNO 168204 (FM-27), IT WAS DISCOVERED THAT THE ELEVATOR TRIM CABLE AND TURNBUCKLE WAS RUBBING ON A BULKHEAD AT STATION 412.5. THE ADDITIONAL 5 AIRCRAFT WERE INSPECTED, AND A TOTAL OF 5 AIRCRAFT OUT OF THE FLEET OF 6 EXHIBISDR 2011FA0000182Control Cable · bindingACFT WAS MODIFIED IAW STC SA00047MC BY A REPAIR STATION ON MAY 28, 2010. DURING THE FIRST PHASE INSP AT 200 HRS, IT WAS DISCOVERED THAT THE ELEVATOR TRIM CABLE TURNBUCKLE WAS DRAGGING ON THE BULKHEAD INSTALLED AT STA 414 AS PART OF THIS STC. THIS REPORT IS TOSDR AOC04006Compressor · damagedPILOT REPORTED FREON AIR CONDITIONING SYSTEM INOPERATIVE FOLLOWING A FLIGHT. FOUND COMPRESSOR CLUTCH PLATE HAS SEPARATED FROM THE COMPRESSOR AND WAS FOUND IN THE LOWER ENGINE COWL. FIRE SLEEVE ON OIL LINE FROM THE OIL COOLER HAD IMPACT DAMAGE (SLEEVE CUT) BUSDR 2003FA0000862Panel · departedWING BOLT PANEL DEPARTED AIRCRAFT WHILE IN FLIGHT. THIS IS THE THIRD OCCURANCE ON THREE DIFFERENT AC IN APPROXIMATELY ONE MONTH. INSPECTION REVEALED THE THE SPRING TAB HAD FAILED. RECOMMEND CLOSE INSPECTION OF THIS PANEL AT EACH PHASE INSPECTION.SDR AU000879Diode · shorted(AUS) CABIN OXYGEN CONTROL SOLENOID TRANSIENT VOLTAGE SUPPRESSION DIODE SHORT CIRCUITED. FAILURE OF PASSENGER OXYGEN MASK AUTOMATIC DEPLOYMENT. (X)SDR 99ZZZX1365Frame · crackedUPON REMOVAL OF THE CABIN DOOR SEAL, FOUND SEVERE CORROSION AND A 9 INCH CRACK IN THE DOOR STEEL STRUCTURE JUST BELOW THE SEAL RETAINER NEAR THE AFT SIDE OF THE HINGE AREA. AIRCRAFT TT: 2,441.4 HOURS.SDR 98ZZZX1101Skin · crackedRIGHT WING UPPER SURFACE JUST OUTBOARD OF WING ATTACH BETWEEN FRONT AND REAR SPARS, WS 124.6 WAS FOUND WRINKLED AND CRACKED DURING A PHASE 2 INSPECTION. LOG BOOK HISTORY SHOWS A WRINKLE WAS FIRST NOTICED (10-27-93) (TT 151 HOURS) AND WAS FOUND OK FOR SERVICE SDR 98ZZZX482Valve · damagedDURING AIRCRAFT REFUELING WHEN THE NOZZLE IS INSERTED INTO THE FUEL FILLER, IT OPENS THE ANTI-SYPHON VALVE FLAPPER DOOR (SPRING LOADED) AND EXTENDS INTO THE TANK AREA. THE AREA OF ANTI-SYPHON VALVE THAT THE FLAPPER DOOR SEALS AGAINST IS CALLED THE PAN. THIS P
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