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 = '421B' 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 = '421B' 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 2005FA0001593Pump · inoperativeTHE PILOT REPORTED THE HEATER HAD STOPPED DURING FLIGHT. AFTER RETURNING TO THE MAINTENANCE SHOP THE HEATER WAS TROUBLESHOT AND INSPECTED. FOUND THE HEATER FUEL PUMP HAD MALFUNCTIONED AND HAD CAUGHT ON FIRE FOR A TIME. WERE ABLE TO SAY IT WAS ON FIRE BECAUSSDR OEJ2005F00000Landing Gear · failedAFTER LANDING, DURING ROLL OUT THE LT MLG FOLDED UP. BEFORE LANDING, ON FINAL APPROACH. THE GEAR WAS VERIFIED BY BOTH PILOTS THAT THE GEAR WAS DOWN AND LOCK WITH ALL GREEN LIGHTS AND ALL SYSTEMS NORMAL. AT THIS TIME NO VERIFICATION ON WHY THIS INCIDENT OCCUSDR 2005FA0001451Engine · making metalAT INITIAL 10 HR OIL CHANGE, A LARGE AMOUNT OF WHAT APPEARS TO BE BEARING MATERIAL WAS FOUND IN THE DRAIN OIL, DRAIN PLUG, AND ON FURTHER EXAMINATION, THE OIL FILTER. ENGINE WAS REMOVED FROM SERVICE AT THIS TIME AND SENT BACK TO OVERHAUL FACILITY FOR FURTHER SDR CA051026007Contact · meltedENGINE STARTER RELAY ARCING, CAUSED THE CONTACTS TO WELD TOGETHER SOLID. WHICH IN TURN CAUSED STARTER TO RUN CONTINOUSLY UNTIL IT OVERHEATED AND BURNED. POTENTIAL FOR ELECTRICAL FIRE IN ENGINE/WING ROOT.SDR 2005FA0000750Starter · inoperativeSTARTER INOPERATIVE. (K)SDR 2005FA0000517Hinge · misinstalledAIRCRAFT WAS HERE FOR COMPLETE EXTERIOR REPAINT. AFTER REMOVING RUDDER, COMPLIED WITH MFG MEB004. IT IS JUST A VISUAL INSPECTION, BUT IT DOES REQUIRE REMOVING THE RUDDER. FOUND THAT RUDDER HINGE ASSY WAS INSTALLED UPSIDE DOWN. FOUND THAT ABOUT 75 PERCENT OSDR 2005FA0000554Torque Tube · crackedLANDING GEAR TORQUE TUBE IS CRACKEDSDR 2005FA0000397Bulkhead · crackedDURING AN ANNUAL INSPECTION, FOUND AFT BULKHEAD OF THE LT WING TIP TANK ASSY. CRACKED THROUGH FROM APPROXIMATE CENTER OF THE IB LIGHTENING HOLE HORIZONTALLY TO THE BULKHEAD IB EDGE. CRACKED AREA IS ADJACENT TO AFT ATTACH POINT FOR THE TIP TANK ASSY. AIRCRAFSDR 2005FA0000396Rib · crackedDURING AN ANNUAL INSP, NOTED CRACKS IN LT AND RT WING T/E RIBS AT FORWARD END AFT SPAR ATTACHMENT POINT AREAS. AFFECTED RIBS ARE FIRST RIBS IB OF SPOILER SYSTEM ACTUATOR ATTACH POINTS. ALSO FOUND CRACKED AREA IN WING OB T/E SKIN PANEL AT ATTACHMENT POINT TO SDR CA050216005Piston Pin · broken(CAN) PISTON (NR1) BROKE AT PIN BOSS RESULTING IN LARGE CHUNKS OF ALUMINUM FALLING INTO THE ENGINE, ENDING UP AT THE BOTTOM OF THE SUMP. SMALLER PIECES OF THE METAL WERE SUCKED UP THROUGH THE OIL PICK-UP AND RAN THROUGH THE OIL PUMP.SDR CA050125013Bearing Cage · disintegrated(CAN) ATTEMPT TO START RT ENGINE AT EXTREME COLD TEMP. ENGINE BACKFIRED, STARTER ADAPTER SHAFT BRG CAGE DISINTEGRATED, SHAFT OIL SEAL BLEW.SDR 2004FA0000927Bracket · misinstalledCOMPLIED WITH MFG MEB 00-4 RUDDER BEARING INSPECTION/REPLACEMENT. FOUND RUDDER LOWER HINGE BEARING BRACKET INSTALLED UPSIDE DOWN FROM FACTORY. REPLACEMENT PROCEDURE DESCRIBED IN MEB FOUND ERRONEOUS AND INADEQUATE TO COMPLETE SATISFACTORY REPLACEMENT OF BRACKSDR 2005FA0000755Rocker · brokenENGINE BECAME ROUGH IN FLIGHT ENGINE SHUTDOWN FOUND RT ENGINE NR 1 CYLINDER EXHAUST ROCKER ARM BROKEN. (K)SDR 2005FA0000125Crankshaft · brokenCRANKSHAFT BROKE AT NR 2 MAIN. NO SIGNS OF OIL STARVATION. NO SIGNS OF CASE FRETTING. CASE WAS DAMAGED BEYOND REPAIR. (K)SDR 1538T001Table · misinstalledINSPECTED RIGHT HAND CABIN EXECUTIVE TABLE AT THE RECOMMENDATION OF ANOTHER MAINTENANCE FACILITY MAINTAINING SAME TYPE OF AIRCRAFT. FOUND A LEFT HAND TABLE INSTALLED. FORWARD CUP HOLDER WAS SCREWED TO THE TABLE MAKING EMERGENCY EXIT REMOVAL DIFFICULT. EMERGSDR 2005FA0000677Main Bearing · delaminatedBEARING CRACKED AND DELAMINATED IN NR2 MAIN BEARING SADDLE. HEATED CRACKS IN NR2 MAIN JOURNAL. THIS HAS BEEN NOTED ON OTHER ENGINES WE HAVE DISASSEMBLED. BEARING BORN DATE 10-02. THIS WAS A NEW CASE AND NO SIGNS OF FRETTING ON THE CASE HALF. (K)SDR 2004FA0000355Cylinder Head · crackedAIRCRAFT NDT SERVICE WAS CONTRACTED TO VERIFY CRACKS IN THE ENGINE CYLINDER HEADS BETWEEN THE SPARK PLUG AND FUEL INJECTOR MOUNTING BOSS. AN EDDY CURRENT EXAMINATION DETERMINED THAT ALL TWELVE CYLINDER HEADS WERE CRACKED. THE OPERATOR REPLACED ALL TWELVE CYLISDR CA040203008Bolt · wrong part(CAN) BOLTS, BUSHINGS SEIZED ON MAIN DOOR TOP HALF. INCORRECT HARDWARE STACK-UP, IE INTERNAL WRENCHING BOLT HAD PLAIN WASHER UNDER RADIUS OF HEAD. SEVERAL AIRCRAFT HAVE HAD THESE SAME PROBLEM OF SEIZED/CORRODED PARTS. CAUSED BY LACK OF LUBRICATION. MAIN DOORSDR AK62004F00002Spar Cap · corrodedDURING AN ATTEMPT TO REPAIR CORROSION AROUND THE LT WING FLAP BELLCRANK, LOCATED IN THE EXHAUST GAS TRAIL ON LOWER SIDE OF WING. DISCOVERED SEVERE INTERGRANULAR CORROSION ON LOWER SPAR CAP (JUST OB OF FACTORY SPLICE PLATE).SDR 2003FA0001035Bearing · destroyedAIRCRAFT LANDED EXITED ONTO TAXIWAY, FELT VIBRATION IN NOSE OF AIRCRAFT, FELL NOSE FIRST ONTO TAXIWAY. THE BEARINGS IN NOSE WHEEL FROZE AND SHEARED AXIAL. LANDING GEAR STRUT STRUCK GROUND AND COLLAPSED. THE BEARING AND ROLLER RETAINER ON ONE SIDE HAD DISINTSDR 2003FA0000976Spark Plug · crackedDURING ROUTINE 100 HR INSPECTION 4 SPARK PLUGS ON RIGHT ENGINE FOUND TO HAVE CRACKS IN THE PLUG BODY BETWEEN THE GASKET SURFACE AND THE WRENCH HEX.SDR AUS20030690Connecting Rod · damaged(AUS) NR 2 CYLINDER CONNECTING ROD PN 655004 BIGEND CAP CONTACTING CAMSHAFT PN 653056 NR 2 CYLINDER EXHAUST LOBE. INSPECTION FOUND A SIMILAR PROBLEM WITH NR 6 CYLINDER CONNECTING ROD BIG END CAP.SDR AUS20030666Cylinder · wrong part(AUS) RT ENGINE HAD TWO UNAPPROVED CYLINDERS FITTED. PN 653452 CYLINDERS ARE NOT APPROVED FOR THE GTSIO520-H MODEL CYLINDERS UNLESS MODIFIED. THE TWO CYLINDERS FITTED WERE NOT MODIFIED IAW APPROVED SCHEME. THE REMAINING PN 653453A4 CYLINDERS FITTED ARE APPROVSDR AUS20030660Injector · misinstalled(AUS) FUEL INJECTOR NOZZLE INCORRECTLY FITTED. TWO RUBBER SEALS AND ONE METAL WASHER FITTED INSTEAD OF THE CORRECT FIT OF ONE RUBBER SEAL AND ONE METAL WASHER. PERSONNEL/MAINTENANCE ERROR.SDR AUS20030659Rod Bearing · worn(AUS) CONNECTING ROD LITTLE END BEARING MOVED AND WORE ON PISTON. INVESTIGATION FOUND TWO MORE LITTLE END BEARINGS LOOSE.SDR 2003FA0000476Arm · brokenRIGHT GEAR INBOARD DOOR CAME OPEN IN FLIGHT. FOUND THE ACTUATOR ARM BROKE LOOSE AND TURNED ON ITS SHAFT. THIS ALLOW THE GEAR DOOR TO COME OPEN IN FLIGHT. ONLY WARNING IS THE ADDED AIR NOISE. THE ARM IS A PRESS FIT ON THIS PART NUMBER AND HAS BEEN SUPERCEDED SDR BLI2003F00001Spacer · wrong partWHILE REPLACING AN ALTERNATOR, NOTICED THAT DRIVE GER RETAINING NUT WOULD NOT RUN DOWN SUFFICIENTLY TO INSTALL SAFETY. DISCOVERED 2 DIFFERENT SPACER SIZES ON OLD AND NEW AACT. REMOVED CORRECT SIZE SPACER FROM ANOTHER OHC ALTERNATOR AND INSTALLED. CONTACTED SDR AUS20030380Line · loose(AUS) LT ENGINE NR 5 CYLINDER FUEL INJECTION LINE LOOSE AT ATTACHMENT TO FLOW DIVIDED.SDR CA030129001Line · blocked(CAN) ON GROUND WARM UP AND RUN ALL WAS NORMAL, ON TAKEOFF RT MANIFOLD STAYED AT 28.5 INCHES, ALL OTHER INDICATIONS AND ENGINE FUNCTIONS NORMAL. TAKEOFF ABORTED AND AIRCRAFT RETURNED TO HANGAR. MANIFOLD LINE FOUND BLOCK IN WING SECTION BETWEEN WING AND A/F. MOSDR 2002FA0001271Windshield · failedWHILE AT CRUISE ALT FL240, PILOTS FRONT WINDSHIELD DEPARTED THE AIRCRAFT ALONG WITH PART OF THE INSTRUMENT GLARE SHIELD AND PILOTS SUN VISOR. LAB EXAM OF WINDSHIELD DID NOT REVEAL POINT OF FAILURE BUT DID STATE NUMEROUS INSTALLATION DISCREPANCIES. MAINTENANCSDR 2002FA0001243Windshield · misinstalledON 27 JUNE 2002 WHILE AT CRUISE ALT FL240, PILOTS FRONT WINDSHIELD DEPARTED THE AIRCRAFT ALONG WITH PART OF THE INSTRUMENT GLARE SHIELD AND PILOTS SUN VISOR. LABORATORY EXAMINATION OF THE WINDSHIELD DID NOT REVEAL THE POINT OF FAILURE BUT DID STATE NUMEROUS ISDR 2002FA0001160Windshield · failedDURING CRUISE FLIGHT NEAR SHR AT 25000 FT., RT WINDSHEILD SUSTAINED AN EXPLOSIVE DECOMPRESSION. PILOT PERFORMED EMERGENCY PROCEDURES AND LANDED WITHOUT FURTHER INCIDENT.SDR AK62002F00001Bearing · failedTHE RT ENGINE APPEARS TO HAVE SUFFERED FROM OIL STARVATION AT THE NR 5 ROD JOURNAL. THIS CAUSED THE ROD TO SEPARATE AND PROTRUDE THRU THE TOP OF THE CRANKCASE.SDR BLIA512C8502Shaft · failedDURING CLIMB TO MK LEVELED AT 18K. ENGINE OPS BECAME ROUGH, THEN TACH WENT TO ZERO. PILOT OBSERVED SMOKEY MIST FROM LOUVERS. ENGINE TURNED OFF AND FEATHERED. DECLARED EMERGENCY AND LANDED. INSPECTED AND FOUND IDLER SHAFT LOOSE IN NACELLE. AIRCRAFT IN STSDR 2003F00162Alternator · failedON PREP FOR DEPARTURE, RETURNED TO RAMP AND CALLED MAINTENANCE. ARRANGED FOR ALTERNATOR REPLACEMENT BY PIEDMONT. AIRCRAFT RETURNED IRS. (M)SDR BLI2002F00001Alternator · failedLEFT ALTERNATOR FAILED TO COME ON LINE WHEN DEPARTURE WAS ATTEMPTED. ALTERNATOR WAS SHIPPED BY US TO REPAIR STATION. THEY INSTALLED IT AND THE AIRCRAFT WAS RETURNED TO SERVICE AND TO OUR FACILITY.SDR 2002FA0000307Windshield · departedAT APPROXIMATELY 17,000 FEET CO-PILOTS WINDSHIELD DEPARTED AIRCRAFT, RECOMMEND LARASCOPE INSPECTION OF WINDSHIELD HOLES. TOTAL TIME ON PART 6,234.9.SDR AUS20020125Exhaust Pipe · leaking(AUS) RH ENGINE FIRE. ENGINE COMPARTMENT DAMAGED. FIRE WAS EXTINGUISHED USING CABIN FIRE EXTINGUISHER. INVESTIGATION FOUND THE FIRE WAS CAUSED BY MISALIGNMENT OF THE EXHAUST SWIVEL JOINT WHICH ALLOWEDEXHAUST GAS TO LEAK INTO THE ENGINE BAY. A LIST OF DAMAGE ISSDR DMV2002F00000Bearing · failedSTARTER ADAPTER HOUSING MAIN BEARING FAILURE, RESULTS IN EXCESSIVE PLAY TO REAR ENGINE GEAR ASSEMBLY ADVISE UPGRADING TO BETTER STYLE OF BEARING DESIGNED FOR BETTER LOADS. PROVIDE A 500 HOUR INSPECTION THAT MIGHT REQUIRE REMOVAL AND INSPECTION OF BEARING TO SDR EKI2001F00000Adapter · failedSTATOR ADAPTOR FAILED AND DAMAGED REAR OF CASE WHERE SHAFT RIDES. ADAPTOR WAS REMOVED 20 HOURS EARLIER AND INSPECTED PER CSB. NO DEFECTS NOTED. THESE UNITS CONTINUE TO FAIL CAUSING VERY EXPENSIVE REPAIRS.SDR 2002FA0000018Bolt · looseALTERNATOR THRU BOLT CAME OUT AND ARCED ON STATOR TERMINAL. INSPECTED ALTERNATOR AND REINSTALLED ALTERNATOR BOLT. CHECKED TORQUE ON REMAINING BOLTS. SUGGEST BENDING LOCK TABS OVER PROPERLY AFTER TORQUING BOLTS.SDR LQU2002F00000Pin · missingRIGHT ENGINE RAN ROUGH AND VIBRATED BADLY IN FLIGHT, SHUT DOWN. VISUAL INSPECTION FOUND OPEN HOLE IN BACK OF CRANKCASE. IDLER GEAR SUPPORT PIN MISSING. FOUND PIN ON ENGINE NACELLE FLOOR UNDER ENGINE. NO VISUAL DAMAGE NOTED TO PIN. ENGINE NEEDS PIN TO HOLDSDR 2001FA0000462Cylinder · malfunctionedLEFT ENGINE EXPERIENCED A VIBRATION. PILOT ELECTED TO LAND . REPLACED NR 2 CYLINDER. CLEANED VALVE GUIDES ON REMAINING CYLINDERS. REPLACED SPARK PLUG ON NR 1 CYLINDER. FLIGHT CHECK GOOD.SDR BLI2002F00000Oil Cooler · leakingOIL LEAK DISCOVERED AFTER ARRIVAL, OIL COOLER, GROUNDED AIRCRAFT, CALLED MAINTENANCE. ANOTHER AIRCRAFT PICKED UP PAX. MAINTENANCE ARRANGED FOR MECHANIC TO TROUBLESHOOT AND REPAIR. LEAK CAUSED BY GASKET BETWEEN COOLER AND ENGINE CASE. GASKET REPLACED, ENGISDR 2001F00738Gasket · leakingOIL LEAK DISCOVERED AFTER ARRIVING AT SAW. GROUNDED AIRCRAFT AND CALLED MAINTENANCE. LEAK CAUSED BY BAD GASKET BETWEEN COOLER AND ENGINE CASE. GASKET REPLACED. ENGINE LEAK CHECKED GOOD. AIRCRAFT RETURNED IRS. (M)SDR 2001FA0000417Nut · failedAIRCRAFT WAS TAXING FROM THE MAIN RUNWAY TO THE GATE, PILOT FELT AND HEARD BUMPING NOISE UPON MAKING A RIGHT TURN. AS HE WAS MAKING RIGHT TURN ONTO RAMP TORQUE LINKS SEPARATED CAUSING THE RIGHT WHEEL AND PISTON ASSEMBLY TO ROTATE ABOUT 135 DEGREES, CAUSING DASDR AUS20010943Bearing · failed(AUS) ENGINE OIL FILTER CONTAMINATED WITH METAL. INVESTIGATION FOUNDNO1 AND NO2 BEARINGS HAD COMPLETELY FAILED WITH THE BEARING SHELLS BROKEN IN HALF. TRANSVERSE CRACKS WERE FOUND AROUND THECRANKSHAFT NO2 MAIN JOURNAL WITH CATASTROPHIC FAILURE IMMINENT.SDR BLI2001F00001Wire · chafedON APPROACH, RIGHT ENGINE FIRE WARNING ON. AIRCRAFT INSPECTED FOR EVIDENCE OF DAMAGE OR EXHAUST LEAK. NONE NOTED. EXTENSIVE GROUND RUNS COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. FURTHER DETAILED INSPECTION FOUND WIRES TO ONE FIRE DETECTOR CHAFEDSDR BLIA512CB1701Wire · chafedAPPROACH TO AIRPORT: RIGHT ENGINE FIRE WARNING ON. REDUCED POWER, CO-PILOT LOOKED FOR SMOKE. NONE NOTED, LIGHT OUT LANDED, CALLED MAINTENANCE AIRCRAFT DID NOT RETURN TO BASE. LIGHT INDICATOR PROBLEM INSPECTED, EXHAUST AND ENGINE FOUND NO EVIDENCE OF DAMAGE SDR 20010511CW010Spar Cap · crackedDURING AN ANNUAL INSPECTION, A CRACK APPROX 3 INCHES LONG WAS FOUND ON LEFT WING AFT SPAR, UPPER AFT CAP. BELOW BAGGAGE RACELLE.
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