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 = '402B' 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 = '402B' 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 97ZZZX4329Valve · failedLEFT ENGINE WENT TO NORMALLY ASPIRATED, DUE TO LT TURBO VALVE FAILURE.SDR 97ZZZX3696Bulkhead · holes defectiveDURING THE COURSE OF A NORMAL PRE-FLIGHT INSPECTION, THE PILOT NOTICED LEFT SPINNER WAS LOOSE. UPON CLOSER INSPECTION, NOTICED THE BULKHEAD ATTACH HOLES WERE WALLOWED OUT THAT ATTACH THAT UNIT TO THE SLIP RING ASSEMBLY. IT IS SUSPECTED THAT WHILE THE ATTACHISDR 97ZZZX2914Bellcrank · brokenUPON COMPLETING A NORMAL TRIP, THE PILOT ON HIS POST FLIGHT INSPECTION NOTICED THE RT INBOARD LANDING GEAR DOOR WAS OPEN. AFTER A CLOSER INSPECTION, DETERMINED THE BELLCRANK ASSEMBLY THAT ACTUATES THE INBOARD GEAR DOOR WAS BROKEN. IT WAS BROKEN IN SUCH A WAYSDR 97ZZZX2818Switch · malfunctionLANDING GEAR SWITCH FOUND TO BE INTERMITTENT. FLIGHT CREW TOOK AIRCRAFT FOR A FLIGHT JUST AFTER WASHING. GEARS WOULD NOT RETRACT. ON INSPECTION, FOUND MOISTURE IN SIDE OF MLG SAFETY SWITCH.SDR AU970756Exit Door · separated(AUS) EMERGENCY EXIT DOOR SEPARATED FROM AIRCRAFT - AIRCRAFT HAD JUST COMPLETED A STRIP AND REPAINT AND IT IS SUSPECTED THAT THE EXIT DOOR HAD BEEN DISTURBED DURING THIS PROCESSSDR 97ZZZX2612Cylinder · leaksDURING 50-HOUR INSPECTION, MECH TURNED PROP AND NOTICED A 'HISSING' SOUND EMITTING FROM NR 4 CYLINDER ON LT ENGINE. UPON CLOSER INSP, THE HISS WAS DETERMINED TO BE COMING FROM THE CHT PROBE HOLE. SLIGHT SIGNS OF SOOT IN AREA. CYLINDER CHECKED WITH DIFFERENTSDR 97ZZZX2616Rib · crackedDURING A 50-HOUR INSPECTION, MECHANIC NOTICED CRACK IN WING SKIN IN THE MOST AFT OTBD SECTION OF RT WING. ALSO, TWO RIVETS WERE SHEARED THAT ATTACH THE OTBD HINGE BRACKET ASSY (CESSNA PN 5021002-13) WHICH ARE THE SAME RIVETS THAT ATTACH TIP TANK SUPPORT BRACKSDR 97ZZZX2615Support Bracket · rivets shearedDURING A 50-HOUR INSPECTION, MECHANIC NOTICED CRACK IN WING SKIN IN THE MOST AFT OTBD SECTION OF RT WING. ALSO, TWO RIVETS WERE SHEARED THAT ATTACH THE OTBD HINGE BRACKET ASSY (CESSNA PN 5021002-13) WHICH ARE THE SAME RIVETS THAT ATTACH TIP TANK SUPPORT BRACKSDR 97ZZZX2614Skin · crackedDURING A 50-HOUR INSPECTION, MECHANIC NOTICED CRACK IN WING SKIN IN THE MOST AFT OTBD SECTION OF RT WING. ALSO, TWO RIVETS WERE SHEARED THAT ATTACH THE OTBD HINGE BRACKET ASSY (CESSNA PN 5021002-13) WHICH ARE THE SAME RIVETS THAT ATTACH TIP TANK SUPPORT BRACKSDR 97ZZZX2117Bulkhead · crackedAFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH SDR 97ZZZX2116Rib · crackedAFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH SDR 97ZZZX2115Bracket · rivets shearedAFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH SDR 97ZZZX2114Bracket · rivets shearedAFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH SDR 97ZZZX2113Bracket · rivets shearedAFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH SDR 97ZZZX2112Skin · crackedAFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH SDR 97ZZZX2068Stud · brokenDURING THE COURSE OF A NORMAL FLIGHT, PILOT NOTICED OIL LEAK ON LEFT ENGINE. AFTER FLIGHT, REMOVED ENGINE COWLING AND SAW 5 CYLINDER STUDS HAD BROKEN ON THE NR 1 CYLINDER. ON ENGINES OPERATED ON 1600 TBO'S, SUSPECT TIME IN SERVICE IS THE MAIN CAUSE FOR BREAKSDR 97ZZZX2849Torque Tube · crackedPILOT REPORTED 'AFTER DEPARTURE, ADVISED BY ANOTHER AIRCRAFT THAT THE LEFT GEAR WAS DOWN AND LOCKED'. AFTER VERIFYING THIS IN MIRROR, HE CONTINUED TO DESTINATION AND EXTENDED GEARS AND A SAFE LANDING WAS MADE. THE PART WAS SUPERCEDED TO A DIFFERENT NUMBER WHSDR 97ZZZX2108Rib · crackedDURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH THE OTBD AILERON HINGE BRACKET ASSY (CESSNA P/N 5021002-12) WHICH ARE SAME RIVETS THAT ATTACH THE TSDR 97ZZZX2107Bracket · rivet shearedDURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH THE OTBD AILERON HINGE BRACKET ASSY (CESSNA P/N 5021002-12) WHICH ARE SAME RIVETS THAT ATTACH THE TSDR 97ZZZX2106Bracket · rivet shearedDURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH THE OTBD AILERON HINGE BRACKET ASSY (CESSNA P/N 5021002-12) WHICH ARE SAME RIVETS THAT ATTACH THE TSDR 97ZZZX2105Bracket · rivet shearedDURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH THE OTBD AILERON HINGE BRACKET ASSY (CESSNA P/N 5021002-12) WHICH ARE SAME RIVETS THAT ATTACH THE TSDR 97ZZZX2104Skin · crackedDURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH THE OTBD AILERON HINGE BRACKET ASSY (CESSNA P/N 5021002-12) WHICH ARE SAME RIVETS THAT ATTACH THE TSDR 97ZZZX2572Engine · failedMSS/HPN - AT 9,500 FEET APPROXIMATELY 15 MINUTES INTO THE FLIGHT, THE LEFT ENGINE RPM STARTED FLUCTUATING ABOUT 150 RPM. ABOUT 5 MINUTES LATER THAT ENGINE FAILED COMPLETELY. AFTER ATTEMPTING A RE-START AND CHECKING GAUGES (FUEL FLOW, 20 FEET MANIFOLD, PRESSUSDR 97ZZZX1955Torque Tube · crackedDURING COURSE OF NORMAL FLIGHT, PILOT NOTICED AIRSPEED WAS APPROXIMATELY 15(+) KNOTS SLOWER THAN NORMAL, AND WHEN LANDING GEAR EXTENDED, PILOT NOTICED LEFT GREEN LIGHT CAME ON FIRST. (IN NORMAL CONDITIONS, THE NOSE LIGHT COMES ON FIRST). THE AIRCRAFT WAS INSPSDR 97ZZZX1472Hub · crackedINSPECTION FOUND HUB CRACK LOCATED IN NR 3 HOLE, 2ND THREAD FROM OUTSIDE EDGE.SDR 97ZZZX1153Cylinder · crackedWHILE TROUBLESHOOTING A LEAKING INTAKE VALVE GUIDE SEAL, FOUND A CRACK IN THE NR 1 CYL EXHAUST PORT. FOUND SAME CRACKS IN NR 4 AND NR 5 CYLINDERS. YOU CANNOT SEE THEM WITHOUT DROPPING THE EXHAUST STACKS OFF THE ENGINE. THESE CYLINDERS HAD APPROX 850 HOURS SDR 97ZZZX1103Fork Bolt · brokenDURING APPROACH TO LAND, PILOT SELECTED GEAR DOWN. NOSE GEAR SHOWED UNSAFE. A FLY-BY WAS DONE AND PERSONNEL ON THE GROUND VERIFIED THE NOSE LANDING GEAR WAS TRAILING AT 45 DEGREES. THE AIRCRAFT RETURNED TO HOME BASE AND A NOSE GEAR UP LANDING WAS MADE. INSSDR 97ZZZX1152Switch · failedAFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT, A/C RETURNED TO BASE. FOUND LANDING GEAR SAFETY SWITCH DEFECTIVE. REPLACED SWITCH WITH CESSNA KIT SK 421-136B. OUR PARTS VENDOR STATED THAT DUE TO UNRELIABILITY, THE OLD STYLE SWITCH IS NO LONGER AVAILABLE SDR AU970081Switch · faulty(AUS) LH MAIN LANDING GEAR DOWNLOCK MICROSWITCH LEAF SPRING BROKENSDR AU970306Rib · cracked(AUS) LH WHEEL BAY CENTRE RIB UPPER CAP CRACKED IN AREA ACROSS ALLTHREE UPPER BRACKET BOLT HOLESSDR 97ZZZM670Bushing · failedFLT 131 - TCM TEARDOWN REPORT FOUND COUNTERWEIGHT BUSHING IN CRANKSHAFT CHECK, NR 2 LEADING EDGE, CRACKED AND BROKE UP AFTER ROTATING IN THE BUSHING BORE. THE COUNTERWEIGHT PIN BROKE THOUGH THE PLATE AND SNAP RING AND THEN ESCAPED FROM THE COUNTERWEIGHT. ALLSDR 97ZZZM257Connecting Rod · failedFLT 131 - EN ROUTE PQI-PWM - FLIGHT CREW LOST RIGHT ENGINE IN FLIGHT. AIRCRAFT LANDED AT BGR WITHOUT INCIDENT. PRE-INSPECTION NOTED OIL PRESENT, DAMAGE TO UPPER COWL. FURTHER INSPECTION NOTED BOTH MAGNETOS DAMAGED, NR 2 CONNECTING ROD THROUGH ENGINE CASE. SDR 97ZZZM210Connecting Rod · failedFLT 131 - PQI-PWM - FLT CREW LOST RIGHT ENGINE IN FLIGHT. AIRCRAFT WAS LANDED AT BANGOR AIRPORT. PRE-INSPECTION NOTED BOTH MAGNETOS DAMGED, NR 2 CONNECTING ROD THROUGH ENGINE CASE. ENGINE WAS OVERHAULED WITH 446.4 HOURS. ( M)SDR 97ZZZX2029Control Cable · frozenON DECEMBER 17, 1996, EN ROUTE, LEFT THROTTLE CABLE BECAME FROZEN UP. FLIGHT CONTINUED ON AND UPON ARRIVAL ON FINAL APPROACH, SHUT THE LEFT ENGINE DOWN AND LANDED UNEVENTFULLY. PUT THE AIRCRAFT IN A HEATED HANGAR UNTIL THE THROTTLE THAWED OUT, THEN BLEW AIR SDR EY2R9601319Races · corrodedRACES CORRODED.SDR 96ZZZX5958Bulkhead · crackedDURING WING INSPECTION, FOUND LEFT MAIN FUEL TANK AFT BULKHEAD HAD CRACKED. REPLACED BULKHEAD WITH NEW FROM CESSNA. SUSPECT THE REASON FOR THE FAILURE IS THE RELATIVE HIGH TIME OF THE AIRPLANE.SDR EY2R9601193Bearing · corrodedRETAIN BEARING FOUND CORRODED.SDR EY2R9600158Hub · crackedPROP HUB ASSY CRACKEDSDR 96ZZZX5657Block Assy · teeth missingPILOT REPORTED THAT ABOUT EVERY 20 MINUTES, THE RT ENGINE WOULD RUN ROUGH FOR A SECOND. FOUND DISTRIBUTOR GEAR TEETH MISSING FROM DISTRIBUTOR BLOCK ASSY. REPLACED MAGNETO WITH NEW.SDR 96ZZZX5903Hub · crackedPROP INSP FOUND HUB CRACKED IN THREAD AREA.SDR 96ZZZX5556Spring · brokenDURING A ROUTINE COMP CHECK, NR 6 CYL WAS NOTED TO HAVE LOW COMP. THE ROCKER COVER WAS REMOVED TO STACK VALVE. AT THAT POINT, IT WAS NOTED THAT THE INT VALVE SPRING WAS BROKEN. THE ADJACENT ROCKER WAS THEN REMOVED AND ANOTHER SPRING WAS FOUND TO BE BROKEN ASDR EY2R9601022Blade · corrodedBLADE, SN F35778YS, FOUND CORRODED.SDR EY2R9601021Blade · corrodedBLADE, SN F35903YS, FOUND CORRODED.SDR EY2R9601020Blade · corrodedBLADE, SN F35930YS, FOUND CORRODED.SDR EY2R9601019Blade · corrodedBLADE, SN F33462YS, FOUND CORRODED.SDR EY2R9601018Blade · corrodedBLADE, SN F35761YS, FOUND CORRODED.SDR EY2R9601017Blade · corrodedBLADE, SN F35476YS, FOUND CORRODED.SDR EY2R9601016Hub · corrodedHUB CORRODED.SDR EY2R9601015Hub · corrodedHUB CORRODED.SDR 96ZZZX5009Fuel Line · chafe/leakDURING PRE-FLIGHT, PILOT NOTICED FUEL COMING FROM BEHIND ENGINE. MAINTENANCE FOUND FUEL LINE CHAFED THROUGH BY A NUTPLATE. THIS LINE WAS APPARENTLY ORIGINAL EQUIPMENT AND SHOWED SEVERAL WEAR SPOTS.
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