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 = 'DC3' 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 = 'DC3' 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 2019FA0000408Truss · crackedDURING SCHEDULED MAINTENANCE/ENGINE CHANGE, CONDUCTED THE SCHEDULED 1000 HOUR SPECIAL INSPECTION OF WELDS ON RH ENGINE TRUSS MOUNT ASSEMBLY (AAIP SPEC INSP #25). VERY SMALL (FINE) CRACK APPROX 3/4" LONG WAS OBSERVED WITH 16X MAGNIFYING GLASS PRIOR TO APPLICATISDR 2018FA0000536Lead · cutTHE POSITION TRANSDUCERS ARE BEING USED AS SENSORS FOR SOME FLIGHT DATA RECORDER (FDR) PARAMETERS AND ARE MANUALLY ATTACHED VIA A STEEL LEAD/LINE TO SENSE SURFACE MOVEMENT. OVER TIME, IT HAS BEEN NOTED THAT THE STEEL LEADS EXTENDING OUT OF THE SENSORS ARE CUTSDR 2017FA0000279Actuator · leakingMULTIPLE FAILURES OF THE R/H LANDING GEAR ACTUATOR. BOTH WERE FOUND TO BE LEAKING HYDRAULIC FLUID. (3) FOUND BAD IN THE PAST 7 MONTHS.SDR CA150604016Housing · restricted(CAN) AN AGB HOUSING LABELED AS PN 3105662-01 WAS REMOVED DURING AN UNSCHEDULED LIGHT OVERHAUL DUE TO IMPROPER PRESERVATION. THE HOUSING WAS FOUND WITH RESTRICTED FLOW AT THE AGB HOUSING CENTER BEARING OIL PASSAGE. FURTHER INSPECTION REVEALED THAT THE SUBJECSDR U97A2013110400001Supercharger · deterioratedENGINE RAN FINE UNTIL THE NR 3 PHASE INSPECTION WAS UNDERWAY. STC OIL FILTER WAS CUT OPEN REVEALING LARGE AMOUNTS OF ALUMINUM/ MAGNESIUM. ENGINE INTEGRAL OIL SCREEN SHOWED THE SAME, INDICATING THAT THE OIL FILTER HAD BYPASSED ALLOWING CONTAMINAUTOION INTO THSDR 2011FA0000588Nut · unsafetiedAFTER TAKEOFF, AILERON WOULD NOT TRAVEL RT VERY FAR. STOP FELT IN YOKE. CONTROL CHECK WAS DONE PRIOR TO FLIGHT, ALL WAS NORMAL. AUTOPILOT WAS TURNED OFF TO ELIMINATE ANY INTERFERENCE WITH FLIGHT CONTROLS. RETURNED TO DEPARTING AIRPORT FOR UNEVENTFUL APPROACSDR U972009F00001Stringer · corrodedAREAS OF STRINGER MATERIAL WITHIN ACFT CTR AND OTBD WING FOUND TO BE SUFFERING FROM MILD EXFOLIATION CORROSION. CORROSION MANIFESTED ITSELF AS A LOCALIZED BUMP OR BULGE WITHIN THE VERTICAL LEG OF THE STRINGER MATERIAL. ALL STRINGER MATERIAL SUFFERING FROM THSDR U972009F00000Rib · crackedCRACKS APPROX 4 INCHES IN LENGTH WERE DETECTED VISUALLY ON THE UPPER RETURN OF CTR WING RIBS AT STA 42 LT AND RT. MDG SB NR 228 AND SRM (TO 1C-47-3) SPECIFICALLY DESCRIBES ACCEPTABLE REPAIRS FOR THIS LOCATION ON THIS RIB. SUPP INSP DOCUMENT DOES NOT GIVE GUISDR 7357Stringer · corrodedSTRINGER CORROSION FOUND DURING PHASE INSPECTION ON RIGHT FUSELAGE BELOW FLOOR AT STATION 312.5 TO 450.5, THE STRINGER WAS REMOVED AND REPLACED.SDR JRAA001Panel · corrodedDURING INSPECTION FOUND CORROSION AROUND THE LT TOP NOSE FUSELAGE SKIN PANELS FROM FUSELAGE STATION 49.125 TO 76.5 (COCKPIT ROOF AREA). BOTH LT UPPER SKIN PANELS WERE REMOVED FOR REPLACEMENT. ALSO CENTER WINDOW FRAME WAS REMOVED FOR REPLACEMENT.SDR JRA2002F00000Line · rupturedPRIOR TO TAKEOFF, RUPTURED ITS LEFT-HAND MAIN WHEEL BRAKE EXPANDER TUBE. RUPTURE CAUSED HYDRAULIC FLUID LOSS AND LEFT BRAKE LOSS. AC WAS STOPPED WITH REVERSE THRUST AND ENGINES SHUT DOWN. NORTH OPS WAS ADVISED OF SITUATION BY VICTOR RADIO. SMOKE JUMPERS ANSDR CA990915079Insert · loose(CAN) EXHAUST ROCKER SHAFT INSERT FOUND LOOSE ON THE CYLINDER.SDR 98ZZZX3953Cylinder · failedNR 1 CYLINDER ON NR 2 ENGINE FAILED. SHUT DOWN NR 2 ENGINE AND FEATHERED. RETURNED TO ANCHORAGE.SDR 97ZZZX3832Castle Nut · failedAIRCRAFT WAS AT CRUISE POWER. LEFT ENGINE WENT TO IDLE POWER. FEATHERED LEFT ENGINE AND LANDED. FOUND THROTTLE CONTROL ARM OFF OF CARBURETOR. FOUND PARTS OF THE CRACKED AN 310-4 CASTLE NUT.SDR 97ZZZX3626Valve · failedNR 1 CYLINDER VALVE HEAD CAME OFF AND SPLIT CYLINDER HEAD. ALSO, DAMAGED PISTON.SDR 96ZZZX3797Carburetor · malfunctionENGINE WILL NOT IDLE, DIES/RESTARTS OK. WILL NOT TAKE THROTTLE. WANTS TO BACKFIRE THROUGH CARBURETOR. REMOVED CARBURETOR. REPLACED WITH OVERHAULED UNIT.SDR 95ZZZX5967Cylinder · failedPILOT NOTICED SPARKS COMING FROM THE LEFT ENGINE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION SHOWED THAT NR 14 CYLINDER HEAD SEPARATED FROM ITS BARREL. REPLACED CYLINDER WITH O/H UNIT AND RETURNED ACFT TO SERVICE.SDR 95ZZZX3488Magneto · looseRIGHT ENGINE STARTED RUNNING ROUGH IN-FLIGHT. ENGINE SHUT DOWN AND FEATHERED. FOUND RIGHT MAG HAS COME LOOSE. RE-TIMED AND TORQUED RIGHT MAG. OPS CHECKED SATISFACTORY.SDR 95ZZZX1740Magneto · failedAFTER TAKEOFF, RIGHT ENGINE STARTED TO BACKFIRE AND RUN ROUGH. ENGINE WAS SHUT DOWN AS A PRECAUTIONARY METHOD. UPON TROUBLESHOOTING, FOUND LT MAG BAD. MAG WAS REPLACED WITH A YELLOW TAGGED UNIT. ENGINE WAS GROUND RUN, CHECKED SATISFACTORY. AIRCRAFT WAS RESDR 95ZZZX1739Cylinder · failedNR 13 CYLINDER THERMAL SHOCKED APPROXIMATELY 20 MILES EAST OF MKE. LEFT ENGINE ROUGH AND BACKFIRING. SHUT ENGINE DOWN, RETURNED TO MKE. REPLACED NR 13 CYLINDER POWER AND LEAK CHECK SATISFCATORY. RETURNED AIRCRAFT TO SERVICE.
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