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 = '182E' 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 = '182E' 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 2023FA0000410Data Card · malfunctionedRECEIVED NEW TAWS/TERRAIN DATA CARD FROM GARMIN, CARD DATA DOWNLOAD WAS ACCOMPLISHED ON GARMIN WEBSITE USING GARMIN CARD READER. GARMIN PROGRAM SHOWED TERRAIN AND OBSTACLE DATA DOWNLOAD COMPLETE. WHEN DATA CARD WAS PUT INTO 430W AND UNIT POWERED UP I GOT 2 MESSDR 2023FA0000409Data Card · damagedGARMIN NAV DATABASE CARD CASE HAD 3 OF 4 ASSEMBLY TABS BREAKSDR 2023FA0000408Data Card · unserviceableGARMIN 430W TAWS/TERRAIN DATA CARD CASE TABS BROKE ALLOWING METAL PORTION TO DESPERATE AND CIRCUIT CARD FELL OUT.SDR CA190418005Tube · cracked(CAN) THIS NEW ALTERNATOR CAME EQUIPPED WITH A BLAST TUBE BOLTED TO THE REAR OF THE ALTERNATOR HOUSING FOR DYNAMIC AIR FLOW COOLING OF THE UNIT. THE BLAST TUBE WAS FOUND CRACKED OFF ITS MOUNTS IN ALL 3 LOCATIONS. IT HAD FALLEN DOWN AND WAS RESTING ON THE INTAKSDR 2015FA0000611Control Wheel · crackedDURING A CHECK FLIGHT PILOT'S CONTROL YOKE CRACKED AND SEPARATED ON THE LT SIDE, ON THE LT HORIZONTAL SECTION, 1" FROM THE LT 90 DEGREE BEND FROM VERTICAL. YOKE PN IS UNKNOWN SINCE CURRENT PARTS MANUALS ONLY LIST CURRENTLY AUTHORIZED CONTROL YOKE PNS ALTHOUGHSDR CA150924007Gasket · leaking(CAN) PILOT REPORTED DEFECT, OIL STREAK FOUND DOWN SIDE OF COWL ON PILOT`S SIDE. OIL LEVEL FOUND TO BE DOWN 1 QT FROM BEGINNING OF THE FLIGHT. SUSPECT OIL LEAK. REMOVED COWLS AND INSPECTED FOR OIL LEAKS. FOUND NR 6 CYLINDER ROCKER BOX COVER LEAKING. REMOVEDSDR CA130530009Contact · failed(CAN) UPON ENGINE RUN-UP BEFORE TAKEOFF IT WAS FOUND THAT THE LT MAGNETO WAS VERY ROUGH AND CAUSING THE ENGINE TO BACK FIRE. ACFT WAS RETURNED TO HANGER FOR MAINTENANCE. IT WAS DISCOVERED THAT THE LOWER CONTACT PAD ON THE PN 10-357174 CONTACT ASSY HAD BECOMESDR CA100810002Connecting Rod · failedCATASTROPHIC ENGINE FAILURE, CONNECTING RODS CAME THROUGH CASE AND COWL.SDR 2009FA0000096Roll Pin · brokenPILOT REPORT: ON LANDING SEVERE NOSE WHEEL SHIMMY. FOUND ROLL PIN THAT SECURES PISTON TO DAMPER ROD BROKEN AT PISTON THE DAMPER ROD. REPLACED ROLL PIN AND ALL O-RINGS. OPS NORMAL ON NEXT LANDING. (K)SDR 2007FA0000634Support · crackedMECH DISCOVERED ON A 50 HR INSP, THE SUPPORT COLLAR ON THE AIRBOX MOUNTED TO THE CARBURETOR WAS CRACKED. THIS COULD LEAD TO THE SEPARATION OF THE AIRBOX FROM THE CARBURETOR AND LOSS OF POWER. PN 0750288 WAS REPLACED WITH NEW SUPPORT COLLAR PN 0750288-1 IAW SSDR CA040917006Leg Assy · broken(CAN) WHEN TURNING TO ALIGN AIRCRAFT FOR TAKEOFF ON THE GRASS STRIP AT CPE7 THE LT MAIN LANDING GEAR LEG SNAPPED OFF AT THE OB CHANNEL. THE AIRCRAFT COLLAPSED, THE ENGINE WAS STOPPED WITHOUT A PROP STRIKE BUT THE WING EXTENSION AND TIP WERE DAMAGED AS WELL ASSDR 2003FA0000582Control Wheel · failedPILOT SIDE CONTROL WHEEL FAILURE ON LANDING FLAIR. BRAKE ON TOP LT CORNER WHERE THE HAND GRIP MEETS THE MAIN CROSS SPOKE. THE BRAKE IS CLEAN AND SHOWS NO SIGN OF CRACKING BEFORE THE FAILURE OCCURED.SDR 2001FA0000607Magneto · failedENGINE RAN A LITTLE ROUGH WHEN STARTED. RAN SMOOTHLY AFTER WARMING UP. A 45 MIN FLIGHT WAS MADE AND THEN ENGINE WAS SHUT DOWN. THE ENGINE STARTED AGAIN WITH NO PROBLEM. ABOUT 45 MINUTES INTO THE NEXT LEG, THE ENGINE BEGAN RUNNING ROUGH AND MISSING. INITIALSDR 20010416CW007Bulkhead · crackedWHILE PERFORMING A PRE PURCHASE LOOKOVER, FOUND A STOP DRILLED CRACK IN THE UPPER RADIUS ABOVE THE LEFT RUDDER STOP BOLT. FURTHER INSPECTION FOUND ANOTHER CRACK RADIATING OUTWARD FROM THE UPPER OUTBOARD EDGE OF THE UPPER RIGHT LIGHTENING HOLE.SDR 20001012SH010Bulkhead · crackedNEW PART AS RECEIVED FROM CESSNA. RE-INSTALLATION INSPECTION FOUND THE .3750 INCH DIAMETER BOLT HOLES ELONGATED AND OVERSIZED, EXCEEDING THE ACCEPTABLE LIMITS FOR BOLT HOLES LISTED IN AD 7207-09 PARA C)2)B) AND CESSNA SL SE 72-3. DETERMINED THE FINISHING PROSDR 20001018SH003Bulkhead · crackedVISUAL INSPECTION OF BULKHEAD REVEALED A HAIRLINE CRACK .25 INCH LONG AT THE LEFT RUDDER CABLE CUT-OUT IN THE OUTER RADIUS NEAREST THE BULKHEAD FLANGE. AD 72-07-09 AND SL SE 72.3 REQUIRE INSPECTION OF THIS AREA AND BULKHEAD REPLACEMENT IF FOUND CRACKED. SUBMSDR 20000724SH022Brake Assy · failedAIRCRAFT BRAKED VERY HARD TO CLEAR RUNWAY FOR AIRLINER ON SHORT FINAL. ON TAXI BACK TO RUNWAY FOR TAKEOFF, PILOT NOTICED RT WHEEL ASSY ON FIRE. THE FIRE DEPT FOAMED AIRCRAFT. NOTE: AIRCRAFT HAS ''STC'' SPEED FAIRINGS. SUBMITTER BELIEVED THE DESIGN OF THESDR 20000508SH025Angle · rustedDURING ANNUAL INSPECTION, DISCOVERED PN 0710608-2 ANGLE HEAVILY RUSTED. AIRCRAFT ANNUAL INSPECTION COMPLETED 12 MONTHS PRIOR TO THIS INSPECTION, AND THE AIRCRAFT WAS DELIVERED FOR INSIDE STORAGE. INSPECTION DISCOVERED DRIED MUD AND DEBRIS IN THE BELLY. AIRCSDR AU991090Pushrod · broken(AUS) RIGHT PUSHROD BENT AND BROKEN. INVESTIGATION FOUND RESTRICTION IN ONE OF THE FLAP TRACK ROLLERS.SDR 97ZZZX174Angle · rustedINSPECTION OF LDG GEARBOX BULKHEAD LOWER AFT SIDE, FOUND ANGLES RUSTED COMPLETELY THROUGH IN SEVERAL LOCATIONS ON FLANGES. SUBMITTER SUGGESTED CAUSE IS DUE TO TRAPPED DIRT AND WATER AND INADEQUATE DRAIN HOLES OR LOCATION.SDR AU960620Piston Ring · wrong part(AUS) INCORRECT PISTON RING SETS FITTED TO ALL PISTONS - PNO 632932 PISTONS FITTED WHICH SHOULD HAVE RECTANGULAR TOP RINGS AS PER SB M91-4 - PISTONS WERE FITTED WITH TAPERED RINGS - DAMAGE TO PISTONS AND MINOR SCORING TO CYLINDERS - VALVE SEATS APPEAR TO BEINSDR 96ZZZX2029Fuel Cap · defectiveFUEL CAPS ARE ALLOWING WATER TO BE INTRODUCED INTO THE FUEL TANKS. SUBMITTER STATED THIS CAN CAUSE ENGINE FAILURE.SDR AU960532Fitting · corroded(AUS) LH MAIN LANDING GEAR FORGED ALUMINIUM ATTACHMENT FITTING CORRODEDON THE UPPER EDGE BENEATH THE FLOOR SHEETINGSDR AU960286Door Post · corroded(AUS) LH REAR DOOR POST CORRODED THROUGH IN AREA OF ATTACHMENT TO UNDERCARRIAGE BULKHEAD IN UNDER FLOOR AREASDR EY2R9601455Blade · damagedBLADE SN C89035YS, THREAD DAMAGESDR EY2R9600034Hub · crackedHUB CRACKED IN NR 1 SOCKETSDR 95ZZZX2707Spar · crackedAT ANNUAL INSPECTION, FOUND RT ELEVATOR SPAR CRACKED WITH ONE INCH CRACK RADIATING AWAY FROM RIVET HOLE AT OUTBOARD HINGE ATTACH. POSSIBLE TAIL SECTION IMPACT WITH T-HANGAR MAY BE A CONTRIBUTING FACTOR. REPLACED ELEVATOR SPAR.SDR 95ZZZX2953Cowl Flap · departedPILOT WAS FLYING THE AIRCRAFT EN ROUTE, 15 MINUTES INTO THE FLIGHT, A THUMP WAS HEARD, PILOT RETURNED TO THE DEPARTING AIRPORT WITHOUT FURTHER INCIDENT. INSPECTION AND INVESTIGATION REVEALED THE RIGHT COWL FLAP HAD TOTALLY SEPARATED AND DEPARTED THE AIRCRAFT,SDR 95ZZZX2715Adapter · defectiveWHEN INSPECTING FILTER ADAPTER IAW SEB 93-1R1A, FOUND FRETTING OF THE MOUNTING THREADS. THIS RENDERED THE ADAPTER UNAIRWORTHY. ADAPTER REPLACED WITH NEW UNIT.
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