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 = 'P206B' 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 = 'P206B' 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 CA140226001Axle · corroded(CAN) DURING CPCP INSPECTION, WHILE ACCOMPLISHING SID 32-13-01, CORROSION WAS FOUND IN INNER BORE OF AXLE. AXLE WAS REPLACED.SDR CA140212006Bracket · cracked(CAN) DURING CPCP INSPECTION OF ACFT. SUPPLEMENTAL INSPECTION NR 57-51-01, AILERON SUPPORT STRUCTURE INSPECTION. RT WING INBD AILERON BRACKET ASSY WAS FOUND TO HAVE MULTIPLE CRACKS IN BEND RADIUS WHERE IT ATTACHES TO REAR SPAR. PART WAS REPLACED WITH NEW ASSSDR 2008FA0000364Trim Switch · inoperativePILOT REPORTED IN FLIGHT WHEN AUTOPILOT/ELECTRIC TRIM ENABLE, TRIM SERVO "RAN ON", WHEN ELECTRIC TRIM TURNED OFF MANUAL TRIM WHEEL OPERABLE AND NO MALFUNCTION OF SYSTEM NOTED, UPON INSPECTION NOTICED SOLDERED CONNECTION ON BASE OF SWITCH BENT AND JUMPED BETWEESDR AU990732Bulkhead · cracked(AUS) FUSELAGE AFT BULKHEAD LOCATED AT STN 209.0 CRACKED IN THE UPPER RT CORNER ADJACENT TO THE RT HORIZONTAL STABILIZER ATTACHMENT FITTING.SDR AU990731Frame · cracked(AUS) LEFT DOORPOST FRAME CRACKED. FUSELAGE SKIN RIVETS LOOSE IN AREA ADJACENT TO THE WING STRUT.SDR 99ZZZX96Support · crackedDURING AN ENGINE CHANGE, THE ALTERNATOR SUPPORT BRACKET WAS FOUND CRACKED. THE CRACK WAS ABOUT 1.25 INCHES LONG AND SEEMS TO HAVE STARTED AT THE MANUFACTURER'S WELD. CESSNA SIL SE 79-5 CALLS FOR REPLACEMENT OF THIS PART WITH AN INTEGRAL ENGINE MOUNT LEG/ALTESDR CA980623021Cylinder · separated(CAN) NR 5 CYLINDER WAS FOUND TO HAVE A CYLINDER SEPARATION.SDR CA970909007Collar · broken(CAN) THE AIRCRAFT IS USED FOR TRANSPORTING SKY DIVERS AND IS SUBJECT TO LONG TAKEOFF RUNS AND CROSSWINDS. THIS CONDITION SUBJECTS THE LANDING GEAR STRUT TO HIGH STRESS LOADS WHICH CONTRIBUTED TO THE STRUT COLLAR FAILURE.SDR AU970418Crankshaft · failed(AUS) ENGINE CRANKSHAFT FAILED FROM CRACKING AT THE REAR FILLET RADIUS OF NO2 MAIN BEARING JOURNAL DUE TO FRICTION FROM CONTACT WITH THE BEARING SHELLSSDR EY2R9601557Blade · strippedBLADE SN EJ247YS, THREADS CHIPPEDSDR EY2R9601556Blade · damagedBLADE SN EJ299YS, THREADS CHIPPED.SDR CA960620009Gasket · leaking(CAN) SLIGHT LEAK AT FUEL PUMP BODY GASKET REPLACEDSDR EY2R9600279Cylinder · corrodedPROP ASSY CYLINDER IS CORRODEDSDR 95ZZZX6028Door · departedRT CABIN DOOR WAS HEAVILY MODIFIED FOR SKY DIVING APPLICATIONS. FORWARD LATCH PIN WAS WORN AND ALLOWED DOOR TO UNLATCH IN-FLIGHT. DUE TO THE HIGH SPEEDS INVOLVED, THE DOOR BROKE IN HALF AND DEPARTED THE AIRCRAFT.SDR 96ZZZX2148Channel · rivets shearedDURING ROUTINE PROPELLER REMOVAL FOR OVERHAUL, DETERMINED 6 AN470 4-4 RIVETS COMPLETELY SHEARED OFF AND MISSING FROM RIGHT FRONT ENGINE SUPPORT AND CHANNEL ASSY, PN 1213433-14, AND SUPPORT, PN 1213433-17. FURTHER INSPECTION REVEALED NO OTHER DAMAGE OR SHEAREDSDR 96ZZZX2147Support · rivets shearedDURING ROUTINE PROPELLER REMOVAL FOR OVERHAUL, DETERMINED 6 AN470 4-4 RIVETS COMPLETELY SHEARED OFF AND MISSING FROM RIGHT FRONT ENGINE SUPPORT AND CHANNEL ASSY, PN 1213433-14, AND SUPPORT, PN 1213433-17. FURTHER INSPECTION REVEALED NO OTHER DAMAGE OR SHEARED
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