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 = '337G' 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 = '337G' 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 CA980311016Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADES WERE REPAIRED IN THE FIELD AND FOUND TO BE BELOW MANUFACTURERS MINIMUM WIDTHS (LIMITS).SDR 97ZZZX3017Spring · brokenCUSTOMER COMPLAINED THAT UPON PERFORMING REAR ENGINE MAGNETO CHECK, ONE MAGNETO PRODUCED NO DROP, THE OTHER MAGNETO WOULD CAUSE ENGINE DECELERATE TO THE POINT OF STOPPING. MAGNETO'S WERE REMOVED AND INSPECTED. FOUND IMPULSE COUPLING SPRING BROKEN. THIS IS TSDR CA970722043Gear Switch · bent(CAN) NOSE WHEEL RETRACTED AND COULD NOT BE EXTENDED DUE TO FAILURE OF THE SQUAT SWITCH BRACKET TO MAKE POSITIVE CONTACT WITH THE SWITCH. THE AIRCRAFT MADE A NOSE WHEEL GEAR UP LANDING.SDR 96ZZZX5555Bulkhead · defectiveSPINNER BULKHEAD RECEIVED FORM CESSNA WITH HEAVY TOOL MARKS IN THE RADIUS OF THE INNER FLANGE. THE MOUNTING BOLT HOLES DO NOT LINE UP BETWEEN THE FLANGE AND FLANGE DOUBLER. ALSO, DEEP SANDING MARKS AT BOLT HOLE AREA AND UNDER AND AROUND RIVET BUCK TAILS OF FSDR CA960927007Alternator · broken drive(CAN) THE ALTERNATOR FAILED IN FLIGHT AND GROUND INSPECTION REVEALED THE DRIVE SHAFT HAD SHEARED.SDR CA960715011Alternator · broken shaft(CAN) THE ALTERNATOR DRIVE SHAFT FAILED AT THE BASE OF THE ALTERNATOR. THIS SHAFT APPEARED TO BE CRACKED OR HAD A PREVIOUS FLAW. THIS ALLOWED THE REMAINING SHAFT AND DRIVE GEAR TO MOVE FORWARD RUBBING ON THE CAM GEAR. THE RUBBER BUSHING, P/N 632050, AND METAL SDR CA960604003Cylinder · not firing(CAN)IN CRUISE AT 9.5K, ENGINE RAN ROUGH AND BACKFIRED, SHUTDOWN.SDR CA960502049Piston Pin · fractured(CAN) CLIMBING THROUGH 5,200 FEET, REAR ENGINE RPM STARTED FLUCTUATING 200-300 RPM. OIL PRESSURE DROPPED TO ZERO, ENGINE FEATHERED. ENGINE TEARDOWN REVEALED BROKEN PISTON PIN. SUPERIOR AIR PART.SDR CA960422010Bulkhead · cracked(CAN)FRONT ENGINE SPINNER BULKHEAD ASSEMBLY CRACKED IN NUMEROUS PLACES STARTING AT THE PROP MOUNTING HOLES AND RUNNING TO THE OUTSIDE DIAMETER.SDR CA960422009Bulkhead · cracked(CAN)REAR ENGINE PROP SPINNER BULKHEAD ASSEMBLY CRACKED IN NUMEROUS PLACES STARTING AT THE PROP MOUNTING HOLES RUNNING RADIALLY TO OUTER DIAMETER.SDR CA960422008Cylinder Head · cracked(CAN)FRONT ENGINE #5 CYLINDER CRACKED APPROXIMATELY 3 INCHES LONG ACROSS THE ROCKER ARM CAVITY AREA.SDR CA960223006Drive Assembly · poles adrift(CAN)CUSTOMER BROUGHT IN THE ALTERNATOR FOR TEST AND REPAIR. DISASSEMBLY FOUND THE ROTOR ASSEMBLY LOOSE FROM THE SHAFT AND ABLE TO ROTATE ON THE SHAFT ABOUT 10 DEGREES.SDR AU960122Control Cable · corroded(AUS) FORWARD ENGINE PROPELLER PITCH CONTROL CABLE CORRODED INTERNALLY AND STIFF TO OPERATE - CABLE WAS PURCHASED NEW ON 14/1195 AND HAS BEEN IN SERVICE FOR LESS THAN THREE MONTHS - SUSPECT CABLE WAS INSUFFICIENTLY LUBRICATED AT MANUFACTURE WHICH ALLOWED CORROSDR 95ZZZX4474Spar · brokenAT ANNUAL, FOUND RIGHT RUDDER SPAR BROKEN AT BALANCE WEIGHT RIB ATTACH.
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