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 = 'D55' 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 = 'D55' 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 AU960893Rib · corroded(AUS) VERTICAL STABILISER AFT SPAR UPPER RIB PNO 96-640000-11 AND LOWERRIB PNO 96-640000-105 SEVERELY CORRODED - RIBS SUPPORT RUDDER PIVOT FLANGES - INVESTIGATION FOUND MORE CORROSION IN FUSELAGE AND AFT CABIN FLOOR STRUCTURE, LUGGAGE DOOR FRAME - STEP SUPPORTSDR AU960579O-Ring · wrong part(AUS) PROPELLER BLADE RETENTION NUT 'O' RINGS WERE THE INCORRECT TYPE CAUSING EXCESSIVE BINDING ON FERRULE - PERSONNEL/MAINTENANCE ERROR - UNAPPROVED PARTSDR AU960033Bulkhead · cracked(AUS) FUSELAGE BULKHEADS LOCATED AT FS 257.6 AND FS 271.92 CRACKED - BULKHEADS ARE LOCATED AT THE FORWARD AND AFT HORIZONTALSTABILISER STUB SPARS - FURTHER INVESTIGATION FOUND THAT THE CRACK WAS IDENTIFIED AS A SCORE MARKSDR AU960017Bellcrank · corroded(AUS) LH RUDDER BELLCRANK SEVERELY CORRODED - AIRCRAFT IS USED TO CARRYLIVE SEAFOOD WITH SUBSEQUENT CONTAMINATION BY SALT LADEN PRODUCTSSDR AU960009Spar · corroded(AUS) LH WING SPAR CORRODED IN AREA BEHIND LH ENGINE - FOUND DURING INSPECTION IAW AD/B55/29 AMDT1 - AIRCRAFT HAD BEEN PREVIOUSLYOPERATED IN A SALT LADEN ENVIRONMENT BY THE LAST OWNERSDR 95ZZZX6562Flap · failedUPON EXITING THE AIRCRAFT, THE WEIGHT OF THE PILOT STANDING ON THE RT FLAP, TORE THE ACTUATOR ATTACH BRACKET, RIPPED THE SKIN AND PULLED THE RIB ATTACHMENT OUT OF THE FLAP. THIS CONDITION ALLOWED THE FLAP TO GO TO THE EXTENDED POSTION. IN-FLIGHT, AN UNNOTICESDR 95ZZZX3529Drive Gear · brokenFOUND ALTERNATOR HUB ASSEMBLY AND ALTERNATOR DRIVE GEAR BROKEN, CAUSE UNKNOWN.SDR 95ZZZX2261Oil Pan · crackedDURING FLIGHT, PILOT NOTICED OIL STREAMING FROM RT COWLING. INSPECTION BY MAINTENANCE PERSONNEL REVEALED A 2 INCH CRACK IN THE OIL PAN AT LOWER RADIUS. SUSPECT FATIGUE, POOR STAMPING, DURING MANUFACTURING.SDR 95ZZZX1099Cylinder · crackedDURING A 200-HOUR INSPECTION ALL CYLINDERS OF LT ENGINE PASSED A DIFFERENTIAL COMPRESSION TEST. CLOSER INSPECTION OF CLYLINDER ASSYS REVEALED CRACKS BETWEEN COOLING FINS OF SEVERAL CYLINDERS IN THE EXHAUST PORT AREA. NOTE: CRACKS ORIGINATING IN THIS AREA AR
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