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 = '150M' 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 = '150M' 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 CA960131009Nozzle Assembly · malfunctioning(CAN) AT GROUND RUN-UP AT 15 DEGREES C AT 1700 RPM, SAME PROBLEM AS SDR 960131010. THE NOZZLE HAD BEEN CHANGED ON 3 APRIL 1995. THE AIRCRAFT WAS FLOWN FOR 436.9 HOURS WITHOUT A SIMILAR PROBLEM - HAVE CHANGED THE CARBURETOR, INSTALLED MA-3SPA P/N 10-4894V, S/N SDR 96ZZZX71Quick Drain · failedCOMPONENTS FELL OUT OF THE OIL QUICK-DRAIN. SUBMITTER SUGGESTS RE-DESIGN SO IT CANNOT HAPPEN AGAIN.SDR 95ZZZX6553Elt · defectiveDURING THE ANNUAL INSPECTION REQUIRED BY FAR91.207(D), THE POINTER ELT WOULD NOT OPERATE USING THE G-SWITCH TEST. WHEN SWITCHED TO THE 'ON' POSITION, IT WOULD ONLY WORK WHEN THE CASE WAS BUMPED, AND WHEN IT DID WORK, THE OUTPUT WAS WEAK.SDR 95ZZZX4351Control Arm · fracturedINSPECTION FOUND CARBURETOR AIR INTAKE HOUSING ASSEMBLY WITH CARBURETOR HEAT CONTROL ARM FRACTURES.SDR 95ZZZX3208Elt · rupturedAT ANNUAL INSPECTION, FOUND ELT CASE HAD RUPTURED VIOLENTLY DESTROYING ELT, BATTERIES HAD NOT RUPTURED. THERE WAS NO CORROSION ON AIRFRAME. ELT HAD BEEN OVERHAULED IN 1992, BATTERIES WERE 2 YEARS OLD. THIS IS SECOND SHARC 7 ELT FOUND IN THIS CONDITION IN 2 YSDR 95ZZZX1608Flange · crackedWHILE REMOVING WHEEL TO ROTATE TIRE, FOUND BOTH INBD FLANGES NEXT TO BRAKE DISK CRACKED. TAB FLANGE FOR COVER DELAMINATED BOTH SIDES OF TAB. CRACKS IN RELIEVED AREA .1250 INCH TO .50 INCH LONG. THE 1 INCH REPLACEMENT FLANGE ALSO CRACKED. HEAT FROM BRAKE DISDR 95ZZZX1607Spar · corrodedAFTER REMOVING HEADLINER TO REPLACE SPEAKER, FOUND REAR CARRY-THROUGH SPAR WITH CORROSION. CORROSION NOT VISIBLE WITH HEADLINER IN PLACE. SUSPECT LINER IS HOLDING MOISTURE THAT GETS IN AROUND WING TO FUSELAGE FAIRING ASSY.SDR 95ZZZX2714Valve Guide · failedENGINE MAJOR OVERHAULED WITH CYLINDERS SUPPLIED BY AERO AVIATION. CYLINDERS WENT 100 HOURS AND VALVE GUIDES FAILED DUE TO IMPROPER INSTALLATION. THEY WERE INSTALLED SO LOOSE THAT FIRE WAS EATING AWAY AT THE OUTSIDE OF THE GUIDE WHERE IT IS SUPPOSED TO BE A PSDR 95ZZZX951Bracket · corrodedDURING AN ANNUAL INSPECTION, SIGNS OF CORROSION WERE NOTICED AT THE BASE OF THE CENTER SEAT BELT ATTACH BRACKET. UPON REMOVAL OF BRACKET, FOUND BOTH THE BOTTOM OF THE BRACKET AND THE ALUMINUM STRUCTURE HAD EXTENSIVE AMOUNTS OF CORROSION. THIS CORROSION IS A RSDR 95ZZZX1129Engine · ran roughAD 93-18-03 AND PRECISION AIRMOTIVE SB NR MSA-2 R1, WAS DONE ON THIS CARB. AT 1521 HRS SMOH WHICH IS THE SINGLE PIECE VENTURI. IT WAS DONE BY A REPAIR STATION. AT 1771 HRS SMOH, ENGINE BEGAN TO RUN EXTREMELY ROUGH. OAT WAS ABOUT 27 DEGREES FAHRENHEIT. INVE
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