Lycoming O235N2C
Service difficulty reports · 55
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'O235N2C' 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 engine_model_key = 'O235N2C' 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 98ZZZX1020Coil · failedMAG COIL AT 500 HOURS BURNED THROUGH ON THE OPPOSITE SIDE OF HIGH TENSION LEAD. HAVE TO PULL COIL OUT TO SEE DAMAGED SPOT. ENGINE LOST POWER, TOOK MORE MANIFOLD PRESSURE TO MAINTAIN SAME RPM.SDR CA980302008Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADES NOT ANODIZED AT LAST OVERHAUL. CORROSION FOUND UNDER PAINT.SDR CA970507017Hub · cracked(CAN) PROPELLER RECEIVED FOR COMPLIANCE WITH FAA AD 97-06-16. ANODIZING REMOVED, LIQUID PENETRANT INSPECTION (LPI) FAILED TO FIND CRACK. EDDY CURRENT INSPECTION FOUND CRACK. CRACK AREA HOLLOWED OUT TO .040 AND CRACK WAS EVIDENT THROUGH LPI. PROPELLER WAS SCRAPSDR 97ZZZX1988Push Rod · crackedPUSH ROD CRACKED BOTH ENDS. CRACKS APPROXIMATELY .50 INCH LONG. AD'S 80-25-02K2 AND 95-03-10 DO NOT APPLY. ENGINE FACTORY REMANUFACTURED APPROXIMATELY 3300 HOURS AGO. FIELD OVERHAUL APPROXIMATELY 900 HOURS AGO. RECORDS WOULD INDICATE 3300 HOURS ON PUSH ROSDR 95ZZZX6537Pushrod · failedPUSHROD MARKED AS 73806# FAILED AT END OF PUSHROD. LYCOMING MANDATORY SB OA-522 IN CONJUNCTION WITH AD 95-03-10, WAS ACCOMPLISHED 2-16-95. NO DEFECTS IN ENGINE VALVE TRAIN OR VALVES STICKING WERE NOTED. PARTS WERE REPLACED AND ENGINE RAN OK AND RETURNED TO
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