Aero Commander 500 S
Service difficulty reports · 107
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 aircraft_model_key = '500S' 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 = '500S' 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 95ZZZX5959Mount · corrodedFOUND MOUNT CORROSION BETWEEN PLATE AND CAST BEAM ON ALL FOUR SIDES. AREA BETWEEN PLATE AND BEAM CAN HOLD MOISTURE. RECOMMEND REMOVE PLATES, CLEAN CORROSION. FILL WITH PRC AND REASSEMBLE. REPAIR WILL REQUIRE DER.SDR 95ZZZX5958Mount · corrodedFOUND MOUNT CORROSION BETWEEN PLATE AND CAST BEAM ON ALL FOUR SIDES. AREA BETWEEN PLATE OF BEAM CAN HOLD MOISTURE. RECOMMEND REMOVE PLATES, CLEAN CORROSION, FILL WITH PRC, AND REASSEMBLE. REPAIR WILL REQUIRE DER.SDR 95ZZZX5767Mount · corrodedCORROSION BETWEEN PLATE AND CAST BEAM ALL FOUR SIDES. AREA BETWEEN PLATE AND BEAM CAN HOLD MOISTURE. CORROSION LOCATED UNDER P/N 62003211 BLOCK. RECOMMEND REMOVE PLATES, CLEAN CORROSION. FILL WITH PRC AND REASSEMBLE. REPAIR WILL REQUIRE DER APPROVAL.SDR 95ZZZX5766Mount · corrodedCORROSION BETWEEN PLATE AND CAST BEAM ALL FOUR SIDES. AREA BETWEEN PLATE AND BEAM CAN HOLD MOISTURE. CORROSION LOCATED UNDER PN 62003211 BLOCK. RECOMMEND REMOVE PLATES, CLEAN CORROSION, FILL WITH PRC AND REASSEMBLE. REPAIR WILL REQUIRE DER APPROVAL.SDR 95ZZZX5707Trim Tab Rib · crackedDURING C/W SB 198A, PART I, CRACKS WERE FOUND RT FWD SCREW HOLE IN LEFT AND RIGHT RIBS ON BOTH TRIM TABS. FOUND NO OTHER DAMAGE AND RIBS WERE REPAIRED/MODIFIED PER SB 198A, PART II.SDR 95ZZZX3327Valve · crimp nut looseINSPECTED VALVE ASSEMBLY PER LYCOMING SB 518C. FOUND SLIGHT MOVEMENT OF NUT IN CRIMP AREA. MODIFIED VALVE IAW LYCOMING SI 1423.SDR 95ZZZX1293Spacer · stud fracturedPILOT REPORTED NO NOSE GEAR LIGHT. GROUND PERSONNEL REPORTED SEEING THE NOSE GEAR OUT. UPON LANDING, AIRCRAFT STARTED LEFT. WHEN CORRECTION WAS MADE, THE NOSE GEAR COLLAPSED. INVESTIGATION FOUND THE SHIMMY DAMPENER ROD END UNATTACHED AT THE STRUT COLLAR AS
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