JASC 6210

Service difficulty reports · 1,561

Reports filed under 6210 · Main Rotor Blades, newest first.

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 jasc_code = '6210'
  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.

SDR HEEA954461Blade · crackedNOSE SHELL CRACKED.Mar 1, 1995 · N5029H · Bolkms BO105SSDR HEEA954460Blade · defectiveAFTER SETTING BLADE INTO GROUND TRACK AND BALANCE(.095 IPS), AIRCRAFT PICKED UP INTO A HOVER. BLADE CLIMBED OUT AND IPS READING WENT TO .6.Mar 1, 1995 · N86CH · Bolkms BO105SSDR 95ZZZX1500Blade · bulgedMAIN ROTOR BLADE BALANCE WEIGHT IS COMPRESSING DUE TO CENTRIFUGAL FORCE CAUSING THE LEAD TO BULGE THE BLADE BEYOND MANUFACTURER'S LIMITS, THUS, RENDERING THE BLADE UNSERVICEABLE.Feb 22, 1995 · N118LL · Bolkms BK117A3SDR 95ZZZX1328Blade · bulgedMAIN ROTOR BLADE BALANCE WEIGHT IS COMPRESSING DUE TO CENTIFUGAL FORCE WHICH CAUSES A BULGE IN THE BLADE OUTER SKIN BEYOND MFG'S LIMITS, RENDERING THE BLADE UNSERVICEABLE.Feb 22, 1995 · N214AE · Bolkms BK117B1SDR 95ZZZX1051Blade · defectiveMAIN ROTOR BLADE BALANCE WEIGHT IS SHIFTING DUE CENTRIFUGAL FORCE WHICH CAUSES LEAD WEIGHT TO BULGE THE BLADE OUTER SKIN BEYOND MFG'S LIMITS RENDERING THE BLADE UNSERVICEABLE.Feb 22, 1995 · N214AE · Bolkms BK117B1SDR 95ZZZX2077Blade · separationSEPARATION AT ROOT END OF BLADE. REMOVED AND REPLACED BLADE.Feb 17, 1995 · N365WM · Aerosp AS365N2SDR HEEA954324Blade · crackedNOSE AND NECK SHELL CRACKED NEAR THE CUFF AREA. THE INBOARD LEADING EDGE STRIP HAS SOME SEPARATION BUT WITHIN LIMITS.Feb 6, 1995 · N5418A · Bolkms BO105SSDR HEEA954323Blade · crackedNOSE AND NECK SHELL CRACKED NEAR THE CUFF AREA.Feb 6, 1995 · N5418A · Bolkms BO105SSDR 95ZZZX1090Blade · crackedDURING A PRE-FLIGHT INSPECTION, PILOT IDENTIFIED THE SUSPECTED DEFECT AND NOTIFIED MAINTENANCE. UPON INSPECTION, A CRACK WAS DETECTED ON THIS MAIN ROTOR BLADE AT STATION 1360MM. CRACK LENGTH WAS 150MM CORDWISE. AS355 MAIN ROTOR BLADES HAVE A HISTORY OF THISJan 20, 1995 · N707WR · Aerosp AS355F1SDR HEEA954241Blade · crackedCRACK IN THE SKIN OF THE LOWER SIDE LOCATED AT STATION 2228MM. THE CRACK STARTS 45MM FROM THE TRAILING EDGE AND EXTENDS TO 96MM FROM THE TRAILING EDGE.Jan 15, 1995 · N5786D · Aerosp AS355F1SDR 95ZZZX1330Blade · crackedDURING INSPECTION, FOUND 9 INCH CRACK ON LOWER SIDE, 7 FEET FROM ROOT END.Jan 12, 1995 · N736H · Bell 212
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