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.
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
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 CA990630003Blade · cracked(CAN) DURING SCHEDULED MAINTENANCE, A 3 INCH CHORDWISE CRACK WAS FOUND ON THE M/R BLADE. THIS CRACK WAS LOCATED 36 INCHES OUTWARD FROM THE BLADE ROOT.SDR 99ZZZX2531Tip Cap · misinstalledWHILE ATTEMPTING TO INSTALL TIP CAP ONTO MAIN ROTOR BLADE, DISCOVERED INSUFFICIENT CLEARANCE BETWEEN INNER DOUBLERS - WILL NOT FIT FORWARD END OF TIP PLATE. COMPONENT P/N 76150-09100-952.SDR CA990630002Blade · cracked(CAN) DURING SCHEDULED MAINTENANCE, A 6 INCH CHORDWISE CRACK WAS FOUND ON THE LOWER SURFACE OF THE M/R BLADE. THE CRACK STARTED AT APPROXIMATELY 78 INCHES OUTWARD FROM THE BLADE ROOT.SDR 99ZZZX3211Bushing · wornBUSHINGS WORN ON MAIN ROTOR. REF: MCN 34. REMOVED AND REPLACED.SDR HEEA061726Blade · won't trackUNABLE TO TRACK MAIN ROTOR BLADE.SDR HEEA061725Blade · won't trackUNABLE TO TRACK MAIN ROTOR BLADE.SDR HEEA061724Blade · won't trackUNABLE TO TRACK AND BALANCE BLADE.SDR HEEA061615Blade · splitTRAILING EDGE SPLIT OPEN NEAR THE OUTER TIP.SDR HEEA061614Blade · splitTRAILING EDGE SPLIT OPEN NEAR THE TIP.SDR HEEA061705Abrasion Strip · damagedOUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.SDR HEEA061704Abrasion Strip · damagedOUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.SDR HEEA061703Abrasion Strip · damagedOUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.SDR HEEA061702Doubler · crackedTRAILING EDGE DOUBLER ON BLADE HAS THREE CRACKS. THE LAST CRACK IS 10.75 INCHES FROM THE INBOARD END.SDR HEEA061701Abrasion Strip · damagedOUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.SDR HEEA061700Abrasion Strip · crackedOUTBOARD LEADING EDGE ABRASION STRIP ON BLADE CRACKED AT THE SPLICE JOINT.SDR HEEA061699Abrasion Strip · separatedBOTH LEADING EDGE STRIPS ON BLADE SEPARATED AT THE SPLICE JOINT BEYOND LIMITS.SDR HEEA061698Blade · won't trackUNABLE TO TRACK AND BALANCE BLADE.SDR HEEA061697Blade · tornOUTBOARD LEADING EDGE STRIP ON BLADE HAD PIN HOLES THROUGH AND EROSION SHIELD TORN AT THE TIP END.SDR HEEA061669Blade · won't trackCOULDN'T TRACK BLADE.SDR HEEA061612Blade · bulgingLEADING EDGE BULGING OUTWARD.SDR HEEA061611Blade · separatedLEADING EDGE SPLICE SEPARATED AND BLADE IS DUE FOR TIME EXTENSION.SDR HEEA061610Blade · crackedLEADING EDGE CRACKED AND SEPARATION AT STATIONS 145 AND 168.SDR HEEA061609Blade · crackedLEADING EDGE SEPARATED AND CRACKED AT STATIONS 65 AND 76 ON MAIN ROTOR BLADE.SDR HEEA061608Blade · brokenEXTREME TRAILING EDGE AND TIP BROKEN OFF.SDR HEEA061607Blade · brokenFIBERGLASS BETWEEN THE INNER AND OUTER DOUBLER ON THE UPPER SURFACE IS BROKEN.SDR HEEA061606Blade · separatedINTERNAL DOUBLER SEPARATED ON TIP CAP.SDR 99ZZZX1952Blade · corrodedDURING DAILY INSPECTION FOUND TRAILING EDGE EXTRUSION HEAVILY CORRODED.SDR 99ZZZX3259Blade · crackedOUTBOARD TRIM TAB CRACKED.SDR 99ZZZX3258Blade · crackedOUTBOARD TRIM TAB CRACKED.SDR 99ZZZX3257Blade · crackedOUTBOARD TRIM TAB CRACKED.SDR 99ZZZX3256Blade · crackedOUTBOARD TRIM TAB CRACKED.SDR 99ZZZX1657Blade · crackedBLADE REMOVED FROM AIRCRAFT DUE TO BIM INDICATION. ALL CRACKS WERE LOCATED ON BOTTOM SIDE OF THE BLADE. SB-64E-62-10-01, WHICH ULTRASONICALLY INSPECTS THE TWO MOST OUTBOARD BOLT HOLES ON THE TOP AND BOTTOM SIDE, WAS C/W 39.8 HOURS PRIOR TO REMOVAL OF THE BLASDR 99ZZZX1682Blade · corrodedGRIP FINGER DOUBLER CORRODED AND DEBONDED BEYOND LIMITS.SDR NZBL061027Blade · delaminatedTHIS MAIN ROTOR BLADE WAS REMOVED FOR DELAMINATED ABRASION STRIP REPLACEMENT AT 664.1 HOURS TT. SUBSEQUENT DELAMINATION ON THIS SET OF BLADES HAVE CAUSED REJECTION OF THE SET.SDR NZBL061026Blade · delaminatedTHIS MAIN ROTOR BLADE WAS REMOVED FOR DELAMINATED ABRASION STRIP REPLACEMENT AT 396.7 HOURS TT. SUBSEQUENT ABRASION STRIP DELAMINATIONS ON THIS SET OF BLADES HAVE CAUSED REJECTION OF THE SET.SDR NZBL061025Blade · delaminatedTHIS MAIN ROTOR BLADE WAS REMOVED FOR DELAMINATED ABRASION STRIP REPLACEMENT AT 664.1 HOURS TT. THE BLADE WAS NEXT REMOVED AT 846.9 HOURS TT FOLLOWING ANOTHER ABRASION STRIP DELAMINATION.SDR NZBL061024Blade · delaminatedTHIS MAIN ROTOR BLADE WAS REMOVED FOR THE REPLACEMENT OF A DELAMINATED ABRASION STRIP AT 569.4 HOURS TT. SUBSEQUENT FAILURES ON THIS SET HAVE CAUSED REJECTION OF THE FULL SET OF BLADES.SDR NZBL061023Blade · delaminatedTHIS MAIN ROTOR BLADE WAS REMOVED FOR DELAMINATED ABRASION STRIP REPLACEMENT AT 396.7 HOURS TT. SUBSEQUENT FAILURES ON THIS SET HAVE CAUSED REJECTION OF THE FULL SET OF BLADES.SDR CA990401004Folding Pin · broken(CAN) IT WAS NOTICED ON POST-FLIGHT INSPECTION THAT THE BOTTOM PART OF THE AFT GREEN M/R BLADE FOLDING PIN WAS HANGING DOWN LOWER THAN THE LEAD-LAG LINK. ALL PARTS OF THE PIN WERE STILL IN PLACE AND THE LEVER ARM WAS STILL HOLDING THE SELF-LOCKING NUT. NO VSDR 99ZZZX1681Blade · corrodedCORROSION BENEATH GRIP FINGER DOUBLER EXTENDING APPROXIMATELY 3 INCHES OUTBOARD ALONG SPAR.SDR HEEA060963Blade · debondedMAIN ROTOR TRIM TAB IS DEBONDED ALONG THE TOP INBOARD EDGE.SDR HEEA060986Blade · erodedMAIN ROTOR BLADE HAS FIBERGLASS ERODED AT CENTER JOINT, TRIM TABS CORRODED.SDR CA990318062Bearing · brinnelling(CAN) INNER RACE OF FLAPPING HINGE BEARING WAS FOUND BRINNELLED (.001 INCH).SDR 99ZZZX1950Blade · debondedDURING DAILY INSPECTION FOUND CORROSION AND DEBONDING AT SKIN/SPAR BENEATH LOWER GRIP FINGER DOUBLER.SDR HEEA060639Blade · damagedBLADE DAMAGED ON THE UPPER SURFACE CENTER AT STA 120.SDR HEEA060638Blade · damagedOUTBOARD LEADING EDGE STRIP HAS EROSION HOLES.SDR HEEA060637Blade · tornEROSION SHIELD TORN ON THE OUTER END.SDR HEEA060636Blade · mismanufacturedWILL NOT FLY WITH OTHER BLADE SINCE THE NEW 18 INCH DOUBLER WAS BONDED NEAR THE TIP.SDR 99ZZZX1480Blade · delaminatedMAIN ROTOR BLADE DELAMINATED AT LEADING EDGE ABRASION STRIP BOND. DELAMINATION WAS FOUND BEYOND LIMITS. TSN: 846.9. THIS MAIN ROTOR BLADE WAS REPAIRED AT TSN: 664.1 FOR SAME DISCREPANCY AS NOTED 6-23-98.SDR 99ZZZX4027Bushing · wornTEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Back to JASC 6210