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 CA980504003Blade · dented(CAN) PILOT LANDED TOO CLOSE TO A TREE. TREE STRIKE RESULTED IN DENTS TO BOTH BLADES NEAR THE TIPS.SDR HEEA0013208Grip · wornDRAG BRACE BUSHINGS AND PITCH HORN BORES WORN BEYOND LIMITS.SDR HEEA0013193Blade · tornUPPER EROSION SHIELD TORN AND SEPARATED AT THE OUTBOARD END.SDR HEEA0013173Blade · separatedABRASION STRIP SEPARATED ON THE INBOARD END BOTH SURFACES BEYOND LIMITS.SDR HEEA0013172Blade · separatedABRASION STRIP SEPARATED ON THE INBOARD END LOWER SIDE BEYOND LIMITS.SDR HEEA0013131Blade · unbondedM/R BLADE HAS FRETTING PAD UNBONDED ON LOWER LEADING EDGE SURFACE.SDR HEEA0013122Blade · crackedBLADE HAS BEEN REPAIRED PREVIOUSLY ON UPPER SURFACE AT STATION 121.25". THERE WAS EVIDENCE OF SKIN CRACK AT THE EDGE OF THE REPAIR.SDR 98ZZZX1495Blade · unbondedDURING SCHEDULED INSPECTION, FOUND LOWER ROOT FITTING TO DOUBLER BOND LINE ADHESIVE MISSING. AREA OF MISSING ADHESIVE WAS APPROXIMATELY 1 INCH LONG AND .100 INCH UNDER ROOT FITTING. BLADE WAS SENT TO BLADE REPAIR FACILITY AND FOUND TO BE UNREPAIRABLE. BLADESDR 99ZZZX747Blade · brokenAIRCRAFT WAS SECURED ON PLATFORM OFFSHORE. ALL MAIN ROTOR BLADES WERE SECURED USING SIKORSKY TIE DOWN CLAMPS. WINDS OF 80+ MPH CAUSED ONE M/R BLADE TO BREAK OFF APPROXIMATELY 3 FEET FROM ROOT. SPECIAL INSPECTION WAS C/W AND BLADE AND SPINDLE CHANGED. AIRCRSDR HEEA0012837Bearing · failedRUBBER EXTRUSION BEYOND LIMITS.SDR HEEA0012783Blade · separationM/R BLADE FIBERGLASS SEPARATED UNDERNEATH THE SPLICE TITANIUM AT STATION 112.5 ON BOTH SURFACES. THE TRIM TAB HAS SOME SEPARATION ALSO.SDR HEEA0012782Blade · defectiveBLADE TRIM TAB SPLIT OPEN AND SEPARATED.SDR HEEA0012781Blade · unbondedM/R BLADE TIP RIB UNBONDED.SDR HEEA0012779Blade · damagedPIECE OF INBOARD ABRASION STRIP MISSING ON THE TOP OUTBOARD END OF M.R BLADE.SDR HEEA0012778Blade · errodedM/R BLADE OUTBOARD LEADING EDGE STRIP WITH EROSION HOLES THROUGH THE STRIP.SDR HEEA0012777Blade · damagedHOLES IN THE M/R BLADE OUTBOARD LEADING EDGE ABRASION STRIP.SDR HEEA0012768Tip Cap · damagedBLADE END CAP OF TIP CAP IS DAMAGED.SDR CA980220001Blade · corroded(CAN) MAIN ROTOR BLADES REMOVED FROM HUB FOR MAINTENANCE. BLADE BORES WERE FOUND CORRODED BEYOND LIMITS. THIS 4TH TIME AFTER BORE BUSHING CHANGES THE CORROSION HAS REAPPEARED.SDR HEEA0012723Tip Cap · crackedM/R BLADE HAS MULTIPLE CRACKS ON LEADING EDGE ABRASION WITH SEPARATION.SDR HEEA0012701Blade · separationBLADE HAS SEPARATION AT THE TWO CENTER SCARF JOINTS BEYOND LIMITS AND A SMALL AMOUNT AT THE TIP OF THE BLADE.SDR 98ZZZX1411Blade · delaminatedNORMAL INSPECTION OF MAIN ROTOR BLADES FOUND DELAMINATED LOWER SURFACE INBOARD AT TIP. NO BLADE STRIKE.SDR 98ZZZX1410Blade · delaminatedNORMAL INSPECTION OF MAIN ROTOR BLADES FOUND DELAMINATED LOWER SURFACE INBOARD AT TIP. NO BLADE STRIKE.SDR HEEA0012577Blade · crackedBLADE HAS SKIN CRACK NEAR THE INBOARD TRIM TAB ON THE LOWER SURFACE WHERE A REPAIR WAS DONE PREVIOUSLY AT COMPOSITE TECHNICS WITH A TOTAL TIME OF 7978:15.SDR HEEA0012576Blade · defectiveUNABLE TO TRACK AND BALANCE BLADE.SDR AU980002Blade · debonded(AUS) MAIN ROTOR BLADE DOUBLER DEBONDED IN AREA OF BLADE ROOT LOWER SURFACE. DEPTH OF DEBOND 55MM (2.165IN).SDR HEEA0012432Blade · separationM/R BLADE HAS SEPARATION ON THE TRAILING EDGE DOUBLER WHICH IS BEYOND THE LIMITS.SDR HEEA0012431Blade · unbondedM/R BLADE HAS BOTH UPPER FRETTING PADS UNBONDED.SDR HEEA0012430Blade · defectiveBLADE RECEIVED FROM VENDOR WITH NO WEIGHTS IN FORWARD ROOT POCKET; BLADE IS HEAVY AND CANNOT BALANCESDR CA980430001Blade · cracked(CAN) PILOT REPORTED MR VIBRATION. ENGINEER FOUND ONE CHORDWISE CRACK FROM THE BLADE SPAR TO THE TRAILING EDGE AT APPROX 90.5 INCHES FROM THE TIP.SDR HEEA0012409Blade · defectiveM/R BLADE HAS SKIN VOID ON THE UPPER SURFACE JUST TO THE OUTBOARD OF THE MIDSPAN TAB AT STATION 208".SDR 98ZZZX1257Blade · crackedDISCOVERED DURING 500-HOUR INSPECTION, FOUND M/R BLADE SKIN CRACKED AT FORWARD EDGE OF TRIM TAB.SDR HEEA0012363Blade · separationM/R BLADE HAS SEPARATION ON THE LEADING EDGE ABRASION STRIP WHICH IS BEYOND LIMITS.SDR 98ZZZX86Blade · crackedDURING 100-HOUR INSPECTION, NOTICED PATCH ON BLADE LIFTING, REMOVED PATCH. FOUND 10 INCH CRACK RUNNING CHORD-WISE FROM REPAIR. THIS BLADE CAME FROM MANUFACTURER WITH PATCH AS NEW.SDR HEEA0012335Blade · defectiveM/R BLADE HAS VOID ON UPPER AND LOWER SURFACE AT STA. 216.5" AND 1.25". FROM TRAILING EDGE THE VOID IS APPROXIMATELY 2" IN DIAMETER. SCRAPPED BLADE.SDR 98ZZZX247Blade · damagedDISCOVERED DURING DAILY INSPECTION, FOUND M/R BLADE LEADING EDGE DAMAGED AT STA 3955 MM DUE TO IMPACT OF FOREIGN OBJECT.SDR 98ZZZX242Blade · debondedDISCOVERED DURING 11,750 HOUR INSPECTION, M/R BLADE, LOWER ROOT END LAMINATE DEBONDED BEYOND ALLOWABLE LIMITS PER SA4047-76-5, CHAPTER 2. SENT TO SIKORSKY AIRCRAFT FOR FURTHER EVALUATION/REPAIR.SDR 98ZZZX243Blade · crackedDISCOVERED DURING DAILY INSPECTION, M/R BLADE LOWER SURFACE SKIN CRACKED AT STA 1000 MM LEADING EDGE EROSION STRIPS DEBONDED. REPAIRED BY CTI, RETURNED TO SERVICE.SDR 98ZZZX250Blade · delaminatedDISCOVERED DURING DAILY INSPECTION, M/R BLADE SKIN DELAMINATED OVER SPAR AT TIP AND CORROSION OF TIP.SDR 98ZZZX475Blade · corrodedDISCOVERED DURING DAILY INSPECTION, M/R BLADE TRAILING EDGE EXTRUSION CORRODED CAUSING APPROXIMATELY 10 INCH LONG SEPARATION.SDR 98ZZZX259Blade · corrodedDISCOVERED DURING DAILY INSPECTION, M/R BLADE SKIN SEPARATED AND CORRODED AT TIP.SDR 98ZZZX258Blade · corrodedDISCOVERED DURING DAILY INSPECTION, M/R BLADE SKIN SEPARATED AND CORRODED AT TIP.SDR 98ZZZX257Blade · corrodedDISCOVERED DURING DAILY INSPECTION, SKIN CORROSION AND SEPARATION AT TIP.SDR 98ZZZX256Blade · crackedDISCOVERED DURING DAILY INSPECTION, M/R BLADE SPAR CRACKED AT TIP.SDR 98ZZZX254Blade · corrodedDISCOVERED DURING DAILY INPSECTION, M/R BLADE SKIN CORRODED AND SEPARATED AT TIP AND RAILING EDGE EXTRUSION CORRODED.SDR 98ZZZX253Blade · crackedDISCOVERED DURING DAILY INSPECTION, M/R BLADE SPAR CRACKED AT TIP.SDR 98ZZZX252Blade · corrodedDISCOVERED DURING DAILY INSPECTION, M/R BLADE HAD CORROSION AND SKIN DEBOND AT BLADE TIP.SDR 98ZZZX255Blade · debondedDISCOVERED DURING 500-HOUR INSPECTION, M/R BLADE TIP RIB STRAP AND DOUBLERS DEBONDED.SDR HEEA0012134Blade · separationBLADE SEPARATION ON THE TRIM TAB WHICH IS BEYOND LIMITS.SDR HEEA0012133Blade · separationBLADE SEPARATION ON THE TITANIUM AND NICKEL ABRASION STRIP WHICH IS BEYOND LIMITS. SENT TOSDR CA971219004Pin · broken(CAN) ON POST-FLIGHT INSPECTION, A BROKEN BLADE PIN WAS FOUND ON THE YELLOW BLADE. THE FOLDING BLADE PIN HAD STAYED TOGETHER. NO DAMAGE TO THE MAIN ROTOR BLADE ON THE LEAD LAG LINKS.
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