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 HEEA0012119Blade · corrodedBLADE HAS DRILL HOLE IN THE SPAR FROM BELL. AFTER CLEANING THE CORROSION IN THE DRILL MARK IN THE SPAR, THE SPAR MEASURED ONLY .092" WHICH IS BELOW THE ALLOWABLE LIMIT. BLADESDR 98ZZZX267Bushing · defectiveBUSHING HAS DEFECTIVE PHONELIC LINING. REMOVED AND REPLACED.SDR AU971346Pin · broken(AUS) MAIN ROTOR BLADE PIN BROKEN OFF IN AREA OF THREADED SHANK.SDR HEEA0011717Skin · tornSKIN TORN ON THE LOWER SIDE, JUST AFT OF THE LEADING EDGE STRIP.SDR HEEA0011652Tip Cap · mismanufacturedTIP CAP NEEDS BALANCING. RECEIVED PART WITH NO FORWARD WEIGHTS, THEREFORE, TIP CAP IS LIGHT. TIME SINCE REPAIR 0:00.SDR CA971028012Tip Cap · failed(CAN) TIE DOWN WAS INSTALLED ON FORWARD AND REAR BLADE OF AIRCRAFT DUE TO HIGH WINDS. TIP CAP FAILED DUE TO FLAPPING CAUSED BY HIGH WINDS THEN FORWARD MAIN ROTOR BLADE CONTACTED WIRE STRIKE KIT, CAUSING DAMAGE TO MAIN ROTOR BLADE.SDR HEEA0011603Blade · debondedTWO UPPER FRETTING PADS UNBONDED.SDR HEEA0011598Stop Pin · wornLOWER FLAPPING STOP ON ORANGE BLADE WORN. REPLACED WITH SERVICEABLE STOP.SDR HEEA0011580Spar · crackedBLADE HAS A CRACK IN THE SPAR AT THE ROOT END. SCRAPPED BLADE.SDR CA971125003Blade · debonding(CAN) DEBONDING OF POCKET FROM MAIN ROTOR BLADE. A SECTION 8 INCHES BY 8 INCHES CAME OFF.SDR MVH0064279Pin · corrodedREMOVED BLADE PINS SN'S M10720, M9864, M10730, M10306, M10171, M10137, 8044, M9266 DUE TO CORROSION. INSTALLED NEW PINS SN'S M3081, M3020, M3023, M3024, M3025, M3039, M3187, M3227.SDR HEEA0011341Bearing · separatedBEARING SEPARATED BEYOND LIMITS.SDR HEEA0011242Blade · crackedBLADE NOSE AND NECK SHELLS CRACKED.SDR HEEA0011234Tip Cap · splitBLADE TRAILING EDGE NEAR THE TIP IS SPLIT OPEN.SDR HEEA0011232Blade · separationBLADE SEPARATION AT THE INBOARD SPLICE AREA.SDR HEEA0011226Tip Cap · damagedDAMAGED AT THE TIP END NEAR THE METAL CAP.SDR HEEA0011225Tip Cap · erosionTIP CAP HAS EROSION THROUGH THE END CAP AND FILLER CRACKED ON BOTH SURFACES.SDR 98ZZZX246Blade · debondedDISCOVERED DURING EVALUATION OF BLADE ASSEMBLY PRIOR TO SHIPMENT TO REPAIR FACILITY, TIP RIB ASSEMBLY DEBONDED.SDR 98ZZZX245Blade · debondedMALFUNCTION WAS DISCOVERED DURING 11,750 HOUR INSPECTION, M/R BLADE ROOT END LAMIMATES DEBONDED BEYOND ACCCEPTABLE LIMITS.SDR HEEA0011029Tip Cap · separationTIP CAP HAS SEPARATION ON TRAILING EDGE NEAR TIP END. ABRASION STRIP HAS A CRACK.SDR HEEA0011027Blade · defectiveBONDING BRAID BROKEN NEAR THE INBOARD END OF THE ABRASION STRIP.SDR HEEA0011026Blade · separationM/R BLADE SEPARATION ON TRIM TAB WHICH IS BEYOND REPAIRS.SDR HEEA0010987Blade · corrodedINNER GRANULAR CORROSION ON THE LEADING EDGE SPAR.SDR 97ZZZX3979Blade · crackedWHILE PERFORMING POST-FLIGHT INSPECTION, MECHANIC SAW WHAT APPEARED TO BE A CRACK IN THE UPPER SURFACE OF M/R BLADE SKIN. UPON FURTHER INSPECTION, FOUND THE SKIN WAS CRACKED AS WELL AS A VOID HAD APPEARED UNDER THE AREA OF THE CRACK.SDR HEEA0010795Bearing · failedRUBBER EXTRUSION.SDR HEEA0010794Bearing · failedRUBBER EXTRUSION.SDR HEEA0010777Tip Cap · separationTIP HAS CRACKS, SEPARATION AND PIECES MISSING FROM THE LEADING EDGE STRIP.SDR HEEA0010761Tip Cap · separationTIP CAP HAS SEPARATION OF THE TRAILING EDGE NEAR THE TIP.SDR 97ZZZX3841Blade · crackedSPAR IS CRACKED ON THE BOTTOM SIDE BACKWALL RADIUS APPROXIMATELY 112.1 INCHES FROM TIP END. SPAR AT CRACK LOCATION SHOWS NO OBVIOUS SIGNS OF DAMAGE ON THE EXTERIOR SURFACE.SDR HEEA0010617Blade · separationM/R BLADE SEPARATION ON THE INBOARD LEADING EDGE ABRASION STRIP BEYOND THE MAX LIMITS.SDR CA970722013Bushing · rotating(CAN) BLADE PIN BUSHING ROTATING.SDR 97ZZZX4658Blade · crackedM/R BLADE FAILED BLADE INSPECTION. EXCESSIVE SKIN BULGING AND CRACKS.SDR 97ZZZX4657Blade · crackedM/R BLADE FAILED BLADE INSPECTION. EXCESSIVE SKIN BULGING AND CRACKS.SDR 97ZZZX4595Blade · crackedFAILED BLADE INSPECTION. EXCESSIVE SKINS CRACKS AND BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 97ZZZX4594Blade · crackedFAILED BLADE INSPECTION. EXCESSIVE SKINS CRACKS AND BUILDING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR HEEA0010422Blade · crackedONE BLADE HAS CRACKED SKIN AND PEELING PAINT ON BOTH BLADES.SDR HEEA0010421Tip Cap · crackedTIP CAP HAS LEADING EDGE ABRASION STRIP CRACK IN SEVERAL AREAS, ONE HAS SEPARATION NEXT TO THE CRACK.SDR 97ZZZX3454Blade · crackedBLADE HAS A COMPLETE CHORD-WISE CRACK IN THE NICKEL LEADING EDGE ABRASION STRIP LOCATED 170 INCHES FROM THE ROOT END OF BLADE. THE NICKEL STRIP IS SEPARATED OUTBOARD OF THE CRACK ON LOWER SIDE, 12 INCHES ALONG TRAILING EDGE OF STRIP AND INBOARD OF THE CRACK 2SDR CA970722011Bushing · rotating(CAN) BLADE PIN BUSHINGS ROTATING.SDR HEEA0010281Blade · crackedBLADE NOSE AND NECK SHELLS CRACKED.SDR HEEA0010237Blade · crackedM/R BLADE NOSE AND NECK SHELLS CRACKED.SDR CA970731018Blade · cracked(CAN) THREE INCH CRACK FOUND IN THE LOWER SKIN OF A MAIN BLADE. CRACK LOCATED 53 INCHES IN FROM THE BLADE ROOT. CRACK RUNS 90 DEGREES FROM LEADING EDGE.SDR 97ZZZX4593Blade · crackedFAILED BLADE INSPECTION. EXCESSIVE SKINS CRACKS AND BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 97ZZZX4592Blade · crackedFAILED BLADE INSPECTION. EXCESSIVE SKINS CRACKS AND BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR HEEA0010123Blade · wornBLADE WORN.SDR 97ZZZX3013Blade · crackedBLADE OPERATED BY ERICKSON FOR APPROXIMATELY 350.0 HOURS AND WAS REMOVED FOR A BLACK BIM INDICATION. A NITROGEN LEAK WAS DETECTED BETWEEN BLADE POCKETS NR 24 AND NR 25 ON THE LOWER SPAR SURFACE. IT APPEARED TO ORIGINATE UNDER AN APPROVED MILITARY APPLIED PATSDR HEEA0010079Tip Cap · crackedCRACK IN THE LEADING EDGE ABRASION STRIP WITH SEPARATION BEYOND LIMITS. THE "C" CHANNEL ALSO HAS SEPARATION.SDR HEEA0010078Tip Cap · splitTIP CAP HAS THE TRAILING EDGE SPLIT OPEN NEAR THE TIP.SDR HEEA0010077Blade · crackedBLADE IS CRACKED. NOSE SHELL CRACKED.SDR HEEA0010076Blade · crackedBLADE IS CRACKED. NOSE AND NECK SHELLS CRACKED. THE TIP CAP IS ALSO UNBONDED.
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