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 99ZZZX1224Blade · corrodedDISCOVERED DURING DAILY INSPECTION, CORROSION AND SEPARATION AT TIP.SDR 99ZZZX1283Blade · corrodedDISCOVERED DURING DAILY INSPECTION, TRAILING EDGE EXTRUSION CORRODED.SDR HEEA060362Blade · mismanufacturedMAIN ROTOR BLADES RECEIVED WITH FACTORY DEFECT.SDR HEEA060361Blade · mismanufacturedMAIN ROTOR BLADE RECEIVED WITH FACTORY DEFECT.SDR HEEA060202Blade · looseBLADE BOLT BUSHING SHIFTED POSITION.SDR HEEA060075Bearing · damagedBEARING REMOVED FROM SPINDLE ASSY S/N A134-02545 DUE TO ELASTOMERIC SEPARATION. REPLACED WITH SERVICEABLE BEARING.SDR HEEA060058Blade · debondingMAIN ROTOR BLADE HAS SKIN DEBONDING CENTER AT STATION 52 ON THE UPPER SURFACE.SDR R7MA0000562Tip Cap · separatedMAIN ROTOR BLADE TIP CAP TRAILNG EDGE SEPARATING. (X)SDR 99ZZZX1949Blade · debondedDURING DAILY INSPECTION FOUND CORROSION AND DEBONDING AT SKIN/SPAR BENEATH GRIP FINGER DOUBLER.SDR 99ZZZX901Blade · crackedDURING DAILY INSPECTION, FOUND CRACK 1.75 INCHES LONG COMING FROM DOUBLER ON LOWER SIDE OF BLADE. THERE IS A DELAMINATION AREA FROM EDGE OF CRACK AFT APPROXIMATELY 1 INCH AND APPROXIMATELY .50 INCH UNDER DOUBLER. BLADE REMOVED FOR REPAIR.SDR 99ZZZX46Blade · corrodedDISCOVERED DURING DAILY INSPECTION, HEAVY CORROSION ALONG TRAILING EDGE (APPEARS TO BE INTERGRANNULAR CORROSION IN TRAILING EDGE EXTRUSION).SDR 99ZZZX45Blade · corrodedDISCOVERED DURING DAILY INSPECTION, HEAVY CORROSION ALONG T/R, (APPEARS TO BE INTERGRANNULAR CORROSION IN TRAILING EDGE EXTRUSION).SDR 99ZZZX44Blade · corrodedDISCOVERED DURING DAILY INSPECTION, HEAVY CORROSION ALONG TRAILING EDGE (APPEARS TO BE INTERGRANNULAR CORROSION IN TRAILING EDGE EXTRUSION).SDR 99ZZZX43Blade · corrodedDISCOVERED DURING DAILY INPSECTION, HEAVY CORROSION ALONG TRAILING EDGE (APPEARS TO BE INTERGRANNULAR CORROSION IN TRAILING EDGE EXTRUSION).SDR CA981230006Blade · cracked(CAN) ON PRE-FLIGHT, FOUND CRACK AND SLIGHT VOID IN THE TIP OF THE MAIN ROTOR BLADE.SDR HEEA0016863Cover · crackedPOTTING COMPOUND ON BOTTOM OF BLADES TRAILING EDGE WEIGHT POCKET CRACKING AND FLAKING OFF AND CAUSING COVER TO CORRODE. (3 EACH BLADES). REMOVED OLD POTTING COMPOUND AND CLEANED CORROSION ON COVER. TREATED AREA AND PRIMED AREA. FILLED LOW AREAS OF COVER WSDR HEEA0016830Blade · crackedCRACK ON THE LOWER SIDE OF BLADE.SDR HEEA0016829Blade · crackedCRACK ON THE LOWER SIDE OF BLADE.SDR HEEA0016828Blade · crackedCRACK ON THE LOWER SIDE OF BLADE.SDR 98ZZZX4437Blade · crackedDURING DAILY INSPECTION, FOUND TIP CAP DOUBLER CRACKED. WHEN TIP CAP WAS REMOVED FOR REPLACEMENT, AFT TIP CAP ANCHOR NUT SUPPORT CAME UNBONDED. THIS BLADE HAD 720.4 HOURS ON IT SINCE IT HAD BEEN TO OVERHAUL FACILITY FOR C-BLOCK MODIFICATION.SDR 98ZZZX4815Blade · crackedDURING COMPLIANCE OF AGUSTA TB 109-50B PT. 2, 25-HOUR MAIN ROTOR BLADE INSPECTION, A CRACK WAS FOUND STARTING FROM THE TRAILING EDGE EXTENDING CHORD-WISE FOR APPROXIMATELY 40 MM, 2070 MM FROM THE BLADE ROOT.SDR CA981123002Blade · cracked(CAN) ON DAILY INSPECTION, CHORDWISE CRACK FROM TRAILING EDGE AT 130CM OUTBOARD FROM BLADE ROOT MOUNTING PIN.SDR HEEA0016555Blade · contaminatedBLADE TIP EXTREMELY HEAVY, SUSPECT WATER IN BLADE.SDR HEEA0016554Blade · contaminatedBLADE TIP EXTREMELY HEAVY, SUSPECT WATER IN BLADE.SDR HEEA0016248Blade · unbondedTRIM TAB UNBONDED DURING TRACKING AND BALANCING OF AIRCRAFT.SDR HEEA0016247Blade · tornFIBERGLASS TORN AT STA 120 ON THE UPPER SURFACE JUST AFT OF THE LEADING EDGE STRIP. THE NICKEL STRIP HAS NUMEROUS AMOUNT OF CRACKS.SDR HEEA0016202Blade · crackedMAIN ROTOR BLADE CRACKED.SDR HEEA0016186Blade · wornLEADING EDGE STRIP OUTBOARD SEPARATED BEYOND LIMITS. ALSO HAS EROSION HOLE ON THE OUTBOARD END. THE TOP AFT FRETTING PAD IS UNBONDED.SDR AU981343Blade · delaminated(AUS) MAIN ROTOR BLADE DELAMINATED. PART TC: 6,347.SDR CA981022003Blade · cracked(CAN) ON SCHEDULED MAINT, CRACK ON TOP OF BLADE, 10.25 INCHES LONG FROM TRAILING EDGE FORWARD, 1/3 DISTANCE FROM HUB TO TIP, NEAR 'YELLOW' CENTER OF BALANCE STRIP.SDR HEEA0016106Blade · improper partTHIS BLADE CANNOT BE USED ON A/C S/N 53159 PER PER T.B. 407-98-8.SDR CA981022002Blade · malfunctioned(CAN) M/R BLADE BIM INDICATION IN-FLIGHT. BLADE REMOVED AND SENT FOR TESTING IAW S61 MAINT MANUAL. SPAR PRESSURE TESTED FOR 10 DAYS. BLADE RETURNED TO SERVICE. 70 FLIGHT HOURS LATER, SAME INDICATION RECURRED.SDR AU981241Pin · broken(AUS) MAIN ROTOR BLADE RETAINING PIN BROKEN. PART TC: 4,180.SDR HEEA0016027Blade · mismanufacturedBLADE TIP TOO HEAVY FROM VENDOR.SDR CA980922009Blade · cracked(CAN) DURING A FUEL STOP, ENGINEER FOUND CRACK IN BLADE. NO ABNORMAL FLIGHT CHARACTERISTICS. CRACK RUNS FROM THE INBOARD CORNER OF THE TRIM TAB, FORWARD TO THE SPAR AND THEN INBOARD ALONG THE SPAR FOR 6 INCHES. BELL ASB 205-96-67 IS BEING DONE DAILY, BUT THISDR 98ZZZX3617Blade · crackedCRACKS FOUND IN M/R BLADE TRIM TAB AREA. SUSPECT TRIM TAB BENDING TOOL.SDR 98ZZZX3616Blade · crackedCRACKS FOUND IN M/R BLADE TRIM TAB AREA. SUSPECT TRIM TAB BENDING TOOL.SDR CA981006004Blade · cracked(CAN) ON INSPECTION, CRACK NOTICED ON UNDERSIDE OF BLADE AT STA 75. CRACK IS 6 INCHES LONG.SDR 99ZZZX1235Blade · corrodedDISCOVERED DURING DAILY INSPECTION, CORROSION AND SEPARATION AT TIP.SDR 99ZZZX1234Blade · corrodedDISCOVERED DURING DAILY INSPECTION, CORROSION AND SEPARATION AT TIP.SDR 99ZZZX1223Blade · peelingDISCOVERED DURING 500-HOUR INSPECTION, UPPER SURFACE PAINT PEELING EXCESSIVELY.SDR AU981088Blade · faulty(AUS) MAIN ROTOR BLADES FAULTY. BLADES FAILED TO MEET THE REQUIREMENTS OF ALERT B.T. NR 109-106. PART TC: 3,196.SDR AU981087Blade · faulty(AUS) MAIN ROTOR BLADES FAULTY. BLADES FAILED TO MEET THE REQUIREMENTS OF B.T. NR 109-106. PART TC: 2,760.SDR HEEA0015662Blade · mismanufacturedTIP CAP DOES NOT MATCH THE HOLES ON THE TIP RIB OR THE TIP BLOCK.SDR HEEA0015639Blade · mismanufacturedBLADE UNACCEPTABLE FOR PHI USE. RECEIVED WITH FACTORY DEFECT.SDR HEEA0015638Trim Tab Assy · mismanufacturedTRIM TAB ASSEMBLY MISMANUFACTURED. COULD NOT FIT THIS TAB ON M/R BLADE DUE TO IMPROPER BONDING.SDR HEEA0015511Blade · dentedMAIN ROTOR BLADE DENT NEAR THE TRAILING EDGE AT STATION 123 ON THE LOWER SIDE.SDR CA980827009Blade · cracked(CAN) ON DAILY INSPECTION, FOUND REPAIR PATCH MISSING FROM THE UNDERSIDE OF BLADE S/N A-833. DURING REMOVAL OF RESIDUAL ADHESIVE, A CRACK WAS FOUND IN THE SKIN AT 111.25 INCHES FROM TIP AND 6 INCHES FROM LEADING EDGE. THE 20 INCH LONG CRACK ORIGINATES AT A NSDR CA980827008Blade · delaminated(CAN) ON DAILY INSPECTION, VOID FOUND IN NR 2 DOUBLER EXCEEDING LIMITS. BLADE REPLACED.SDR 98ZZZX3339Blade · crackedHELICOPTER INBOUND FOR LANDING WHEN PILOT NOTICED VIBRATION, MADE NORMAL LANDING. MAINT EXAM OF ROTOR SYS FOUND YELLOW BLADE CRACKED FROM TRAILING EDGE OF BLADE, BOTH TOP AND BOTTOM TO MAIN SPAR. CRACK LOCATED AT BLADE STA 71 OR 19.3750 INCHES FROM END OF AD
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