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 MVH0064100Blade · damagedMAIN ROTOR REMOVED FOR DAMAGE TO INBOARD LEADING EDGE.SDR 96ZZZX5666Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR HEEA967551Blade · crackedBLADE IS CRACKED. (SEVERAL CRACKS ON THE TITANIUM STRIP WITH SEPARATION. THE CRACK AT STA. 123" HAS MULTIPLE BRANCHES.SDR HEEA967549Tip Cap · crackedTIP CAP IS CRACKED. (TIP CAP HAS THE ABRASION STRIP CRACK AND SEPARATED. ALSO HAS SEPARATION ON THE OUTER AND INNER DOUBLER.SDR 96ZZZX4273Blade · defectiveFOUND APPROXIMATELY 8.50 INCH SECTION OF MAIN ROTOR BLADE NICKLE LEADING EDGE STRIP MISSING APPROXIMATELY 48 INCHES FROM THE TIP CAP. THIS AREA HAD A CRACK IN THE LEADING EDGE AND IT WAS REPAIRED PER THE COMPOSITE REPAIR MANUAL. SUSPECT DISBONDING UNDER THE SDR CA960716007Blade · cracked(CAN) DURING HELI LOGGING OPERATION THE PILOT NOTICED INCREASED RIGHT PEDAL REQUIRED TO MAINTAIN POSITION. WHEN IT BECAME OBVIOUS THAT WIND CONDITIONS WERE NOT RESPONSIBLE THE HELICOPTER LANDED WHERE IT WAS FOUND THAT THE BLADE HAD A 10" CRACK CHORDWISE ACROSSSDR 96ZZZX4848Blade · crackedDAILY SERVICE CHECK FOUND M/R BLADE CRACKED ABOUT 2.50 INCHES TO ABOUT 3 INCHES RUNNING SPAN-WISE JUST OUTBOARD OF FINGERS.SDR CA960703002Blade · cracked(CAN) A BORESCOPE INSPECTION OF BLADE ROOT END REVEALED A CRACK ON LEADING EDGE OF SPAR APPROXIMATELY 2" FROM ROOT END AND APPROXIMATELY 1" IN LENGTH. EXACT LENGTH UNKNOWN AS CRACK PROCEEDS UNDER A PHENOLIC BLOCK.SDR HEEA967434Tip Cap · tornTIP CAP HAS THE SKIN TORN NEXT TO THE ABRASION STRIP ON THE LOWER SIDE.SDR 96ZZZX4348Blade · defectiveRECEIVED THE NEW BLADES AND REINSTALLED. WERE UNABLE TO TRACK AND BALANCE THE M/R SYSTEM TO AN ACCEPTABLE LEVEL DUE TO ONE BLADE BEING OUT OF TRACK AND WAS UNABLE TO CONTROL THIS PROBLEM WITH STANDARD ADJUSTMENTS.SDR 96ZZZX5757Blade Bolt · wornBLADE BOLT WORN BEYOND LIMITS. SCRAPED PARTS ON SITE. REPLACED 2 EA.SDR HEEA967413M/R Blade · crackedTHE NOSE SHELL AND NECK SHELL CRACKED.SDR HEEA967412Blade · crackedTHE NOSE SHELL CRACKED AND SEPARATED.SDR HEEA967411Blade · crackedCRACKS IN THE NOSE SHELL NEAR THE CUFF AREA.SDR HEEA967410Blade · crackedCRACKS IN THE NOSE AND NECK SHELL AT THE CUFF AREA.SDR HEEA967408Blade · corrodedHAS EXCESSIVE AMOUNT OF EXFOLIATION ON UPPER LEADING EDGE NEAR THE TIP WITH PIECE MISSING.SDR HEEA967405Tip Cap · crackedCRACKED FIBERGLASS SKIN BETWEEN THE INNER AND OUTER DOUBLER.SDR HEEA967402Blade · watwer contamBLADE IS SUSPECTED TO HAVE WATER INGRESSION.SDR HEEA967401Blade · water contamBLADE IS SUSPECTED TO HAVE WATER INGRESSION.SDR HEEA967400Blade · water contamBLADE IS SUSPECTED TO HAVE WATER INGRESSION.SDR HEEA967399Blade · water contamBLADE IS SUSPECTED TO HAVE WATER INGRESSION. (BLADE IS CUSTOMER PROPERTY)SDR HEEA967398Blade · crackedBLADE HAS A HOLE IN THE OUTBOARD LEADING EDGE STRIP.SDR HEEA967397Blade · crackedCRACKS IN THE NOSE AND NECK SHELL AT THE ROOT END.SDR HEEA967396Blade · crackedCRACKS IN THE NOSE AND NECK SHELL AT THE ROOT END.SDR 96ZZZX3484Blade Spar · crackedDISCOVERED DURING 500-HOUR INSPECTION, BLADE SPAR CRACKED AT ROOT END BUSHING HOLE.SDR HEEA967318Blade · crackedBLADE IS CRACKED. (SPAR CRACK NEAR THE ROOT END.) SCRAPPED,SDR HEEA967317Tip Cap · brokenTIP CAP OUTER TRAILING EDGE BROKEN OFF.SDR HEEA967296Blade · separationSEPARATION ON THE NICKEL STRIP AND ON THE INBOARD SECTION OF THE TRAILING EDGE.SDR HEEA967292Blade · separationLEADING EDGE SEPARATION ON THE INBOARD END UPPER AND LOWER SURFACE BEYOND LIMITS.SDR AU960690Bracket · cracked(AUS) MAIN ROTOR BLADE PENDULUM VIBRATION ABSORBER ASSEMBLIES (4OFF) LOWER PLATE BRACKETS CRACKED IN AREA OF INBOARD FLANGE DUE TOEXFOLIATION CORROSIONSDR 96ZZZX5663Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX5662Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX5661Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX5660Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX3164Blade · skin separatedINSPECTION FOUND UPPER SURFACE SKIN SEPARATED FROM SPAR AT BLADE TIP. UPON FURTHER INSPECTION, INNER SPAR WAS FOUND HEAVILY CORRODED. SUBMITTER STATED BEFORE NEW BLADE IS PUT INTO SERVICE, REMOVE TIP WEIGHT ASSY, TREAT INSIDE OF SPAR WITH ALODINE AND KORPON SDR HEEA967112Tip Cap · unbondedINBOARD END OF THE TRAILING EDGE STRIP UNBONDED. THE UPPER INTERNAL DOUBLER IS UNBONDED.SDR CA960606011Locking Pin · loose(CAN) PIP PIN USED TO HOLD BLADE BOLT IN BLADE FOLDING SETUP, MISSING BALL BEARINGS.SDR 96ZZZX5844Blade Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR HEEA967018Blade · crackedBLADE NOSE AND NECK SHELL CRACKED AND DISCOLORED BELOW ROOT/WRAP AND PENDULUM WRAP.SDR HEEA967017Blade · separationSPLICE ON THE LEADING EDGE AT STATION 168 WITH SEPARATION BEYOND LIMITS.SDR HEEA967016Tip Cap · separatedLOWER INTERNAL DOUBLER SEPARATED BEYOND THE MAX LIMITS.SDR 96ZZZX2195Blade · leakageDURING A 3-HOUR BIM CHECK, PILOT NOTED A RED BIM INDICATION. DURING A PRELIMINARY INSPECTION, LEAKAGE HAS BEEN NOTED TO BE EMANATING FROM THE SEAM BETWEEN POCKETS 19 AND 18. REPLACED BLADE IAW SIKORSKY S-58T MM.SDR 96ZZZX2589Blade · damagedDURING A PRE-FLIGHT INSPECTION, A MECHANIC FOUND M/R BLADE LEADING EDGE TORN AND RIPPED ABOUT 2I INCHES FROM THE LEADING EDGE ABRASION STRIP. THE METAL WAS IN THE PROCESS OF PEELING AWAY FROM THE BLADE. IT WAS DETERMINED THAT FOD CAUSED THE INITIAL DENT. THSDR CA960412005Blade · vibrating(CAN)MAIN ROTOR BLADES WERE REMOVED TO DO HIGH VERTICAL VIBRATION. ALTHOUGH TRACK WAS OK, THE VIBRATION SEEMED TO GET PROGRESSIVELY WORSE. REPLACEMENT BLADES P/N 3160S-13-65-000-00 WERE INSTALLED AND PROBL EM WAS ALLEVIATED.SDR 96ZZZX3593Blade Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX3592Blade Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX3591Blade Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX3590Blade Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX2588Adapter Sleeve · corrodedDURING INSPECTION, FOUND LEFT SKID SLEEVE LOOSE. UPON REMOVAL, NOTED IT WAS SEVERELY CORRODED TO THE POINT OF PENETRATION AND FAILURE OF SLEEVE. SUBMITTER STATED THIS IS THE SECOND SLEEVE THAT HAS BEEN FOUND IN THIS CONDITION, ON 2 HELICOPTERS.SDR HEEA966873Blade · defectiveREMOVE EXCESS WEIGHT AND PAINT AND REFINISH BLADES AND SEAL THE EDGE OF THE INBOARD TRIM TAB ON BLADE S/N A94.
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