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 QR9R2023100200001Blade · crackedDURING MAST MOMENT A THRU F INSPECTION, MAINTENANCE DETECTED THE RED MAIN ROTOR BLADE CRACKED IN THE SMALL RADIUS OF THE BLADE LUG. REMOVED AND REPLACED MAIN ROTOR BLADE.SDR EVCA20230919001Blade · crackedHOTIZONTAL CRACK APPROX 4" FOUND ON MAIN ROTOR BLADE ROOTSDR 2023FA0000434Bearing · damagedIN FLIGHT VIBRATION REPORTED. FOUND MRB SPINDLE BEARINGS BRINELLED. SPINDLE ASSEMBLIES P/N A005-15, SPINDLES P/N A158-3, S/N 2842 & S/N 2843, BEARING SETS P/N A159-3, S/N 2214106 & S/N 2214093. SPINDLES & BEARING SETS TSN: 435.8. NO OVERSPEEDS REPORTEDSDR QR9R2023062300004Blade · failed inspM/R BLADE UNABLE TO PASS BONDING CHECK AND IS UNSERVICEABLE (BAD FROM SUPPLY). REPLACED M/R BLADE IAW AMM 62-10-00, 4-1.SDR 2023FA0000106Bearing · debondedELASTOMERIC FEATURE OF ROD-END BEARING FAILED CAUSING LATERAL PLAY OF BEARING AND PROTRUDING SHIMS DAMAGED BLADE LAG DAMPER LUG.SDR QR9R2023020900001Bearing · crackedDURING INSPECTION OF THE VIBE ABSORBER BALL BEARING, MAINTENANCE FOUND THE BALL BEARING WAS CRACKED ALONG THE CENTER RADIUS. REMOVED AND REPLACED BALL BEARING.SDR EVCA202301240001Tab · crackedMR BLADE TRIM TAB CRACKEDSDR EVCA2023011100001Blade · crackedVAN HORN MAIN ROTOR BLADE INBOARD TAB ATTACHMENT TO BLADE SURFACE HAS CRACKS AT BOTH INBOARD AND OUTBOARD ATTACH POINTS ON BOTH UPPER AND LOWER BLADE SURFACES.SDR 2022FA0000675Bearing · brinelledPILOT REPORTED ABNORMAL AND HEAVY CYCLIC FORCES DURING AUTO-ROTATION AND LOW POWER DESCENTS. FOUND BOTH MR SPINDLES TO BE BRINELLED. REMOVED SPINDLE ASSEMBLIES AND PERFORMED MR SPINDLE BEARING REPLACEMENT IAW RHC COMPONENT MAINTENANCE MANUAL. REINSTALLED MR BLSDR 2022FA0000674Bearing · brinelledPILOT REPORTED ABNORMAL AND HEAVY CYCLIC FORCES DURING AUTO-ROTATION AND LOW POWER DESCENTS. FOUND BOTH MR SPINDLES TO BE BRINELLED. REMOVED SPINDLE ASSEMBLIES AND PERFORMED MR SPINDLE BEARING REPLACEMENT IAW RHC COMPONENT MAINTENANCE MANUAL. REINSTALLED MR BLSDR 2022FA0000514Blade · crackedMAIN ROTOR BLADE HAS A 25 MM CRACK ADJACENT TO THE WEIGHT POCKET ON THE TOP OF THE BLADE.SDR 8HBR20220829047Bearing · brinelledPILOTS REPORTED ABNORMAL CYCLIC MOVEMENTS IN FLIGHT. INSPECTION OF THE MAIN ROTOR SPINDLES SHOWED BRINELLING OF THE SPINDLE BEARINGS.SDR JYDR20220818228DBlade · crackedCRACKS IN PAINT AT BSTA 74, TOP SIDE OF BLADE. THIS INFORMATION HAS BEEN SUPPLIED TO THE MANUFACTURE AND THEY ARE INVESTIGATING.SDR JYDR20220818228BBlade · crackedCRACKS IN PAINT AT BSTA 214, TOP SIDE OF BLADE. THIS INFORMATION HAS BEEN SUPPLIED TO THE MANUFACTURE AND THEY ARE INVESTIGATING.SDR JYDR20220818228CBlade · crackedCRACKS IN PAINT AT BSTA 214, TOP SIDE OF BLADE. THIS INFORMATION HAS BEEN SUPPLIED TO THE MANUFACTURE AND THEY ARE INVESTIGATING.SDR JYDR20220817228ABlade · crackedPAINT CRACK FOUND AT BSTA 114, 214 AND 285 SKIN AREA, TOP SIDE OF BLADE. THIS INFORMATION HAS BEEN SUPPLIED TO THE MANUFACTURE AND THEY ARE INVESTIGATING.SDR 8HBR20220730046Bearing · brinelledPILOTS REPORTED: CYCLIC HARD TO PUSH FORWARD, CYCLIC JUMP WHEN LOWERING THROUGH COLLECTIVE SETTING. INSPECTION OF THE MAIN ROTOR SPINDLES SHOWED BRINELLING OF THE SPINDLE BEARINGS.SDR 2022FA0000299None · malfunctionedPILOT REPORTED THE FOLLOWING: "AT ROUGHLY 230 P.M., I WAS MAKING MY WAY BACK FROM A NORTH CANYON TOUR LANDING SOUTH TAKEOFF WEIGHT 3767 POUNDS. WINDS WERE ABOUT 9 KTS GUSTING 18 FROM THE DIRECTION OF A ABOUT 220 AND I RECEIVED VERY LITTLE TO NO TURBULENCE THOSDR 2022F00264None · malfunctionedPILOT REPORTED THE FOLLOWING: "WHILE ON THE DOWNWIND IN STRAIGHT AND LEVEL FLIGHT AT APPROXIMATELY 70KTS I REDUCED POWER FOR A 60KT AIRSPEED. THE AIRCRAFT IMMEDIATELY BEGAN AN AGGRESSIVE VERTICAL HOP MOVING ME AND THE FRONT SEAT PASSENGER ABOUT IN OUR SEATS SDR 8HBR20220228040Bearing · brinelledPILOTS REPORTED: CYCLIC HARD TO PUSH FORWARD, CYCLIC JUMP WHEN LOWERING THROUGH COLLECTIVE SETTING. INSPECTION OF THE MAIN ROTOR SPINDLES SHOWED BRINELLING OF THE SPINDLE BEARINGS. THERE WERE NO REPORTED ROTOR OVER SPEEDS ON THIS AIRCRAFT.SDR QMLA2021112420061Blade · out of balanceAIRCRAFT CONTINUED TO HAVE TRACK AND BALANCE ISSUES FOR PRIOR 2 MONTHS. EACH TIME THE TRACK AND BALANCE COULD BE ALLEVIATED BUT THE AIRCRAFT CAME BACK NOW IN ITS WORST ITERATION, READING .7 IPS VERTICAL AND .7 LATERAL. I MADE A LARGE ADJUSTMENT ON BLUE AND RECSDR 8HBR202111176038Spindle · brinelledPILOT'S REPORTING NEEDING TO USE A SIGNIFICANT INCREASE OF PRESSURE ON CYCLIC FOR FORWARD FLIGHT. ALSO NOTED LOSS OF CYCLIC PRESSURE WHEN PREFORMING AUTOROTATION'S. BRINELLING FOUND ON SPINDLE BEARINGS FOR THE SECOND TIME IN RECENT HISTORY. TIME IN SERVICE OF SDR 8HBR20211105035Spindle · brinelledPILOTS REPORTED UNUSUAL LOW FREQUENCY VIBRATIONS AND UNUSUAL CYCLIC PRESSURE IN FORWARD FLIGHT AND AUTOROTATION. UPON INSPECTION OF MR BLADE SPINDLE BEARINGS IN REFERENCE TO "TRACK AND BALANCE TROUBLESHOOTING" R22 MM SECTION 10.234 FOUND THE SPINDLE BEARINGS TSDR QR9R20210920001Blade · failed inspMAIN ROTOR BLADE FAILED RESISTANCE CHECK.SDR 8HBR20210920032Bearing · brinelledPILOT'S REPORTING NEEDING TO USE A SIGNIFICANT INCREASE OF PRESSURE ON CYCLIC FOR FORWARD FLIGHT. ALSO NOTED LOSS OF CYCLIC PRESSURE WHEN PREFORMING AUTOROTATION'S. BRINELLING FOUND ON SPINDLE BEARINGS. POSSIBLE MANUFACTURER INSTALLATION ERROR FROM ROBINSON.SDR EVCA202108064001Blade · debondedVAN HORN MAIN ROTOR BLADE TRIM TAB DEBONDED.SDR 8HBR20210920031Bearing · brinelledPILOT REPORTING NEEDING TO USE A SIGNIFICANT INCREASE OF PRESSURE ON CYCLIC FOR FORWARD FLIGHT. ALSO NOTED LOSS OF CYCLIC PRESSURE WHEN PREFORMING AUTOROTATION'S. BRINELLING FOUND ON SPINDLE BEARINGS. POSSIBLE MANUFACTURER INSTALLATION ERROR FROM ROBINSON.SDR EVCA2021072200002Blade · corrodedCORROSION FOUND ON TRAILING EDGE OF BOTH M/R BLADES.SDR EVCA202107220001Blade · corrodedCORROSION FOUND ON TRAILING EDGE OF BOTH M/R BLADES.SDR EVCA06182021Blade · damagedMAIN ROTOR BLADE SPAN-WISE WEIGHT COVER SEPARATED FROM BLADE IN FLIGHT.SDR EVCA06022021Blade · damagedMAIN ROTOR BLADE SPAN-WISE WEIGHT COVER SEPARATED FROM BLADE IN FLIGHT.SDR Z1RA76005032021Tab · missingONE INBOARD TRIM TAB MISSING DURING PREFLIGHTSDR 8HBR20210920030Bearing · brinelledPILOT'S REPORTING NEEDING TO USE A SIGNIFICANT INCREASE OF PRESSURE ON CYCLIC FOR FORWARD FLIGHT. ALSO NOTED LOSS OF CYCLIC PRESSURE WHEN PREFORMING AUTOROTATION'S. BRINELLING FOUND ON SPINDLE BEARINGS. POSSIBLE MANUFACTURER INSTALLATION ERROR FROM ROBINSON.SDR EVCA042820212Blade · corrodedBOTH MAIN ROTOR BLADE LEADING EDGES ARE PITTED AND HAVE CORROSION.SDR EVCA04282021Blade · corrodedBOTH MAIN ROTOR BLADE LEADING EDGES ARE PITTED AND HAVE CORROSION.SDR EVCA04242021(1)Blade · crackedBOTH VAN HORN M/R BLADES ARE CRACKED.SDR EVCA04242021Blade · crackedBOTH VAN HORN M/R BLADES ARE CRACKED.SDR AC2A2021033113901Blade · debondedMAIN ROTOR BLADE TIP CAP ATTACHMENT BOND LINE SEPARATION.SDR EVCA2021021903Blade · crackedORANGE MR BLADE HAS CRACK IN EROSION STRIP APPROX BLADE STA 107.SDR EVCA2021021902Blade · crackedGREEN MR BLADE HAS 2 CRACKS IN EROSION STRIP APPROX BLADE STA 104 AND 108.SDR 2021FA0000051Blade · crackedBLUE MR BLADE HAS CRACK IN EROSION STRIP APPROX BLADE STA 110.SDR 2021FA0000048Blade · damagedMAIN ROTOR BLADE DAMAGE. DURING CLIMB EXPERIENCED LOUD THUD PERFORMED PER-CAUTIONARY TO BASE LANDING FOUND HOLE THROUGH BLUE MAIN ROTOR BLADE AND LEADING EDGE DAMAGE. NO FLIGHT CONTROL DEFICIENCIES NOTED. HOLE AND DAMAGE IS LOCATED AT APROX 165 MM FROM ROOT OFSDR EVCA202010213Blade · debondedDURING ROUTINE MAINTENANCE, MR BLADE LEADING WAS FOUND DEBONDED ON UPPER SURFACE APPROXIMATELY 3 INCHES FROM TIP.SDR EVCA202010091Tab · crackedVIBRATION FELT IN CRUISE FLIGHT WHICH LESSENED AT LOWER SPEEDS. INSPECTION FOUND CRACKED TRIM TAB ON MAIN ROTOR BLADE.SDR EVCA20200811001Blade · delaminatedDURING ROUTINE INSPECTION, MAIN ROTOR BLADE SN:A-4318 EROSION STRIP HAS DELAMINATION EXTENDING 1.75 INCHES BY 1.3 INCHES FROM OUTBOARD TIP OF BLADE.SDR EVCA202007302Blade · crackedTWO CRACKS FOUND ON MAIN ROTOR BLADE NICKEL ABRASION STRIP AT BLADE STATION 204.5 EXTENDING CORD WISE 40 % AND 30% OF LEADING EDGE.SDR EVCA202007301Blade · crackedCRACK FOUND ON MAIN ROTOR BLADE NICKEL ABRASION STRIP AT BLADE STATION 203 EXTENDING CORD WISE 60% OF LEADING EDGE.SDR HDNA2020060200167Blade · crackedONE EA MAIN ROTOR BLADE FOUND TO HAVE TRAILING EDGE DAMAGED CONSISTING OF A 3.5 INCH CRACK EXTENDING CORD-WISE LOCATED 73 INCHES FROM BLADE ROOT. DAMAGE SUSPECTED TO BE FROM A LARGE BIRD IMPACT DUE TO BIRD REMNANTS BEING FOUND ON THE LT ENGINE COWLING. CREW SDR HDNA202004149494Attach Bolt · shearedGREEN M/R BLADE SECONDARY ATTACHMENT BOLT HEAD (ONLY) WAS FOUND SHEARED ON THE TECHNICIAN'S DAILY AIRWORTHINESS CHECK. INSPECTION WAS PERFORMED ON THE REMAINING SECONDARY BOLTS WITH NO DEFECTS NOTED.SDR UG8A2020030911201Attach Bolt · crackedDURING THE MAIN ROTOR INSPECTION (REMOVED) TASK 621133 STEP 37 VISUALLY FOUND A CRACK IN THE GREEN BLADE 2B BOLT RADIUS. BOLT WAS LIQUID FLUORESCANT PENETRANT INSPECTED BY AIRCRAFT NDT SERVICES (CRS N3DR341N) WHICH CONFIRMED A CRACK WAS PRESENT. CRACK WAS VE
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