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.

SDR 2006FA0001168Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Dec 4, 2006 · N511CC · Robsin R44RAVENIISDR 2006FA0001167Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Dec 4, 2006 · N424SH · Robsin R44RAVENIISDR 2006FA0001164Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Dec 4, 2006 · N424SH · Robsin R44RAVENIISDR 2006FA0001165Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Dec 3, 2006 · N424SH · Robsin R44RAVENIISDR 2006FA0001176Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Dec 3, 2006 · N69KA · Robsin R44SDR 2006FA0001175Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Dec 3, 2006 · N69KA · Robsin R44SDR 2006FA0001174Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Dec 3, 2006 · N69KA · Robsin R44SDR 2006FA0001173Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Dec 3, 2006 · N69KA · Robsin R44SDR 2006FA0001161Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Nov 9, 2006 · N424SH · Robsin R44RAVENIISDR 2006FA0001160Housing · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Nov 4, 2006 · N424SH · Robsin R44RAVENIISDR 2006FA0001166Boot · leakingFLUID LEAKING FROM MAIN ROTOR BLADE PITCH BEARING HOUSING.Nov 4, 2006 · N424SH · Robsin R44RAVENIISDR CA061018002Blade · damaged(CAN) UPON POST FLIGHT INSPECTION, A TEAR AND PROTRUTION OF THE LOWER SKIN, JUST AFT OF THE LEADING EDGE OUTBOARD ERROSION STRIP WAS DISCOVERED APPROXIMATELY 4 INCHES INBOARD FROM THE TIP OF THE BLADE AT STATION 206. (TC# 20061018002)Oct 14, 2006 · Bell 407SDR HEEA110594Blade · separatedEXPERIENCED VIBRATION DURING TAKEOFF FROM OFFSHORE PLATFORM. THE AIRCRAFT WAS RETURNED TO AND LANDED AT THE SAME PLATFORM. FOUND SKIN SEPERATION FROM LEADING EDGE ABRRASION STRIP AT TIP APPROXIMATELY 1.5 INCHES CHORDWISE X 9.75 INCHES SPANWISE.Aug 2, 2006 · N27805 · Bell 212SDR CA060706002Blade · cracked(CAN) CRACK ON BOTH SIDES OF BLADE BOLT BORE. TRAVELLING IN CHORDWISE DIRECTION. THE LEADING EDGE CRACK TRAVELS RIGHT TO THE LEADING EDGE AND THE TRAILING EDGE CRACK IS APPROXIMATLEY 6 INCHES LONG. IT APPEARS ALL DOUBLERS ON THE LOWER PART OF THE BLADE ARE Jul 4, 2006 · Bell 205A1SDR 2006FA0000888Blade · debondedROTOR BLADE HAD A LARGE SKIN DEBOND ON THE LOWER SURFACE FROM THE TRIM TAB OB, BETWEEN STA 227 AND STA 329, APPROXIMATELY 475-500 SQUARE INCHES (ALLOWABLE REPAIR LIMITS ARE 20 INCHES SPAN WISE AND 13 INCHES CHORD WISE. UNBONDED SKIN WAS REMOVED TO EXPOSE HONEJun 8, 2006 · Boeing 234SDR KBM2006F00230Spherical Bearin · crackedM/R SPHERCIAL THRUST BEARING, (1 EA) HAS DEEP CRACK AND SEPARATING, REMOVED AND REPLACED. (K)Jun 8, 2006 · N751H · Snias AS350B2SDR CA060605012Blade · cracked(CAN) MAIN ROTOR BLADE SMALL DEBOND FOUND ON LOWER SURFACE APPROX 81.5 INCHES FROM BUTT END JUST AFT OF THE STAINLESS STEEL LEADING EDGE STRIP ON DISASSEMBLY. (APRIL 07 2006) BLADE WILL BE INSPECTED WHEN ARRIVING BACK FOR REPAIR EVALUATION. PAINT REMOVED FROM May 25, 2006 · Bell 212SDR 2006FA0000496Blade · crackedCRACK FOUND ON LOWER SURFACE OF MAIN ROTOR BLADE NEAR STATION 1000. EXACT CAUSE OF CRACK WOULD ONLY BE SPECULATIVE. (K)May 5, 2006 · N5806H · Snias AS350BSDR 2007FA0000418Blade · debondedIN FLIGHT BREAK UP. HELICOPTER CRASHED KILLED 2 HUMANS. NO REACTION TIME TO LAND SAFELY, PILOT WAS EJECTED OUT OF SEAT BY BLADE, KILLED INSTANTLY.May 1, 2006 · Robsin R44RAVENIISDR 2007FA0000449Blades · debondedIN FLIGHT BREAK UP. HELICOPTER CRASHED KILLED 2 HUMANS. NO REACTION TIME TO LAND SAFELY, PILOT WAS EJECTED OUT OF SEAT BY BLADE KILLED INSTANTLY.May 1, 2006 · Robsin R44RAVENIISDR 2006FA0000483Bolt · gougedUPON RECEIPT OF THE AIRCRAFT, THE MAIN ROTOR BLADE BOLTS WERE REMOVED FOR INSPECTION. IT WAS DISCOVERED THAT ONE BLADE BOLTS HAS A RADIAL GOUGE MARK AT THE LOWER BLADE TO HUB BUSHING LOCATION. THE DAMAGE IS OUTSIDE THE AMM PERMITTED REPAIR LIMITS. THE AC TTApr 28, 2006 · N140HS · Agusta AB139SDR 2006FA0000446Bolt · gougedDURING ACCOMPLISHMENT OF THE MAIN ROTOR BLADE REMOVAL, IT WAS DISCOVERED THAT EACH OF THE BLADE BOLTS HAS RADIAL GOUGE MARKS AT THE BLADE TO HUB BUSHING LOCATIONS. THE DAMAGE IS OUTSIDE THE AMM PERMITTED REPAIR LIMITS. (REFERENCE: 39A62221300A286AB) MFG HAS Apr 10, 2006 · N139HS · Agusta AB139SDR CA060403002Wire Strike · damagedDURING COOL DOWN AT IDLE RPM CYCLIC CONTROL STICK WAS MOVED FORWARD AND MAIN ROTOR BLADE (QTY 2) CONTACTED THE UPPER CUTTER OF THE WIRE STIKE PROTECTION SYSTEM.Mar 30, 2006 · Bell 427SDR DT12006F00000Grip · debondedGRIP FOR MAIN ROTOR BLADE IS COMPOSITE LAMINATE. DEBONDED ON LEADING EDGE. 2ND GRIP ON AIRCRAFT. AIRCRAFT IS POLICE HELICOPTER. (K)Jan 20, 2006 · N315PD · Agusta A119SDR 2006FA0000059Restraint · failedPILOT REPORTED SEVERE VIBRATION AFTER INSPECTION FOUND ORANGE BLADE SHEAR RESTRAINT AT MAIN ROTOR SYSTEM FAILED. CNETER BUSHING HAD BECOME DEBONDED FROM ELASTOMERIC. VISUAL INSPECTION DIFFICULT BECAUSE OF ORIENTATION AT INSTALLATION. (K)Dec 20, 2005 · N430LF · Bell 430SDR AOC05003Blade · crackedDURING A 300 HR INSPECTION, A 1.2500 INCH CRACK WAS DISCOVERED ON THE LEADING EDGE ABRASION STRIP AT APPROXIMATLEY BLADE STATION 133.5. BLADE SENT TO BHTI FOR REPAIR.Dec 13, 2005 · N2869F · Bell 407SDR Z1RA107272Bolt · damaged1 M/R BLADE RETENTION BOLT HAS 1 PULLED THREAD.Dec 6, 2005 · N760AF · Skrsky S76CSDR HDCA107099Blade · crackedDURING ROUTINE MAINTENANCE, DISCOVERED CRACK ON MAIN ROTOR BLADE AT BLADE STATION 41.5 EXTENDING CHORDWISE FROM TRAILING EDGE ON BOTH UPPER AND LOWER SKINS ACROSS FINGERS ON TRAILING EDGE EXTENDING 6.3750 INCHES THEN FOLLOWING FINGERS OB, SPANWISE, 5 INCHES. Dec 1, 2005 · Clark 1000CLARKSDR 2005FA0001567Blades · vibratesHAVE BEEN EXPERIENCING PROBLEMS KEEPING THE M/R BLADES IN ACCEPTABLE TRACK AND BALANCE ON ALL 333/269D CONFIG A AIRCRAFT THAT WE MAINTAIN. ALSO HAVE BEEN FINDING MUCH MORE RAPID DETERIORATION OF THE M/R DAMPERS, FLAPPING HINGE BEARINGS, AND VERTICAL HINGE BEARNov 30, 2005 · N277DT · Scwzer 269DSDR CA051125010Bearing · delaminatedWHILE DOING A 500 HOUR (T)INSPECTION IT WAS NOTED THAT THE RUBBER WAS DELAMINATING ON TWO OUT OF THE THREE SPHERICAL THRUST BEARINGS. CRACKING APPEARS TO BE BETWEEN THE RUBBER AND THE METAL PIECE INBOARD SIDE OF SPHERICAL STOP. THE RUBBER APPEARED WET ALL THNov 24, 2005 · Snias AS350B2SDR HEEA107879Blade · debondedUNBONDED ABOVE TRIM TAB AREA IN TWO PLACES.Nov 21, 2005 · N975AE · Aerosp AS355*SDR QOF2005F00003Blades · out of balanceBLADES CAME OUT OF BALANCE SITTING STATIC OVER A PERIOD OF 4 DAYS, FOR REASON OR REASONS UNKNOWN. (K)Oct 20, 2005 · N944AK · Robsin R44RAVENIISDR AU510001906Blade · distorted(AUS) MAIN ROTOR BLADE BENT. BEND LOCATED IN AREA APPROXIMATELY 200MM (7.8IN) OB OF THE BLADE DOUBLER AND RUNNING ALONG THE CHORDWISE AXIS. A STRINGLINE WAS RUN DOWN THE LEADING EDGE OF THE BLADE AND THE DEVIATION FROM THIS AT THE BEND WAS 19MM TO 20MM (0.74IOct 9, 2005 · Robsin R22ALPHASDR CA050930002Blade · unserviceable(CAN) COCKPIT BIM INDICATOR ILLUMINATED ON TAKEOFF. AIRCRAFT RETURNED TO RAMP. VISUAL INDICATION REVELED (BLUE) MAIN ROTOR BLADE BIM INDICATOR IN THE BLACK. MAIN ROTOR BLADE REPLACED.Sep 21, 2005 · Skrsky S61NSDR 2005F00099Strip · debondedMAIN ROTOR BLADE OUTBOARD EROSION STRIP DEBONDED.Sep 7, 2005 · N564EH · Skrsky S61NSDR CA051212002Blade · failedA SEVERE VERT VIBRATION OCCURRED WHEN HELICOPTER ENTERED A SPRAY RUN. VIBRATION CEASED JUST BEFORE LANDING ON A NEARBY ROAD. ROTOR HEAD WAS REMOVED AND NDT'D FOR CRACKS, NONE FOUND. HELICOPTER WAS RE-ASSEMBLED, ALL FLT CONTROLS WERE CHECKED FOR DAMAGE AND SAug 14, 2005 · Hiller UH12DSDR CA050831002Blade · cracked(CAN) DURING PILOT'S POST FLIGHT INSPECTION A CRACK WAS DETECTED IN THE LOWER SKIN OF MAIN ROTOR BLADE NR 1. THE CRACK IS LOCATED 11' FROM THE INBOARD END (ROOT FITTING) OF THE BLADE, AND 3' AFT OF THE LEADING EDGE. THE CRACK WAS 3' LONG AND WITHIN 1' OF THEAug 3, 2005 · Hughes 369DSDR CA050725002Blade · damaged(CAN) MAIN ROTOR BLADES P/N 206-010-200-133 S/N A6716 AND A6778 WILL NOT FLY LOWEST IPS WAS 1.7 WITH MAXIMUM TABING. THESE ARE NEW BLADES WITH AN APPARENT MANUFACTURING DEFECT.Jul 24, 2005 · Bell 206BSDR CA051117006Blade · cracked(CAN) DURING TRAINING FOR TORQUE EVENT INSPECTION (AWD2003-24-01) A POSSIBLE CRACK WAS FOUND. THE M/R BLADE WAS REMOVED FOR A BETTER VISUAL LOOK WITH THE 10X GLASS. THE BLADE WAS ALSO INSPECTED BY COUGAR NDE LTD. AND CONFIRMED THE CRACK. MHI PO NR 20385. TJul 21, 2005 · Hughes 369DSDR ALG2005F00050Blade · bird strikePRIOR TO TAKEOFF, AFTER INCREASING THE COLLECTIVE FOR TAKEOFF, A SEAGULL STRUCK THE LEADING EDGE OF THE M/R BLADE, THE PILOT SHUT THE AC DOWN AND NOTIFIED MAINTENANCE. THE MECHANIC INSPECTED THE M/R BLADES IAW MM. AC WAS RETURNED TO SERVICE. (K)Jul 21, 2005 · N5759M · Bell 206L1SDR CA051115004Blade · crackedDURING A BFF INSPECTION, A LARGE CHORDWISE CRACK (130MM LONG) WAS DISCOVERED ON THE UPPER SURFACE OF A M/R BLADE APPROX 1150MM FROM BLADE ROOT (AREA C). A/C WAS GROUNDED AND REPLACEMENT BLADE WAS ORDERED.Jul 1, 2005 · Snias AS350B2SDR ALGA105415Blade · corrodedDURING ROUTINE MAINTENANCE INSPECTION CORROSION WAS FOUND ON THE SPAR AT LEADING EDGE SPLICE JOINT / BLADE WAS REMOVED FOR FURTHER INSPECTION, DUE TO EXTENT OF DAMAGE TO SPAR BLADE WAS SCRAPPED!Jun 24, 2005 · Bell 212SDR NXT2005F00001Blade · crackedA CRACKED IN THE M/R BLADE EROSION STRIP AT APPROXIMATELY MID-SPAN. BOTH UPPER AND LOWER SURFACES WERE CRACKED. (K)Jun 14, 2005 · N145CF · Agusta A109ESDR HEEA107334Blade · peelingAT CRUISE SPEED AT 105 KTS, PILOT FELT SOMETHING IN CONTROLS AND AIRCRAFT STARTED SHAKING UP AND DOWN SEVERLY. PILOT IMMEDIATELY LOWERED COLLECTIVE AND REDUCED AIRSPEED. THE AMOUNT OF SHAKING SUBSIDED WITH THE CHANGE IN AIRSPEED. AIRCRAFT WAS FLYABLE WITH VJun 12, 2005 · N5000K · Bell 206L1SDR CA050706011Blade · debondedBOTTOM SKIN OF BLADE DEBONDED FROM TIP ALONG STAINLESS LEADING EDGE FOR 28 INCHES AND APPROX 3 INCHES PEELED BACK, CAUSING SEVERE VERTICAL VIBRATION. PILOT DECLARED A MAYDAY AND CARRIED OUT PRE-CAUTIONARY LANDING. BLADE WAS REMOVED AND SENT TO CTI AS IT WAS Jun 10, 2005 · Bell 212SDR CA050614006Blade · failed(CAN) BLADE WAS DECLARED BEYOND SALVAGE 'SCRAP' ON 12-09-04 AND FOUND WITH SERVICEABLE TAG ON 04-17-05.Jun 10, 2005 · Bell 206BSDR CA050608008Blade · damagedBLADE WAS DECLARED BEYOND SALVAGE (SCRAP) ON 12-09-04 AND FOUND WITH SERVICEABLE TAG ON 04-17-05.Jun 8, 2005 · Bell 206BSDR CA050503015Blade · cracked(CAN) CRACK FOUND DURING M/R BLADE TORQUE EVENT INSP. CRACK IS APPROX. 11 INCHES OUT FROM BLADE GRIP ON LOWER SURFACE OF BLADE. CRACK RUNS CORDWISE AND IS APPROX. 3.5INCHES LONG.May 2, 2005 · Hughes 369DSDR JJWA0061549Blade · fodGROUND CREW CLOTH SAFARI HAD BLEW OFF IN HIGH WIND AND WENT THROUGH MAIN ROTOR. NO VIBRATIONS OR APPARENT DAMAGE FELT IN AIRCRAFT, WAS SMOOTH RETURNING TO AIRPORT. FOUND DENT TOP AND BOTTOM AT STA 141 TO 145, IB OF OB TRIM TABS. OTHER AIRCRAFT SENT TO MOVE Apr 28, 2005 · N25PM · Bell 206BSDR CA050418015Blade · damagedON DESCENT, HEARD SOUND SIMILAR TO WHISTLE & HEARD SOUNDS DURING RT BANK ON APPR. A/C SHUTDOWN, INSP M/R BLADES & STAB BAR FOR CAUSE OF NOISE. SUSPECT BLADE TAPE ON STAB BAR LOOSE. NO DEFECTS FOUND. NO FURTHER NOISE APPARENT. APPROX 1-2 MINS INTO NEXT FLTApr 12, 2005 · Bell 212
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