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 2011FA0000703Blade · crackedAT FIRST BIM CHECK, PILOTS REPORTED HEARING A CHIRPING NOISE COMING FROM THE MAIN ROTOR BLADES. INSPECTED BLADES. FOUND THE TIP WEIGHT ON MAIN ROTOR BLADE PROTRUDING THROUGH THE TIP CAP. BLADE WAS REPLACED. OPENAug 29, 2011 · N194AC · Skrsky S64ESDR ALGA8411A1250Blade · crackedMAIN ROTOR BLADE L/E CRACKED AT STA 90.00. TRACER STRANDS BREAKING THROUGH ON LOWER SURFACE SKIN AND TRIM TAB EARS DEBONDED.Aug 4, 2011 · N409AL · Bell 407SDR ALGA8411A1355Blade · crackedMAIN ROTOR BLADE L/E CRACKED AT STA 35.75. TRACER STRANDS BREAKING THROUGH ON UPPER AND LOWER SURFACES AND TRIM TAB, EARS DEBONDED.Aug 4, 2011 · N647AL · Bell 407SDR 2011FA0000530Blade · crackedA CRACK WAS FOUND ON 1 OF THE MAIN ROTOR BLADES L/E ABRASION STRIP DURING A ROUTINE 30 DAY/50 HR INSP. CRACK IS 65MM IN LENGTH AND LOCATED 6` 4" FROM BLADE ROOT, TOP SECTION OF L/E. REMOVED BLADE FOR REPAIR BY MFG CERTIFIED BLADE REPAIR SHOP. `Aug 2, 2011 · N132H · Agusta A109ESDR CA110714006Blades · damagedAD 2011-12-10 CARRIED OUT. FOUND PIN HOLES IN BLADE BOND LINE. BOTH BLADES SCRAP.Jul 14, 2011 · Robsin R44RAVENIISDR QMLDMR0282Blade · crackedCRACK FOUND IN MAIN ROTOR BLADE T/E AT BLADE STATION 74.5" APPROX .5" LONG.Jun 14, 2011 · Urocop EC135P2SDR QMLDMR0281Blade · cracked(4) CRACKS IN MAIN ROTOR BLADE UPPER SKIN AT BLADE STATION 75" APPROX 3" LONG, T/E AT BLADE STATION 78" APPROX .5" AND (2) IN INBD TRIM TAB AT BLADE STATION 152" APPROX .5" EA.Jun 14, 2011 · N138LN · Urocop EC135P2SDR CA110525012Blade · crackedWHILE DOING A DAILY CHECK/INSP OF THE M/R BLADES, 4 CRACKS WERE FOUND DEVELOPING ON THE L/E ABRATION STRIP. M/M STATES 2 CRACKS ARE ALLOWED. MFG IS AWARE OF THE CRACKING.May 21, 2011 · Bell 407SDR CA110525011Blade · crackedWHILE DOING AN DAILY CHECK/INSP OF THE M/R BLADES THE ENGINEER FOUND 7 CRACKS DEVELOPING ON THE L/E ABRASION STRIP.May 20, 2011 · Bell 407SDR CA110509012Blade · crackedDURING AN AFTER LAST FLIGHT CHECK, A CRACK WAS FOUND ON THE TAIL ROTOR BLADE RUNNING PARALLEL WITH THE T/E, ADJACENT TO THE CHORDWISE BALANCE WEIGHT.May 6, 2011 · Bell 206BSDR QMLA2011050611054Blade · damagedDURING THE PILOTS PRE FLIGHT, FOUND THAT THE TRIMMING SURFACE ON THE YELLOW BLADE WAS MISSING. UPON INSPECTION FOUND THE TWO RIVET HOLES, WHERE THE RIVETS HELP HOLD THE TRIMMING SURFACE TO THE BLADE, WAS IN ALMOST PERFECT CONDITION. SENT MAIN ROTOR BLADE TO AMMay 6, 2011 · N779LF · Bolkms BK117C2SDR CA110429006Blades · crackedWHILE DOING AN INSP OF THE MAIN ROTOR BLADES, IT WAS FOUND THE CRACKS 4 PER BLADE WERE DEVELOPING ON THE L/E ABRASION STRIP. THIS OCCURED ON ALL 4 M/R BLADES THE REST OF THE PN 407015001137, SN BLADES ARE A-4093, A-4122.Apr 29, 2011 · Bell 407SDR ALGAR4201102984Blade · crackedDURING ROUTINE INSP, LOWER SURFACE SKIN WAS FOUND TO HAVE A CHORDWISE CRACK AT R STA. 73.00, 7 INCHES IN LENGTH EXTENDING FROM TOOLING HOLE TOWARDS T/E.Apr 20, 2011 · N881AL · Skrsky S76CSDR CA110506005Erosion Shield · debondedON ANNUAL INSP THE EROSION STRIP OF THE MAIN ROTOR BLADE TIP CAP ASSY WAS FOUND DEBONDED & SEPARATING ON MAIN ROTOR BLADE PN 206-015-001-107 SN A-2908. MAIN ROTOR BLADE WAS REMOVED FROM SERVICE & A LOANER INSTALLED. BLADE WAS SENT TO MFG CERTIFIED REPAIR STATIApr 14, 2011 · Bell 206L1SDR CA110414009Sealant · damagedWHILE COMPLETING 100 HR INSP 5-22A A VOID WAS FOUND IN THE SEALANT OF THE DOUBLER AT THE ROOT END OF THE BLADE. DUE TO THE HOURS ON THE BLADE IT WAS DETERMINED THAT IT IS A MFG FLAW. VOID DEPTH .162" MAX ALLOWABLE DEPTH IS .060"Apr 13, 2011 · Bell 212SDR CA110317004Blade · cracked(CAN) MAIN ROTOR BLADE, PN 212-015-501-115 WITH TTSN 2986 .4 HR WAS REMOVED FROM HELICOPTER ON OCTOBER 20 2010 & SENT INTO FACILITY IN FEBRUARY 2011. BLADE WAS SENT IN FOR INSPECTION & FULL CHORD SKIN & HONEYCOMB CORE REPAIR AT STATION 244.0 - 253.0 UPON INSPMar 16, 2011 · Bell 212SDR CA110331023Blade · debonded(CAN) DURING A 100 HR INSPECTION, PERFORMED A TAP TEST INSPECTION OF MAIN ROTOR BLADE IAW RHC SERVICE LETTER SL-31. A DE-BONDED AREA APPROX 3.5 INCHES BY 1.5 INCHES WAS NOTED AT STATION 121. MAIN ROTOR BLADE REPLACED.Mar 9, 2011 · Robsin R44RAVENIISDR ALGA030611607ALBlade · crackedDURING DAILY SERVICE CHECK FOUND CRACKED L/E ON ORANGE MAIN ROTOR BLADE.Mar 6, 2011 · N607AL · Bell 407SDR CA110304007Blade · delaminated(CAN) TAP TEST OF MAIN ROTOR BLADE PERFORMED AT 100 HR INSPECTION REVEALED AREA OF DELAMINATION ON UPPER SKIN. DELAMINATION CENTER OF MASS IS 77.5" FROM BLADE TIP AND 4.5" FROM T/E. DELAMINATION AREA IS 1.5" X 3.5". NO SIGNS OF IMPACT DAMAGE TO UPPER SKIN INMar 2, 2011 · Robsin R44RAVENIISDR 1EXA01282011001Blade · debondedON PREFLIGHT INSP, FOUND THE INBD BLADE SPOILER SEPARATED ABOUT 6 INCHES FROM THE OTBD SECTION OF SPOILER, PILOT SAID ON HIS WAY, THAT HE FELT A THAT THE FLIGHT WAS NOT AS SMOOTH, AFTER REACHING DESTINATION, ON INSP OF THE BLADE FOUND THE SEPARATION ON THE BLAJan 28, 2011 · N272SM · Agusta A109ESDR 2011F00024Blade · delaminatedM/R BLADE T/E "WEDGE" CAME DEBONDED. REMOVED REMAINING PORTION OF WEDGE AND TOUCHED UP PAINT IAW MFG PRODUCT SUPPORT ENGINEERING.Jan 28, 2011 · N397AL · Bell 412SDR QMLA2011012611015Blade · crackedMECHANIC WAS PERFORMING A VISUAL INSP OF THE MAIN ROTOR BLADES WHEN HE DETECTED A CRACK AT STA 2900 ON THE TOP OF THE BLADE. THE CRACK IS 45MM LONG WITH THE OTBD EDGE OF THE CRACK APPROX 735MM FROM THE INBD EDGE OF THE TRIM TAB. THE OTBD END OF THE CRACK IS Jan 26, 2011 · N89SM · Aerosp AS365N2SDR QMLA2011012411014Blade · crackedDURING A SCHEDULED MX INSP, THE MECHANIC FOUND A CRACK IN THE UPPER SKIN OF THE MAIN ROTOR BLADE. THE BLADE IS CURRENTLY BEING SENT FOR REPAIR. A RENTAL BLADE HAS BEEN ORDERED TO RETURN THE ACFT TO SERVICE.Jan 24, 2011 · N365UC · Aerosp SA365N1SDR QMLA2011011211006Blade · crackedDURING ROUTINE AIRWORTHINESS CHECK FOUND 2 CRACKS IN THE L/E OF ONE OF THE MAIN ROTOR BLADES.Jan 12, 2011 · N407UH · Bell 407SDR EVCA00010Blade · leakingCONSTANT WEEPING FROM THE (RED) MAIN ROTOR BLADE VENT HOLE - CONSTANT STREAK.Dec 12, 2010 · N258AE · Bell 206L1SDR ALGA12710A3826Blade · separatedTIP ASSEMBLY DEBONDED AND SEPARATING.Dec 7, 2010 · N9YBRS · Bell 412EPSDR 2010FA0001220Blade · separated(9C9S) FAILED AD 2007-26-12 INSP BECAUSE BLADE SKIN SEPARATION UNDER TIP CAP.Nov 18, 2010 · N7687H · Robsin R22BETASDR 2010FA0001219Blade · damaged(9C9S) MAIN ROTOR BLADE FAILED AD 2007-26-12 INSPECTION. BECAUSE BLADE SKIN SEPARATION UNDER TIP CAP.Nov 11, 2010 · N7687H · Robsin R22BETASDR 2010FA0001218Blades · damaged(9C9S) MAIN ROTOR BLADE FAILED INSPECTION FOR AD 2007-26-12 AND MFG SB NR 72, R44II.Nov 5, 2010 · N7523S · Robsin R44RAVENIISDR 2010FA0001217Blades · separated(9C9S) ROTOR BLADE FAILED INSPECTION FOR AD 2007-26-12 AND MFG SB NR72 R44II.Nov 5, 2010 · N7523S · Robsin R44RAVENIISDR CA101026003Blade · crackedDURING 600HR/6 MONTH INSP CRACKS WERE FOUND ON THE L/E EROSION STRIP ON 2 OF THE 4 BLADES. THE CRACKS STARTED AT THE L/E AND GO TOWARD THE T/E. ALL THE CRACKS ARE ON THE TOP OF THE BLADE AND OTBD OF BLADE STA 138.0. BLADES WERE REMOVED FROM SERVICE FOR REPAOct 8, 2010 · Bell 407SDR CA101006012Blade · failed(CAN) DURING A DAILY INSPECTION A LARGE (4.5") CIRCULAR BLISTER WAS NOTED ON THE MAIN ROTOR BLADE. BOTH TOP AND BOTTOM OF THE BLADE WERE AFFECTED. THE AREA OF DELAMINATION WAS 28` OUTBOARD OF THE ROOT OF THE BLADE, DIRECTLY ADJACENT TO THE LAST OUTBOARD DOUBLESep 24, 2010 · Bell 206BSDR QML3MR0244Blade · debondedDURING INSP ROTOR BLADE FOUND APPROX 2" DEBONDING OF MIDDLE TRIM TAB LOWER SIDE AT BS 90.1-92.1 AND 1.25" TEAR IN LOWER BLADE SKIN AT BS 101.4Aug 5, 2010 · N408MA · Bell 222BSDR CA100803004Bushing · crackedM/R BLADE PIN BUSHING THAT IS BONDED IN LOWER M/R HEAD SLEEVE WAS FOUND CRACKED DURING 100 HR INSP. CRACK IS LOCATED ON THE INBD SIDE OF SLEEVE AND IS LOCATED ON THE ANTI-ROTATION TANG.Aug 1, 2010 · Snias AS350B2SDR 2010FA0001065Counterweight · looseACFT WAS PERFORMING A TRAINING MISSION WHEN THE MID SPAR MAIN ROTOR BLADE WEIGHT CAME LOOSE. THE ACFT PRECAUTIONARY LANDED WITH NO INJURIES. THE MID SPAR BLADE BLEW OUT THE MAIN ROTOR END CAP. THE END CAP DID NOT COME COMPLETELY OFF BUT WAS TORN LOSE AT THEJul 27, 2010 · Bell 206BSDR QMLA2010071210034Blade · debondedDURING 100 HR INSP DAMAGE LOCATED APPROX 1.25 INCHES FROM THE OTBD END OF THE BLADE TIP, ALONG THE AFT EDGE OF THE ABRASION STRIP ON THE LOWER SURFACE, AND MEASURES 1.00 INCH WIDE BY .50 INCHES LONG (FWD/AFT). THE OVERALL SIZE OF THE DAMAGE IS ROUGHLY THE SIZJul 12, 2010 · N902LC · Doug MD900SDR CA100707002Blade · delaminatedPILOT REPORTED VIBRATION FELT. LANDED AND FOUND LOWER SURFACE OF BLADE SKIN DELAMINATED AND CURLED BACK FROM THE L/E. ACFT IS GROUNDED WAITING FOR A REPLACEMENT BLADE.Jul 5, 2010 · Bell 407SDR 2010F00141Blade · debondedLOWER MAIN ROTOR BLADES SKIN DELAMINATION FROM BLADE STATION 196 TO BLADE STATION 210.Jul 4, 2010 · N402SH · Bell 407SDR CA100623003Blade · cracked(CAN) 16 CM CRACK FOUND ON MAIN ROTOR BLADE INTRADOS SECTION C LOCATED 144 CM FROM STATION 0.0 MM CORDWISE.Jun 21, 2010 · Snias AS350BASDR 2010FA0000639Spar · unserviceable((QR9R)) MAIN ROTOR BLADE MID SPAR WEIGHT CAME LOOSE DURING OPERATION CAUSING THE WEIGHT TO BLOW OUT THE END CAP. DEFECT WAS NOTICED ON POST FLIGHT INSP. PILOT DID NOT REPORT ANY UNUSUAL VIBRATIONS. THIS IS NOT THE FIRST BLADE THAT THE MID WEIGHT HAS COME LJun 15, 2010 · N67950 · Bell 206BSDR CA100603003Blade · delaminatedTHE PILOT AND CO-PILOT WERE THE ONLY 2 PERSONS ONBOARD THE ACFT DURING A TRAINING FLIGHT. AT APPROX 11,000`, PA AND 110 KIAS THE PILOTS NOTICED AN UNUSUAL VIBRATION AND ELECTED TO MAKE A PRECAUTIONARY LANDING. POST FLIGHT INSP BY A MX REVEALED DELAMINATION BMay 26, 2010 · Bell 222USDR CA100527004Pin · worn(CAN) BLADE PIN FOUND TO BE CRACKED BY PILOT ON A VISUAL INSPECTION. IT IS AN EXPANDABLE PIN WITH A NUT TO ADJUST TENSION. PIN FOUND TO BE CRACKED AT THE END OF THE THREADS, PIN HAD 779.4 HOURS REMAINING ON IT.May 17, 2010 · Hughes 369DSDR CA100505001Trim Tab · delaminatedAREA 3 INCHES AROUND TRIM TAB DELAMINATED, THIS TAB WAS REPLACED AT 2500 HOURS.May 3, 2010 · Bell 407SDR CA100429011Blade · cracked(CAN) UPON AN INSPECTION IT WAS NOTED THAT THAT A SURFACE CRACK WAS DEVELOPING NEAR THE BLADE BOLT HOLE . FURTHER INVESTIGATION REVEALED THAT THE CRACK HAD THIS RED/ORANGE PLASTIC MATERIAL COMING OUT OF IT.Apr 28, 2010 · Bell 407SDR 2010FA0000298Blade · cracked(JBZR) DURING PILOT PRE-FLIGHT INSP, FOUND APPROX (1) 2.5 INCH LONG DELAMINATION AND A (2ND) .7500 INCH LONG DELAMINATION OF THE END PLIES OF ONE MAIN ROTOR BLADE, ALONG THE BLADE TIP END.Mar 19, 2010 · N21RX · Agusta A109ASDR ALGA39105908Blade · debondedFOUND MAIN ROTOR BLADE LOWER SURFACE NR 1 GRIP FINGER DOUBLER CORRODED AND DEBONDED APPROX 2.25".Mar 9, 2010 · N69AL · Bell 206L4SDR ALGA39106254Blade · debondedFOUND MAIN ROTOR BLADE UPPER SURFACE NR 4 GRIP FINGER DOUBLER CORRODED AND DEBONDED APPROX 3.5".Mar 9, 2010 · N278AL · Bell 206L4SDR RMXA021620100070Blade · delaminatedDURING A DAILY INSPECTION, THE TECH DISCOVERED A 'L' SHAPED DELAMINATION ON 1 MAIN ROTOR BLADE UPPER SKIN NEAR THE BLADE ROOT OR 'CUFF'. THE DELAMINATION MEASURES 18MM L X 8MM W. MAIN ROTOR BLADE IS BEING REPLACED & DEFECTIVE BLADE BEING SENT BACK TO MFG FOR RFeb 16, 2010 · N919WM · Urocop EC135P1SDR ALGA21110A3811Blade · contaminatedMOISTURE INGRESS AT T/E ROOT CLOSURE.Feb 11, 2010 · N9YSKY · Bell 412EPSDR 2010FA0000074Nut · cracked2 NUTS FITTED TO MAIN ROTOR BLADE PITCH CHANGE HORNS ON ACFT R227/09 FOUND CRACKED IN SERVICE. FURTHER ENQUIRIES FOUND OTHER NUTS FROM SAME LOT NR 16838 SUPPLIED 7/09 FITTED TO H369 M/R DRAG DAMPER 7 OUT OF 12 NUTS ALSO CRACKED. INVESTIGATION LABS DISCOVERED HJan 13, 2010 · Hughes 369
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