JASC 6410

Service difficulty reports · 1,148

Reports filed under 6410 · Tail 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 = '6410'
  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 2017FA0000004Blade · delaminatedDURING PRE-FLIGHT INSPECTION FOUND TAIL ROTOR BLADE PN. 500P3100-105 SN. C774 LEADING EDGE ABRASION STRIP DELAMINATED.Jan 5, 2017 · N2066W · Hughes 369ESDR 2017FA0000409Blade · delaminatedTAIL ROTOR BLADEWAS FOUND IN A DELAMINATED STATE DURING A POST FLIGHT INSPECTION. THE ABRASION STRIP HAD DELAMINATED FROM THE LEADING EDGE OF THE BLADE. THIS BLADE HAD BEEN INSTALLED FOR 3 DAYS AND ONLY HAD 7.1 HRS ON IT FROM REPAIR. PROBABLE CAUSE OF THE DDec 23, 2016 · N506PH · Hughes 369ESDR 2017F00012Abrasion Strip · delaminatedDURING POST FLIGHT INSPECTION FOUND TAIL ROTOR BLADE LEADING EDGE ABRASION STRIP DELAMINATED.Dec 23, 2016 · N506PH · Hughes 369ESDR JYDR20161128318Blade · unbondedTAIL ROTOR BLADE CAUSED VIBRATION ON AIRCRAFT. UPON DISASSEMBLY AT REPAIR STATION, A LARGE AMOUNT OF WATER WAS FOUND IN THE FAIRING. THE WATER WAS ALLOWED ENTRY BECAUSE OF A FAILURE IN A BOND LINE.Nov 28, 2016 · N247AC · Skrsky S64ESDR 9EKA20161102018Blade · cracked0.25 INCH CRACK FOUND ON INBOARD SIDE OF THE TRAILING EDGE OF THE TAIL ROTOR BLADE ASSEMBLY. THIS WAS FOUND DURING PREFLIGHT BY THE SCHEDULED PILOT ON DUTY, BUT THERE WERE NO FLIGHTS SCHEDULED FOR THE DAY. AFTERWARD THE MECHANIC ON DUTY VERIFIED THE CRACK WIOct 30, 2016 · N814EH · Snias AS350B2SDR QMLA2016092816111Blade · crackedFOUND SMALL CRACK IN TAIL ROTOR BLADE ON FLAT SURFACE JUST INBOARD OF CURVED SECTION OF ROOT AREA. THIS IS THE THIRD CRACK IN THE SAME LOCATION. BLADE HAD BEEN REPAIRED.Sep 28, 2016 · N407NA · Bell 407SDR 2016FA0000459Blade · crackedFOUND SMALL CRACK IN TAIL ROTOR BLADE ON FLAT SURFACE JUST INBOARD OF CURVED SECTION OF ROOT AREA. BLADE HAD BEEN REPAIRED.Sep 28, 2016 · N407NA · Bell 407SDR 9EKA20160920015Blade · crackedDURING AN INSPECTION, A MECHANIC NOTICED SOME PAINT FLAKING OFF THE TAIL ROTOR BLADE ABOUT MID-SPAN SO HE CLEANED IT UP AND NOTICED WHAT APPEARED TO BE A CRACK ON CLOSER INSPECTION IT WAS FOUND TO BE AN ACTUAL CRACK. CRACK LENGTH - 1.5", CRACK DISTANCE FROM Sep 20, 2016 · N359EV · Snias AS350B3SDR N9NA201607210001Blade · crackedDURING APPROACH, THE PILOT NOTICED SLIGHT BUZZ AND UPON LANDING HEARD SLIGHTLY DIFFERENT SOUND FROM TAIL ROTOR, PILOT CHECKED T/R ON SHUTDOWN AND FOUND CRACKED BLADE SKIN. BLADE IS CRACKED COMPLETELY THROUGH STARTING AT INBOARD END OF TRAILING EDGE TAB 19" INJul 14, 2016 · N350AW · Snias AS350B3SDR IGAR2016FA0000184Blade · corrodedTAIL ROTOR BLADE DEVELOPED DEEP CORROSION PIT AT BLADE ROOT.Apr 11, 2016 · N212AH · Bell 212SDR IGAR2016FA0000183Blade · corrodedTAIL ROTOR BLADE DEVELOPED DEEP CORROSION PIT AT BLADE ROOT.Apr 11, 2016 · N212AH · Bell 212SDR AC2R2016040801Erosion Shield · brokenTAIL ROTOR BLADE LIGHTNING BONDING STRIP BROKE IN FLIGHT AND CONTACTED MAIN ROTOR BLADE. REPLACED LIGHTNING BONDING STRIP, TAIL ROTOR BLADE AND MAIN ROTOR BLADE.Apr 7, 2016 · N639NA · Agusta AW139SDR K2DA20160308001Blade · delaminatedUPON THE DAILY INSPECTION, A COIN TAP TEST WAS PERFORMED ON THE TAIL ROTOR BLADES. TAIL ROTOR BLADE, PN 500P3100-105, SN C519 WAS DISCOVERED TO BE DELAMINATED. THE DELAMINATION CONSISTS OF A 1.5 INCH AREA OF THE LE ABRASION STRIP ON THE OTBD SIDE OF THE BLADMar 5, 2016 · N506PH · Hughes 369ESDR 2016FA0000076Blade · delaminatedUPON THE DAILY INSPECTION, A COIN TAP TEST WAS PERFORMED ON THE TAIL ROTOR BLADES AND BLADE WAS DISCOVERED TO BE DELAMINATED. THE DELAMINATION CONSISTS OF A 2" AREA OF THE L/E ABRASION STRIP ON THE OTBD SIDE OF THE BLADE AND A 1" AREA OF THE L/E ABRASION STRIFeb 9, 2016 · N506PH · Hughes 369ESDR CA160209008Blade · delaminated(CAN) PILOT HEARD SINGLE BANG DURING HELI SKI OPERATIONS ENROUTE TO HELI PAD. PERFORMED FLY PAST FOR CHECK FROM GROUND. NO INSTRUMENT OR FLIGHT ANOMALIES FOUND. NORMAL LANDING AT BASE WAS PERFORMED. AFTER SHUTDOWN THE INBD SIDE OF 1 TAIL ROTOR BLADE WAS FOUNFeb 8, 2016 · Bell 407SDR CA160209007Blade · mismanufactured(CAN) PN 4G6410A00133, THE BONDING STRIP IS IN FULL CONTACT WITH A DATA PLATE THERE IS NO SEALANT BETWEEN THE BONDING STRIP AND T/R BLADE THERE IS NO SEALANT AROUND THE CONNECTOR OR CONNECTOR ATTACHMENT SCREWS THERE IS A NON-STANDARD FILLISTER HEAD SCREW RETAIFeb 5, 2016 · Agusta AW139SDR CA160128008Blade · cracked(CAN) DURING INSPECTION OF THE TAIL ROTOR BLADE A CRACK WAS FOUND ON THE TRAILING SIDE BELOW THE BLADE BOLT. THE PAINT WAS REMOVED TO CONFIRM THE BLADE WAS CRACKED. THE BLADE HAS BEEN REMOVED AND SENT TO THE MFG FOR ANALYSIS.Jan 27, 2016 · Agusta A109SSDR 2016FA0000033Blades · failedAIRCRAFT PICKED UP TO A HOVER AND PILOT HEARD A LOUD SHUDDER NOISE AND PUT AIRCRAFT ON GROUND. ON INSPECTION, FOUND ALL 13 NOTAR FAN BLADES DESTROYED WITH DAMAGE TO LINER. UNKNOWN CAUSE OF BLADE FAILURE.Jan 7, 2016 · Doug 600NSDR K2D2016011200001Blade · delaminatedAFTER THE DAY`S FLIGHTS AND DURING THE DAILY INSPECTION WE FOUND, BY TAP TEST, THE L/E OF 1 OF THE TAIL ROTOR BLADES WAS DELAMINATED IN VARIOUS PLACES, VARYING IN LENGTH FROM .5 TO 2 INCHES.Dec 31, 2015 · N506PH · Hughes 369ESDR K2DA20160107001Blade · delaminatedDURING DAILY INSPECTION, AFTER THE DAYS FLIGHTS, ONE OF THE TAIL ROTOR BLADES WAS FOUND TO HAVE VARIOUS SPOTS, VARYING IN LENGTH FROM .5 INCHES TO 2 INCHES, WHERE THE LE WAS DELAMINATING FROM THE BLADE, PN 500P3100-105, SN C700. WE TAP TEST THE LE DAILY.Dec 31, 2015 · N506PH · Hughes 369SDR K2D2016F00000Blade · delaminatedON SUNDAY 12 13 15, A TAIL ROTOR BLADE, PN 500P3100-105, SN C922, 491.6 TSR, WAS FOUND IN A DELAMINATED STATE, DURING A PREFLIGHT INSPECTION. THE LE HAD DELAMINATED FROM THE BLADE ABOUT 2" IN LENGTH. PROBABLE CAUSE OF THE DELAMINATION IS IMPROPER CURE TIME FDec 13, 2015 · N58243 · Hughes 369DSDR K2DA2015121501Blade · delaminatedDURING PREFLIGHT INSPECTION, FOUND TAIL ROTOR BLADE, PN 500P3100-105, SN C922 LE DELAMINATED FOR APPROX 2 INCHES ON BOTH SIDES OF THE BLADE.Dec 13, 2015 · N58243 · Hughes 369DSDR CA151014002Bearing · cracked(CAN) DURING AN INSPECTION IT WAS NOTICED THE THE ELASTOMERIC BEARINGS HAD CRACKS THAT EXCEEDED LIMITS AND WERE REMOVED.Oct 6, 2015 · Snias AS350B2SDR CA150917008Blade · debonded(CAN) DURING SCHEDULED INSPECTION THE L/E EROSION STRIP WAS FOUND DEBONDED DURING CLEANING PRIOR TO INSPECTION, AS IT CRINKLED WITH FINGER PRESSURE.Sep 17, 2015 · Hughes 369DSDR QMLA2015082615079Blade · crackedON A PREFLIGHT, THE PILOT FOUND SMALL CRACKS ON EACH SIDE OF A RIVET ON THE END CAP OF A TAIL ROTOR BLADE. UPON REVIEW, THE ASSEMBLY WAS R & R. THIS ACFT HAS RETURNED TO SERVICE.Aug 26, 2015 · N284AM · Bell 407SDR 8LFA20150813001Blade · crackedDISCOVERED CRACK IN LE CAP OF TAIL ROTOR BLADE, APPROX CRACK IS 7MM IN LENGTH, STARTING 2MM FROM TIP END OF LE CAP, CRACK CONFIRMED USING DYE PENETRANT METHOD. ACFT TAKEN OUT OF SERVICE UNTIL REPLACEMENT PARTS COULD BE INSTALLED. ROTOR BLADE CAME NEW WITH ACAug 11, 2015 · N756LF · Agusta AW119MKIISDR MKHA20150507001Tail Rotor · brokenDURING A FLIGHT THE PILOT EXPERIENCED EXCESSIVE VIBRATION. THE PILOT MADE A PRECAUTIONARY LANDING & NOTIFIED MX. MX DISCOVERED THE PITCH HORN ON THE OTBD TAIL ROTOR BLADE WAS BROKEN OFF.May 1, 2015 · N369MH · Hughes 369DSDR CA150210006Blade · delaminated(CAN) AFTER 7 DAYS OF SITTING OUTSIDE IN THE RAIN THE ACFT WAS STARTED UP FOR REPOSITIONING. ONCE THE ACFT WAS AT FLIGHT IDLE, A AIRFRAME VIBRATION WAS FELT & THE TAKEOFF WAS ABORTED & THE ENG WAS SHUT DOWN. UPON INSPECTION THE TAIL ROTOR BLADE WAS INSPECTEDFeb 5, 2015 · Snias AS350B2SDR CA141121006Blade · cracked(CAN) SEVERAL CRACKS FOUND AFTER LAST FLIGHT OF THE DAY ON TAIL ROTOR BLADE BOND ASSY 76101-05020-045, PART OF TAIL ROTOR BLADE ASSY 76101-05101-041.Nov 18, 2014 · Skrsky S76ASDR CA141022010Blade · debonded(CAN) DURING INSPECTION CRACKS WERE NOTED IN THE SEALANT COVERING THE ROOT FITTING TO DOUBLE ADHESIVE. SEALANT WAS REMOVED TO EXPOSE THE ADHESIVE BOND LINE. ROOT FITTING ATTACH BOLTS WERE LOOSENED TO RELIEVE THE FITTING. A DISBOND IN THE ROOT FITTING TO DOUOct 22, 2014 · Hughes 369DSDR CA141016002Blade · debonded(CAN) TAIL ROTOR BLADES, L/E STRIPS FOUND DEBONDED AT BLADE TIPS. EDGE OF L/E STRIP SEPARATED FROM AIRFOIL. BOTH BLADES REMOVED FROM SERVICE AND REPLACED BY NEW UNIT SAME PN.Oct 7, 2014 · Hughes 369ESDR 2014FA0000562Blade · crackedDURING A DAILY INSPECTION , A ONE INCH CRACK ON ONE OF THE TWO TAIL ROTOR BLADES WAS DETECTED. INITAL INSPECTION WAS VISUAL A 10X GLASS WAS USED TO VARIFY. AIRCRAFT WAS REMOVED FROM SERVICE AND WILL RETURN TO SERVICE AFTER A SERVICEABLE TAIL ROTOR BLADE IS ISep 25, 2014 · N261HC · Agusta AW109SPSDR QMLA2014091114111Blade · crackedPAINT FOUND CRACKED BY MECHANIC WHILE PERFORMING A PREFLIGHT AIRWORTHINESS CHECK OF THE TAIL ROTOR BLADE PN 406-016-100-119, SN BH93897. UPON FURTHER INVESTIGATION BY REMOVING PAINT, IT WAS NOTED THAT CRACKS WERE EMANATING FROM THE BLADE & BLOCK BETWEEN THE TSep 11, 2014 · N905HA · Bell 407SDR CA140619011Blade · cracked(CAN) DURING A DAILY INSPECTION OF THE T/R BLADES IT WAS NOTED THAT A HAIR LINE CRACK WAS VISBLE NEAR THE ROOT OF THE BLADE S/N 393. UPON FURTHER INVESTIGATION USING A 10X MAGIFIER THE CRACK SPAND THE CORD LENGTH OF THE BLADE. THE AIRCRAFT WAS REMOVED FROM SERJun 19, 2014 · Bolkms BK117B2SDR CA140516007Counter · cracked(CAN) THIS ACFT WAS OPERATING, LOCATED AT 3000 FT ABOVE SEA LEVEL. IT TOOK OFF FOR A MISSION WITH 2 CREW, 2 PASSENGERS AND 400 LBS OF FUEL, IAW CREW TESTIMONIALS, ONCE IN AIR, 1 MINUTE AFTER TAKING OFF THE PILOT FELT HEAVY VIBRATION ON PEDALS AND TRANSMITTED May 12, 2014 · Bell 206L4SDR QMLA2014050614051Blade · crackedDURING THE 12 MONTH AAIP INSPECTION, FOUND 7 OF 13 NOTAR BLADES WITH SMALL CRACKS COMING FROM THE DRAIN HOLE OF EACH BLADE CUFF. REPLACEMENT PARTS HAVE BEEN ORDERED & THE ACFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION.May 6, 2014 · N900UM · Doug MD900SDR CA140502002Bearing · cracked(CAN) BOTH INBD FEATHERING BEARINGS WERE FOUND TO BE CRACKED. BLADES REMOVED FROM SERVICE.May 1, 2014 · Bell 206L1SDR AC2A201311080004Blade · damagedON POST FLIGHT INSPECTION, PILOT FOUND FOD DAMAGE ON TAIL ROTOR BLADE APPEARING TO BE FROM A BOLT.Oct 26, 2013 · N39LR · Bell 206L1SDR CA131009002Blade · separated(CAN) A SUDDEN MEDIUM FREQUENCY VIBRATION WAS FELT IN FLIGHT. A PRECAUTIONARY LANDING WAS CARRIED OUT. AFTER VISUAL INSPECTION, IT WAS DISCOVERED THAT THE TIP CAP FILLER HAD SEPARATED CAUSING THE VIBRATION. BOTH BLADES WERE REPLACED, THE TAIL ROTOR WAS BALAAug 24, 2013 · Bell 205A1SDR 2013FA0000484Spar · crackedDURING P-CHECK MECHANIC NOTED CRACKLING SOUND EMANATING FROM TAIL ROTOR SPAR DURING FLEXING. DISASSEMBLY OF TAIL ROTOR BLADE CONFIRMED VIABLE CRACK IN SPAR.Aug 9, 2013 · N850BP · Snias AS350B3SDR CA130805020Blade · delaminated(CAN) THE PILOT WAS CARRYING OUT HIS DAILY CHECK ON THE TAIL ROTOR BLADES. HE NOTICED A SOFT AREA BY FEEL . AN ENGINEER CARRIED OUT A TAP TEST AND FOUND THE BLADE HAD AN DELAMINATION 2" FROM TIP AND .5" FROM ABRASION STRIP. APPROXIMATE AREA DELAMINATED 10.5Aug 5, 2013 · Bell 206L1SDR CA130805019Blade · delaminated(CAN) THE PILOT WAS CARRYING OUT HIS DAILY CHECK ON THE TAIL ROTOR BLADES. HE NOTICED A SOFT AREA BY FEEL. AN ENGINEER CARRIED OUT A TAP TEST AND FOUND THE DELAMINATION 1.5" FROM TIP AND .5" FROM ABRASION STRIP. APPROXIMATE AREA DELAMINATED, 8" SQ, 4 X 2". Aug 5, 2013 · Bell 206L1SDR CA130730001Blade · damaged(CAN) MFG DISCOVERED T/R BLADE ABRASION STRIP BONDING VOIDS AROUND AND EXTENDING AT PROXIMITY OF THE BLADES` DRAIN HOLE.Jul 26, 2013 · Bell 407SDR CA130726004Blade · debonded(CAN) WHILE CARRYING OUT A 25 HOUR INSPECTION, PERFORMED A TAP TEST WITH A BELL TAP HAMMER, FOUND THE EROSION STRIP PARTIALLY DEBONDED. TAIL ROTOR HUB AND BLADE ASSY, PN 212-011-701-123, TAIL ROTOR BLADE, PN 212-010-750-127FM.Jul 19, 2013 · Bell 412SDR CA130722009Blade · delaminated(CAN) AN AME NOTICED T/R BLADE HAD SOME PAINT MISSING. FURTHER INVESTIGATION THE AME FOUND NEAR THE TIP OF THE T/R BLADE A DELAMINATION HAD OCCURRED ON THE ONE SIDE OF THE T/R BLADE THROUGH A TAP TEST. HE INSPECTED THE SECOND T/R BLADE AND FOUND A DELAMINATIJul 18, 2013 · Bell 206L4SDR QMLA2013070513091Blade · dentedDURING DAILY AIRWORTHINESS CHECK, NOTICED A DENT TO THE L/E ERROSION STRIP ON TAIL ROTOR BLADE. ACFT TAKEN OUT OF SERVICE. DETERMINED TAIL ROTOR BLADE TO BE UNSERVICEABLE. INVESTIGATION INTO CAUSE OF DAMAGE IS IN PROGRESS. THE ACFT HAS SINCE RETURNED TJul 5, 2013 · N138HH · Bolkms BK117A4SDR ALGA201306067433Spar · crackedSPAR CRACKED AT ELIPTICAL PLUG.Jun 5, 2013 · N862AL · Skrsky S76CSDR ALGA052320137416Blade · splitDURING 500 HR ROUTINE INSPECTION, FOUND BLADE SPAR SPLINTERED ON "B" SIDE AT APPROXIMATE STATION 10.5May 21, 2013 · N864AL · Skrsky S76CSDR CA130220007Blade · delaminated(CAN) TAIL ROTOR DEBONDED ON DOUBLER AT BS 20.00".Feb 8, 2013 · Bell 212SDR CA121012016Bearing · cracked(CAN) ON INSPECTION IAW ASB 01-00-65 TAIL ROTOR HALF SHELLS FOUND WORN AND CRACKED. REPLACED ALL 4 BEARING.Oct 9, 2012 · Snias AS350*
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