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 ALGA106747Blade · noneC/W AD 2004-24-08 AS PER ASB 206L-04-127 / SENT TO RBI TO C/W AD 2004-24-08 AS PER ASB 206L-04-127Oct 8, 2005 · N158H · Bell 206B3SDR ALG2005F00083Blade · damagedDURING THE DAILY MAINTENANCE INSPECTION, IT WAS DETERMINED THE TAIL ROTOR BLADE TIP WAS DAMAGED BY STRIKING AN UNDETERMINED OBJECT. COMPLIED WITH THE CONDITIONAL INSPECTION, 5-28 SUDDEN STOPPAGE/ACCELERATION-TAIL ROTOR. (K)Oct 6, 2005 · N275AL · Bell 206L4SDR CA051003013Blade · cracked(CAN) TAILING EDGE CRACKED. BLADES WHERE DESTROYED, ONLY HAD 125 HOURS REMAINING ON THEM. INSTALLED A NEW SET OF BLADES SAME PART NUMBER.Sep 10, 2005 · Snias AS350BASDR KBM2006F00052Bearing · crackedHALF SHELL BEARINGS, UNIT CRACKED, REMOVED AND REPLACED WITH NEW. (K)Aug 30, 2005 · N350SH · Snias AS350BASDR KBM2005F00243Bearing · crackedUNIT HAS MULTIPLE CRACKS. REMOVED AND REPLACED UNIT. (M)Aug 20, 2005 · N1188P · Snias AS350BASDR CA050720005Blade · delaminatedAFTER DISCUSSION WITH A FSR FROM BHTC, LEARNED THAT THE TAIL ROTOR ON THIS AIRCRAFT HAD BEEN DAMAGED IN 2004. THE TECHNICAL LOG OF THE AIRCRAFT DID NOT DEMONSTRATE THAT THE PROPER INSPECTION WAS CARRIED OUT AS PER MM CHAP 5-28. BHTC CONFIRMED THAT THE PREVIOJul 6, 2005 · Bell 206L4SDR KBM2005F00148Case · crackedHALF SHELL, UNIT HAS MULTIPLE CRACKS. REMOVED AND REPLACED. (K)Jun 13, 2005 · N884SH · Snias AS350B2SDR AU510002099Blade · delaminated(AUS) TAIL ROTOR BLADE DELAMINATED. AREA OF DELAMINATION APPROXIMATELY 38.1MM LONG BY 9.525MM WIDE (1.5IN BY 0.375IN). SEE ATTACHMENT FOR PHOTOGRAPHS. (OTHER CAUSE: VOID DEVELOPED FROM POOR PREP WHEN REPAIRED BY HTC ) (CASA 510002099)Jun 10, 2005 · Hughes 369ESDR KBM2005F00138Bearing · wornHALF SHELLS, WORN. REMOVED AND REPAIRED. (K)Jun 9, 2005 · N37SH · Snias AS350BASDR KBM2005F00132Bearing · wornHALF SHELL BEARINGS, WORN. REMOVED AND REPLACED. (K)Jun 4, 2005 · N313LV · Snias AS350B2SDR CA050526002Blade · eroded(CAN) THE BO105 BASED IN THE WEST HAS IN THE PAST EXPERIENCED PROBLEMS WITH PAINT EROSION ON THE TAIL ROTOR BLADES. NEW STYLE BLADES WERE INSTALLED IN THE BELIEF THAT THIS WOULD SOLVE THE PROBLEM WE WERE EXPERIENCING WITH PAINT EROSION. 50 HOURS AFTER INSTALLAMay 24, 2005 · Bolkms BO105SSDR ALGA104359Sleeve · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOPMay 24, 2005 · N176AL · Bell 206L4SDR ALGA104358Bearing · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP.May 24, 2005 · N176AL · Bell 206L4SDR CA050524005Blade · damaged(CAN) 427 TAIL ROTOR BLADE SKIN SEPARATION. AFT OF LEADING EDGE NEAR THE TIP OF THE BLADE ON APPROX. 2 SQ. IN. OUTBOARD SIDE.May 20, 2005 · Bell 427SDR CA050513006Trim Tab · cracked(CAN) THE PILOT WAS DOING A PRE FLIGHT ON THE HELICOPTER AND NOTICED A CRACK IN THE PAINT ON THE T/R TRIM TAB. THE T/R ASSEMBLY WAS REMOVED FOR FURTHER INVESTIGATION.AFTER REMOVING THE T/R ASSY AND REMOVED SOME PAINT IT APPEARED TO BE STILL CRAC KED ON THE TRIMay 12, 2005 · Snias AS350BASDR KBM2005F00104Bearing · tornHALF SHELL BEARING KIT, TORN LAMIFICATIONS, REMOVED AND REPLACED. (K)May 11, 2005 · N345SH · Snias AS350B2SDR ALGA104360Bearing · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP.May 1, 2005 · N176AL · Bell 206L4SDR ALGA104357Sleeve · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP.May 1, 2005 · N176AL · Bell 206L4SDR CA050513002Spar · cracked(CAN) NOISE HEARD ON PITOT DAILY INSPECTION AS PART OF EUROCOPTERS CRITERIA. DISASSEMBLED BY ENGINEER AND FOUND CRACKED.Apr 19, 2005 · Snias AS350B2SDR KBM2005F00208Bearing · wornHALF SHELL LAMINATED BEARINGS, WORN BEYOND LIMITS. REMOVED AND REPLACED. (K)Apr 16, 2005 · N53SH · Snias AS350B1SDR ALGA099525Blade · chippedCHROME MONOXIDE SURFACE CHIPPED BEYOND LIMITS. SEND TO AMERICAN EUROCOPTER FOR WARRANTY CONSIDERATION.Feb 13, 2005 · N516AL · Urocop EC120BSDR CA050215005Blade · contaminated(CAN) AFTER AIRCRAFT RECONFIGURATION AT OUR FACILITY, NORMALLY INSTALLED THE RADS EQUIPMENT FOR VIBRATION ANALYSIS ON THE T/R SYSTEM. NOTICED A SLIGHTLY HIGH VIBRATION LEVEL WHICH WERE UNABLE TO BRING TO A STANDARD LEVEL. AFTER INVESTIGATION, FOUND OUT THAT Feb 12, 2005 · Bell 427SDR K2D2005F00000Blade · damagedREF: K2DA320J TAIL ROTOR BLADE ABRASION STRIP AND TIP CAP DEPARTED BLADE ASSY, INFLIGHT. (WP13200506018) (K)Jan 28, 2005 · N142MK · Hughes 369ESDR CA050124005Blade · debonded(CAN) TAIL ROTOR BLADE DOUBLER DEBOND ON APPROX. 6.5 IN. FROM THE TIP OF THE DOUBLER.Jan 20, 2005 · Bell 430SDR 2005FA0000413Blade · vibrationON FIRST GROUND RUN, AFTER APPROX 24 HOURS OF HARD RAIN, THE HELICOPTER DEVELOPED A SEVERE VIBRATION. THE VIBRATION WAS TRACED TO A TAIL ROTOR BLADE. SUSPECT BLADE COLLECTED THE RAIN WATER. THE BLADE WAS SCRAPPED IAW THE MM. (K)Jan 11, 2005 · N304FD · Bell 412EPSDR AC2A099720Blade · damagedAVERAGE SKIN THICKNESS .00684 LOWER SURFACE NOT REPAIRABLE AS PER ASB 206L-04-127 AND 206-04-100 REV B PART III. SCRAPPED BLADE. REQUEST WARRANTY.Dec 23, 2004 · N31079 · Bell 206L3SDR AC2A099719Blade · damagedAVERAGE SKIN THICKNESS .00673 LOWER SURFACE NOT REPAIRABLE AS PER ASB 206L-04-127 AND 206-04-100 REV B PART III. SCRAPPED BLADE. REQUEST WARRANTY.Dec 23, 2004 · N31079 · Bell 206L3SDR KBM2005F00002Bearing · wornHALF SHELLS WORN. REMOVED AND REPLACED.Dec 15, 2004 · N345SH · Snias AS350B2SDR ALGA098355Blade · crackedREPORTS OF CRACKS AND DEFORMATION IN SKIN AND WEIGHTS, SENT TO RBI TO CW AD 2004-24-08.Dec 10, 2004 · N8WH · Bell 206L1SDR KBM2005F00000Bearing · crackedHALF SHELLS CRACKED. REMOVED AND REPLACED. (K)Nov 28, 2004 · N1188P · Snias AS350BASDR ALGA098105Blade · crackedINSPECTION FOR SKIN ON THE AREA OF TRAILING EDGE OF BALANCE WEIGHT C/W ASB206L-04-127 REVB PT3.Nov 23, 2004 · N362AL · Bell 206L3SDR GJD2005F00000Blade · fracturedDURING ACCIDENT INVESTIGATION, FOUND EVIDENCE OF FATIGUE FRACTURE ON TAIL ROTOR BLADE. OPPOSING BLADE WAS FRACTURED DUE TO APPARENT OVERLOAD. BOTH BLADES SENT TO MFG LABS UNDER NTSB ESCORT. TEARDOWN REPORT INDICATES BOTH BLADES HAD PROGRESSIVE FATIGUE EMANANov 18, 2004 · N7825S · Bell 47G3B2SDR BAQ2005F00000Blade · crackedFOUND CRACK ON 1 SIDE OF T/R BLADE AT STA 540.00, CRACK EXTEND FROM DOUBLER BACK 4 INCHES ALONG STA 540. CORDWISE REF FIG. 1 OF AD 2002-25-51 AIRCRAFT WAS POST MOD. (K)Nov 10, 2004 · N911UF · Agusta A109ESDR 11072110704Blade · crackedPILOT FELT VIBRATION IN TAIL ROTOR PEDALS DURING APPROACH. POST FLIGHT INSPECTION REVEALED THAT 1 TAIL ROTOR BLADE HAD A CHORD WISE CRACK BEGINNING AFT OF THE SPAR AND EXTENDING THROUGH THE TRAILING EDGE OF THE BLADE. THE CRACK WAS THROUGH BOTH SKINS AND THENov 7, 2004 · N200BK · Agusta A109ESDR AC2A099711Blade · crackedTHE PILOT REPORTED PICKING UP A MAIN ROTOR VIBRATION IN FLIGHT AND WAS INSTRUCTED BY FIELD BASE MAINTENANCE PERSONNEL TO RETURN TO BASE. MAIN ROTOR BLADE WAS FOUND TO BE CRACKED NEAR CUFF ON LOWER SIDE. BLADE WAS REPLACED.Nov 1, 2004 · N8776 · Bolkms BO105SSDR CA041224006Bearing · misaligned(CAN) SUBJECT TAIL ROTOR BLADE ASSY WAS REMOVED FROM A/C DUE TO EXCESSIVE T/R VIBRATIONS AT 1.1 IPS. OPERATOR'S OVERHAUL SHOP PERFORMED AN INSPECTION AND AN ALIGNMENT OF SPHERICAL BEARINGS CHECK. IT HAS BEEN DETERMINED THAT THE BEARINGS ALIGNMENT WAS OVER LINov 1, 2004 · Bell 206LSDR JYDRMDR04065Spacer · crackedPART OF THE OB ROOT END SPACER BLOCK BROKE OFF AND WAS SENT THROUGH THE TIP CAP. THE OB SPACER BLOCK HAS SPLIT AROUND THE L/E THROUGH BOLT. PRIOR TO DISASSEMBLY THE OB MOST SPACER BLOCK COULD BE SEEN AS MISSING A PORTION THAT IS ABOUT THE SAME SIZE AS THE HOOct 20, 2004 · N179AC · Skrsky CH54BSDR JJWA0059046Blade · failedTAIL ROTOR BLADE, SENT TR BLADES INSPECTION, BLADE FAILED SKIN THICKNESS TEST WAS .0064 ON UPPER SURFACE, NOT REPAIRABLE. WARRANTY CLAIM.Oct 15, 2004 · N25PM · Bell 206BSDR ERAA098186Blade · vibrationVIBRATION AFTER 3 DAYS OF HEAVY RAIN. NO BALANCE WEIGHTS ON BALANCE BRACKETS. REMOVED T/R BLADE A-10206 AND SENT TO CTI FOR EVALUATION. REMOVED T/R BLADES, VISUALLY INSPECTED ALL COMPONENTS, INSTALLED SERVICEABLE T/R BLADES, LUBED TRUNNION, MARVEL BALANCED,Oct 9, 2004 · N421EH · Bell 412SDR KBM2004F00233Bearing · crackedBEARING HALF SHELLS CRACKED BEYOND LIMITS. REMOVED AND REPLACED.Oct 3, 2004 · N884SH · Snias AS350B2SDR PG92004F00013Blade · crackedT/R SPAR FOUND TO HAVE 5 INCH LONG SPANWISE SPAR CRACK, FOUND BY PILOT UPON TURN AROUND CHECK. THIS CONDITION PERSISTS ON THIS MODEL HELICOPTER AND PN COMPONENT. REPLACED ENTIRE T/R BLADE WITH SERVICEABLE UNIT. RETURN HELICOPTER TO SERVICE.Sep 29, 2004 · N170PA · Snias AS350B2SDR KBM2004F00227Bearing · wornT/R BLADE WORN. REMOVED AND REPLACED HALF SHELLS.Sep 27, 2004 · N37SH · Snias AS350BASDR PG92004F00014Blade · crackedT/R SPAR FOUND CRACKED DURING COMPLIANCE OF SB 05.11R5. THIS CONDITION PERSISTS ON THIS MODEL HELICOPTER AND PN COMPONENT. REPLACED T/R BLADE WITH NEW UNIT. RETURNED HELICOPTER TO SERVICE.Sep 27, 2004 · N890AK · Snias AS350BASDR ALGA097360Blade · defectiveREMOVED DEFECTIVE BLADE FROM SERVICE AND INSTALLED NEW BLADE.Sep 20, 2004 · N2759N · Bell 206L1SDR 2005FA0000661Blade · delaminatedDURING A ROUTINE ALF INSPECTION, THE MECHANIC DISCOVERED DELAMINATION ON THE TAILROTOR BLADE. THE TAILROTOR SHOWED NO SIGNS OF IMPACT. THE DELAMINATED TRIM TAB WAS APPROXIMATELY 3 INCHES LONG AND 2 INCHES IB OF THE TRIM TAB RIVET. THE TAILROTOR ASSY WAS REMSep 13, 2004 · N350EV · Snias AS350B2SDR 2005FA0000660Blade · crackedTAIL ROTOR BLADE, FOUND CRACK APPROX 3.2500 INCH LONG, RUNNING PARALLEL TO TRIM TAB. (K)Sep 12, 2004 · N350EV · Snias AS350B2SDR KBM2004F00223Bearing · wornBEARING HALF SHELLS WORN AND TORN. REMOVED AND REPLACED.Sep 10, 2004 · N215LA · Snias AS350B1SDR TXER100924Tail Rotor · wornTAIL ROTOR, OUT OF LIMITS IAW 64-21-00,6-9 PG. 602 ZONE E.Aug 24, 2004 · N690WR · Urocop EC120BSDR 2005FA0000659Blade · delaminatedDURING A ROUTINE ALF INSPECTION, THE MECHANIC DISCOVERED DELAMINATION ON THE TAILROTOR BLADE. THE DELAMINATED TRIM TAB WAS APPROX 3 INCHES LONG AND 2 INCHES IB OF THE TRIM TAB RIVET. THE TAILROTOR ASSY WAS REMOVED AND SENT TO A BLADE REPAIR FACILITY FOR EVALAug 10, 2004 · N353EV · Snias AS350B2SDR CA040804002Blade · deformed(CAN) TRAILING EDGE SKIN WHERE THE BALANCE WEIGHTS ARE ATTACHED, WAS FOUND DISPLACED APPROXIMATELY 0.080 INCH FROM THE CHORD-LINE. DISCREPANCY WAS DETECTED WHEN A BONDING FAILURE WAS NOTICED IB FROM THE WEIGHTS ON THE BLADE ROOT CLOSE-OUT. THERE WAS NO INDIJul 28, 2004 · Bell 206L3
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