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.
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
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 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-04-127SDR 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)SDR 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.SDR KBM2006F00052Bearing · crackedHALF SHELL BEARINGS, UNIT CRACKED, REMOVED AND REPLACED WITH NEW. (K)SDR KBM2005F00243Bearing · crackedUNIT HAS MULTIPLE CRACKS. REMOVED AND REPLACED UNIT. (M)SDR 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 PREVIOSDR KBM2005F00148Case · crackedHALF SHELL, UNIT HAS MULTIPLE CRACKS. REMOVED AND REPLACED. (K)SDR 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)SDR KBM2005F00138Bearing · wornHALF SHELLS, WORN. REMOVED AND REPAIRED. (K)SDR KBM2005F00132Bearing · wornHALF SHELL BEARINGS, WORN. REMOVED AND REPLACED. (K)SDR 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 INSTALLASDR ALGA104359Sleeve · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOPSDR ALGA104358Bearing · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP.SDR 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.SDR 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 TRISDR KBM2005F00104Bearing · tornHALF SHELL BEARING KIT, TORN LAMIFICATIONS, REMOVED AND REPLACED. (K)SDR ALGA104360Bearing · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP.SDR ALGA104357Sleeve · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP.SDR CA050513002Spar · cracked(CAN) NOISE HEARD ON PITOT DAILY INSPECTION AS PART OF EUROCOPTERS CRITERIA. DISASSEMBLED BY ENGINEER AND FOUND CRACKED.SDR KBM2005F00208Bearing · wornHALF SHELL LAMINATED BEARINGS, WORN BEYOND LIMITS. REMOVED AND REPLACED. (K)SDR ALGA099525Blade · chippedCHROME MONOXIDE SURFACE CHIPPED BEYOND LIMITS. SEND TO AMERICAN EUROCOPTER FOR WARRANTY CONSIDERATION.SDR 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 SDR K2D2005F00000Blade · damagedREF: K2DA320J TAIL ROTOR BLADE ABRASION STRIP AND TIP CAP DEPARTED BLADE ASSY, INFLIGHT. (WP13200506018) (K)SDR CA050124005Blade · debonded(CAN) TAIL ROTOR BLADE DOUBLER DEBOND ON APPROX. 6.5 IN. FROM THE TIP OF THE DOUBLER.SDR 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)SDR 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.SDR 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.SDR KBM2005F00002Bearing · wornHALF SHELLS WORN. REMOVED AND REPLACED.SDR ALGA098355Blade · crackedREPORTS OF CRACKS AND DEFORMATION IN SKIN AND WEIGHTS, SENT TO RBI TO CW AD 2004-24-08.SDR KBM2005F00000Bearing · crackedHALF SHELLS CRACKED. REMOVED AND REPLACED. (K)SDR ALGA098105Blade · crackedINSPECTION FOR SKIN ON THE AREA OF TRAILING EDGE OF BALANCE WEIGHT C/W ASB206L-04-127 REVB PT3.SDR 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 EMANASDR 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)SDR 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 THESDR 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.SDR 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 LISDR 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 HOSDR JJWA0059046Blade · failedTAIL ROTOR BLADE, SENT TR BLADES INSPECTION, BLADE FAILED SKIN THICKNESS TEST WAS .0064 ON UPPER SURFACE, NOT REPAIRABLE. WARRANTY CLAIM.SDR 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,SDR KBM2004F00233Bearing · crackedBEARING HALF SHELLS CRACKED BEYOND LIMITS. REMOVED AND REPLACED.SDR 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.SDR KBM2004F00227Bearing · wornT/R BLADE WORN. REMOVED AND REPLACED HALF SHELLS.SDR 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.SDR ALGA097360Blade · defectiveREMOVED DEFECTIVE BLADE FROM SERVICE AND INSTALLED NEW BLADE.SDR 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 REMSDR 2005FA0000660Blade · crackedTAIL ROTOR BLADE, FOUND CRACK APPROX 3.2500 INCH LONG, RUNNING PARALLEL TO TRIM TAB. (K)SDR KBM2004F00223Bearing · wornBEARING HALF SHELLS WORN AND TORN. REMOVED AND REPLACED.SDR TXER100924Tail Rotor · wornTAIL ROTOR, OUT OF LIMITS IAW 64-21-00,6-9 PG. 602 ZONE E.SDR 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 EVALSDR 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 INDI
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