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 H5FA2012F00177Blade · bentTAIL ROTOR BLADE T/E SKIN DEFORMED AT CORDWISE BALANCE WEIGHT.Oct 3, 2012 · N911FF · Bell 206L3SDR 2012FA0000656Blade · misinstalledDURING A PHASE 1 INSPECTION, TAIL ROTOR BLADE CLEARANCE FROM VERTICAL STABILIZER WAS INSUFFICIENT AS IT HAD BEEN IMPROPERLY SHIMMED AND INSTALLED ON THE 90 DEGREE GEAR BOX.Sep 17, 2012 · N7247J · Bell UH1HSDR QMLA2012083012142Blade · brokenONE TENSION-TORSION (TT) STRAP ON TAIL ROTOR HUB, HAD ONE BROKEN BLADE FROM THE LAMINATED PACK THAT WAS DISCOVERED DURING AN INSPECTION/CLEANING OF THE TAIL ROTOR HUB. NO DISCREPANCIES WERE NOTED PRIOR TO ITS DISCOVERY DURING FLIGHT OR SHUTDOWN. THE BROKEN BAug 30, 2012 · N245AM · Urocop EC130B4SDR 2012FA0000611Blade · crackedTAIL ROTOR BLADE MAKING A POPPING NOISE COMING FROM THE SPAR WHEN FLEXED. FOUND BLADE SPAR CRACKED IN TWO PLACES, ONE APPORXIMATELY 48 MM OTBD FROM CENTER OF SPAR , 20 MM LONG FROM L/E TO CENTER OF SPAR ON TARGET BLADE AND ONE APPROX 51 MM LONG FROM L/E TO CAug 29, 2012 · N6095U · Snias AS350B2SDR ALGA2012072301Blade · damagedTAIL ROTOR BLADE WAS FOUND TO HAVE HOLE IN TIP END OF BLADE.Jul 23, 2012 · N177AL · Bell 206L4SDR EVCA2012071600032Blade · damagedON DAILY INSPECTION, MECHANIC FOUND RIVET MISSING FROM THE TAIL ROTOR BLADE TIP.Jul 16, 2012 · N496AE · Bell 206L4SDR CA120716010Blade · damaged(CAN) ON THE DAILY INSPECTION THE PILOT NOTICED THE SKIN ON THE TAIL ROTOR BLADE T/E WAS DELAMINATED, THE SKIN HAD SEPARATED. THE ACFT WAS GROUNDED, MAINTENANCE STAFF INSPECTED THE BLADE AND CONFIRMED THE DEFECT. A NEW BLADE WAS ORDERED AND INSTALLED. MFG PRJul 13, 2012 · Bell 407SDR CA120912006Blade · delaminated(CAN) ON A DAILY INSPECTION, THE PILOT NOTICED ONE OF THE TAIL ROTOR BLADES WAS DELAMINATING/SKIN SEPARATING ON THE T/E NEAR THE TIP. A REPLACEMENT WAS ORDERED.Jul 11, 2012 · Bell 407SDR CA120906011Blade · wrong part(CAN) IT HAS BEEN REPORTED THAT ACFT HAS HAD THE WRONG TAIL ROTOR BLADES FITTED. IT HAS BEEN FLOWN WITH 206-011-810-135 BLADES, LONG SHAFT, FITTED ON A -103 GEARBOX, SMALL SHAFT, FOR APPROXIMATELY 100 HOURS IN THIS CONFIGURATION. THE TAILBOOM HAS NOT BEEN CJun 13, 2012 · Bell 206BSDR ALGA2012061109Spar · failedDURING ROUTINE INSPECTION, SPAR ASSY WAS FOUND TO BE SPLINTERED ON SIDE "B" AT APPROX STA 11.0 ON BOTH PYLON AND OTBD EDGES.Jun 11, 2012 · N865AL · Skrsky S76CSDR ALGA2012061108Spar · damagedDURING ROUTINE INSPECTION, FOUND EDGE OF SPAR SPLINTERED AT APPROX STA 10.5 SIDE "B" OTBD SIDE.Jun 11, 2012 · N865AL · Skrsky S76CSDR 2012FA0000361Blade · crackedDURING PREFLIGHT INSPECTION, FOUND POSSIBLE CRACK AT TAIL ROTOR BLADE. LOCATION WHERE THE FWD STRAP MEETS THE POCKET ON THE L/E, APPROX LENGTH .750. REMOVED TAIL ROTOR BLADE FROM SERVICE FOR FURTHER INSPECTION.May 29, 2012 · N7NJ · Agusta AW139SDR 2012FA0000342Blade · crackedDURING DAILY CHECK AFTER FLIGHT, MECHANIC NOTICED CRACK ON 1 TAIL ROTOR BLADE, JUST AFT OF EROSION SHIELD, EXTENDING FROM THE INBD END OF EROSION SHIELD TO WITHIN APPROX 8" OF OTBD TIP OF THE BLADE. MAX OPENING OF CRACK, APPROX .1875" AT INBD END. CRACK IS EMay 27, 2012 · N917AH · Agusta AW139SDR 2012F00097Blade · dentedDAILY AIRCRAFT CHECK NOTED DENTS ON TAIL ROTOR BLADES OUTER SURFACE. NON-SHARP DENTS ON OTBD FACE OF BOTH BLADES. NO INDICATION OF STRIKE TO BLADE L/E.May 4, 2012 · N307MH · Bell 206L3SDR QMLD2012022310212Rotor · damagedA TAIL ROTOR IS IN THE SHOP FOR A 36 MONTH INSPECTION. ON BEGINNING THE INSPECTION, HAVE WHAT SEEMS TO BE A LIGHTNING STRIKE. AFFECTED ARE THE SPLINED FLANGE, PN L642A2019201, LAMINATED TORSION BAR, PN 350A33318000, AND 1 OF THE SLIDING RING BUSHINGS, PN L642Feb 23, 2012 · N557LF · Urocop EC135P2SDR YTRA201203901Tip Cap · damagedON PRE-FLIGHT DISCOVERED TIP CAP OF TAIL ROTOR PADDLE MISSING.Feb 8, 2012 · N610HG · Skrsky S76ASDR 2011FA0000715Blades · defectiveMECHANIC CONDUCTING DAILY INSPECTION OF THE TAIL ROTOR ASSY HEARD "CRUNCHING" SOUNDS WHEN FLEXING THE BLADES. A BOROSCOPE INSP OF THE INTERNAL CUFFS REVEALED FIBERGLASS FIBERS PROTRUDING FROM THE SPAR AND A CRACK THROUGH THE RUBBER BLOCK AND INTO THE BLADE INOct 11, 2011 · N3972A · Snias AS350B3SDR 2011FA0000714Rotor · out of balanceAFTER INSTALLATION OF REPAIRED TAIL ROTOR, A MAIN ROTOR TRACK AND BALANCE WAS REQUIRED AND CONDUCTED. BOTH THE TRACK AND THE BALANCE OF THE MAIN ROTOR SYS WAS FOUND TO BE OUT OF LIMITS. THE ONLY MX PERFORMED ON THIS SYS WAS THE RE-TORQUE REQURIED AFTER THE AOct 11, 2011 · N3972A · Snias AS350B3SDR 2011FA0000713Shaft · mismanufacturedAFTER INSTALLATION OF REPAIRED TAIL ROTOR ASSY, A VIBRATION CHECK AND BALANCE CHECK OF THE "SHORT SHAFT" IS REQUIRED. THE BALANCE WAS OUT BY A CONSIDERABLE AMOUNT AND AS THESE PART WERE NEVER REMOVED OR ALTERED DURING THE REPLACEMENT OF THE TAIL ROTOR ASSY, IOct 11, 2011 · N3972A · Snias AS350B3SDR ALGAR91311A245005Blade · crackedTAIL ROTOR BLADE FOUND TO BE SPLINTERED AND CRACKED AT INBD EDGE RT STA 11.00Sep 12, 2011 · Skrsky S76CSDR 2011FA0000599Counterweight · departedAT APPROXIMATELY 21:15 THE EVENING OF 31 AUG 2011, DEPARTED THE COUNTY RAMP IN FOR A NIGHT VISION GOGGLE TRAINING MISSION WITH A CONTRACT INSTRUCTOR PILOT. WEATHER AT THE TIME WAS VFR. ALL PRE-FLIGHT CHECKS WERE NORMAL, AS WAS TAKEOFF AND CLIMB HEADING SOUTAug 31, 2011 · N56AL · Bell 206BSDR QMLDMG2491Blade · debondedWHILE PERFORMING A 1200 HOUR/36 MONTH INSP OF THE TAIL ROTOR ASSEMBLY, FOUND 3 TAIL ROTOR BLADES P/N L642A2002101 S/N M715, M8073, AND M8075 BALANCE WEIGHT POCKETS DEBONDED FROM THE BLADES AND ONE IS CRACKED AND HAS A PIECE MISSING. NOTE: THESE 3 BLADES WERE Aug 19, 2011 · N969ME · Urocop EC135T1SDR E3MA20110602Blade · wornPILOT COMPLAINED OF A VIBRATION THAT WAS MOST NOTICEABLE IN THE TAIL ROTOR PEDALS. UPON INSPECTION OF THE TAIL ROTOR A BLADE WAS DICOVERED TO HAVE EXCESSIVE LEAD-LAG MOVEMENT.Jun 1, 2011 · N944ME · Urocop EC135T2SDR RMXA383298Blade · damagedUPON APPROACH, ACFT SUSTAINED A BIRD STRIKE ON THE PILOT SIDE WIND SCREEN AND WAS PROJECTED INTO THE TAIL ROTOR DUE TO THE DOWN WASH OF THE MAIN ROTOR SYS TECH INSPECTED WINDSCREEN WITH NO DEFECTS NOTED. TAIL ROTOR BLADE AND SPIDER ASSY HAD EVIDENCE OF THE BIRMay 2, 2011 · N4282 · Snias AS350B3SDR ALGAR4141100364XBlade · damagedPADDLE "B" L/E FOD APPROX 1" LONG AT STA 27.00.Apr 14, 2011 · N702AL · Skrsky S76ASDR CA110330005Blade · cracked(CAN) UPON MAINTENANCE, THE TAIL ROTOR BLADE OUTER SKIN WAS FOUND CRACKED APPROXIMATELY 2.5" LONG ON A CHORDWISE PLANE-APPROXIMATELY 5.5" FROM THE BLADE ROOT.Mar 29, 2011 · Bolkms BK117B2SDR CA110323007Blade · cracked(CAN) SKIN CRACKED 4.25" LONG ON CHORD WISE PLANE, APPROX 5.5" FROM BLADE ROOT.Mar 22, 2011 · Bolkms BK117B2SDR CA110322004Blade · delaminated(CAN) DURING DAILY INSPECTION, THE TAIL ROTOR BLADE WAS FOUND TO HAVE DELAMINATED SKIN ON THE OTBD SIDE OF THE BLADE, 4 INCHES FROM END TIP OF BLADE & AFT OF LE STAINLESS STEEL STRIP. THE ALUMINUM SKIN HAD DEBONDED FROM THE SPARE APPROX 5 INCHES SPAN WISE & 3Mar 18, 2011 · Bell 212SDR CA110315004Blade · cracked(CAN) DURING THE INSPECTION 600 HOURS/ANNUAL, WE PERFORMED VISUAL INSPECTION OF THE TAIL ROTOR BLADES AND OBSERVED A SPANWISE CRACKS AT THE TRAILING EDGE SKINS . ACCORDING TO THE MANUFACTURER SCHWEIZER, NO CRACKS ARE ALLOWED AT THE TAIL ROTOR.Mar 11, 2011 · Hughes 269C1SDR ALGA011911920ALRetaining Nut · missingON APPROACH, CREW REALIZED TAIL ROTOR EFFECTIVENESS HAD BEEN LOST. CREW ABORTED APPROACH AND PERFORMED SUCCESSFUL RUN-ON LANDING AT NEARBY AIRPORT. UPON SHUTDOWN AND INSPECTION BY MX, IT WAS FOUND THAT THE TAILROTOR PITCH BEAM RETAINING NUT AND LOCK RING WEREJan 19, 2011 · N920AL · Skrsky S92ASDR HEEA129840Pitch Horn · crackedON DAILY INSPECTION FOUND TAIL ROTOR PITCH HORN CRACKED. REPLACED T/R ASSEMBLY.Nov 30, 2010 · N274X · Skrsky S76CSDR CA110105010Spar · cracked(CAN) DURING A SCHEDULED 500 HR TAIL ROTOR BOROSCOPE, MRS 35974, FOUND FWD AND AFT L/E OF SPAR CRACKED FROM BS 9.6 TO 13.25. TAIL ROTOR PADDLE ASSY REPLACED. CONTINUE 500 HR INSPECTIONS.Oct 21, 2010 · Skrsky S76ASDR CA101102011Blades · debonded(CAN) AIRCRAFT WAS IN FOR A 100HR INSPECTION. ON INSPECTION AS PER MANUAL FOUND A SMALL AMOUNT OF DEBONDING ON THE LEADING EDGE. NO IMPACT MARKS WHERE FOUND ON EITHER BLADE. MANUFACTURER REPORT FOUND THE BLADES SCRAP DUE TO DIMENSIONAL DIMENSIONS ON ONE BLAJul 5, 2010 · Snias AS350B2SDR U0G2010F00000Blade · damagedPRECAUTIONARY LANDING WAS MADE DUE TO T/R VIBRATION. T/R BLADE TIP HAS LARGE PIECE OF PAINT MISSING. REPLACED T/R ASSY, OPS CHECK GOOD TL-017656-2010.Jun 8, 2010 · N129EH · Bolkms BO105SSDR JBZA2010F00088Blade · crackedDURING AD 2005-04-09A VISUAL INSP COMPLIANCE, FOUND APPROX .2500 INCH ONE LEG BY .7500 INCH SECOND LEG CRACK IN THE DESIGNATED INSP AREA OF THE TARGET TAIL ROTOR BLADE.Mar 19, 2010 · N34NR · Bell 222SDR 1E9R201001Blade · crackedACFT WAS FLOWN TO FACILITY, REPORTED DEBONDING OF TAIL ROTOR BLADE L/E AT TIP OF BLADE. UPON FURTHER INVESTIGATION OF BLADE, IT WAS DISCOVERED THAT THE ROOT END OF THE BLADE HAD CRACKED AND THE SKIN WAS SEPARATED FROM THE BLADE END. INFO SUBMITTED TO MFG PROFeb 19, 2010 · N430TX · Bell 430SDR 2010FA0000164Blade · detachedDURING GROUND RUN FOLLOWING COMPLETION OF ANNUAL INSP AND CHECK OF GENERATOR BEING INOPERATIVE. A VIB. WAS NOTED WITH THE ENGINE SHUTDOWN. INSP OF THE ACFT SHOWED A HOLE IN THE AFT COWLING TO THE RT SIDE OF THE OIL COOLER. THE DAMAGE CONTINUED THROUGH 2 BULFeb 18, 2010 · N213SJ · Bell 212SDR CA091013003Blade · delaminated(CAN) DURING DAILY INSP PILOT NOTICED THE OTBD T/E SKIN WAS DELAMINATED 6 INCHES FROM THE TIP ON TAIL ROTOR BLADE PN 206-016-201-131, SN CS-12194 BLADE HAS 120.8 HOURS REMAINING BEFOR RETIREMENT. BOTH BLADES WERE REPLACE WITH NEW BLADES AND THE ASSY WAS BALANCOct 10, 2009 · Bell 206LSDR ALGA09290900861Spar · crackedIN AN ATTEMPT TO TRACK AND BALANCE 2 EACH NEWLY INSTALLED T/R BLADE ASSEMBLIES, A VERY HIGH VIBRATION WAS NOTED AND IMMEDIATE SHUTDOWN OCCURRED. THE T/R BLADE ASSEMBLIES WERE REMOVED AND RETURNED TO OUR BLADE SHOP. UPON PERFORMING A PRELIMINARY INSP ON THE BLASep 29, 2009 · N883AL · Skrsky S76CSDR ULXR2009091683124Blade · debondedTAIL ROTOR BLADE LEADING EDGE STRIP DEBONDING.Sep 16, 2009 · N305FD · Agusta AW139SDR QMLR MC708Blade · crackedFOUND TAIL ROTOR BLADE ROOT TO BE CRACKED IN VICINITY OF PITCH HORN.Aug 27, 2009 · N556UH · Bell 430SDR HEEA125379Spar · crackedWHILE PERFORMING 500 HOUR TAIL ROTOR SPAR INSPECTION FOUND RED TAIL ROTOR BLADE SPAR CRACKED ALONG FORWARD EDGE. MAINTENANCE REPLACED THE TAIL ROTOR BLADE ASSY. NOTE: PREVIOUSLY SUBMITTED ON 7/24/09.Jul 16, 2009 · N725P · Skrsky S76CSDR HEEA124870Blade · crackedWHILE PERFORMING 1500 HOUR TAIL ROTOR BLADE INSPECTION FOUND CRACK IN INBOARD SIDE SURFACE SKIN APPROX. 2 INCHES IN LENGTH ON RED TAIL ROTOR BLADE. MAINTENANCE REPLACED TAIL ROTOR BLADE ASSY. NOTE: PREVIOUSLY SUBMITTED ON 6/22/09.Jun 21, 2009 · N718P · Skrsky S76CSDR CA090505006Blade · separated(CAN) PILOT DURING HIS PREFLIGHT NOTICED SEPARATION IN THE TAIL ROTOR BLADE TIP WEIGHT AREA,Apr 30, 2009 · Bell 407SDR CA090407012Bearing · damaged(CAN) DURING A SERVICEABILITY CHECK AT T/R ASSY SECTION (BLADE S/N CS-10215) BEARING MOVING INSIDE THE BLADE, FOUND.Apr 7, 2009 · Bell 206LSDR CA090324006Blade · debonded(CAN) DURING A DAILY INSP, THE ENGINEER NOTICED CRACKS IN THE BONDING SUROUNDING THE EFFECTED TAIL ROTOR TIP CAP. FURTHER INVESTIGATION REVEALED DELAMINTAION OF THE SKIN TO THE TIP CAP ON BOTH SIDES OF THE BLADE. NO ABNORMAL VIBRATIONS WERE REPORTED FOLLOWING Mar 19, 2009 · Bell 212SDR CA080813002Pitch Horn · loose(CAN) THE STUD WHICH HOLDS THE PITCH LINKS ONTO THE PITCH HORN CAME LOOSE. THIS CAUSED A VIBRATION FELT IN THE PEDALS. THE TAILROTOR HUB WAS 2400 HOURS TSO AND BLADES WERE 2300 TSN. THERE IS NO REQUIREMENT TO OVERHAUL THE PITCH HORNS SO NO RECORD AS TO TOTAL TAug 13, 2008 · Bell 206LSDR CA080728009Blade · cracked(CAN) FOUND T/R BLADE CRACKED NEAR TIP OF BLADE AND TRAILING EDGE ON DAILY INSPECTION. BLADE REMOVED FOR EVALUATION BY MFG.Jul 19, 2008 · Snias AS350B2SDR CA080715007Pitch Horn · damaged(CAN) THE PITCH HORN STUD FAILED WHILE INSTALLING A NUT P/N MS14145L5. A "CLICKER-TYPE" TORQUE WRENCH SET TO 60 INCH/LBS WAS USED TO INSTALL THE NUT. THE REQUIRED FINAL TORQUE FOR THIS NUT IS 50-60 INCH/LBS PLUS TARE. THE TIGHTENING TORQUE NEVER REACHED 60 INCJul 15, 2008 · Bell 206BSDR EGI2008F00002Blade · damagedDURING SCHEDULED 100 HOUR INSP OF AC, INSP OF TAIL ROTOR BLADES REVEALED THAT ONE T/R BLADE HAD MECHANICAL DAMAGE. THE DAMAGE WAS CONFINED TO THE T/E WHICH CONSISTED OF A DENT AT T/R BLADE STA 16.5 APPROXIMATELY .010 INCH DEEP AND THE T/E BENT IN A SPAN OF APJun 26, 2008 · N255EV · Bell 206L3
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