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 MDR03026Strap · crackedTHE STRAP IS CRACKED ON THE OUTBOARD SIDE OF THE BLADE, APPROXIMATELY 9.5 INCHES FROM THE TRAILING EDGE OF THE FAIRING. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARD THE TIP END OF THE BLADE APPROXIMATELY 2 INCHES. THE CRACK STARTS WHERE TSDR HEEA088660Blade · peelingTAIL ROTOR BLADE PAINT PEELING.SDR HEEA088659Blade · peelingTAIL ROTOR BLADE PAINT PEELING.SDR PH92003F00001Blade · crackedTAIL ROTOR BLADE HAS 4000 HOURS TBR(SLL). UNIT FAILED AT 2760.0 TTSN. MASSIVE SPAR CRACK ON LAMINATED SPAR. UNIT RETURNED TO MFG.SDR PH92003F00000Blade · crackedTAIL ROTOR BLADE HAS 4000 HOURS TBR(SLL). UNIT FAILED AT 2740.3 TTSN. MASSIVE SPAR CRACK ON LAMINATED SPAR. UNIT RETURNED.SDR HEEA088449Blade · corrodedTAIL ROTOR BLADE FRETTING CORROSION ON BLADE MATING SURFACE CAUSED BY LOST TORQUE ON PITCH HORN HARDWARE.SDR HEEA088448Blade · corrodedTAIL ROTOR BLADE HAS FRETTING CORROSION ON BLADE MATING SURFACE CAUSED BY LOST TORQUE ON PITCH HORN HARDWARE.SDR HEEA088447Pitch Horn · corrodedFRETTING CORROSION ON BLADE MATING SURFACE CAUSED BY LOST TORQUE ON PITCH HORN HARDWARE.SDR HEEA088446Pitch Horn · corrodedFRETTING CORROSION ON BLADE MATING SURFACE CAUSED BY LOST TORQUE ON PITCH HORN HARDWARE.SDR MDR03020Strap · crackedSTRAP IS CRACKED ON THE OB SIDE OF THE BLADE APPROXIMATELY 9.125 INCHES FROM THE TRAILING EDGE OF THE FAIRING. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARD THE TIP END OF THE BLADE APPROXIMATELY 1 INCH. THE CRACKS START WHERE THE LEADING SDR MDR03019Strap · crackedTHE STRAP IS CRACKED ON THE OUTBOARD SIDE OF THE BLADE APPROXIMATELY 9.187 INCHES FROM THE TRAILING EDGE OF THE BLADE. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARDS THE TIP END OF THE BLADE APPROXIMATELY 1 INCH. THE CRACKS START WHERE THESDR BAQA090156Blade · nickedNICKS IN BLADE, AND OUT OF LIMITS. COPY OF TAIL ROTOR HEAD ASSEMBY ENCLOSED.SDR KBMA088326Bearing · crackedTAIL ROTOR BLADE HALF SHELL BEARINGS HAVE CRACKS. REPLACED WITH NEW 4 EACH HALF SHELL BEARING KIT.SDR HEEA088367Blade · erodedPRIMARY RUBBER ON THE LEADING EDGE HAS ERODED TO THE FIBERGLASS SKIN AND WIRE MESH OR TAIL ROTOR BLADE.SDR HEEA088366Blade · wornPRIMARY RUBBER ON THE LEADING EDGE HAS ERODED TO THE FIBERGLASS SKIN AND WIRE MESH OF TAIL ROTOR BLADE.SDR MDR03018Strap · crackedTHE STRAP IS CRACKED N THE OUTBOARD SIDE OF THE BLADE, APPROXIMATELY 9.125 INCHES FROM THE TRAILING EDGE. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS APPROXIMATELY 1.25 INCHES TOWARDS THE TIP END OF THE BLADE. THE CRACK STARTS WHERE THE BACK WASDR HEEA087309Blade · damagedSEPARATION ON TRAILING EDGE AT THE TIP. REPAIRED.SDR HEEA087307Blade · damagedCLICK NOISE WHEN BLADES ARE FLAPPED. REPAIRED.SDR HEEA087306Blade · peelingPAINT PEELING OFF BLADES. REPAIRED.SDR HEEA087132Blade · damagedHOLE IN BLADE. REPLACED TAIL ROTOR ASSEMBLY.SDR CA030710002Blade · failed(CAN) VOID IN S.S. LEADING EDGE STRIP OUTBOARD BLADE TIP JUNCTION OF BLADE SKIN. VOID AREA APPROXIMATELY 0.175 INCH CHORDWISE X 0.375 INCH SPANWISE. BLADE REMOVED AND SENT FOR REPAIR. SN A-7719.SDR CA030610002Blade · cracked(CAN) DURING A DAILY INSPECTION A CRACK WAS FOUND IN THE INBOARD SIDE OF THE TRAILING EDGE POCKET. THE CRACK STARTED AT THE TRAILING EDGE AND PROPAGATED FORWARD APPROXIMATELY 70MM. (2.75 INCHES)SDR 3144052803Blade · delaminatedT/R BLADES NEED PAINTING.SDR HEEA086560Blade · erodedFIBERGLASS ERODED UNDER THE PRIMARY RUBBER. SENT COMPOSITES FOR INSPECTION.SDR HEEA086559Blade · damagedTRAILING EDGE OF PADDLE "A" NEAR THE TIP HAS SOME SEPERATION.SDR ERAA087101Blade · crackedSPAR HAS A FIBERGLASS SPLINTER STICKING OUT AND LEADING EDGE STRIP IS CRADKED ON ONE BLADE. AREA OF SPLINTER UT INSPECTED PER 2ATI 3098, NO DELAMINATION FOUND SPLINTER REMOVED AND REPAIRED BY CTI.SDR ERAA087084Blade · damagedTHIS INFO FOR FAA SDR. HOLE IN BLADE TIP AND FEATHERING BEARINGS LOOSE. PITCH HORN BUSHINGS MISSING. FEATHERING BEARINGS WORN AND BLADE HAD VOID AT TIP. TRUNNION BEARINGS HAD SOME ROUGHNESS. ACTION TAKEN: DISASSEMBLED, CLEANED & VISUALLY INSPECTED PARTS.SDR ERAA087083Blade · damagedTAIL ROTOR ASSY HAS HOLE IN BLADE TIP. TAIL ROTOR BLADE SN A-9675 HAS VOID AT TIP. REMOVED BLADES FROM YOKE ASSY. INSTALLED SERVICEABLE BLADE SN A-10483 AND TOUCHED UP PAINT ON BLADE SN 9724. CHECKED TRUNNION CENTERING AND PURGE LUBED . ASSEMBLED AND BALSDR HEEA087971Blade · tornTAIL ROTOR BLADE PRIMARY RUBBER TORN BEYOND LIMITS.SDR CA030408003Blade · debonded(CAN) WHILE DOING A DAILY INSPECTION ON THE TAIL ROTOR BLADES IT WAS NOTICED THAT THE LEADING EDGE WAS DEBONDING ON THE TRAILING EDGE OF THE LEADING EDGE ABRASION STRIP. THE LOCATION IS ABOUT 8 INCHES FROM THE TIP OF THE BLADE AND THE TOTAL LENGTH OF THE DELAMSDR AUS20030393Blade · corroded(AUS) TAIL ROTOR BLADE LEADING EDGE CONTAINED SMALL HOLES.SDR BAQA085883Blade · peelingTAIL ROTOR BLADE HAS PAINT PEELING OFF. UNABLE TO BALANCE. REPLACED WITH SERVICEABLE UNIT.SDR YT2R110913Bearing · crackedTAIL ROTOR LAMINATES, PART REMOVED, DUE TO CRACKING.SDR 2003FA0000247Blade · brokenWHILE IN FLIGHT , PILOT EXPERIENCE VIBRATION WITH LOSS OF TAIL ROTOR CONTROL AUTHORITY. AFTER LANDING ,INSPECTION REVEALED THE BLADE PITCH HORN HAD BROKEN INTO TWO PIECES, RENDERING ONE BLADE WITH NO PITCH CONTROL.SDR HEEA085080Bearing · delaminatedTAIL ROTOR BLADE BEARING IS WORN, DETERIORATED AND DELAMINATED.SDR BAQA084840Blade · erodedTAIL ROTOR BLADE HAS EROSION.SDR HEEA085071Blade · erodedT/R BLADE HAS PAINT EROSION.SDR HEEA085070Blade · erodedT/R BLADE HAS PAINT EROSION.SDR AC2A084864Bearing · wornTAIL ROTOR BEARINGS ARE WORN. REPLACED WITH NEW BEARINGS.SDR HEEA084198Blade · crackedTRAILING EDGE HAS SEPARATION AND A 5 INCH CRACK. REPLACED WITH SERVICEABLE PART.SDR HEEA084169Blade · damagedTAIL ROTOR BLADE PRIMARY RUBBERS ON BOTH PADDLES TORN.SDR ALGA084091Blade · peelingFOUND PAINT PEELING FROM NEW TAIL ROTOR BLADES. TIME SINCE NEW ON BLADES IS 23.7 HOURS.SDR BAQA084063Blade · out of balanceBLADES WOULD NOT BALANCE. REPLACED WITH SERVICEABLE UNITS S/N 413 AND 414.SDR YT22003F00001Bearing · crackedTAIL ROTOR LAMINATED BEARINGS CRACKED.SDR ALG2003F218APlug · debondedDISCOVERED DURING ROUTINE MAINTENANCE INSPECTION. SPAR ELLIPTICAL PLUG 100 PERCENT DEBONDED. NEW PLUG INSTALLED AT MFG O AND R 12-26-00 AT COMPONENT TOTAL TIME 11978.5.SDR 2003FA0000069Grip · looseGRIP BUSHINGS WERE ROTATING INSIDE OF GRIP CAUSING GRIP INSIDE DIAMETER TO WEAR BEYOND LIMITS.SDR 2003FA0000067Grip · looseGRIP BUSHINGS WERE ROTATING INSIDE OF GRIP CAUSING GRIP INSIDE DIAMETER TO WEAR BEYOND LIMITS.SDR HEEA083535Blade · splitTAIL ROTOR BLADE TRAILING EDGE OF PADDLE "A" IS SPLIT OPEN. TO BE SENT TO VENDOR FOR INSPECTION AND REPAIR.SDR VY1L103169Bearing · crackedTAIL ROTOR BEARING CRACKED BEYOND LIMITS.SDR BAQA082884Blade · damagedTAIL ROTOR BLADE HAS EXCESSIVE PLAY IN SPOOL. REPLACED WITH SERVICEABLE UNIT.
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