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 20001215SH034Hinge · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A33-2153-00, CORRECTED PROBLEM. TWO TEETERING BEARINGS EQUALS 1 KIT. (X)SDR 20001101SH026Pitch Horn · looseDURING A 100-HOUR INSPECTION, ONE OF THE MECHANICS FOUND THE STUD PN 206-010-744-105 LOOSE IN THE PITCH HORN, PN 206011-809-107. THE POSSIBLE CAUSE IS UNKNOWN AT THIS TIME. (X)SDR 20001101SH015Hinge · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A33-2153-00 CORRECTED PROBLEM. TWO TEETERING BEARINGS EQUALS ONE KIT. (X)SDR CA000925011Blade · cracked(CAN) THE T/R SPINDLE INSPECTION WAS BEING C/O AT WHICH TIME A CRACK IN THE SKIN OF THE TAIL ROTOR BLADE WAS DISCOVERED. THE BLADE WAS REMOVED FROM SERVICE AND IMMEDIATELY SENT BACK TO THE MANUFACTURER FOR REPAIR EVALUATION. (X)SDR AC2A0000092Blade · peelingTAIL ROTOR BLADE PAINT PEELING AND BEARINGS WORN BEYOND LIMITS. INSPECTED, REPLACED 2 EACH BEARINGS, SANDED THE PAINT AND REPAINTED. INSTALLED 2 EACH SLEEVES PN 206-010-733-003 PNAV 300549, 2 EACH BEARINGS PN 206-310-105-101 TRACKING NR 39858. (X)SDR AC2A0000091Blade · peelingTAIL ROTOR BLADE PAINT PEELING AT 370.2 HOURS SINCE NEW. VISUAL INSPECTED, SANDED PAINT AND REPAINTED. (X)SDR 20000816SH001Blade · damagedNEW PART RECEIVED FROM HONEYWELL WITH DAMAGE ON ONE BLADE. LOT NR: 4,685. (X)SDR 20001101SH014Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, FROM 1 EACH KIT P/N 355A09-1036-01, CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS ONE KIT. (X)SDR 20000810SH002Blade · crackedPILOT FOUND TAIL ROTOR BLADE ROOT FITTING CRACKED ON A PRE-FLIGHT INSPECTION. THIS IS THE SECOND OCCURRENCE ON THIS AIRCRAFT. THE LAST BLADE, S/N 009999-1489, ONLY TWO SERIAL NUMBERS DIFFERENCE. (X)SDR CA001205004Blade · delaminated(CAN) TAIL ROTOR BLADE DELAMINATION FOUND BETWEEN THE SKIN AND THE TIP BLOCK THAT WAS BEYOND LIMITS. TAILROTOR ASSEMBLY REPLACED.SDR CA000719021Bearing · loose(CAN) EXCESS BEARING PLAY. BEARING WAS LOOSE IN THE SLEEVE. REPLACED BEARINGS IN ACCORDANCE WITH BHT 206L M&O.SDR CA000718019Tail Rotor · missing(CAN) WHILE IN FLIGHT,TAIL ROTOR TIP CLOSURE FROM BLADE S/N A-9612 DEPARTED BLADE. ENSUING, EXTREME VIBRATION, CAUSED PILOT TO LAND IMMEDIATELY, WITHOUT FURTHER DAMAGE TO A/C. INSPECTION OF T/R SHOWED TIP CLOSURE OF BLADE S/N A-9612 TO BE GONE IN ITS ENTIRETYSDR AC2A0000053Blade · separatedSEPARATION IN THE ROOT CLOSURE. THIS WAS THE ORIGINAL TAIL ROTOR BLADE RECEIVED WITH THIS AIRCRAFT. IT WAS REMOVED THE FIRST TIME AT AIRCRAFT TT: 589.4 HOURS FOR BEARINGS CRACKED. REPLACED TAIL ROTOR BLADE ASSY WITH SERVICEABLE PART. (X)SDR R7MA714332494Bushing · worn2 EA BUSHINGS, TELFON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM.SDR R7MA714332495Bushing · worn2 EA BUSHINGS, TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM.SDR CA001206002Blade · damaged(CAN) BOTTOM 1 INCH OF TAIL ROTOR SKIN PEELED OFF AND DEPARTED IN-FLIGHT. (X)SDR HEEA068391Bearing · separatedLAMINATED SEPARATION AT THE END OF THE BEARING.SDR 20000609SH001Bearing · wornBEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. (X)SDR AU000603Blade · delaminated(AUS) AFTER APPROXIMATELY A ONE HOUR FLIGHT IN HEAVY RAIN, THE PILOT DISCOVERED THE DELAMINATION ON ONE TAIL BLADE HAD PROPAGATED TO APPROXIMATELY 3.5CM (1.37 INCH). PROBLEM WAS INITIALLY FOUND ABOUT 18 HOURS EARLIER, HOWEVER, THE DELAMINATION WAS WITHIN LIMSDR 20000605SH016Bearing · wornLAMINATED TAIL BEARING, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000605SH026Laminated Hinge · wornLAMINATED HINGE, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000605SH002Laminated Hinge · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000717SH015Bearing · delaminatedBEARING DELAMINATING. (X)SDR CA000511005Blade · torn(CAN) POST FLIGHT INSPECTION REVEALED TWO TEARS IN TAIL ROTOR BLADE POCKET (19 & 16 INCH FROM TIP). IT APPEARS THAT LEADING EDGE TAPE CAME LOOSE AND FLAPPED AGAINST BLADE CAUSING THE TWO TEARS.SDR 20000607SH015Bushing · unserviceableBUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. (X)SDR 20000607SH014Bushing · wornBUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. (X)SDR 20000608SH030Bushing · wornBUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. (X)SDR 20000608SH029Bushing · wornBUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. (X)SDR 20000605SH015Laminated Hinge · wornLAMINATED HINGE, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR CA000322001Blade · cracked(CAN) DURING HELI-SKIING OPERATIONS, PILOT LANDED ON HELIPAD AND NOTICED VIBRATIONS. PILOT CHECKED T/R BLADES AND FOUND ICE BUILD-UP. PILOT THEN DID START-UP BUT VIBRATION WAS STILL PRESENT AND SHUT-DOWN WAS CARRIED OUT. PILOT THEN INSPECTED T/R BLADES FURSDR 20000810SH003Blade · crackedCRACKED BLADE WAS FOUND ON POST-FLIGHT AFTER THE PILOT FELT AN IN-FLIGHT VIBRATION. THE TAIL ROTOR BLADE WAS CRACKED FROM THE INBOARD ROOT FITTING, 1.5 INCHES LONG WITH A 90-DEGREE TURN FOR ANOTHER .5 INCH. (X)SDR 20000605SH021Laminated Hinge · wornLAMINATED HINGE, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000605SH018Bearing · wornLAMINATED TAIL BEARING, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000605SH025Laminated Hinge · wornLAMINATED HINGE - ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000407SH005Blade · crackedITEM CRACKED AT ROOT ATTACH POINT OF TAIL ROTOR BLADE. REMOVED TAIL ROTOR BLADE FROM ASSY AND DISCOVERED TAIL ROTOR BLADE ATTACH BOLTS WERE NOT TORQUED TO MANUFACTURER SPECIFICATIONS. (X)SDR 20000608SH028Bushing · wornBUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000608SH027Bushing · wornBUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR AC2A066556Bearing · damagedBEARINGS WERE GAULING AND CAUSING STIFF PEDALS AT 100 PERCENT. INSTALLED 4 NEW BEARINGS IN THE BLADES.SDR AC2A0000019Bearing · galledBEARINGS WERE GALLING AND CAUSING STIFF PETALS AT 100 PERCENT. INSTALLED 4 NEW BEARINGS IN THE BLADES. (X)SDR 20000413SH010Blade · crackedPITCH CHANGE BEARINGS CRACKED. REMOVED AND REPLACED. (X)SDR 20000413SH009Blade · crackedPITCH CHANGE BEARINGS CRACKED. REMOVED AND REPLACED. (X)SDR HEEA065874Bearing · wornWORN FEATHERING BEARINGS. SERIAL NUMBERS REMOVED ARE A-2248 AND A-2252. REPLACED WITH SERIAL NUMBERS A-2099 (DMR NR 6861800) AND A-2098 (DMR NR 6861801).SDR ERAA065956Blade · chippingTAILROTOR BLADES REPAIRED POG143564 4/99. PAINT CRACKED BEYOND LIMITS AND PAINT CHIPPING OFF.SDR 20000605SH017Laminated Hinge · wornLAMINATED HINGE, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000605SH013Laminated Hinge · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR HEEA065605Blade · flakingPAINT ON TAIL ROTOR BLADE FLAKING.SDR HEEA065604Blade · flakingPAINT ON TAIL ROTOR BLADE FLAKING.SDR 20000424SH015Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR HEED065762Bearing · crackedCRACKED T/R FEATHER BEARING AND PLAY IN TRUNNION BEARING. REPLACED UNIT.SDR HEEA065323Bearing · wornWORN BEARINGS.
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