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 CA010724035Blade · damaged(CAN) ON INSPECTION OF OPPOSITE TAIL ROTOR BLADE, THIS TAIL ROTOR BLADE WAS FOUND TO HAVE NO ABRAISON STRIP ON LEADING EDGE OF BLADE. FURTHER INSPECTION REVEALED THAT FILLER WAS USED UNDER PAINT TO BUILD UP EDGE. BOTH BLADES WERE REMOVED AND SENT TO SCHWEIZER SDR CA010724034Blade · cracked(CAN) ON DAILY INSPECTION OUTBOARD PART OF BLADE SKIN WAS FOUND TO BE CRACKED. CRACK IS FORMED AROUND TIP BLOCK ON BLADE. THE CRACK IS APPROX. 3 INCHES LONG, STARTING FROM BEHIND ABRASION STRIP TO ABOUT MIDDLE OF BLADE.SDR 2001F00517Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT PART NR 355A33-2153-00 CORRECTED PROBLEM. 2 TEETERING BEARINGS EQUALS 1 KIT. (M)SDR CA010703013Blade · failed(CAN) T/R BLADES WERE SUBJECTED TO A MINOR CONTACT ON THE OUTBOARD SKIN AREA WITH A PINE BOUGHT IN SLOW FORWARD FLIGHT, A/C THEN LANDED TO INSPECT THE BLADES. BLADES WERE REMOVED TO HAVE CRACKS IN THE FILLER AROUND THE EDGE OF THE TABS REPAIRED ( WARRANTY WORKSDR 2001F00518Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 KIT P/N 355A33-2153-00 CORRECTED PROBLEM. 2 TEETERING BEARINGS EQUALS 1 KIT. (M)SDR 2001F00513Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01 CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS 1 KIT. (M)SDR KBMA88714Spar · delaminatedDELAMINATED SPAR.SDR CA011029020Skin · cracked(CAN) 131 MM CRACK ORIGINATING FROM THE RIVET HOLE FOR THE TRAILING EDGE TAB ON BOTH THE UPPER AND LOWER SURFACE.SDR NO. 20010112018 AND 2019 ADDRESSES THIS SAME DEFECT.SINCE DISCOVERY OF THIS DEFECT EUROCOPTER FRANCE HAS ISSUED INFO TELEX 00000035 REQUIRING ASDR AC2A075796Bearing · crackedBEARINGS ARE CRACKED. REPLACED BEARINGS WITH NEW.SDR TI1R001466Bearing · wornBEARING SET, WORN. REMOVED AND REPLACED.SDR HEEA073116Bearing · crackedTAIL ROTOR BEARINGS CRACKED.SDR HEEA073101Bearing · separatedSEPARATED AT EDGES.SDR HEEA073099Blade · crackedCRACK AT TRIM TAB AREA ON TRAILING EDGE.SDR HEEA073025Blade · damagedVOID BETWEEN SKIN AND BLOCK.SDR KBMA88743Bearing · wornBEARINGS WORN. REPLACED WITH NEW BEARINGS, AS REQUIRED.SDR 2001F00519Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A33-2153-00 CORRECTED PROBLEM. 2 TEETERING BEARINGS EQUALS 1 KIT. (M)SDR CA010706014Pitch Horn · loose(CAN) DURING A DAILY INSPECTION, WE DISCOVERED THAT THE TORQUE OF THE BOLTS HOLDING THE PITCH HORN TO THE TAIL ROTOR BLADE WAS LOOSE. THE LOCKWIRE WAS STILLIN PLACE BUT THE 2 BOLTS WERE NO LONGER TORQUED.DURING THE DISMANTLING NO OTHER ANORMALITIES. THE PITCH SDR 2001F00512Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 KIT P/N 355A09-1036-1 CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS 1 KIT. (M)SDR HEEA071922Blade · damagedTRAILING EDGE OF PADDLE A IS SPLIT OPEN. THE CENTER PLUG IS ALSO DEBONDED. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR.SDR ALG2001F00005Bearing · separatedOCCURED DURING DAILY. ELASTOMER SEPARATION.SDR 2001F00515Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01 CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS 1 KIT. (M)SDR R7MR32670Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS FROM 1 EACH KIT PART NUMBER 355A09-1036-01 CORRECTED PROBLEM. 4 HALF SHELLS EQUALS 1 KIT.SDR R7MR32667Hinge · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS FROM 1 EACH KIT PART NUMBER 355A33-2153-00, CORRECTED PROBLEM. 2 TEETERING BEARINGS EQUALS 1 KIT.SDR HCMA075358Blade · peelingWHITE PAINT IS PEELING OFF BLADE AND IS EXTREMELY HARD TO BALANCE. PLEASE REPAIR UNDER FULL WARRANTY.SDR 2001F00516Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 KIT PART NR 355A09-1036-01 CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS 1 KIT. (M)SDR KBMA97422Bearing · wornBEARING WORN BEYOND LIMITS.SDR R7MR32671Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS FROM 1 EACH KIT PART NUMBER 355A09-1036-01, CORRECTED PROBLEM. 4 HALF SHELLS EQUALS 1 KIT.SDR R7MR32629Blade · peelingPAINT PEELING. REPLACED WITH NEW UNIT CORRECTED PROBLEM.SDR AC2A072805Blade · crackedFEATHERING BEARINGS CRACKED. FEATHERING BEARINGS WERE REPLACED BEFORE THIS AT TIME 589.4. THE BLADE HAS 1152.8 SINCE REPLACEMENT OF BEARINGS. REPLACED BLADESDR KBMA99400Laminated Hinge · delaminatedREPLACED LAMINATED HINGE BEARINGS DUE TO DELAMINATION.SDR 20001229SH017Hinge · wornREPLACED OLD BEARING WITH NEW. (X)SDR 20001229SH016Bearing · wornREPLACED OLD BEARINGS THAT WERE WORN. (X)SDR CA010112018Blade · cracked(CAN) 15 MM CRACK ON TRAILING EDGE ON UPPER AND LOWER SURFACE ORIGINATING UNDER TRIM TAB. SEE ATTACHED PHOTO WITH TRIM TAB REMOVED. NOT DETECTED UNTIL TRIM TAB REMOVED FOR ANOTHER REASON. TC COMMENTS: THIS PARTICULAR BLADE HAS A LIFE OF 4000 HOURS BUT WAS FOUNSDR CA010112017Blade · cracked(CAN) 40 MM CRACK ON TRAILING EDGE TOP AND BOTTOM SURFACE ORIGINATING UNDER TRIM TAB. SEE ATTACHED PHOTO WITH TRIM TAB REMOVED. TC COMMENTS: THIS PARTICULAR BLADE HAS A 4000 HOUR LIFE AND WAS FOUND WITH CRACK AT 1862.8 HOURS TSN. ORIGINATOR REPORTS THAT THIS ISDR 20001229SH014Blade · crackedDURING DAILY INSPECTION, BLADE CRACKED AT WEEP HOLE, ON THE INBOARD LEADING EDGE. CRACK EXTENDED AFT FOR ABOUT 1.50 INCHES. (X)SDR CA001218017Blade · cracked(CAN) - UNABLE TO BALANCE TAIL ROTOR ASSEMBLY. REMOVED TAIL ROTOR ASSEMBLY FOR INVESTIGATION. REMOVED HUB ASSEMBLY & BEARING FROM TAIL ROTOR ASSEMBLY, TO MOVE TAIL ROTOR TIP UP & DOWN & HEAR ABNORMAL NOISE. CLICKING NOISE WAS HEARD. RE: DGAC AD 84-064-037(BSDR 20001229SH015Blade · crackedDURING DAILY INSPECTION, BLADE CRACKED AT WEEP HOLE, ON THE INBOARD LEADING EDGE. CRACK EXTENDED AFT FOR ABOUT 1.25 INCHES. (X)SDR R7MR32672Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS FROM 1 EACH KIT PART NUMBER 355A09-1036-01 CORRECTED PROBLEM. 4 HALF SHELLS EQUALS 1 KIT.SDR R7MR32665Hinge · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS FROM 1 EACH KIT PART NUMBER 355A332153-00, CORRECTED PROBLEM. 2 TEETERING BEARINGS EQUALS 1 KIT.SDR R7MABushing · worn2 EA BUSHINGS, TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED BUSHINGS, TEFLON LINERS WITH NEW UNITS, CORRECTED PROBLEM.SDR R7MA722932517Bushing · worn2 EA BUSHINGS, TEFLON LINERS WORN BEYOND SERVICABLE LIMITS. REPLACED BUSHING, TEFLON LINERS WITH NEW UNITS, CORRECTED PROBLEM.SDR 20001214SH024Blade · crackedDURING POST-FLIGHT INSPECTION, A 2.50 INCH CHORDWISE CRACK WAS FOUND APPROXIMATELY .50 INCH INBOARD FROM THE TRAILING EDGE AND 14 INCHES FROM THE TIP OF THE BLADE. CORROSIVE OPERATING CONDITIONS. SUSPECT INTERGRANULAR CORROSION EMANATING FROM THE INTERIOR OFSDR 20001215SH038Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01, CORRECTED PROBLEM. 4 HALF SHELLS EQUALS 1 KIT. (X)SDR 20001215SH024Hinge · 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 20001215SH023Bearing · delaminatedELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01, CORRECTED PROBLEM. 4 HALF SHELLS EQUALS 1 KIT. (X)SDR 20001215SH025Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01, CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS 1 KIT. (X)SDR AU001016Blade · fod(AUS) TAIL ROTOR BLADE DAMAGED BY DZUS FASTENER WHICH SEPARATED FROM THE TAIL ROTOR GEARBOX COWLING. FOD. (X)SDR 20001214SH043Bearing · delaminatedELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM ONE EACH KIT, P/N 355A09-1036-01, CORRECTED PROBLEM. 4 HALF SHELLS EQUALS 1 KIT. (X)SDR HCMA075318Rod · wornPART IS WORN BEYOND LIMITS.PLEASE REPLACE BEARINGS UNDER WARRANTY.SDR 20001215SH035Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01, CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS 1 KIT. (X)
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