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 CHI1543Blade · delaminatedBOTH BLADES WERE FOUND DELAMINATED ON THE DOUBLERS AT THE BUTT END. NOTE: THE BLADES WERE REPAINTED IN 1991 - 353.7 HOURS AGO. REFERENCE: OPERATOR CONTROL NR 96ZZZX3668. (X)SDR 96ZZZX3668Blade · delaminatedBOTH BLADES WERE FOUND DELAMINATED ON THE DOUBLERS AT THE BUTT END. NOTE: THE BLADES WERE REPAINTED IN 1991 - 353.7 HOURS AGO. REFERENCE: OPERATOR CONTROL NR CHI1543. (X)SDR HEEA967015Blade · erodedPART IS ERODED. (EROSION THROUGH THE LEADING EDGE ABRASION STRIP ON PADDLE "B")SDR HEEA967014Blade · erodedPART IS ERODED. (LEADING EDGE ABRASION STRIP HAS EROSION HOLE THROUGH THE STRIP.SDR 96ZZZX3961Bearing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM.SDR HEEA966933Bearing · defectiveTEFLON RACE LOOSE IN BEARING. ALSO REPLACED 2 EACH NEW SLEEVES P/N 206-010-733-003.SDR 96ZZZX3951Hinge · wornLAMINATED HINGE HAS ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.SDR 96ZZZX2604Tail Rotor Assy · separationSEPARATION BETWEEN TIP WEIGHT SUPPORT BLOCK AND BLADE SKIN. RECOMMEND ALL IN SERVICE BLADES BE INSPECTED FOR DEBONDING OF TIP WEIGHT CHAMBER.SDR 96ZZZX2603Tail Rotor Assy · separationSEPARATION BETWEEN TIP WEIGHT SUPPORT BLOCK AND BLADE SKIN. RECOMMEND ALL IN SERVICE BLADES BE INSPECTED FOR DEBONDING OF TIP WEIGHT CHAMBER.SDR HEEA966863Bearing · crackedRETIRED BLADE. REMOVED BEARINGS TO CHECK FOR SERVICEABILITY. FOUND BEARING CRACKED. SCRAPPED LOCALLY.SDR 96ZZZX1979Bearing · crackedINNER RACE CRACKED FROM EDGE OF RACE TOWARDS CENTER OF BALL. REPLACED WITH NEW PN 206-310-105-101 BEARINGS WITH REDUCED CROSS-SECTION OF INNER RACE.SDR 96ZZZX1978Bearing · crackedINNER RACE CRACKED FROM EDGE OF RACE TOWARDS CENTER OF BALL. REPLACED WITH NEW PN 206-310-105-101 BEARINGS WITH REDUCED CROSS-SECTION OF INNER RACE.SDR HEEA966835Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 2 EACH SLEEVES, P/N 206-010-733-003 AND 4 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS.SDR HEEA966834Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS.SDR HEEA966833Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS.SDR HEEA966832Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS.SDR HEEA966831Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS.SDR HEEA966830Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS.SDR HEEA966829Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR # 6826 THROUGH #6835 FOR ADDITIONAL BEARINGS REPLACED.SDR HEEA966828Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS.SDR HEEA966827Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS.SDR HEEA966826Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101.NOTE: SEE MMIR #6826 THROUGH #6835 FOR ADDITIONAL BEARINGS REPLACED.SDR HEEA966825Bearing · crackedDISASSEMBLED T/R HUB AND BLADE ASSEMBLY FOR OVERHAUL. FOUND INBOARD BEARINGS CRACKED ON BLADE S/N CS4037 AND BLADE S/N CS4316. ALSO REPLACED 4 EACH SLEEVES P/N 206-010-733-003 AND 8 EACH SPACERS P/N 206-011-742-101.SDR HEEA966824Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 2 EACH SLEEVES P/N 206-010-733-003 AND 4 EACH SPACERS P/N 206-011-742-101. HELD AT PHI FOR CSR SIGNATURE. NOTE: SEE MMIR# HEEA0006823 FOR 2 EACH ADDITIONAL BEARINGS REMOVED.SDR HEEA966823Bearing · crackedBEARINGS CRACKED. ALSO REPLACED 2 EACH SLEEVES P/N 206-010-733-003 AND 4 EACH SPACERS P/N 206-011-742-101.SDR 96ZZZX1932Bearing · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECTED PROBLEM.SDR 96ZZZX1931Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1930Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1929Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1928Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1927Bearing · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECTED PROBLEM.SDR 96ZZZX1926Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1925Bearing · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECTED PROBLEM.SDR 96ZZZX1924Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1923Bearing · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECTED PROBLEM.SDR 96ZZZX1922Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1921Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1920Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1913Bearing · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECTED PROBLEM.SDR 96ZZZX1912Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX1911Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 96ZZZX3952Hinge · wornLAMINATED HINGE HAS ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.SDR 96ZZZX3955Hinge · wornLAMINATED HINGE HAS ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.SDR HEEA966706Bearing · wornBEARING DETERIORATED.SDR 96ZZZX3953Hinge · wornLAMINATED HINGE HAS ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.SDR 96ZZZX1077Blade · dentedT/R BLADE DENTED. S/N A554 AND A535. REPLACED WITH NEW FIXTURE.SDR 96ZZZX1409Blade · crackedDURING C/W TAIL ROTOR BLADE VISUAL INSPECTION IN AD 96-01-08, A 5.3 INCH LONG CORD-WISE CRACK WAS DISCOVERED ON THE CONVEX SURFACE OF THE BLADE .25 INCH BELOW THE END OF THE DOUBLER. CRACK SIZE AND LOCATION IS THE SAME AS SHOWN IN THE ILLUSTRATION CONTAINED ISDR HEEA966695Bearing · wornBLADE BEARINGS WORN BEYOND LIMITS. (SDR 96ZZZX2526Hinge · wornTAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00. CORRECTED PROBLEM.SDR HCMA968Bearings · worn excessivelyBEARING IS WORN EXCESSIVELY. REMOVED AND REPLACED. ORIGINAL PART CAME ON T/R BLADE ASSY S/N 6068.
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