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 95ZZZX5536Plates · failedPILOT LOST TAIL ROTOR AUTHORITY WHILE SPRAYING TOMATOES. HELICOPTER MADE HARD LANDING WITH SUBSTANTIAL DAMAGE. ONE TAIL ROTOR BLADE DEPARTED HELICOPTER PRIOR TO LANDING. INVESTIGATION REVEALED TENSION. TORSION PLATES (11) FAILED ALLOWING BLADE TO DEPART.SDR 95ZZZX6096Blade · bearing crackedDURING MAINTENANCE ON T/R HUB AND BLADE (HIGH FREQ VIB), FOUND INBOARD BEARINGS CRACKED, TOTAL TIME OF BEARINGS, 921.7 HOURS.SDR 95ZZZX6095Blade · bearing crackedDURING MAINTENANCE ON T/R HUB AND BLADE (HIGH FREQ VIB), FOUND INBOARD BEARINGS CRACKED, TOTAL TIME OF BEARINGS, 921.7 HOURS.SDR 95ZZZX5456Blade · separationDAILY INSPECTION FOUND BLADE SEPARATED 9 INCHES FROM TIP AND 2 INCHES FROM LEADING EDGE ON CAMBER SIDE OF BLADE. SEPARATED AT FACE PLATE TRANSITION AREA. SEPARATION BEYOND LIMITS.SDR HEEA955597Bearing · crackedBLADE BEARING CRACKED. ALSO DISCARDED 4 EACH SLEEVES P/N 206-010-733-003. BEARINGS SCRAPPED LOCALLY.SDR 95ZZZX5472Blade · paint peelNORMAL MAINTENANCE FOUND PAINT PEELING ON TIP OF T/R BLADE FROM LEADING EDGE.SDR 95ZZZX6098Blade Bearing · wornPILOT COMPLAINED OF HIGH FREQUENCY VIBRATION. FOUND INBOARD BEARING CRACKED. TOTAL TIME OF BEARINGS, 663.9 HOURS.SDR 95ZZZX6097Blade Bearing · wornPILOT COMPLAINED OF HIGH FREQUENCY VIBRATION. FOUND INBOARD BEARING CRACKED. TOTAL TIME OF BEARINGS, 663.9 HOURS.SDR 95ZZZX5059Blade · coil looseCOIL LOOSE. REPLACED BLADE.SDR 95ZZZX5515Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR HEEA955479Bearing · crackedINBOARD OUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS6082, T.T. 1453:05. ALSO REMOVED 4 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955478Bearing · crackedOUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N A4984, T.T. 3723:15. ALSO REMOVED 2 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955477Bearing · crackedINBOARD BEARING CRACKED. REMOVED FROM T/R HUB S/N A4984, T.T. 3723:15. ALSO REMOVED 1 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955476Bearing · crackedINBOARD BEARING CRACKED. REMOVED FROM T/R HUB S/N A4984, T.T. 3723:15. ALSO REMOVED 1 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955475Bearing · crackedINBOARD AND OUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS6932, T.T. 1310:25. ALSO REMOVED 4 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955474Bearing · crackedOUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS5139, T.T. 3119:20. ALSO REMOVED 2 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955473Bearing · crackedINBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS5139, T.T. 3119:20. ALSO REMOVED 2 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY. 87.SDR HEEA955472Bearing · crackedINBOARD AND OUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS4999, T.T. 3206:50. ALSO REMOVED 4 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955471Bearing · crackedINBOARD AND OUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS6342, T.T. 1868:40. ALSO REMOVED 4 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955470Bearing · crackedINBOARD AND OUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS7023, T.T. 509:40. ALSO REMOVED 4 EACH SLEEVES 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955469Bearing · crackedINBOARD AND OUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS5787, T.T. 1116:05. ALSO REMOVED 4 EACH SLEEVES 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955468Bearing · crackedINBOARD AND OUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS5784, T.T. 2090:15. ALSO REMOVED 4 EACH SLEEVES 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955467Bearing · crackedOUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS6948, T.T. 1152:30. ALSO REMOVED 2 EACH SLEEVE 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR HEEA955466Bearing · crackedINBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N AFS6948, T.T. 1152:30. ALSO REMOVED 2 EACH SLEEVE 206-010-733-003. PARTS SCRAPPED LOCALLY.SDR 95ZZZX5593Bearing · wornLAMINATED BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-00, CORRECTED PROBLEM.SDR F6LM95105Blade Tab · separationBLADE HAS TRAILING EDGE TAB SEPARATION OUTBOARD OF RIVET ON BOTH BLADES. INSTALLED RENTAL T/R BLADE.SDR F6LM95101Bearing · tornBEARINGS TORN BEYOND LIMITS BEARINGS REPLACED BY AMERICAN EUROCOPTER DURING BLADE MINOR REPAIR, (WO 04153)SDR 95ZZZX3741Blade Spar · crackedTAIL ROTOR REMOVED FOR DEBONDING OF STAINLESS STEEL LEADING EDGE. SENT TO AEC FOR EVALUATION AND REPAIR. TAIL ROTOR BLADE SCRAPPED BY AEC FOR SPAR CRACK AT REINFORCMENT AND LOWER SURFACE, BLADE NR 2 BEYOND REPAIR LIMITS.SDR 95ZZZX3742Blade Spar · crackedTAIL ROTOR REMOVED FOR DAMAGE PENETRATION OF ONE BLADE STAINLESS STEEL LEADING EDGE. SENT TO AEC FOR EVALUATION AND REPAIR. AEC CONDEMNED FOR SPAR REINFORCEMENT PAD CRACK BEYOND LIMITS.SDR HEEA955346Blade · pittedEXCESSIVE PITTING IN THE BOX BEAM OF PADDLE "B". (REPLACEMENT OF BOX BEAM AND PITCH HORN ONLY)SDR 95ZZZX4272Blade · delaminatedTAIL ROTOR BLADE ASSY REMOVED FOR HAIL DAMAGE AND LEADING EDGE DELAMINATON. RETIREMENT TIME IS 4,000 HOURS.SDR 95ZZZX5049Blade · erodedBLADE LEADING EDGE ERODED.SDR 95ZZZX5504Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 95ZZZX4179Blade · bearing crackedTAIL ROTOR REMOVED FROM AIRCRAFT BECAUSE OF HIGH FREQUENCY VIBRATION IN-FLIGHT. FOUND 4 EACH BEARINGS, PN 206-010-765-001, WITH INNER RACES CRACKED.SDR 95ZZZX4178Blade · bearing crackedTAIL ROTOR REMOVED FROM AIRCRAFT BECAUSE OF HIGH FREQUENCY VIBRATION IN-FLIGHT. FOUND 4 EACH BEARINGS, PN 206-010-765-001, WITH INNER RACES CRACKED.SDR 95ZZZX4099Blade · paint peelROUTINE INSPECTION FOUND PAINT PEELING OFF BLADE. SUSPECT CAUSE - POOR PREPARATION BEFORE PAINTING.SDR 95ZZZX4090Blade · bearing wornTAIL ROTOR ASSEMBLY REMOVED BECAUSE IT WOULD NOT BALANCE. HIGH FREQUENCY VIBRATION DURING PHASE INSPECTION. FOUND 2 EACH 206-010-765-001 BEARINGS WORN BEYOND LIMITS.SDR HEEA955230Blade · groovedGROOVE ON THE PITCH HORN OF PADDLE "A" WHICH IS BEYOND LIMITS.SDR 95ZZZX5560Bearing · wornLAMINATED BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-00, CORRECTED PROBLEM.SDR HEEA955195Blade · defectivePADDLE "A" OF THIS ASSEMBLY HAS A HOLE IN THE LEADING EDGE WITH SEVERAL CRACKS AROUND THE HOLE.SDR EGRA95102Blade · crackedFOUND SIX FENESTRON BLADES TO HAVE SURFACE CRACKS IN THE SURFACE PENETRATING INTO THE FIBER AFTER SANDING PAINT AND PRIMER. REF: MWC 64.21.00.602 CHAP 2-3. S/N'S OFF 19249/19251/19253/19254/19360/19395. INSTALLED THE FOLLOWING S/N'S 25131/25129/25136/25130/251SDR 95ZZZX5510Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 95ZZZX5058Blade · coil looseCOIL LOOSE. REPLACED BLADE.SDR 95ZZZX5057Blade · coil looseCOIL LOOSE. REPLACED BLADE.SDR 95ZZZX5056Blade · coil looseCOIL LOOSE IN T/R BLADE. REPLACED BLADE.SDR 95ZZZX5553Bearing · wornLAMINATED BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-00, CORRECTED PROBLEM.SDR 95ZZZX3977Laminated Pack · corrodedUPON INSPECTION OF PARTS FOR REPAIR OF TAIL ROTOR ASSEMBLY, FOUND CORROSION BEYOND LIMITS ON CENTER SECTION OF LAMINATED PACK DUE TO SALT ATMOSPHERE IN WHICH THE AIRCRAFT FLIES. PART WAS SCRAPPED DUE TO CORROSION BEYOND LIMITS.SDR 95ZZZX3877Bearing · wornHALF SHELL BEARING WORN BEYOND LIMITS.SDR 95ZZZX5565Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 95ZZZX4212Blade · paint peelBLADE PAINT PEELING (ONLY 17.6 HOURS SINCE LAST PAINT).
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