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 AU970788Blade · delaminated(AUS) TAIL ROTOR BLADE LEADING EDGE EROSION STRIP DELAMINATED (DEBONDED) - DEBONDING EXTENDS SPANWISE FROM AN AREA 105MM(4.13IN) FROM THE INBOARD END OF THE STRIP TO 98MM (3.85IN) FROM THE OUTBOARD END AND CHORDWISE FROM THE TRAILING EDGE TO 25MM (1IN) TOWARDSSDR HEEA0010364Nut · wornT/R WORN.SDR HEEA0010362Bearing · wornFEATHER BEARING WORN EXCESSIVELY.SDR HEEA0010280Blade · separationSKIN SEPARATION ON THE AIRFOIL AREA ON PADDLE "B" PYLON SIDE.SDR 97ZZZX4708Blade · bearing bindingACFT TT: 13,497.8 HOURS. 104.2 HR. TWO NEW T/R BLADES P/N 206-016-201-131, SN CS-2814 AND SN CS-2815 WERE INSTALLED. PILOT'S COMPLAINT ABOUT T/R PEDAL PROBLEM. HELICOPTER WAS INSPECTED AND THE FOUR BEARINGS (2 EACH ON BLADES) ON T/R BLADES WERE FOUND BINSDR 97ZZZX4707Bearing · bindingACFT TT: 13,497.8 HOURS. 104.2 HR. TWO NEW T/R BLADES P/N 206-016-201-131, SN CS-2814 AND SN CS-2815 WERE INSTALLED. PILOT'S COMPLAINT ABOUT T/R PEDAL PROBLEM. HELICOPTER WAS INSPECTED AND THE FOUR BEARINGS (2 EACH ON BLADES) ON T/R BLADES WERE FOUND BINSDR AU970841Blade · delaminated(AUS) TAIL ROTOR BLADE DELAMINATED IN DOUBLER AREASDR CA970709001Blade · damaged(CAN) AIRCRAFT FLEW THROUGH HAIL STORM WHICH PEELED BACK TRAILING EDGE OF TAIL ROTOR BLADES. ALL FIVE BLADES DAMAGED. TWO SUBSTANIALLY DAMAGED.SDR 97ZZZX3451Blade · defectiveTAIL ROTOR BLADE ASSY WAS REPAIRED BY SIKORSKY JUST 422.4 HOURS AGO. PAINT AND EROSION STRIP NEEDS TO BE REWORKED.SDR HEEA0010143Bearing · deterioratedT/R BEARING DETERIORATED RUBBER.SDR 97ZZZX4701Laminated Hinge · wornLAMINATED HINGE ELASTOMERICS SPLIT CAUSING EXCESSIVE T/R VIBRATION. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR HEEA0010118Blade · damagedNICK ON TRAILING EDGE ON BLADE S/N A1678 AND BLADE S/N A1681. REPLACEMENT PART SERIAL NUMBERS ARE A1577 AND A1752.SDR 97ZZZX4694Laminated Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, FROM KIT 350A33-2153-00 CORRECTED PROBLEM.SDR 97ZZZX4134Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM 350A33-2153-00, CORRECTED PROBLEM.SDR 97ZZZX4074Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR HAIHEEA9964Blade · separationBLADE SEPARATION OVER THE TIP WEIGHT POCKET ON PADDLE "A". BOTH PRIMARY RUBBERS ARE WORN THROUGH.SDR HAIHEEA9952Blade · crackedBLADE SEPARATION AT TIP CAP.SDR HAIHEEA9951Blade · crackedBLADE IS CRACKED. (CRACK NEAR BUTT END)SDR HAIHEEA9948Blade · separationPADDLE "A" OF ASSEMBLY HAS SOME SEPARATION NEAR THE TIP WEIGHT COVER.SDR 97ZZZX4080Bearing · wornLAMINATED BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECTED PROBLEM.SDR 97ZZZX4079Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR CA970530009Blade · debonding(CAN) NEW LEADING EDGE INSTALLED PER MDHS NOTICE 187 PT.II .. LEADING EDGE STRIP FOUND STARTING TO DELAMINATE 18 CMS FROM TIP AND 3 CM TOWARD ROOT. BLADE FLOWN 111.4 HOURS AFTER REPAIR .SDR 97ZZZX4076Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 97ZZZX4075Bearing · wornLAMINATED BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECTED PROBLEM.SDR 97ZZZX4118Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 97ZZZX4117Bearing · wornLAMINATED BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECTED PROBLEM.SDR 97ZZZX4136Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR HAIHEEA9619Blade · separationSEPARATION AT BLADE ROOT. VENDOR UNABLE TO SUPPLY REPLACEMENT.SDR HAIHEEA9541Blade · paint peelT/R BLADE PAINT PEELING. TIME SINCE REPAIR 99:25.SDR HAIHEEA9540Blade · req repaintNO DISCREPANCIES, BLADE REQ REPAINT TO BALANCE.SDR HAIHEEA9498Blade · errodedPITCH HORN UP FOR RETIREMENT AND THE LEADING EDGE ABRASION STRIP HAS EROSION HOLE. SENT TO COMPOSITE TECHNIC FOR INSPECTION AND REPAIR.SDR HAIHEEA9492Blade · damagedTHRUST PLATE SANDED THROUGH NETTING ON BLADE S/N 031.SDR HAIHEEA9458Bearing · wornFEATHERING BEARINGS (INBOARD) BEING WORN AND CORRODEDSDR HAIHEEA9447Blade · blade voidVOID AT TIP OF T/R BLADE.SDR HAIHEEA9355Blade · cover missingSHORTLY AFTER TAKEOFF, AIRCRAFT DEVELOPED SEVERE VIBRATION. LANDED IMMEDIATELY WITHOUT INCIDENT. FOUND TIP COVER MISSING FROM ONE T/R BLADE.SDR HAIHEEA9334Blade · separationTIP WEIGHT COVER SEPARATED ON PADDLE "A". SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR.SDR 97ZZZX4695Laminated Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR 97ZZZX4131Bushing · wornBUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.SDR 97ZZZX4073Bushing · wornBUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.SDR 98ZZZX1795Blade · defectiveT/R BLADE PAINT PEELING CAUSING HIGH FREQUENCY VIBRATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 97ZZZX4077Hinge · wornLAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM.SDR HAIHEEA9247Blade · paint peelBLADE PAINT PEELING.SDR 97ZZZX1680Cuff · crackedIAW AD 77-07-05(S) AND HILLER SB 36-1 REV 3, PARA 2(G). FOUND CRACK AT CONTROL BLADE CUFF INBOARD BOLT HOLE DURING 100-HOUR REPETATIVE DYE-PENETRANT INSPECTION. NOTE: 6,860 HOUR LIFE-LIMIT.SDR 97ZZZX1679Cuff · crackedIAW AD 77-07-05(S) AND HILLER SB 36-1 REV 3, PARA 2(G). FOUND CRACK AT CONTROL BLADE CUFF INBOARD BOLT HOLE DURING 100-HOUR REPETATIVE DYE-PENETRANT INSPECTION. NOTE: 6,860 HOUR LIFE-LIMIT.SDR HEEA979181Blade · damagedDAMAGE TO TRAILING EDGE ON BLADE S/N 067.SDR HEEA979179Blade · hole pluggedDRAIN HOLE ON PADDLE "A" PLUGGED UP.SDR HEEA979176Blade · defectivePADDLE "A" OF THE ASSEMBLY HAS A VOID OVER THE TIP WEIGHT COVER.SDR 97ZZZX1685Bearing · crackedCRACKED FEATHERING BEARING ON TAIL ROTOR BLADE P/N 206-016-201-127. OCCURRED DURING NORMAL OEPRATION, FOUND DURING ROUTINE INSPECTION. SUSPECTED GAP BETWEEN BEARING AND BLADE. RECOMMENDED AD OR ASB BE ISSUED TO REPLACE FEATHERING BEARING INSTEAD OF T.B. 206SDR 97ZZZX1684Bearing · crackedCRACKED FEATHERING BEARING ON TAIL ROTOR BLADE P/N 206-016-201-127. OCCURRED DURING NORMAL OEPRATION, FOUND DURING ROUTINE INSPECTION. SUSPECTED GAP BETWEEN BEARING AND BLADE. RECOMMENDED AD OR ASB BE ISSUED TO REPLACE FEATHERING BEARING INSTEAD OF T.B. 206SDR 97ZZZX1683Bearing · crackedCRACKED FEATHERING BEARING ON TAIL ROTOR BLADE P/N 206-016-201-127. OCCURRED DURING NORMAL OPERATION, FOUND DURING ROUTINE INSPECTION. SUSPECTED GAP BETWEEN BEARING AND BLADE. RECOMMENDED AD OR ASB BE ISSUED TO REPLACE FEATHERING BEARING INSTEAD OF T.B. 206
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