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 TXER096972Blade · crackedCRACK AT TRAILING EDGE NEAR TRIM TAB.SDR ERAA097511Blade · damagedVOIDED AT TIP BLOCK AREA. X-RAYED, ULTRASONIC, INSPECTED, PERFORMED ALL SCHEDULED INSPECTIONS UP TO AND INCLUDING 1500 HR INSPECTION. REPLACED BOTH PRIMARY POLYURETHANE STRIPS. REPLACED BOTH SUPPLEMENTAL POLYURETHANE STRIPS AND REPAIRED TIP WEIGHT COVER ON SDR TXER096973Blade · delaminatedTAIL ROTOR BLADE HAS DELAMINATION.SDR CA041214002Blade · cracked(CAN) THE BLADE HAS A CHORDWISE CRACK AT BLADE STATION 12.64. THE CRACK IS 2.65 IN. (67.3MM) LONG ON THE DATA PLATE SIDE OF THE BLADE AND 0.4 IN. (10MM) LONG ON THE OTHER SIDE.SDR ERAA097510Blade · erodedT/R BLADE HAS EROSION. SENT TO CTI FOR REPAIR. UNIT X-RAYED, ULTRASONIC INSPECTED PER QATI3016.3261 AND 3098 PERFORMED ALL SCHEDULED INSPECTIONS UP TO AND INCLUDING 1500 HOUR INSPECTION IN ACCORDANCE WITH COMPOSITE MM 4047-76-5 TABLE 3-2 AND MM 4047-76-2, 65SDR CA050804002Blade · damaged(CAN) UPON PILOT DAILY INSPECTION DAMAGE NOTED TO T/R BLADE ASSY. BLADE ASSY VISUALLY INSPECTED AND FOUND DAMAGED BEYOND ACCEPTABLE LIMITS. BLADE REPLACED.SDR CA040623009Blade · perforated(CAN) WHILE CARRYING OUT REQUIREMENTS OF AD CF-2004-05(BHTC ASB 206L-04-127 REV A) A PIN HOLE IN THE EPOXY FILLER, APPROXIMATELY .012 IN. DIA, INTRUDING INTERNALLY, WAS FOUND. WATER WAS OBSERVED DRAINING FROM THE HOLE. BLADE HAS BEEN SCRAPPED.SDR KBM2004F00204Bearing · wornT/R HALF SHELLS WORN. REMOVED AND REPLACEDSDR CA040518011Blade · cracked(CAN) CHORDWISE CRACK, APPROX 2.8 INCHES LONG, OBSERVED TO START AT LEADING EDGE RUNNING TOWARDS TRAILING EDGE. LOCATED 0.5 INCHES AWAY FROM THE OB TIP OF DOUBLER. ONLY ONE SIDE OF THE TAIL ROTOR BLADE IS CRACKED.SDR HXSD2004517Blade · crackedINSPECTOR FOUND CRACK IN TAIL ROTOR PROTRUDING OUT OF RIVET LOCATION ON TRIM TAB. CRACK WAS FOUND DURING INSPECTION IAW AD 2001-26-55. (AL05200402466)SDR ERAA096627Blade · damagedT/R BLADE HAS VOID AT OUTBOARD TIP, SKIN LIFTING. SENT TO CTI FOR REPAIR. INSPECTED PER 204-099-223 VOLUME X SECTION 1.1 AND 1.2 REV 1; COMPLIED WITH ASB 412-00-106; REPAIRED SKIN DAMAGE AT TIP FWD EDGE ON BOTH SURFACES PER 212-64-10-002 AND 8110-38497; REPSDR BAQA094322Blade · damagedUNABLE TO BALANCE BLADES AND PAINT IS STARTING TO PEEL.SDR R322004F00000Blade · debondedTAIL ROTOR BLADES, NO MECHANICAL DIFFICULTIES NOTED ON PREFLIGHT. UPON LANDING, SHUTDOWN AIRCRAFT. AFTER EXITING AIRCRAFT, NOTICED TAIL ROTOR BLADE (C5-4834) HAD DEBONDED FROM SKIN. DEFECT IN MFG PROCESS.SDR BAQA094647Blade · peelingEC135 M/R BLADE S/N 1573, INTERGRATED PU FILM PEELING OFF.SDR CA040616001Blade · debonded(CAN) TAILROTOR BLADE OB DOUBLER, NEAR ROOT END OF BLABE, FOUND DEBONDED ON APPROX 6 INCHES.SDR ERAA094434Blade · peelingT/R BLADE SENT FOR REPAIR 5/29/2003. BLADE HAS ONLY 110.2 HRS SINCE REPAIR AND IS PEELING. RETURNING ON REPAIR ORDER RW-898678 REQUESTING WARRANTY REPAIR.SDR MDR04048Blade · crackedDURING ROUTINE INSPECTION, THE POCKET (PN 6516100010041) WAS FOUND CRACKED ON THE OB SIDE APPROX 6 INCHES FROM THE LE AND 56.5 INCHES FROM THE TIP END. THE CRACK RUNS UNDER THE STIFFENER ON THE POCKET. THE CRACK IS APPROXIMATELY 1.25 INCHES IN LENGTH. PROBASDR MDR04049Strap · crackedDURING ROUTINE INSP, THE STRAP WAS FOUND CRACKED ON THE OB SIDE OF THE BLADE APPROX 9.375 INCHES FROM THE TE OF THE FAIRING THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARD THE TIP END OF THE BLADE APPROX 1.0 INCH. THE STRAP IS CRACKED ON THE SDR CA040401007Blade · cracked(CAN) DURING DAILY INSPECTION AND DAILY COMPLIANCE WITH AD 2001-640-089(A), A CHORDWISE CRACK WAS DETECTED APPROXIMATELY 3 INCHES IB OF THE BLADE-TIP.SDR CA040413006Blade · contaminated(CAN) ONE TAILROTOR BLADE FOUND TO HAVE ABSORBED WATER, THROWING THE TAIL ROTOR OUT OF BALANCE AND CREATING EXCESSIVE VIBRATIONS.SDR KBM2004F00029Bearing · wornREMOVED AND REPLACED BEARINGS, WORN OUT.SDR PG9R118900Blade · crackedTAIL ROTOR BLADE HAS SPAR CRACK. (RMA NR R047450)SDR PG92004F00012Spar · crackedDURING PERIODIC INSPECTION (500HR) AND COMPLIANCE OF ECF SB 05.11. FOUND CRACKED SPAR ON T/R BLADE SN 9289. THIS IS THE 3TH T/R BLADE WE HAVE REJECTED IN 6 MONTHS. ALL HAVE HAD THE EXACT SAME CRACK. SUGGEST MANUFACTURER REEVALUATE. THE MFG PROCESS OF THESSDR CA040226002Blade · peeling(CAN) TAIL ROTOR BLADES RECEIVED FROM MFG WITH THE PAINT REFINISHED AFTER REPAIR OR INSPECTION ARE PEELING OR SHREDDING TO THE BLADE BODY SURFACE BELOW. THIS IS OCCURRING USUALLY WITHIN THE FIRST 100 HOURS OF OPERATION. THE NEW REFINISHED PAINT SURFACE IS THSDR ALGA098103Blade · crackedINSPECTED FOR SKIN CRACKS AND TRAILING EDGE OF BALANCE WEIGHT C/W ASB206L-04-127 REVB PT3.SDR AC2A093325Restraint · debondedRESTRAINT DISBONDED. PIN DISBONDED FROM RESTRAINT. RETAINING PLATES WERE DAMAGED. REPLACED PARTSDR ERAA097513Blade · erodedTIP RIVETS ERRODED. TIP RIVETS OF BLADE A11405 ERRODED, TRUNNION ROUGH, FEATHER BEARINGS HAVE PLAY ONE BEARING GALLED, T/R BLADES. REMOVED TO F.O.M. REMOVED YOKE BEARINGS, TRUNNION ASSY, NDT INSPECTED, BEARING BORES, INSTALLED NEW BEARINGS, STAKED IAW 412 CSDR MDR04042Blade · crackedDURING NORMAL AIRCRAFT INSPECTION, THE FOLLOWING WAS FOUND; THE OB SIDE OF THE POCKET IS CRACKED 1.8125 INCHES FROM THE TRAILING EDGE AND .25 INCH FROM THE TIP END. THE CRACK IS RUNNING SPAN WISE AND IS .6875 INCH LONG. PROBABLE CAUSE IS UNKNOWN.SDR MDR04041Blade · crackedDURING NORMAL AIRCRAFT INSPECTIN, THE FOLLOWING WAS FOUND. THE OB SIDE OF THE POCKET HAS THREE CRACKS RUNNING SPANWISE APPROXIMATEL .398 INCH FROM THE TRAILING EDGE. THE FIRST CRACK IS 75 INCH FROM THE TIP END AND .835 INCH LONG. THE SECOND CRACK IS 9 INCH SDR MDR04040Blade · crackedDURING NORMAL AIRCRAFT INSPECTION, THE FOLLOWING WAS FOUND: TWO SPANWISE CRACKS EXIST AT THE TRAILING EDGE ON THE OB SIDE. THE FIRST CRACK IS 7.25 INCH FROM OB END OF THE POCKET AND IS 1.25 INCH IN LENGTH. THE SECOND CRACK IS 14.5 INCHES FROM THE OB END OF SDR BAQA092251Blade · crackedTAIL ROTOR BLADE SUSPECTED TO BE CRACKED. HARDCARDS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 01/27/2004SDR ALGA097931Blade · unknownC/W 206L-04-127 REV B PT 3/ SENT TO REPAIR STATION.SDR PG92004F00004Bearing · failedTAIL ROTOR BEARING FAILED WITH ONLY 354 HOURS. (K)SDR KBM2004F00015Bearing · wornDURING POSTFLIGHT, FOUND TAIL ROTOR BLADE SHELL LAMINATED LEG IS WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW. (K)SDR BAQA091493Blade · damagedTAIL ROTOR BLADE NEEDS PAINT REPAIR. REPLACED WITH SERVICEABLE UNITS.SDR CA040217011Blade · damaged(CAN) DURING ROUTINE FLIGHT, A 6.5 INCH PIECE OF DOUBLER BROKE OFF FROM THE BLADE, CAUSING VIBRATIONS.SDR CA031126009Pin · broken(CAN) BLADE PIN FOUND TO BE BROKEN WHERE THREAD MEETS THE PIN.SDR PG92004F00007Blade · crackedTAIL ROTOR BLADE SPAR CRACKED. (RMA NR R045704) (K)SDR CA031103006Blade · oversized(CAN) CHAMFERS 44 DEG 30 INCHES - 45 DEG 30 INCHES (2 PLACES) X .395 - .415 DIMENSION ARE ACTUALLY OVERSIZE TO .450. BLADES CAN BE REWORKED BY RE-MACHINING THE CHAMFERS TO THE REQUIRED DIMENSION. THE CHAMFERS ARE LOCATED AT THE ROOT END OF THE BLADE WHERE IT SDR CA031113010Blade · cracked(CAN) DURING A 500 HR INSPECTION, PERFORMED A TAIL ROTOR SPAR INSP WITH DISASSEMBLY AS REQUIRED BY AD.1D(3). FOUND A LARGE PIECE OF SPAR SEPARATED ON EDGE IN LONGITUDINAL DIRECTION APPROX. 8 MM IN WIDTH AND 2 MM THICK. SEPARATION EXTENDS FROM REINFORCED ATTACSDR ERAA093710Blade · damagedPOLYURETHANE STRIP ERODED BOTH BLADES, TRAILING EDGE TAB DAMAGED. EROSION NEAR TIP. SENT FOR REPAIR. X RAYED ULTRASONIC INSPECTED IAW QATI 3016 AND 3098, PERFORMED ALL SCHEDULED INSPECTIONS UOP TO AND INCLUDING 1500 HR INSP IAW COMPOSITE MATERIALS MANUAL 4SDR KBM2003F00037Bearing · crackedHALF SHELL BEARINGS HAVE CRACKED. REPLACED WITH NEW HALF SHELL BEARINGS.SDR AUS20031069Blade · debonded(AUS) TAIL ROTOR BLADE TAB DEBONDED AND SEPARATED FROM BLADE CAUSING EXCESSIVE VIBRATION. TAIL ROTOR BLADE TRAILING EDGE DAMAGED. INVESTIGATION FOUND FAILURE WAS DUE TO INCORRECT SOLVENT USED DURING TAB BONDING PROCEDURE AT OVERHAUL. SECONDARY EFFECTS OF TASDR ERAA091805Blade · debondedTRAILING EDGE ERRODED AND UNBONDED. SENT FOR REPAIR INSPECTED IAW SA 4045-31E CHAPTER / SECTION 65-20-01 AND NAVAIR 0395B-126 CHANGE 1; REPLACED RUBBER CAP IAW S61 L/N SRM SA 4045-31E CHAPTER 65-20-01 PROCEDURE 13 AND CHAPTER 65-10-01 PROCEDURE 5.A; REPLACEDSDR AUS20030917Blade · cracked(AUS) TAIL ROTOR BLADE CRACKED CHORDWISE FROM WATER DRAIN HOLE LOCATED AT BLADE ROOT. CRACK LENGTH APPROXIMATELY 40MM (1.57IN).SDR ERAA097520Blade · damagedBLADE SENT TO AEC FOR REPAIR. REPLACED LEADING EDGE, REFINISHED BLADE, REPLACED ROOT TAPE.SDR 36020820Blade · debondedTRIM TAB DISBONDED ON RED TAIL ROTOR BLADE. RESULTING IN APPROXIMATELY 1.25 INCH LONG SEPARATION.SDR AUS20030852Bearing · loose(AUS) TAIL ROTOR BLADE OUTBOARD BEARING LOOSE IN HOUSING.SDR MDR03028Strap · crackedTHE STRAP IS CRACKED ON THE INBOARD SIDE OF THE BLADE APPROXIMATELY 9.25 INCHES FROM THE TRAILING EDGE OF THE FAIRING. THE CRACK STARTS AT THE CUFF END OF THE BLADE APPROXIMATELY 1.5 INCHES. THE CRACK STARTS WHERE THE LEADING EDGE OF THE FAIRING, PN 65161-00SDR MDR03027Strap · crackedON THE INBOARD SIDE OF THE BLADE, THERE IS A CRACK IN THE STRAP AND POCKET. THE CRACK STARTS AT THE ROOT END SIDE OF THE STRAP AND EXTENDS 3.75 INCHES TOWARD THE TIP END, INTO THE POCKET. THE CRACK IS 9.25 INCHES FROM THE TRAILING EDGE OF THE FAIRING. CAUSE
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