JASC 6210
Service difficulty reports · 1,561
Reports filed under 6210 · Main 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 = '6210' 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 = '6210' 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 HEEA955177Tip Cap · crackedTWO CRACKS IN THE ABRASION STRIP AND SEPARATION. THE FIBERGLASS BETWEEN THE INNER AND OUTER DOUBLER ON THE UPPER SURFACE IS CRACKED.SDR 95ZZZX5082Bushing · wornBUSHING DUE REPLATING - WORN. REMOVED AND REPLACED.SDR 96ZZZX1665Bushing · wornTEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 8 EACH NEW UNITS, CORRECTED PROBLEM.SDR GMAL9601251Blade · crackedMAIN ROTOR BLADE CRACKED. CRACK AT BLADE STA 124, 2.9345 INCHES LONG. (X)SDR HEEA955074Blade · crackCRACK ON THE LOWER SURFACE AT STATION 1835MM. THE CRACK STARTS 20MM FROM THE TRAILING EDGE AND EXTENDS 157MM FROM THE TRAILING EDGE.SDR HEEA955056Blade · wt missingM/R BLADE INSTALLED AND DURING THE BALANCE CHECK IT WAS DISCOVERED THE BLADE WAS EXTREMELY LIGHT AT THE TIP DUE TO THE ABSENCE OF THE TIP WEIGHTS. BLADE WAS SENT TO COMPOSITE TECHNICS 4-29-94 FOR TIP WEIGHT STUD STRIPPED OUT. CTI WAS UNABLE TO REPLACE THE STSDR HEEA955010Blade · crackedNOSE AND NECK SHELL CRACK NEAR THE ROOT END.SDR HEEA954986Blade · crackedNOSE AND NECK SHELLS CRACKED.SDR HEEA954985Blade · crackedNOSE AND NECK SHELLS CRACKED.SDR HEEA954966Tip Cap · edge splitTIP CAP HAS THE TRAILING EDGE SPLIT OPEN APPROXIMATELY THREE INCHES.SDR HEEA954953Blade · unbonded#1 LOWER FINGER UNBONDED BEYOND THE MAXIMUM LIMIT.SDR HEEA954950Tip Cap · damagedTIP CAP HAS A CREASE IN THE ABRASION STRIP ON THE LOWER SIDE AS MARKED.SDR 95ZZZY0960Bushing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. UNITS SCRAPPED ON SITE. SEE LOG BOOK ENTRY ATTACHED. REPLACED WITH NEW UNIT(S), CORRECTED PROBLEM.SDR 95ZZZY0937Elastic Bushing · wornELASTOMERICS WORN BEYOND SERVICABLE LIMITS. REPLACED WITH NEW UNIT(S), CORRECTED PROBLEM.SDR 95ZZZY0933Bushing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT(S) CORRECTED PROBLEM.SDR HEEA954909Blade · defectiveSEPARATION ON THE MIDSPAN TRIM TAB EAR, PAINT PEELING ON TOP AND BOTTOM SIDE OF THE BLADE. BLADE NEEDS 2500 HOUR INSPECTION. REPLACED TRIM TAB EARS, FEATHERED THE PEELING PAINT, COMPLIED WITH 2500 HOUR INSPECTION.SDR HEEA954908Blade · defectiveROOT END RUBBER TORN. BLADE NEEDS 2500 HOUR INSPECTION, PAINT PEELING ON TOP AND BOTTOM SIDE OF BLADE. REPLACED ROOT END RUBBER, COMPLIED WITH 2500 HOUR INSPECTION AND FEATHERED PEELING PAINT.SDR 95ZZZX2799Blade · corrodedDURING ROUTINE INSPECTION, FOUND M/R BLADE HAS EXCESSIVE LEADING EDGE CORROSION. POSSIBLE IMPROPER HEAT TREAT BY MATERIAL OR ALLOY FORMULATION.SDR 95ZZZX2798Blade · mismanufacturedDURING INSPECTION, SPAR OBSERVED DRILLED AT TIP WEIGHT INSTALLATION LOCATIONS. TIP WEIGHT BLOCK AREA, HOLES DRILLED THROUGH TO SPAR INNER SKIN AT TIME OF MANUFACTURE.SDR HEEA954902Blade · crackedCLOSURE AT BLADE ROOT TRAILING EDGE SIDE CRACKED. REPAIRED THREE TIMES PREVIOUSLY.SDR EGRA9566Guard Washer · wornMAIN ROTOR BLADE GUARD WASHERS WORN BEYOND LIMITS REPLACED MAIN ROTOR BLADE GUARD WASHERSSDR EGRA9554Bushing · wornMAIN ROTOR BLADE PRIMARY BUSHINGS FOUND WORN BEYOND LIMITS REPLACED BUSHINGSSDR EGRA9553Flange Bushing · scoredBLUE AND YELLOW MAIN ROTOR BLADE GRIP SECONDARY BUSHINGS SCORED AND PITTED REPLACED BUSHINGSSDR EGRA9552Trim Tab Assy · crackedYELLOW MAIN ROTOR BLADE OUTBOARD TRIM TAB CRACKED REPLACED TRIM TABSDR EGRA9551Elastic Bushing · wornMAIN ROTOR BLADE SECONDARY BUSHINGS WORN BEYOND LIMITS REPLACED MAIN ROTOR BLADE SECONDARY BUSHINGS WITH NEW ONES FROM KHC STOCKSDR 95ZZZX5728Seal · leakingFOUND FREEWHEEL INPUT SEAL LEAKING OIL. REMOVED FREEWHEEL ASSY TO REPLACE SEAL ASSY. INSTALLED NEW SEAL, PN 2890-52017, 1 EACH AND O-RINGS, PN MS2961-237, 1 EACH, AND PN MS29561-215, 1 EACH.SDR 95ZZZX5724Blade · skin deformedBLADE FAILED INSPECTION FOR SKIN DEFORMATION AND LOOP ROVING. BLADE IS LOCATED AT CTI.SDR 95ZZZX5723Blade · skin deformedBLADE FAILED INSPECTION FOR SKIN DEFORMATION AND LOOP ROVING. BLADE IS LOCATED AT CTI.SDR 95ZZZX5722Blade · skin deformedBLADE FAILED INSPECTION FOR SKIN DEFORMATION AND LOOP ROVING. BLADE IS LOCATED AT CTI.SDR 95ZZZX5721Blade · skin deformedBLADE FAILED INSPECTION FOR SKIN DEFORMATION AND LOOP ROVING. BLADE IS LOCATED AT CTI.SDR RMXA9520737Blade · defectiveBLADE DEFECTIVE. HUB VABRATION.SDR RMXA9520736Blade · defectiveBLADE DEFECTIVE. HUB VABRATION.SDR HEED956Blade · damagedDAMAGED BLADE. ORDERED NEW BLADESDR HEEA954823Blade · crackedNOSE AND NECK SHELLS CRACKED.SDR HEEA954788Blade · debondingSKIN DEBONDING CENTERED AT STATION 62" ON THE LOWER SURFACE DUE TO EXCESSIVE HEAT FROM THE ENGINE.SDR HEEA954787Blade · crackedNUMEROUS CRACKS ON THE NICKEL STRIP. THE TIP RIB IS PARTIALLY UNBONDED. THERE ARE NO MODIFICATIONS DONE TO THE TIP END FOR THE CSN TO BE COMPLIED WITH AND THIS BLADE ALSO MEETS THE TIME REQUIREMENT FOR THE ULTRA SONIC INSPECTION FOR TIME EXTENSION.SDR EGRA9527Elastic Bushing · deteriorationELASTIC BUSHING REMOVED BECAUSE OF RUBBER PROTRUSION. REPLACED WITH NEW ELASTIC BUSHINGS.SDR HEEA954720Tip Cap · defectiveTIP CAP HAS A PREVIOUS REPAIR THAT HAS COLLAPSED AND HAS EXCESSIVE PAINT PEELING.SDR 95ZZZX2207Tip Cap · missingCREW FELT A SUDDEN VIBRATION FROM THE MAIN ROTOR SYSTEM. MADE A PRECAUTIONARY LANDING. FOUND ONE-THIRD OF THE TRAILING EDGE OF THE TIP CAP MISSING. S-76 IPC CHAPTER 65, SECTION 11, UNIT 00, FIGURE 1, ITEM 3.`SDR HEEA954646Blade Bolts · wornSECONDARY BLADE BOLTS FOUND WORN BEYOND LIMITS ON INSPECTION. REPLACED WITH SERVICEABLE BLADE BOLTS AND RETURNED TO SERVICE. S/N PHI513 & PHI 514SDR RMXA9520567Bolt · scoredBLADE PIN BOLT SCORED. REMOVED AND REPLACED.SDR HEEA954592Tip Cap · crackedCRACK IN THE ABRASION STRIP WITH SEPARATION.SDR 95ZZZX2082Blade · crackedNR 3 LEADING EDGE EROSION GUARD CRACKED.SDR 95ZZZX2081Blade · crackedNR 3 LEADING EDGE STRIP CRACKED.SDR 95ZZZX2093Blade · crackedDISCOVERED WHEN COMPLYING WITH AD 84-10-2, 500-HOUR INSPECTION. FOUND CRACK IN SPAR AT ROOT END LOWER SIDE ON BLADE EXTENDING FROM FORWARD OUTBOARD BUSHING HOLE TO LEADING EDGE APPROXIMATELY 1.5 INCHES LONG.SDR 95ZZZX2092Blade · crackedDEFECT DISCOVERED DURING C.A.M.P. 500-HOUR BLADE INSPECTION, FOUND CRACK IN SPAR AND LOWER SKIN AT TIP END EXTENDING INBOARD FROM APPROXIMATELY STA 249.88 TO STA 247.65. CAUSE UNKNOWN.SDR 95ZZZX5563Bushing · wornBUSHING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WTH 8 EACH NEW UNIT(S) CORRECTED PROBLEM.SDR 95ZZZX1499Bearing · failedWHILE PERFORMING A 400-HOUR INSPECTION OF THIS AIRCAFT, THE INNER RACE OF THE FLAPPING HINGE BEARING WAS FOUND BRINNELLED IN TWO AREAS BEYOND THE ACCEPTABLE LIMITS. THIS BEARING WAS NEW AT THE LAST 400-HOUR INSPECTION. SUSPECT CONTAMINATION INTRODUCED DURINGSDR EGRA954Bolt · scoredSECONDARY BLADE BOLT HAS SCORE MARKS ON BOLT SURFACE BEYOND LIMITS. REPLACED BOLT.SDR HEEA954462Blade · crackedNOSE SHELL CRACKED.
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