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 97ZZZX85Bolt · crackedAN ULTRASONIC (UT) INSPECTION OF THE M/R BLADE BOLTS RETAINING THE MAIN ROTOR BLADE SPAR TO THE BLADE CUFF WAS PERFORMED IAW THE MANUFACTURER'S INSTRUCTIONS. DURING THE UT INSPECTION, CRACKS WERE DETECTED ON ONE OR MORE BOLTS ON EACH BLADE. BOLTS THAT WERE RSDR 97ZZZX84Bolt · crackedAN ULTRASONIC (UT) INSPECTION OF THE M/R BLADE BOLTS RETAINING THE MAIN ROTOR BLADE SPAR TO THE BLADE CUFF WAS PERFORMED IAW THE MANUFACTURER'S INSTRUCTIONS. DURING THE UT INSPECTION, CRACKS WERE DETECTED ON ONE OR MORE BOLTS ON EACH BLADE. BOLTS THAT WERE RSDR 97ZZZX83Bolt · crackedAN ULTRASONIC (UT) INSPECTION OF THE M/R BLADE BOLTS RETAINING THE MAIN ROTOR BLADE SPAR TO THE BLADE CUFF WAS PERFORMED IAW THE MANUFACTURER'S INSTRUCTIONS. DURING THE UT INSPECTION, CRACKS WERE DETECTED ON ONE OR MORE BOLTS ON EACH BLADE. BOLTS THAT WERE RSDR 97ZZZX82Bolt · crackedAN ULTRASONIC (UT) INSPECTION OF THE M/R BLADE BOLTS RETAINING THE MAIN ROTOR BLADE SPAR TO THE BLADE CUFF WAS PERFORMED IAW THE MANUFACTURER'S INSTRUCTIONS. DURING THE UT INSPECTION, CRACKS WERE DETECTED ON ONE OR MORE BOLTS ON EACH BLADE. BOLTS THAT WERE RSDR HEEA968662Blade · defectiveBLADE NOT ACCEPTABLE FOR PHI USE. BLADE RECEIVED WITH A DEPRESSION IN IT.SDR HEEA968653Blade · crackedTO COMPLY WITH 500 HOUR INSPECTION. BLADE HAS SEVERAL CRACKS ON THE TITANIUM STRIP WITH SEPARATION. THE CRACK AT STATION 123 HAS MULTIPLE BRANCHES.SDR HEEA968629Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED IN THE ROOT END AREA)SDR HEEA968628Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED IN THE ROOT AND CUFF AREAS)SDR HEEA968627Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED IN THE ROOT END AREAS)SDR HEEA968626Blade · crackedNOSE AND NECK SHELLS CRACKED IN THE ROOT AND CUFF AREA.SDR HEEA968624Blade · shield peelEROSION SHIELD PEELING ON THE INBOARD END. THE OUTBOARD LEADING EDGE ABRASION STRIP HAS A COMPLETE CHORDWISE CRACK WITH SEPARATION NEAR THE INBOARD END OF THE STRIP.SDR HEEA968623Tip Cap · separationSEPARATION ON THE TRAILING EDGE NEAR THE OUTBOARD END BEYOND THE MAX DEPTH ALLOWED. SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR.SDR HEEA968620Tip Cap · damagedTIP CAP HAS EXCESSIVE DAMAGE ON THE TRAILING EDGE NEAR THE INBOARD END.SDR 97ZZZX207Washer · crackedDURING A WEEKLY INSPECTION THE M/R BLADE BOLT LOWER WASHER WAS FOUND CRACKED. REMOVED WASHER. INSTALLED SERVICEABLE WASHER. ACFT TT 8079.6.SDR 97ZZZX943Blade · separationDISCOVERED DURING DAILY INSPECTION FOUND CORROSION AND SEPARATION BENEATH LOWER GRIP DOUBLES AND BETWEEN LOWER SKIN AND SPAR. CORROSION ON TRAILING EDGE UPPER AND LOWER SURFACES.SDR 97ZZZX939Blade · corrodedDISCOVERED DURING DAILY INSPECTION, FOUND TIP BLOCK AND WEIGHT PACKAGE CORRODED AND CAUSED SPAR TO BECOME DEFORMED AT TIP.SDR 97ZZZX934Blade · debondedDURING A LIGHTNING STRIKE INSPECTION, FOUND CORROSION AND DEBONDING OVER SPAR AT TIP (SKIN).SDR 97ZZZX933Blade · debondedLIGHTNING STRIKE INSPECTION FOUND M/R BLADE CORRODED AND DEBONDED AT TIP OF BLADE.SDR HEEA968523Blade · crackedBLADE IS CRACKED. (CRACK IN THE UPPER SKIN AT STATION 83.5" RUNNING IN A 45 DEGREE DIRECTION.SDR HEEA968518Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED)SDR HEEA968517Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED) SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR.SDR HEEA968516Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED)SDR HEEA968513Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED)SDR HEEA968512Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED)SDR HEEA968511Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED)SDR 97ZZZX241Blade · corrodedROUTINE INSPECTION FOUND CORROSION AT TIP OF BLADE.SDR 97ZZZX992Blade · paint flakePAINT FLAKING OFF LEADING EDGE AT TIP.SDR 97ZZZX991Blade · paint flakePAINT FLAKING OFF LEADING EDGE AT TIP.SDR 97ZZZX346Bolt Nut · mismanufacturedPURCHASE NEW MAIN ROTOR BLADE NUT FROM BELL SERVICE CENTER. DURING INSTALLATION, IT BECAME EVIDENT THAT THREADED BORE OF NUT WAS NOT PERPENDICULAR TO BEARING FACE OF NUT. TORQUING NUT TO REQUIRED 215 FOOT/POUND WOULD PUT EXTREME STRESS LOADS ON NUT AND HOLLOSDR 97ZZZX637Blade · crackedM/R BLADE CRACKS AND SKIN BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 97ZZZX636Blade · crackedM/R BLADE CRACKS AND SKIN BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR HEEA968467Blade · defectiveTOO LIGHT TO BALANCE. BLADE BOLT HOLE WAS MAX. OUT, STILL WITH NO SUCCESS.SDR HEEA968466Blade · crackedNOSE AND NECK SHELLS CRACKED AND SEPARATED.SDR HEEA968465Blade · crackedBLADE TRIM TAB CRACKED ON THE LOWER SURFACE.SDR HEEA968463Tip Cap · crackedTIP CAP HAS ABRASION STRIP CRACKED WITH SEPARATION. FIBERGLASS BROKEN BETWEEN THE DOUBLER ON THE UPPER SURFACE.SDR HEEA968445Blade · crackedTIP RIB CRACKED. THE NICKEL STRIP HAS SEVERAL AREAS OF SEPARATION.SDR HEEA968444Blade · separationSEPARATION IN THE SKIN NEAR THE TIP RIB AREA WITH CRACKS IN THE SKIN JUST BELOW THE SPAR ON THE LOWER SIDE.SDR HEEA968437Blade · crackedBLADE NOSE & NECK SHELL CRACKED AND SEPARATED.SDR HEEA968436Blade · crackedBLADE NOSE AND NECK SHELL CRACKED AND SEPARATED.SDR HEEA968435Blade · crackedBLADE HAS NOSE AND NECK SHELLS CRACKED WITH SEPARATION. SUSPECTED CRACKED FILLER NEAR MOLD LINE ON LOWER SURFACE.SDR HEEA968434Blade · crackedBLADE HAS NOSE AND NECK SHELL CRACKED AND SEPARATED. INBOARD LEADING STRIP SEPARATED BEYOND LIMITS.SDR 97ZZZX229Blade · crackedDURING 500 HOUR INSPECTION FOUND BLADE LEADING EDGE CRACKED AND SEPARATED AT RIGHT STATION 114 AND RIGHT STATION 154, LEADING EDGE LOWER SURFACE DEBONDED AT RIGHT STANDARD 100, TRAILING EDGED CRACKED AT RIGHT STATION 62.SDR 97ZZZX238Blade · corrodedDURING DAILY INSPECTION, BLADE TIP BLOCK AND WEIGHT PACKAGE CORRODED CAUSING DEFORMATION OF SPAR AT TIP.SDR 97ZZZX244Blade · corrodedDURING DAILY INSPECTION, FOUND M/R BLADE SPAR LEADING EDGE CORRODED BEYOND LIMITS.SDR 96ZZZX5841Blade · wornDURING NORMAL AIRCRAFT USAGE NEW YORK HELICOPTER HAS NOTED THE LEADING EDGE OF THE MAIN ROTOR BLADE IS EXPERIENCING ABNORMAL WEAR IN THE FORM OF SCALING/SPLINTERING ON A MODERATE LEVEL. NEW YORK HELICOPTER IS AWAITING RECOMMENDATIONS FROM BELL HELICOPTER TEXTSDR 97ZZZX259Blade · crackedDISCOVERED DURING 500 HOUR INSPECTION, FOUND BLADE SKIN CRACKED ALONG FORWARD EDGE OF TRIM TAB.SDR 97ZZZX258Blade · debondedDURING 500 HOUR INSPECTION FOUND BLADE TIP RIB DEBONDED.SDR 97ZZZX257Blade · debondedDURING 500 HOUR INSPECTION FOUND UPPER SURFACE SKIN DEBONDED APPROXIMATELY 5 INCHES BY 6.50 INCHES AT RIGHT STA 53. SKIN CRACKED AT FORWARD EDGE OF TRIM TAB.SDR 97ZZZX311Screws · defectiveDURING 500 HR INSPECTION OF BLADES AS SCREWS WERE BEING INSTALLED TORQUE VALUE WAS REACHED WITH ONLY APPROXIMATELY ONE-THIRD THREAD ENGAGEMENT OF ENTIRE GRIP LENGTH. DISTORTED THREADS IN ONE AXIAL LOCATION ALONG GRIP LENGTH.SDR 97ZZZX310Screws · defectiveDURING 500 HR INSPECTION OF BLADES AS SCREWS WERE BEING INSTALLED TORQUE VALUE WAS REACHED WITH ONLY APPROXIMATELY ONE-THIRD THREAD ENGAGEMENT OF ENTIRE GRIP LENGTH. DISTORTED THREADS IN ONE AXIAL LOCATION ALONG GRIP LENGTH.
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