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 HAIHEEA9336Blade · crackedNOSE AND NECK SHELLS CRACKED BEYOND LIMITS NEAR THE ROOT END.SDR HAIHEEA9330Blade · bulgingBLADE BULGING BEYOND LIMITS.SDR CA970521002Blade · cracked(CAN) IN FLIGHT BIM INDICATION. BLADE REMOVED, SENT OUT FOR REPAIR. CRACK FOUND STARTING FROM CUFF ATTACHMENT BOLT HOLES.SDR 97ZZZX4132Blade · defectiveM/R BLADE FAILED BLADE INSPECTION PROGRAM. EXCESSIVE BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR HAIGJQR0111Blade · peelingLARGE PATCHES OF PAINT PEELING FROM BLADES.SDR CHI1753Blade · vacuum leakEVACUATED BLADE SPAR INDICATOR SYSTEM (ISIS) SHOWED POSITIVE. BLADE REMOVED FROM SERVICE TO INVESTIGATE SOURCE OF LEAK. THE LEAK WAS DETERMINED COMING FROM A SMALL CORROSION PIT WHICH IS LOCATED IN A TOOLING MARK AT STA 252. THE TOOLING MARK IS APPROXIMATELSDR NYBA9713Blade · defectiveRED BIM INDICATION REPLACED MAIN ROTOR BLADESDR NYBA978Blade · erodedBLADE IS ERODED. REPLACED MAIN ROTOR BLADESDR HEEA979208Blade · damagedMAIN ROTOR TIP DAMAGE OUTWARD - 1 INCH CRACK ON TIP.SDR HEEA979180Tip Cap · crackedTRAILING EDGE SPLIT OPEN AND A CRACK ON THE LEADING EDGE ABRASION STRIP ON THE UPPER SURFACE.SDR HEEA979177Blade · not drilledRECEIVED FROM THE VENDOR WITH A NEW LEADING EDGE ABRASION STRIP INSTALLED BUT THE HOLES WERE NEVER DRILLED FOR THE WEIGHT POCKET.SDR HEEA979168Blade · separationSEPARATION ON THE NUMBER TWO CENTER LEADING EDGE STRIP ON THE INBOARD END BEYOND LIMITS.SDR CA970421008Blade · cracked(CAN) MAIN ROTOR BLADE FOUND WITH CHORDWISE CRACK. CRACK 35.43" OUTBOARD OF ROOT.SDR 97ZZZX1272Blade · corrodedDISCOVERED DURING DAILY INSPECTION, CORROSION AND SKIN SEPARATION AT SPAR TIP. CORROSION AT ROOT END WEAR PADS.SDR 97ZZZX1285Blade · separationDURING DAILY INSPECTION FOUND SKIN SEPARATED AND CORRODED OVER SPAR AT TIP.SDR 97ZZZX1284Blade · separationDURING DAILY INSPECTION FOUND SKIN SEPARATED OVER SPAR AND BLADE TIP.SDR 97ZZZX1275Blade · separatedDURING DAILY INSPECTION, FOUND UPPER SKIN SEPARATED AT SPAR TIP. CORROSION OR ROOT END AT WEAR PADS.SDR 97ZZZX1270Blade · corrodedDURING DAILY INSPECTION FOUND SKIN CORRODED AND SEPARATED AT TIP. CORROSION AT WEAR PADS OR ROOT END.SDR HEEA979077Tip Cap · holedTIP CAP HAS A HOLE IN THE LOWER SKIN JUST AFT OF THE LEADING EDGE ABRASION STRIP.SDR HEEA979076Blade · crackedBLADE OUTBOARD LEADING EDGE ABRASION STRIP WITH A CHORDWISE CRACK NEAR THE INBOARD END. THE EROSION SHIELD HAS AN EXCESSIVE JAGGED EDGE NEAR THE TIP.SDR HEEA979075Blade · defectiveBLADE DEFECT, EXCESSIVE LATERAL VIBRATION -- UNABLE TO TRACK.SDR HEEA979074Blade · defectiveM/R BLADE HAS SKIN VOID ON THE LOWER SIDE WHICH STARTS FROM STATION 263" TO STATION 271" SPANWISE AND 2.5" CHORDWISE.SDR HEEA979073Blade · crackedT/R BLADE HAS PARTIAL CHORDWISE CRACK ON THE OUTBOARD LEADING EDGE ABRASION STRIP AT THE SPLICE AREA.SDR HEEA979070Blade · crackedM/R BLADE SPAR CRACKED AT THE ROOT END COMING FROM THE FORWARD OUTBOARD BUSHING HOLE. SCRAPPED M/R BLADE.SDR HEEA979053Blade · crackedBLADE HAS NOSE AND NECK SHELL CRACKED AND THE #1 ONE INBOARD LEADING EDGE STRIP SEPARATED BEYOND LIMITS.SDR HEEA979052Blade · crackedBLADE IS CRACKED. NOSE AND NECK SHELL CRACKED AND SMALL AREAS OF SEPARATION ON THE LEADING EDGE STRIPS.SDR HEEA979051Blade · crackedBLADE HAS NOSE AND NECK SHELL CRACKED. THE LEADING EDGE STRIP IS SEPARATED AT THE TIP AND SCARF JOINT AREAS.SDR HEEA979050Blade · separatedBLADE HAS THE NUMBER TWO CENTER LEADING EDGE STRIP SEPARATED 62MM ON THE INBOARD END TOP SURFACE.SDR HEEA979049Blade · crackedBLADE IS CRACKED. NOSE AND NECK SHELL CRACKED. HAS SMALL AMOUNT OF SEPARATION ON THE LEADING EDGE, BUT INBOARD STRIP IS SEPARATED BEYOND LIMITS.SDR HEEA979044Tip Cap · tornTIP CAP HAS LOWER AND UPPER SKIN TORN OUT OF LIMITS. ALSO THE SKIN BETWEEN OUTER DOUBLER AND INNER DOUBLER BROKEN AT THE LEADING EDGE STRIP. SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR.SDR HEEA979043Tip Cap · tornTIP CAP HAS THE SKIN TORN ON THE LOWER SIDE BEYOND MAX LIMITS.SDR HEEA979039Tip Cap · crackedTIP CAP HAS A CRACKED ABRASION STRIP ON THE LOWER SIDE.SDR HEEA979038Tip Cap · tornTIP CAP HAS THE SKIN TORN ON THE LOWER SIDE BEYOND THE MAXIMUM LIMITS.SDR HEEA979035Blade · separationSEPARATION ON THE INBOARD LEADING EDGE ABRASION STRIP BEYOND THE LIMITS.SDR HEEA979034Blade · separationBLADE HAS SEPARATIONS ON THE THREE-IN-BOARD LEADING EDGE STRIPS.SDR AU970145Blade · debonded(AUS) MAIN ROTOR BLADE INBOARD TRIM TAB DEBONDED AND LOOSE ON BLADESDR CA970210002Blade · delamination(CAN) BUBBLE DELAMINATION ON LOWER SURFACE OF ABRASION STRIP - APPROXIMATELY 1/2" X 2" LONG EXTENDING WITHIN 3/8" OF THE TRAILING EDGE.SDR 97ZZZX1408Blade · crackedDURING DAILY INSPECTION, FOUND SKIN CRACKED AT STA 1000 MM.SDR 97ZZZX1286Blade Rib · dedbondedDISCOVERED DURING 500 HOUR INSPECTION THAT BLADE TIP RIB WAS DEBONDED.SDR 97ZZZX1283Blade · separatedDISCOVERED DURING ROUTINE MAINTENANCE, SKIN SEPARATED FORM SPAR AT BLADE TIP.SDR HEEA978871Blade Bolt · defectiveCENTER PLUNGER GETS STUCK WHEN PUSHED IN.SDR HEEA968799Blade · defectiveHOLES IN THE LEADING EDGE ROOT SECTION. PAINT PEELING. SENT TO MCDONNELL DOUGLAS FOR INSPECTION.SDR HEEA968798Blade · defectiveHOLES IN THE LEADING EDGE ROOT SECTION. PAINT PEELING.SDR HEEA968797Blade · paint peelM/R BLADE PAINT PEELING.SDR HEEA968796Blade · paint peelM/R BLADE PAINT PEELING.SDR HEEA968795Blade · defectiveHOLE IN THE LEADING EDGE AT ROOT SECTION. PAINT PEELING.SDR HEEA968794Blade · skin voidSKIN VOID ON UPPER AND LOWER SURFACES NEAR BLADE STATION 43.5" APPROXIMATELY 2.5" FROM TRAILING EDGE. EACH VOID IS APPROXIMATELY 4" IN DIAMETER.SDR 97ZZZX306Blade · crackedPILOT NOTICED A STRANGE NOISE DURING SHUT DOWN. UPON INSPECTION OF THE AIRCRAFT, HE FOUND THAT M/R BLADE S/N 009999-H994 HAD A CRACK ON BOTH THE TOP AND BOTTOM SKINS 15.75 INCH FROM THE DAMPER BRG CASTING. THE AIRCRAFT HAD BEEN IN 18 HRS BEFORE WITH A VERTICASDR 97ZZZX87Bolt · 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 97ZZZX86Bolt · 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 R
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