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.

SDR HAIHEEA9336Blade · crackedNOSE AND NECK SHELLS CRACKED BEYOND LIMITS NEAR THE ROOT END.Apr 15, 1997 · N3539T · Bolkms BO105SSDR HAIHEEA9330Blade · bulgingBLADE BULGING BEYOND LIMITS.Apr 15, 1997 · N8765J · Bolkms BK117A3SDR CA970521002Blade · cracked(CAN) IN FLIGHT BIM INDICATION. BLADE REMOVED, SENT OUT FOR REPAIR. CRACK FOUND STARTING FROM CUFF ATTACHMENT BOLT HOLES.Apr 10, 1997 · Skrsky S61NSDR 97ZZZX4132Blade · defectiveM/R BLADE FAILED BLADE INSPECTION PROGRAM. EXCESSIVE BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Mar 25, 1997 · N911VU · Bolkms BK117B1SDR HAIGJQR0111Blade · peelingLARGE PATCHES OF PAINT PEELING FROM BLADES.Mar 24, 1997 · N98W · Bell 212SDR 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 APPROXIMATELMar 20, 1997 · N192CH · Kawski KV1072SDR NYBA9713Blade · defectiveRED BIM INDICATION REPLACED MAIN ROTOR BLADEMar 18, 1997 · N26567 · Skrsky S58ETSDR NYBA978Blade · erodedBLADE IS ERODED. REPLACED MAIN ROTOR BLADEMar 17, 1997 · N125NH · Bell 206L4SDR HEEA979208Blade · damagedMAIN ROTOR TIP DAMAGE OUTWARD - 1 INCH CRACK ON TIP.Mar 12, 1997 · N9214U · Doug MD900SDR HEEA979180Tip Cap · crackedTRAILING EDGE SPLIT OPEN AND A CRACK ON THE LEADING EDGE ABRASION STRIP ON THE UPPER SURFACE.Mar 12, 1997 · N4253S · Skrsky S76ASDR HEEA979177Blade · not drilledRECEIVED FROM THE VENDOR WITH A NEW LEADING EDGE ABRASION STRIP INSTALLED BUT THE HOLES WERE NEVER DRILLED FOR THE WEIGHT POCKET.Mar 12, 1997 · N23023 · Bell 412SDR HEEA979168Blade · separationSEPARATION ON THE NUMBER TWO CENTER LEADING EDGE STRIP ON THE INBOARD END BEYOND LIMITS.Mar 12, 1997 · N911HM · Bolkms BO105SSDR CA970421008Blade · cracked(CAN) MAIN ROTOR BLADE FOUND WITH CHORDWISE CRACK. CRACK 35.43" OUTBOARD OF ROOT.Feb 26, 1997 · Snias AS350B1SDR 97ZZZX1272Blade · corrodedDISCOVERED DURING DAILY INSPECTION, CORROSION AND SKIN SEPARATION AT SPAR TIP. CORROSION AT ROOT END WEAR PADS.Feb 18, 1997 · N3195P · Bell 206L1SDR 97ZZZX1285Blade · separationDURING DAILY INSPECTION FOUND SKIN SEPARATED AND CORRODED OVER SPAR AT TIP.Feb 13, 1997 · N5760A · Bell 206L1SDR 97ZZZX1284Blade · separationDURING DAILY INSPECTION FOUND SKIN SEPARATED OVER SPAR AND BLADE TIP.Feb 13, 1997 · N5760A · Bell 206L1SDR 97ZZZX1275Blade · separatedDURING DAILY INSPECTION, FOUND UPPER SKIN SEPARATED AT SPAR TIP. CORROSION OR ROOT END AT WEAR PADS.Feb 13, 1997 · N366AL · Bell 206L3SDR 97ZZZX1270Blade · corrodedDURING DAILY INSPECTION FOUND SKIN CORRODED AND SEPARATED AT TIP. CORROSION AT WEAR PADS OR ROOT END.Feb 13, 1997 · N3185P · Bell 206L1SDR HEEA979077Tip Cap · holedTIP CAP HAS A HOLE IN THE LOWER SKIN JUST AFT OF THE LEADING EDGE ABRASION STRIP.Feb 11, 1997 · N1545X · Skrsky S76ASDR 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.Feb 11, 1997 · N23023 · Bell 412SDR HEEA979075Blade · defectiveBLADE DEFECT, EXCESSIVE LATERAL VIBRATION -- UNABLE TO TRACK.Feb 11, 1997 · N3893S · Bell 412SDR HEEA979074Blade · defectiveM/R BLADE HAS SKIN VOID ON THE LOWER SIDE WHICH STARTS FROM STATION 263" TO STATION 271" SPANWISE AND 2.5" CHORDWISE.Feb 11, 1997 · N3893S · Bell 412SDR HEEA979073Blade · crackedT/R BLADE HAS PARTIAL CHORDWISE CRACK ON THE OUTBOARD LEADING EDGE ABRASION STRIP AT THE SPLICE AREA.Feb 11, 1997 · N23023 · Bell 412SDR HEEA979070Blade · crackedM/R BLADE SPAR CRACKED AT THE ROOT END COMING FROM THE FORWARD OUTBOARD BUSHING HOLE. SCRAPPED M/R BLADE.Feb 11, 1997 · N1546G · Skrsky S76ASDR HEEA979053Blade · crackedBLADE HAS NOSE AND NECK SHELL CRACKED AND THE #1 ONE INBOARD LEADING EDGE STRIP SEPARATED BEYOND LIMITS.Feb 11, 1997 · N3526T · Bolkms BO105SSDR HEEA979052Blade · crackedBLADE IS CRACKED. NOSE AND NECK SHELL CRACKED AND SMALL AREAS OF SEPARATION ON THE LEADING EDGE STRIPS.Feb 11, 1997 · N3526T · Bolkms BO105SSDR HEEA979051Blade · crackedBLADE HAS NOSE AND NECK SHELL CRACKED. THE LEADING EDGE STRIP IS SEPARATED AT THE TIP AND SCARF JOINT AREAS.Feb 11, 1997 · N3526T · Bolkms BO105SSDR HEEA979050Blade · separatedBLADE HAS THE NUMBER TWO CENTER LEADING EDGE STRIP SEPARATED 62MM ON THE INBOARD END TOP SURFACE.Feb 11, 1997 · N81992 · Bolkms BO105SSDR 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.Feb 11, 1997 · N3526T · Bolkms BO105SSDR 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.Feb 11, 1997 · N31217 · Skrsky S76ASDR HEEA979043Tip Cap · tornTIP CAP HAS THE SKIN TORN ON THE LOWER SIDE BEYOND MAX LIMITS.Feb 11, 1997 · N31217 · Skrsky S76ASDR HEEA979039Tip Cap · crackedTIP CAP HAS A CRACKED ABRASION STRIP ON THE LOWER SIDE.Feb 11, 1997 · N4253S · Skrsky S76ASDR HEEA979038Tip Cap · tornTIP CAP HAS THE SKIN TORN ON THE LOWER SIDE BEYOND THE MAXIMUM LIMITS.Feb 11, 1997 · N1545X · Skrsky S76ASDR HEEA979035Blade · separationSEPARATION ON THE INBOARD LEADING EDGE ABRASION STRIP BEYOND THE LIMITS.Feb 10, 1997 · N8197X · Bolkms BO105SSDR HEEA979034Blade · separationBLADE HAS SEPARATIONS ON THE THREE-IN-BOARD LEADING EDGE STRIPS.Feb 10, 1997 · N8197X · Bolkms BO105SSDR AU970145Blade · debonded(AUS) MAIN ROTOR BLADE INBOARD TRIM TAB DEBONDED AND LOOSE ON BLADEFeb 6, 1997 · Aerosp AS355F1SDR 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.Jan 27, 1997 · Hughes 369DSDR 97ZZZX1408Blade · crackedDURING DAILY INSPECTION, FOUND SKIN CRACKED AT STA 1000 MM.Jan 21, 1997 · N372E · Aerosp AS355ESDR 97ZZZX1286Blade Rib · dedbondedDISCOVERED DURING 500 HOUR INSPECTION THAT BLADE TIP RIB WAS DEBONDED.Jan 20, 1997 · N702AL · Skrsky S76SDR 97ZZZX1283Blade · separatedDISCOVERED DURING ROUTINE MAINTENANCE, SKIN SEPARATED FORM SPAR AT BLADE TIP.Jan 15, 1997 · N5750Y · Bell 206L1SDR HEEA978871Blade Bolt · defectiveCENTER PLUNGER GETS STUCK WHEN PUSHED IN.Jan 14, 1997 · N900AF · Doug MD900SDR HEEA968799Blade · defectiveHOLES IN THE LEADING EDGE ROOT SECTION. PAINT PEELING. SENT TO MCDONNELL DOUGLAS FOR INSPECTION.Dec 30, 1996 · N9214U · Doug MD900SDR HEEA968798Blade · defectiveHOLES IN THE LEADING EDGE ROOT SECTION. PAINT PEELING.Dec 30, 1996 · N9214U · Doug MD900SDR HEEA968797Blade · paint peelM/R BLADE PAINT PEELING.Dec 30, 1996 · N9214U · Doug MD900SDR HEEA968796Blade · paint peelM/R BLADE PAINT PEELING.Dec 30, 1996 · N9214U · Doug MD900SDR HEEA968795Blade · defectiveHOLE IN THE LEADING EDGE AT ROOT SECTION. PAINT PEELING.Dec 30, 1996 · N9214U · Doug MD900SDR 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.Dec 30, 1996 · N8045T · Bell 214STSDR 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 VERTICADec 13, 1996 · N161W · Hughes 369ESDR 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 RDec 11, 1996 · Skrsky S64FSDR 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 RDec 11, 1996 · Skrsky S64F
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