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 97ZZZX309Screws · 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 97ZZZX308Screws · 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 HEEA968194Blade · blisteredON POST FLIGHT WALK AROUND, NOTICED A BLISTER IN THE BOTTOM SIDE OF THE M/R BLADE ABRASION STRIP.SDR HEEA968189Blade · crackedBLADE IS CRACKED. (REMOVED TO COMPLY WITH 500 HOUR INSPECTION - FOUND SEVERAL CRACKS ON THE TITANIUM STRIP WITH SEPARATION. THE CRACK AT STATION 123" HAS MULTIPLE BRANCHES.SDR HEEA968171Blade · separationSEPARATION ON LEADING EDGE ABRASION STRIP ON THE NO. ONE OUTBOARD END AND THE NO.ONE CENTER INBOARD END LOWER SIDE.SDR 96ZZZX5550Blade · crackedDURING A SCHEDULED 100-HOUR INSPECTION WHILE CLEANING THE MAIN ROTOR BLADES, A 6 INCH CRACK WAS DISCOVERED ON THE LOWER SURFACE 4 FEET, 6 INCHES FROM THE ROOT END. STARTING 1 INCH FROM THE TRAILING EDGE TRAVELING CORDWISE, BUT DID NOT MEET THE SPAR AREA. NO SDR HEEA968128Tip Cap · crackedTIP CAP HAS THE ABRASION STRIP CRACKED WITH MULTIPLE BRANCHES AND SEPARATION. ALSO HAS SOME FIBERGLASS EROSION.SDR HEEA968057Blade · crackedBLADE IS CRACKED. (BLADE HAS NOSE AND NECK SHELLS CRACKED AND SEPARATED. THE INBOARD LEADING EDGE STRIP IS SEPARATED ON THE INBOARD END BEYOND LIMITS. THE NO. 2 CENTER STRIP HAS SMALL AREAS OF SEPARATION.SDR HEEA968054Blade · defectiveBLADE HAS THE TIP RIB OUT OF LINE. TIP CAP DOES NOT FIT.SDR HEEA968051Blade · crackedBLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED)SDR HEEA968044Blade · crackedDUE AN ULTRASOUND INSPECTION FOR TIME EXTENSION. BLADE ALSO HAS A COMPLETE CHORDWISE CRACK AT STATION 47". SENT TO COMPOSITE TECHNIC FOR INSPECTION AND REPAIR.SDR 97ZZZX675Retain Nut · groovedBLADE RETAIN BOLT UNIT EXCESSIVELY GROOVED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 97ZZZX652Retain Bolt · groovedBLADE RETAIN BOLT UNIT EXCESSIVELY GROOVED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 97ZZZX651Retain Bolt · groovedBLADE RETAIN BOLT UNIT EXCESSIVELY GROOVED. REPLACED WITH NEW UNIT, CORRECTED PROBLEMSDR 97ZZZX260Blade · debondedDURING DAILY INSPECTION, FOUND UPPER SURFACE SKIN DEBONDED APPROXIMATELY 20 INCHES BY 8.50 INCHES NEAR BLADE TIP.SDR 96ZZZX5163Blade · crackedBLADE BEING INSPECTED AFTER BEING USED AS RENTAL UNIT. WHILE INSPECTING M/R BLADE ROOT END IAW SIKORSKY COMPOSITE MANUAL, SA 4047-76-5, PARAGRAPHS 2-7, A CRACK WAS FOUND COMING OUT FROM UNDERNEATH THE PHOENLIC BLOCK. BLADE REMOVED FROM SERVICE.SDR 96ZZZX5162Blade · crackedBLADE WAS BEING INSPECTED AFTER BEING USED AS A RENTAL UNIT. WHILE INSPECTING M/R BLADE ROOT END IAW SIKORSKY COMPOSITE MANUAL, SA 4047-76-5, PARAGRAPHS 2-7, A CRACK WAS FOUND COMING OUT FROM UNDERNEATH THE PHOENLIC BLOCK. BLADE REMOVED FROM SERVICE.SDR HEEA967809Tip Cap · crackedTIP CAP IS CRACKED. (TIP CAP HAS THE ABRASION STRIP CRACKED AND SEPARATED.SDR HEEA967808Blade · crackedBLADE IS CRACKED. (BLADE HAS CRACKS IN THE TITANIUM LEADING EDGE AS STATION 167". ALONG WITH SEPARATION AND SECTION LIFTING FROM THE BLADE SURFACE.SDR HEEA967802Blade · crackedBLADE IS CRACKED. (BLADE HAS A CRACK IN THE OUTBOARD LEADING EDGE ABRASION STRIP AT STATION 185" COMPLETE CHORDWISE.SDR CA960916007Skin · debonded(CAN) MAIN ROTOR BLADE UPPER AND LOWER SKINS DEBONDED FROM TRAILING EDGE EXTRUSION FOR 66 INCHES FROM THE TIP INBOARDSDR CHI1595Blade Pin · failedDURING THE 100-HOUR INSPECTION WHILE BLADES WERE BEING REMOVED FOR INSPECTION, THE MAIN ROTOR BLADE PIN S/N 09884-6097 FELL APART. THE BLADE PIN SHANK BROKE AT THE POINT WHERE THE THREADS START. PART TT: 4667.2. PART HAS A LIFE LIMIT OF 7600 HRS. (X)SDR CA960925003Blade · delamination(CAN) 7"X14" DELAMINATION OF ABRASION STRIP ON UPPER SURFACE OF MAIN ROTOR BLADE.SDR HEEA967734Tip Cap · defectiveTIP CAP HAS FIBERGLASS BROKEN BETWEEN INNER DOUBLER AND OUTER DOUBLER ON THE UPPER SURFACE.SDR HEEA967719Blade · crackedBLADE IS CRACKED. (BLADE HAS THE TIP RIB UNBONDED, AND A CRACK AT STATION 112" WITH SEPARATION ON EACH SIDE OF THE CRACK ON THE LEADING EDGE.SDR HEEA967718Tip Cap · crackedCRACK IN THE ABRASION STRIP ON THE LOWER SIDE WITH SEPARATION.SDR HEEA967717Tip Cap · skin brokenFIBERGLASS SKIN BROKEN BETWEEN INNER AND OUTER DOUBLERS ON THE LOWER SIDE. THE LEADING EDGE ABRASION STRIP HAS A CRACK WITH A STOP DRILL.SDR HEEA967704Blade · sep[aratedBLADE FRETTING PADS ON THE UPPER SURFACE ARE SEPARATED BEYOND LIMITS.SDR HEEA967703Blade · crackedBLADE IS CRACKED. (TWO CHORDWISE CRACKS ON THE OUTBOARD LEADING EDGE STRIP. THE FIRST CRACK IS AT STATION 180" WHICH IS COMPLETELY CHORDWISE. THE SECOND CRACK IS AT STATION 199.5 WHICH IS ONLY A PARTIAL CHORDWISE CRACK.SDR 97ZZZX942Blade · crackedDURING DAILY INSPECTION FOUND LOWER BLADE SURFACE CRACKED CHORDWISE AT STA 1397 MM. CRACK EXTENDS FROM TRAILING EDGE FORWARD 110 MM.SDR 97ZZZX253Blade · corrodedDURING DAILY INPSECTION FOUND BLADE SKIN CORRODED AND SEPARATED FROM SPAR AT BLADE TIP.SDR 97ZZZX250Blade · delaminatedDURING DAILY INPSECTION, FOUND LOWER SKIN DELAMINATED AND CORRODED AT OUTBOARD END OF GRIP FINGER DOUBLERS. STA 58 - STA 60.SDR 97ZZZX249Blade · corrodedDURING DAILY INPSECCTION FOUND BLADE SKIN CORRODED AND SEPARATED AT BLADE TIP. CORROSION INSIDE OF SPAR AT TIP.SDR 97ZZZX245Blade · corrodedDURING DAILY INSPECTION FOUND BLADE SKIN CORRODED AND SEPARATED FROM SPAR AT BLADE TIP.SDR 97ZZZX240Blade · corrodedDURING DAILY INSPECTION FOUND BLADE SKIN CORRODED AND SEPARATED AT BLADE TIP.SDR 97ZZZX239Blade · corrodedDURING DAILY INSPECTION, FOUND BLADE SKIN CORRODED AND SEPARATED AT TIP.SDR 97ZZZX237Blade · corrodedDURING DAILY INSPECTION FOUND BLADE SKIN CORRODED AND DELAMINATED AT TIP.SDR 97ZZZX234Blade · corrodedDURING DAILY INSPECTION FOUND BLADE SKIN CORROSION AND DELAMINATION AT BLADE TIP.SDR 97ZZZX228Blade · corrodedDURING DAILY INSPECTION FOUND TIP WEIGHTS AND TIP BLOCK CORRODED CAUSING SPAR/SKIN DEBOND.SDR CA960827012Blade · peeling paint(CAN) EXCESSIVE PEELING OF PAINT ON THE UNDERSIDE OF THIS BLADE NEAR THE TIP. THIS BLADE ALSO PRODUCES WHISTLING NOISES THAT CAN BE HEARD FROM INSIDE THE CABIN DURING ROTOR RUNDOWN AFTER THE ENGINE IS STOPPED.SDR CA960827011Blade · bulged(CAN) ON INSPECTION, BULGE FOUND IN BLADE SKIN APPROXIMATELY 12 INCHES LONG X 2.5 INCHES WIDE X 0.5 INCH HIGH NEAR TRAILING EDGE OF BLADE AT THE TIP.SDR CA960909002Blade · cracked(CAN) BLADE TOP SKIN CRACKED AT STATION 203 5 CRACKED APPROXIMATELY 6 INCHES FROM SPAR REARWARDSDR ERAA96299Blade · defectiveBLADES REM'D FROM A/C WITH 767.8 HRS TSN, DUE TO GROUND SHUFFLE. RETURNING REQUESTING ROOT END EXAMINATION AND REPAIR. SERIAL NUMBERS OF BLADES ARE: 72, 95, 98, 100 .SDR HEEA967660Tip Cap · tearINSPECTED BOTTOM SIDE ON M/R BLUE BLADE TIP CAP AND FOUND TEAR ON TIP CAP. SUSPECT AIR BUBBLE IN PAINT MATERIAL CAUSING TEAR. AIR BUBBLE IS NOTABLE.SDR HEEA967641Blade · separationM/R BLADE SEPARATION ON THE LEADING EDGE ABRASION STRIPS BEYOND LIMITS. THE SEPARATION ARE ON THE INBOARD STRIP AND THE TWO CENTER STRIPS.SDR HEEA967640Blade · crackedBLADE IS CRACKED. (SPANWISE CRACK ON THE TRAILING EDGE STRIP CENTER AT STATION 242" APPROXIMATELY 1 1/4" IN LENGTH. SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR.SDR HEEA967639Blade · crackedM/R BLADE IS CRACKED. (NOSE AND NECK SHELL CRACKED AND SMALL AREAS OF SEPARATION ON THE LEADING EDGE STRIPS.SDR HEEA967633Blade · crackedM/R BLADE IS CRACKED. (CRACK IS ABOUT 4 1/2" LONG.SDR 97ZZZX231Blade · debondedDURING 500 HOUR INSPECTION FOUND BLADE LEADING EDGE CRACKED AND DEBONDED AT RIGHT STA 114, AND STA 154.SDR MVH0064102Blade · damagedMAIN ROTOR REMOVED FOR DAMAGE TO INBOARD LEADING EDGE.
Back to JASC 6210