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 HEEA966872Blade · defectiveREMOVE EXCESS WEIGHT AND PAINT AND REFINISH BLADES AND SEAL THE EDGE OF THE INBOARD TRIM TAB ON BLADE S/N A94.SDR 96ZZZX2217Blade · crackedDURING 500-HOUR INSPECTION, FOUND BLADE SPAR CRACKED AT ROOT END BUSHING HOLE. SUBMITTER STATED CAUSE UNKNOWN.SDR HEEA966856Blade · crackedPART IS CRACKED. (NOSE AND NECK SHELL CRACKED AND. THE INBOARD STRIP HAS SEPARATION AT JOINT.SDR HEEA966855Blade · crackedPART IS CRACKED. (NOSE AND NECK SHELL CRACKED AND SEPARATED THERE ARE SEPARATION ALSO PRESENT ON THE THREE INBOARD LEADING EDGE ABRASION STRIP.SDR HEEA966845Blade · unbondedINSPECTION DUE FOR TIME EXTENSION. THE TIP RIB IS UNBONDED, THE NICKEL STRIP HAS NUMEROUS CRACKS WITH SMALL AREAS UNBONDED.SDR CA960412013Blade · cracked(CAN) BLADES ARE MATCHED PAIRS. BLADE 1 - CHORDWISE CRACKS 10 INCHES LONG AT STN. 19 AND 75. BLADE 2 DIAGONAL CRACK AT STN. 15. CRACKS COULD NOT BEEN SEEN WITH BLADES AT REST AND UNDER OWN WEIGHT. FUTURE INSPECTIONS WILL BE WITH BLADE TIP SUPPORT.SDR HEEA966798Blade · unbondedTIP RIB UNBONDED, AND TIME EXTENSION IS ALSO DUE.SDR CA960312027Blade · debonding(CAN)LEADING EDGE STRIP DEBONDED.SDR CA960312026Blade · debonded(CAN)LEADING EDGE ABRASION STRIP DEBONDED.SDR CA960312025Blade · debonding(CAN)LEADING EDGE ABRASION STRIP DEBONDING. TIME THIS INSTALLATION 589.8 HOURS.SDR CA960312024Blade · debonding(CAN)LEADING EDGE ABRASION STRIP DEBONDING. BLADE P/N 369D21100-516A. TIME THIS INSTALLATION 589.8 HOURS.SDR HEEA966709Blade · crackedBLADE NOSE AND NECK SHELLS CRACKED AT THE CUFF AREA)SDR HEEA966699Blade · crackedM/R BLADE NOSE AND NECK SHELLS CRACKED AND SEPARATED AT ROOT END AREA.SDR HEEA966698Blade · crackedM/R BLADE NOSE AND NECK SHELLS CRACKED AND SEPARATED AT ROOT END AREA.SDR 96ZZZX974Blade · defectiveABRASION STRIPS ON 3 BLADES WERE NOT INSTALLED CORRECTLY. THEY DO NOT GO ALL THE WAY TO THE EDGE. BLADES ARE BEING SENT TO RBI FOR REPAIR. SERIAL NUMBERS, H992, H991, AND H990. REFERENCE: OPERATOR CONTROL NR MLTA960213.SDR 96ZZZX3465Bushing · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 8 EACH NEW UNITS, CORRECTED PROBLEM.SDR HEEA966677Blade · strap separatedM/R BLADE TIP ATTACHMENT STRAP SEPARATED ON THE LOWER SIDE.SDR 96ZZZX975Blade · debondedABRASION STRIP WAS FOUND DEBONDED, BOTTOM AREA OF 1 INCH BY 19 INCHES. BLADE SENT TO RBI FOR REPAIR. REFERENCE: OPERATOR CONTROL NR MLTA960205.SDR HEEA966595Blade · corrodedBLADE HAS EXCESSIVE AMOUNT OF EXFOLIATION OF THE LEADING EDGE.SDR HEEA966589Tip Cap · separationFIBERGLASS BROKEN BETWEEN INNER DOUBLER AND OUTER DOUBLER, WITH SOME SEPARATION ON THE LEADING EDGE ABRASION STRIP ON THE UPPER SURFACE.SDR 96ZZZX4108Blade · corrodedDURING A 1,200-HOUR INSPECTION, MAIN ROTOR BLADES WERE REJECTED DUE TO EXFOLIATION ON LEADING EDGE. TSN: 3,200. THESE BLADES HAVE A LIFE OF 5,000.0 HOURS. ACFT TT: 13,200.0 HOURS.SDR 96ZZZX4107Blade · corrodedDURING A 1,200-HOUR INSPECTION, MAIN ROTOR BLADES WERE REJECTED DUE TO EXFOLIATION ON LEADING EDGE. TSN: 3,200. THESE BLADES HAVE A LIFE OF 5,000.0 HOURS. ACFT TT: 13,200.0 HOURS.SDR HEEA966492Tip Cap · crackedTIP CAP HAS INTERNAL DOUBLER SEPARATED BEYOND LIMITS AND LEADING EDGE ABRASION STRIP CRACKED AND SEPARATED.SDR 96ZZZX612Blade · delaminatedDURING ANNUAL INSPECTION, FOUND M/R BLADE WAS DELAMINATED UNDER THE ABRASION STRIP ON THE UPPER SURFACE OF THE BLADE FOR ABOUT 6 SQUARE INCHES. BLADE REMOVED AND SENT IN FOR REPAIR.SDR CA960126019Blade Pins · worn(CAN)FOUND PINS DID NOT PROTRUDE THROUGH BLADES AND LEAD-LAG LINKS PROPERLY, MEASURED AS PER HMI AND FOUND WORN BEYOND LIMITS. 10 PINS AFFECTED.SDR 96ZZZX629Blade · erodedMAIN ROTOR BLADE L/E ABRASION STRIP ERODED AT THE OUTBOARD END OF M/R BLADE NEAR THE TIP. CAUSE OF EROSION - OPERATING IN AND AROUND SAND AND DIRT DURING OFF-AIRPORT LANDINGS. REPAIR MADE TO AREA PER APPROVED ENG. DATA - 8110-3. M/R BLADE RETURNED TO SERVICSDR HEEA966439Tip Cap · mis repairedTIP CAP WAS REPAIRED AT CTI 12-11-95. THE TIP CAP DOES NOT FIT. THE TOP LEADING EDGE HOLE DOES NOT LINE UP AND THE ABRASION STRIP IS NOT STRAIGHT, PREVENTING THE TIP CAP TO FIT PROPERLY, ALSO THERE IS AN EXCESSIVE AMOUNT OF HYSOL EA9309.3NABETWEEN THE TOP ISDR HEEA966431Blade · crackedPART IS CRACKED. BLADE IS DUE FOR TIME EXTENSION AND ALSO HAS SEPARATION ON THE TITANIUM LEADING EDGE STRIP WITH A CHORDWISE CRACK NEAR THE INBOARD END OF THE NICKEL STRIP.SDR 96ZZZX3483Bushing · wornBUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS 2 EACH, CORRECTED PROBLEM.SDR 96ZZZX3147Blade · defectiveM/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX3146Blade · defectiveM/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX3145Blade · defectiveM/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX3144Blade · defectiveM/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX3141Blade · defectiveM/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR HEEA966358Blade · crackedBLADE IS CRACKED. SPAR CRACKED AT ROOT END. SCRAPPED M/R BLADE.SDR HEEA966357Blade · crackedPART IS CRACKED. SPAR CRACK AT THE TIP. THE CRACK STARTED FROM THE OUTER HOLE FOR THE "C" BLOCK BOLT. SCRAPPED M/R BLADE.SDR CA960126014Blade · wont track(CAN)EXTREME DIFFICULTY WITH TRACKING OF MAIN ROTOR BLADE. COULD NOT GET BLADE BALANCED WITH MAXIMUM BALANCE PLATES INSTALLED.SDR HEEA956322Blade · defectiveBLADE HAS A REPAIR NEAR THE LAST FINGER ON THE UPPER SURFACE THAT WAS DONE BY BELL HELICOPTER TEXTRON. WHEN PRIMING THE AREA MOISTURE STARTED SEEPING OUT. BLADE RECEIVED INSTALLED ON AIRCRAFT 12-1-95.SDR HEEA956312Blade · corrodedEXCESSIVE AMOUNT OF EXFOLIATION OF THE LEADING EDGE.SDR HEEA956311Blade · corrodedEXCESSIVE AMOUNT OF EXFOLIATION OF THE LEADING EDGE.SDR HEEA956310Blade · corrodedEXCESSIVE AMOUNT OF EXFOLIATION OF UPPER LEADING EDGE AND LOWER LEADING EDGE NEAR THE TIP WITH PIECES MISSING.SDR 96ZZZX741Blade · debondedDURING 500-HOUR INSPECTION, FOUND BLADE SKIN DEBONDED. LOWER SURFACE OVER SPAR AT BLADE TIP.SDR 96ZZZX301Tip Rib · separatedMAIN ROTOR BLADE TIP RIB WAS FOUND SEPARATED. IT WAS DISCOVERED DURING THE 500-HOUR INSPECTION. TIP RIB AND DOUBLER SEPARATED. SUBMITTER STATED POSSIBLY CAUSED BY EXCESS PRESSURE APPLIED TO TIP CAP SCREWS DURING TIP CAP INSTALLATION. COMPONENT NR 761500910SDR 96ZZZX104Pin · excess wearWHILE REMOVING BLADES FOR M/R SWASHPLATE REPLACEMENT, ONE OF THE BLADE PINS WAS FOUND WITH ABNORMAL WEAR IN THE CAM HANDLE PIVOT BOSS. PIN RETURNED TO MDHC ON SOR NR 300165.SDR HEED95436Bumper · missingBUMBER ON M/R GRIP MISSING REPLACED UNITSDR GMAL951207Blade · crackedMAIN ROTOR BLADE CRACKED. CRACK LOCATED AT STA 109.5, CORDWISE, TOP 10.25 INCHES LONG, 4.5 INCHES AFT OF LEADING EDGE. ONLY 10 HOURS OF FERRY FLIGHT SINCE LAST INSPECTION. AIRCRAFT TOTAL TIME 985 HOURS. (X)SDR GMAL9509142Blade · crackedMAIN ROTOR BLADE FOUND CRACKED, CRACK LOCATED BETWEEN STA 172 AND STA 180, CORDWISE ON BOTTOM OF BLADE AT 13 INCHES LONG, 5 INCHES FROM LEADING EDGE. ONLY 4 HOURS OF FLIGHT SINCE LAST INSPECTION. AIRCRAFT TOTAL TIME 566 HOURS, 3 BLADES FOUND CRACKED AT SAME SDR GMAL9601252Blade · crackedMAIN ROTOR BLADE CRACKED. LOCATION UNKNOWN AT THIS TIME. BLADE RETURNED TO MANUFACTURER. (X)SDR HEEA956098Blade · crackedPART IS CRACKED. (NUMEROUS AMOUNT OF CRACKS ON THE NICKEL STRIP WITH SEPARATION THAT IS BEYOND THE MAX LIMITS.SDR HEED95397Tip Cap · separatedTRAILING EDGE SEPERATED REPLACED UNIT
Back to JASC 6210