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 HEEA064811Blade · unbondedTOP SKIN UNBONDED APPROXIMATELY 58 INCHES SPANWISE BY 4.50 INCHES CHORDWISE.SDR CA991104011Blade · delaminated(CAN) ALL 3 MAIN ROTOR BLADES WERE FOUND TO HAVE DELAMINATION OF THE STAINLESS STEEL LEADING EDGE STRIPS. DELAMINATION FOUND AT BLADE ROOT AREA AND AT OVERLAP AREA OF THE INBOARD AND OUTBOARD EDGE STRIPS.SDR HEEA064798Blade · damagedTHE NR 2 INBOARD ABRASION STRIP ON MAIN ROTOR BLADE HAD SEPARATION ON THE INBOARD END OF THE STRIP.SDR HEEA064776Blade · damagedEROSION SHIELD TORN ON THE INBOARD END OF THE STRIP. .SDR HEEA064775Blade · damagedTHE OUTBOARD ABRASION STRIP HAS NUMEROUS PIN HOLES.SDR HEEA064498Blade · crackedMAIN ROTOR BLADE CRACKED IN TRIM TAB AREA. SERIAL NUMBERS REMOVED ARE A-145, A-442, A-330 AND A-437. REFERENCE: DMR NR 686520. REPLACED WITH SERIAL NUMBERS A-1513, A-1519, A-645, AND A-858.SDR HEEA064471Blade · crackedBLADE CRACKED IN TRIM TAB AREA. SERIAL NUMBERS REMOVED ARE A-869 AND A-879. REPLACED WITH SERIAL NUMBERS A-664 AND A-606. REFERENCE: DMR NR 686522.SDR HEEA064470Blade · crackedMAIN ROTOR BLADE CRACKED IN TRIM TAB AREA. SERIAL NUMBERS REMOVED ARE A-625, A-643, A-635, A-653. REPLACED WITH SERIAL NUMBERS A-848, A-1597, A-390, A-649. REFERENCE: DMR NR 686521.SDR AC2A0000003Blade · crackedCRACKED SPAR AT ROOT END. REPLACED MAIN ROTOR BLADE. (X)SDR CA000404011Pin · broken(CAN) M/R BLADE FOLDING PIN FOUND BROKEN DURING REMOVAL FOR 300 HOUR INSPECTION. ALL THE PINS WERE SUBSEQUENTLY REMOVED FOR INSPECTION.SDR CA991027053Blade · cracked(CAN) CRACK FOUND IN AREA C OF THE TRAILING EDGE (BETWEEN STA 590 AND STA 725).SDR 99ZZZX4035Blade · corrodedDURING DAILY INSPECTION, FOUND TRAILING EDGE EXTRUSION CORRODED.SDR CA990915039Bolt · wrong part(CAN) WHILE DOING A MAIN ROTOR BLADE REPLACEMENT, THE BLADE BOLTS LOOKED DIFFERENT AND WERE LATER CONFIRMED BY MANUFACTURER TO BE BOGUS. ORIGINATOR CHECKING ON PREVIOUS HISTORY OF M/R HEAD ASSY.SDR HEEA063756Blade · blisteredSMALL VOID ON UNDERSIDE OF BLADE NEAR TIP. BLISTER NOTED ON DAILY INSPECTION. REFERENCE: DMR NR 686382.SDR HEEA063751Blade · damagedLOWER POCKET WEIGHT CORROSION, VOID AT STATION 197 ON LOWER SURFACE, HOLE AT STATION 197 ON LOWER. SERIAL NUMBERS REMOVED ARE A285, A341 AND A263. REPLACEMENT PART SERIAL NUMBERS ARE A754, A650 AND A596. REFERENCE: DMR NR 686294.SDR HEEA063452Blade · damagedINBOARD ABRASION STRIP HAD SEPARATION ON THE OUTBOARD END OF THE STRIP.SDR HEEA063451Blade · damagedROTOR BLADE HAD SEPARATION ON THE INBOARD ABRASION STRIP ON THE OUTER END. THE ABRASION STRIP AT THE TIP HAD EROSION HOLES.SDR HEEA063450Blade · damagedEROSION HOLE THROUGH THE OUTBOARD ABRASION STRIP ON MAIN ROTOR BLADE.SDR HEEA063449Blade · damagedTHE NR 1 INBOARD ABRASION STRIP HAS SEPARATION ON THE OUTBOARD END OF THE STRIP.SDR HEEA063295Blade · crackedINBOARD ABRASION STRIP CRACKED NEAR THE SPLICE COVER ON THE UPPER SURFACE. FIBERGLASS CRACKED AROUND THE INBOARD AND MID-SPAN TAB.SDR HEEA063294Blade · debondedSKIN AT SPLICE JOINT AREA UNBONDED.SDR HEEA063293Blade · damagedSEVERAL PIN HOLES IN THE OUTBOARD LEADING EDGE STRIP. THE INBOARD TAB AND CENTER TAB HAD SOME SEPARATION.SDR HEEA063292Blade · crackedBLADE HAD SEVERAL PIN HOLES IN THE OUTBOARD LEADING EDGE STRIP. THE INBOARD TRIM TAB WAS CRACKED.SDR HEEA063270Blade · debondedTOP METAL EROSION SHIELD IS DEBONDING.SDR HEEA063259Blade · corrodedSEVERAL AREAS OF CORROSION ON TRAILING EDGE OF BLADES.SDR HEEA063060Tip Cap · splitTRAILING EDGE SPLIT OPEN NEAR THE TIP LEADING EDGE. ABRASION STRIP CRACKED TOP AND BOTTOM.SDR 2000ZZZX151Bolt · damagedNOT SEIZED ON SHAFT THREADS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 99ZZZX3293Blade · peelingDURING ROUTINE INSPECTION, DISCOVERED LEADING EDGE ABRASION STRIP PEELING OFF. POSSIBLE BONDING METHOD AT TIME OF MANUFACTURE.SDR 99ZZZX3348Blade · corrodedTRAILING EDGE EXTRUSION CORRODED BEYOND REPAIRABLE LIMITS. (INTERGRANULAR CORROSION).SDR HEEA062897Blade · peelingMAIN ROTOR PAINT PEELING.SDR HEEA062896Blade · peelingMAIN ROTOR BLADE PAINT PEELING.SDR HEEA062864Blade · malfunctionedBLADE CLIMBS EXCESSIVELY.SDR HEEA062863Blade · heavyBLADE CLIMBS EXCESSIVELY IN FLIGHT AND IS HEAVY.SDR HEEA062855Blade · won't trackBLADE WILL NOT TRACK.SDR HEEA062781Tip Cap · erodedEND CAP IS ERRODED THROUGH.SDR HEEA062780Tip Cap · weakTRAILING EDGE WEAK ON CAP.SDR 99ZZZX3358Blade · damagedREMOVED IWTH OTHER BLADES AS PRECAUTION PER AEC. MCN 137. REMOVED AND REPLACED.SDR 99ZZZX3051Bolt · looseEXPANSION BOLT BACKED OUT OF BLADE. REF: MCN 140. REMOVED AND REPLACED.SDR 99ZZZX3050Bolt · looseEXPANSION BOLT LOOSE. REMOVED PER AEC. REF: MCN: 139. REMOVED AND REPLACED.SDR 99ZZZX3049Bolt · looseEXPANSION BOLT LOOSE. REF: MCN 138. REMOVED AND REPLACED.SDR 99ZZZX3027Blade · corrodedDURING DAILY INSPECTION, CORROSION AND DEBOND OF SKIN AND SPAR BENEATH GRIP FINGER DOUBLER ON LOWER SURFACE. DAMAGE BEYOND MANUFACTURER'S LIMITS, BLADE SCRAPPED.SDR 99ZZZX2839Dampener · failedTHERE WAS AN APPARENT FAILURE WITHIN THE MAIN ROTOR BLADE CUFF THAT FIXES THE LEAD LAG DAMPENER, AND SPHERICAL BEARING SUPPORT TO THE BLADE ASSEMBLY, AND IS CURRENTLY UNDER INVESTIGATION BY AEC TECHNICAL REPRESENTATIVES.SDR 99ZZZX2600Blade · crackedFOUND HARILINE CRACKS (8 EACH) EXTENDING CHORDWISE ALL THE WAY AROUND THE NICKLE LEADING EDGE EROSION PROTECTION STRIP. CRACKS COULD NOT BE SEEN UNTIL A THOROUGH CLEANING OF THE BLADE LEADING EDGE WAS PERFORMED (REMOVAL OF BUGS/CARBON). SUBMITTER RECOMMENDEDSDR CA990630004Blade · cracked(CAN) DURING SCHEDULED MAINTENANCE, NUMEROUS 10 MM CRACKS WERE NOTED ON THE LOWER INBOARD AREA APPROXIMATELY 1000 MM FROM THE BLADE ROOT.SDR 99ZZZX3026Blade · corrodedDISCOVERED DURING DAILY INSPECTION, HEAVY INTERGRANULAR CORROSION ON TRAILING EDGE.SDR 99ZZZX2490Blade · disbondedDURING DAILY INSPECTION, FOUND VOID AT UPPER AND LOWER SECTION OF TRIM TAB TRAILING EDGE. AIRCRAFT TT: 4,967.8 HOURS. M/R BLADE REMOVED AND SENT FOR REPAIR.SDR CA990630010Blade · damaged(CAN) UPON INSPECTION, A VOID WAS DETECTED IN THE GRIP PLATE THAT IS BEYOND THE MANUFACTURER'S SET FORTH REPAIRABLE LIMITS AND ALSO OUTSIDE THE PARAMETERS OFADS AND SBS THAT CALL FOR INSPECTION FOR THESE PROBLEMS.SDR 99ZZZX3025Blade · corrodedDISCOVERED DURING DAILY INSPECTION, TRAILING EDGE EXTRUSION HEAVILY CORRODED (INTERGRANULAR CORROSION).SDR 99ZZZX2491Blade · disbondedAIRCRAFT HAD VERTICAL VIBRATION ON SHORT FINAL TO LAND. INSPECTED AIRCRAFT, FOUND LOWER TRIM TAB HAD DISBONDED ON M/R BLADE PN 212-015-501-5, SN A262. AFTER CLOSER INSPECTION, FOUND CORROSION UNDER TAB. REMOVED M/R HUB AND BOTH M/R BLADES FOR CONVENIENCE. SDR 99ZZZX2534Blade · corrodedDURING DAILY INSPECTION, FOUND TRAILING EDGE EXTRUSION WITH HEAVY INTERGRANULAR CORROSION, POSSIBLY CAUSED BY IMPROPERLY HEAT TREATED MATERIAL.
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