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 CA981022001Blade · cracked(CAN) M/R BLADE BIM CAUTION LIGHT ACTIVATED. BLADE REMOVED, TESTED SERVICEABLE ON PRESSURE TEST IAW S61 MAINT MANUAL. 5 HOURS AFTER REINSTALL, ANOTHER BIM INDICATION. BLADE SENT TO SIKORSKY WHERE IT FAILED SIKORSKY'S TEST. TEST INDICATED A CRACKED SPAR.SDR HEEA0015307Doubler · mismanufacturedBLADE DOUBLER CUT TOO SHORT. SUBMITTER STATED UNACCEPTABLE FOR PHI USE.SDR HEEA0015289Blade · defectiveCANNOT TRACK OR BALANCE. SUSPECT WATER IN THE BLADE CORE.SDR HEEA0015286Blade · defectiveCANNOT TRACK OR BALANCE. SUSPECT WATER IN THE BLADE CORE.SDR HEEA0015277Blade · unbondedOUTBOARD LEADING EDGE ABRASION STRIP HAS CRACKS WITH MULTIPLE BRANCH.SDR HEEA0015268Blade · unbondedM/R BLADE HAS SEPARATION ON THE OUTBOARD LEADING EDGE STRIP NEAR THE TIP END.SDR 99ZZZX47Blade · debondedDISCOVERED DURING 500-HOUR INPSECTION, TIP RIB STRAP DEBONDED, (RECURRING PROBLEM). TIP RIB STRAPS REPLACED BY C.T.I. 04-04-97, TT: 6,245.1 HOURS. 05-19-97, TT: 6,340.1 HOURS, AND 12-23-97, TT: 7,207.8 HOURS.SDR 98ZZZX3093Blade · debondedDISCOVERED DURING 500-HOUR INSPECTION, TIP RIB STRAP DEBONDED (RECURRING PROBLEM WITH THIS BLADE). TIP RIB STRAPS REPLACED BY C.T.J. 4-4-97 TT 6,245.1 HOURS - 5-19-97 TT 6,340-1 HOURS - 12-23-98 TT 7,207.8 HOURS.SDR 99ZZZX1221Blade · corrodedDISCOVERED DURING DAILY INSPECTION, TRAILING EDGE EXTRUSION CORRODED.SDR 98ZZZX3099Blade · debondedDISCOVERED DURING DAILY INSPECTION, M/R BLADE'S LOWER SURFACE GRIP FINGER DOUBLER DEBONDED. (THIRD DOUBLER DEBONDED APPROXIMATELY 10 INCHES).SDR HEEA0015162Blade · voidVOID AT STATION 144 ON UPPER SURFACE.SDR CA980818018Abrasion Strip · separated(CAN) LOWER ABRASION STRIP SEPARATING 11 CM FROM EDGE OF BLADE INBOARD 4 BY 5 CM TO TRAILING EDGE FROM JUST BEHIND STAINLESS STEEL LEADING EDGE STRIP.SDR 99ZZZX1225Blade · corrodedDISCOVERED DURING DAILY INSPECTION, SKIN CORRODED, SEPARATED AND TORN ON LOWER SIDE TIP.SDR 98ZZZX3262Terminal · crackedDURING OVERHAUL NDT INSPECTION, FOUND CRACKED TERMINAL BORE. CRACK ABOUT .100 INCH INTO THE BORE AND ACROSS THE CLEVIS FACE. REF: CHI WO C7289. WORKSHEET 7-2-98 ITEM 37.SDR CA980916036Blade · damaged(CAN) ON PRE-FLIGHT, VOID FOUND IN THE TIP OF THE BLADE. VOID IS 3 INCHES BY .25 INCH BY .25 INCH DEEP.SDR CA980814001Spar · cracked(CAN) ON 500-HOUR INSPECTION, CRACK IN THE ROOT END OF M/R BLADE. BLADE SCRAPPED.SDR 99ZZZX1226Blade · corrodedDISCOVERED DURING DAILY INSPECTION, CORROSION AND SEPARATION AT TIP.SDR HEEA0015053Erosion Shield · separatedSEPARATION ON THE EROSION SHIELD ON THE M/R BLADE INBOARD END.SDR HEEA0015052Blade · damagedHOLES IN THE OUTBOARD LEADING EDGE ABRASION STRIP.SDR 98ZZZX2832Blade · failedNOTE: THE ACRONYM 'BIM' STANDS FOR BLADE INSPECTION METHOD AND IS A TERM REGISTERED BY SIKORSKY. THE INDICATOR SENSES PRESSURE WITHIN THE BLADE SPAR AND CHANGES COLOR TO DENOTE A LEAK WHICH MAY BE CAUSED BY A CRACKED SPAR INDICATING THIS MDR SUBJECT HAS AIRWSDR 98ZZZX3346Blade · delaminatedFIFTY HOUR INSPECTION FOUND M/R BLADE POTTING COMPOUND DELAMINATED AT OUTBOARD WEIGHT POCKET.SDR 98ZZZX3345Blade · delaminationFIFTY HOUR INPSECTION FOUND M/R BLADE PTTING COMPOUND DELAMINATION AT OUTBOARD WEIGHT POCKET.SDR 98ZZZX3344Blade · delaminatedFIFTY HOUR PHASE INSPECTION FOUND M/R BLADE POTTING COMPOUND DELAMINATING AT OUTBOARD WEIGHT POCKET.SDR 98ZZZX3343Blade · delaminatedFIFTY HOUR INSPECTION FOUND M/R BLADE POTTING COMPOUND DELAMINATION AT OUTBOARD WEIGHT POCKET.SDR HAIGJQR0199Blade · mismanufacturedNEW BLADE INSTALLED 6/2/97. BEST TRACK OBTAINED 1.0 IPS VERTICAL AT 80 KNOTS. TRIED TO GET BLADES TO FLY TOGETHER FOR 1,128 HRS. PULLED BLADE AND PUT ANOTHER BLADE ON SHIP, TRACE NORMAL. INSTALLED BLADE S/N AFS-11686 ON ANOTHER SHIP TO TRY TO USE - COULD NSDR HEEA0014685Blade · debondedLEADING EDGE OF MAIN ROTOR BLADE HAS SEPARATION BEYOND LIMITS ON THE OUTBOARD END OF THE TWO INBOARD STRIPS.SDR 98ZZZX3348Blade · corrodedMAJOR INSPECTION FOUND INTERGRANULAR CORROSION ON TIP END OF BLADE SPAR.SDR HEEA0014671Blade · damagedCOULD NOT BALANCE MAIN ROTOR BLADE. TIP HEAVY. (SUSPECT WATER IN THE CORE).SDR HEEA0014670Blade · faultyMAIN ROTOR BLADE WILL NOT TRACK.SDR HEEA0014669Blade · faultyMAIN ROTOR BLADE WILL NOT TRACK.SDR HEEA0014668Tip Cap · brokenMAIN ROTOR TIP CAP OUTER DOUBLER SEPARATED WITH FIBERGLASS BROKEN BETWEEN THE DOUBLER.SDR HEEA0014595Blade · unbondedFRETTING AND PAD UNBONDED ON UPPER SURFACE. THE TIP OF THE BLADE IS HEAVY.SDR HEEA0014478Blade · damagedHOLE IN THE OUTBOARD LEADING EDGE STRIP NEAR THE TIP.SDR HEEA0014192Blade · defectiveCANNOT BALANCE M/R BLADE ON AIRCRAFT (SUSPECT WATER IN THE CORE)SDR HEEA0014190Blade · damagedM/R BLADE OUTBOARD LEADING EDGE STRIP HAS NUMEROUS PIN HOLES.SDR AU980990Blade · corroded(AUS) MAIN ROTOR BLADE LEADING EDGE UPPER SURFACES PEELING AWAY. FURTHER INSPECTION FOUND INTERGRANULAR CORROSION ON THE LOWER SURFACE. EDDY CURRENT INSPECTION CONFIRMED INTERNAL CORROSION. PART TC: 2,209.SDR 98ZZZX1742Blade · crackedMAIN ROTOR SPAR IS CRACKED 72.81 INCHES FROM TIP UNDER THE NR 6 POCKET, CLOSE (APPROXIMATELY .1 INCH) TO THE SPACE BETWEEN THE NR 6 AND NR 7 POCKETS. THE CRACK RUNS CHORDWISE BETWEEN THE POCKET LEADING EDGE GROOVE, AND THE BACKWALL RADIUS. IT DOES NOT APPEARSDR HAIGJQR0180Blade · damagedRECEIVED NEW BLADE FROM BHT - DAMAGED. REPLACED WITH NEW BLADE FROM BHTSDR CA980504001Blade · cracked(CAN) BLADE CRACKED ON BOTH SKINS AT 77.25 INCHES FROM TIP T/E. CRACK IS 15 INCHES CHORDWISE FORWARD FROM TRAILING EDGE THEN INBOARD 9 INCHES TOP AND BOTTOM.SDR 98ZZZX1493Washer · brokenDURING PRE-FLIGHT INSPECTION, PILOT FOUND THE WASHER UNDER THE NUT OF THE BLADE RETENTION BOLT WAS CRACKED. UPON REMOVAL OF NUT, IT WAS FOUND COMPLETELY BROKEN. WASHER WAS REPLACED AND AIRCRAFT RELEASED FOR FLIGIHT.SDR HEEA0013656Tip Cap · defectiveBOTH INTERNAL DOUBLERS HAVE RIVETS INSTALLED.SDR 99ZZZX39Blade · debondedDISCOVERED DURING DAILY INSPECTION, TRIM TAB DEBONDED AND WASHED OUT.SDR HEEA0013507Blade · defectiveBLADE WAS REPAIRED NEAR THE MIDSPAN TAB WHICH HAS CAUSED THE TIP TO EXCEED THE MAX WEIGHT LIMIT BY 161 GR.SDR HEEA0013506Blade · crackedM/R BLADE NOSE AND NECK SHELL CRACKED AND SEPARATED.SDR HEEA0013505Blade · crackedM/R BLADE NOSE AND NECK SHELL CRACKED AND SEPARATED.SDR HEEA0013454Blade · separationFIBERGLASS SEPARATED UNDERNEATH THE SLICE TITANIUM AT STATION 112.5 ON BOTH SURFACES. THE TRIM TAB HAS SOME SEPARATION ALSO.SDR HEEA0013424Bearing · wornBEARING HAS EXCESSIVE RUBBER WEAR.SDR 98ZZZX1473Bearing · crackedNOTICED BLUE M/R BLADE PENDULUM ABSORBER SOUNDED ROUGH ON PRE-FLIGHT INSPECTION. SUSPECT CAUSE, LACK OF LUBRICATION.SDR HEEA0013357Blade · crackedM/R BLADE CRACKED.SDR 99ZZZX777Blade · debondedBLADE DEBONDING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
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