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 HEED95396Tip Cap · separatedTRAILING EDGE SEPERATED. REPLACED UNITSDR 95ZZZX6889Tip Cap · crackedDURING 500-HOUR M/R INSPECTION, CRACK FOUND AT HOLE ON UPPER INNER CRESCENT DOUBLER. COMPONENT NR 7615009100051.SDR 95ZZZX6888Tip Cap · debondedFOUND AT 500-HOUR INSPECTION, INNER CRESCENT DOUBLER DEBONDED UNDER C-CHANNEL. COMPONENT MODEL NR 7615009000049.SDR HEEA956004Blade · bushing shiftTHE BUSHING SHIFTED UPWARD.SDR 96ZZZX3578Blade Pin · wornBLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 95ZZZX6206Erosion Shield · separatedIN CRUISE FLIGHT OVER THE GULF OF MEXICO, THE AIRCRAFT DEVELOPED A SEVERE VIBRATION. THE PILOT MADE AN IMMEDIATE PRECAUTIONARY LANDING TO AN OFFSHORE DRILLING PLATFORM. EXAMINATION OF THE AIRCRAFT REVEALED THE LOWER EROSION SHIELD ON A MAIN ROTOR BLADE HAD SSDR HEEA955932Strip · worn excessivelyPROTECTION STRIP WORN OFF.SDR 95ZZZX6961Blade Pin · scoredSCORED BLADE PIN. REMOVED AND REPLACED.SDR 95ZZZX6960Bushing · wornINSIDE COATING WORN ON BUSHING. TOTAL OF 8 EACH. SEE MMIR 78451, 78452, AND 78453. REMOVED AND REPLACED.SDR CA951108009Blade · debonding(CAN)M/R BLADE LEADING EDGE ABRASION STRIP DEBONDED.SDR HEEA955869Blade · pittedBLADE HAS A BUSHING PITTED BEYOND LIMITS.SDR HEEA955868Blade · crackedSEVERAL CRACKS IN THE TITANIUM LEADING EDGE STRIP, BUT THE CRACK AT STATION 173" HAS IN EXCESS OF 2.5 INCHES OF SEPARATION. THE INBOARD END OF THE NICKEL STRIP HAS APPROX. 13" OF SEPARATION.SDR HEEA955864Blade · corrodedEXCESSIVE AMOUNT OF EXFOLIATION ON UPPER LEADING EDGE NEAR THE TIP WITH PIECES MISSING.SDR HEED95360Tip Cap · seoarationTRAILING EDGE SEPERATION. REPLACE UNITSDR HEEA955834Blade · crackedBLADE NOSE AND NECK SHELL CRACK IN THE ROOT AREA. FIBERGLASS IN THE ROOT AREA ALSO DISCOLORED AND SEPARATED FROM THE ROVINGS.SDR HEEA955831Tip Cap · crackedBLADE CRACK WITH MULTIPLE BRANCHES ON THE LEADING EDGE ABRASION STRIP.SDR 95ZZZX5920Blade · bearing looseDURING 25-HOUR INSPECTION, DISCOVERED THE M/R BLADE DAMPER ATTACH BEARING (369A7951-15) WAS QUITE LOOSE. BLADE WAS REMOVED, REPAIRED, AND REINSTALLED.SDR HEED95355Tip Cap · separationSEPARATION ON OUTBOARD TRAILING EDGE. REPLACE UNITSDR HEED95354Tip Cap · separationSEPARATION ON OUTBOARD TRAILING EDGE. REPLACE UNITSDR HEEA955813Tip Cap · crackedCRACKED ABRASION STRIP WITH MULTIPLE BRANCH. IT ALSO HAS EXCESSIVE EROSION OF FIBERGLASS NEAR THE TIP.SDR 95ZZZX6088Blade · delaminatedON PRE-FLIGHT, THE ABRASION STRIP WAS FOUND DELAMINATING. FOUND A BUBBLE, .75 INCH WIDE RUNNING AT AN ANGLE FROM THE LEADING EDGE AT STA 135.0 TO THE TRAILING EDGE OF THE ABRASION STRIP AT STA 145.0. PART REMOVED AND SENT IN FOR REPAIR (THIS IS ON THE BOTTOMSDR HEEA955792Blade · cracksNOSE AND NECK SHELL CRACKS.SDR HEEA955775Blade · corrodedBLADE HAS SEVERAL AREAS OF INNER GRANULAR CORROSION ON THE LEADING EDGE SPAR NEAR THE INBOARD SECTION OF THE BLADE.SDR GMAL9509143Blade · crackedMAIN ROTOR BLADE FOUND CRACKED. CRACK LOCATED AT 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. ACFT TOTAL TIME, 566 HOURS, 3 BLADES FOUND CRACKED AT SAME TIME. SDR GMAL9509141Blade · crackedMAIN ROTOR BLADE FOUND CRACKED. CRACK LOCATED AT STA 174, CORDWISE ON BOTTOM OF BLADE AT 10 INCHES LONG, 5 INCHES AFT OF LEADING EDGE. ONLY 4 HOURS OF FLIGHT SINCE LAST INSPECTION. AIRCRAFT TOTAL TIME 566 HOURS. THREE BLADES FOUND CRACKED AT SAME TIME. (XSDR HEEA955656Blade · defectiveBOLT BUSHING PITTED BEYOND THE MAX. LIMIT OF 1.524".SDR HEEA955653Blade · crackedNOSE AND NECK SHELL CRACKED IN THE ROOT AREA. ALSO HAS A SMALL AREA OF SEPARATION NEAR THE TIP ON THE LEADING EDGE STRIP.SDR HEEA955643Tip Cover Assy · defectiveCOVER HAS PREBOND MATERIAL MISSING ALONG THE LEADING EDGE SURFACES.SDR 95ZZZX6498Bracket · defectiveVIBRATION ABSORBER WASHER UNDER BOLT HEAD DOES NOT LAY FLAT ON MOUNT FLANGE AT LEADING END OF BRACKET.SDR 96ZZZX3168Blade · debondedDAILY INSPECTION FOUND OUTBOARD SKIN AT TIP OF BLADE DEBONDED (TOP SIDE). PART DEBONDED BEYOND REPAIR.SDR 95ZZZX5091Fitting · leaksFITTING WAS INSTALLED ON NEW GRIP, PN 206-011-132-113A, SN A-5845. GRIP INSTALLED 8-2-95 AT 6008.2 HOURS ACFT TT. ON 8-11-95, 6011.0 HOURS ACFT TT. THE GREASE FITTING HAD LEAKED A LARGE AMOUNT OF GREASE (30 PERCENT OF TOTAL AMOUNT ONTO HUB). FITTING REPLACSDR 95ZZZX4273Blade · paint peelBLADE HAD RETURNED FROM REWORK RECENTLY AND SINCE INSTALLATION 90.9 HOURS AGO, 3 SECTIONS ON THE BOTTOM OF THE BLADE HAVE BEEN STRIPPED OF PAINT IN SHEETS ABOUT 75 SQUARE INCHES OF AREA EXPOSED AFFECTING THE LATERAL BALANCE OF THE ROTOR SYSTEM.SDR HEEA955364Blade · crackedCRACK ON THE LEADING EDGE NEAR THE TIP IN A CHORDWISE DIRECTION.SDR 95ZZZX5732Blade · crackedCRACK AROUND AFT WASHER OF M/R BLADE TIP CAP. REPLACED WITH SERVICEABLE.SDR HEED95275Blade · separationSKIN SEPERATION ON M/R BLADE TOP ARE AT ALL SIKORSKY TOOLING HOLES STATION 72.06, 121.50, AND 186.50. ORDER REPLACEMENT PARTSDR HEEA955348Blade · crackedNOSE AND NECK SHELL CRACKED IN ROOT END AREA.SDR HEEA955347Tip Cap · crackedFIBERGLASS SKIN BROKEN BETWEEN THE INNER AND OUTER DOUBLER ON BOTH SURFACES.SDR 95ZZZX4419Blade · crackedDURING 500-HOUR INSPECTION, FOUND CRACK IN SPAR ORIGINATING FROM ROOT END BUSHING HOLE. COMPONENT P/N 7600009300013.SDR 95ZZZX4418Blade · crackedDURING 500-HOUR INSPECTION, FOUND CRACK IN SPAR ORIGINATING FROM BUSHING HOLE. COMPONENT P/N 7600009300013.SDR HEEA955298Blade · crackedCRACK IN SKIN ON TOP APPROXIMATELY 5'9" OUTBOARD OF ATTACH POINT.SDR HEEA955297Blade · crackedCRACK IN SKIN ON TOP APPROXIMATELY 6'8" OUTBOARD OF ATTACH POINT.SDR HEEA955229Blade · separationNOSE SHELL SEPARATED NEAR THE LEADING EDGE STRIP.SDR 95ZZZX5726Blade · skin deformedBLADE FAILED INSPECTION FOR SKIN DEFORMATION AND LOOP ROVING. BLADE IS LOCATED AT CTI.SDR 95ZZZX5725Blade · skin deformedBLADE FAILED INSPECTION FOR SKIN DEFORMATION AND LOOP ROVING. BLADE IS LOCATED AT CTI.SDR HEEA955211Blade · crackedM/R BLADE CRACKED AT STATION 1810.SDR 95ZZZX3925Blade · doubler separateOUTBOARD UPPER SPAN DOUBLER SEPARATED FROM BLADE IN-FLIGHT. DOUBLER WAS REPLACED 2/91. TT SINCE REPAIR, 820 HRS.SDR HEEA955196Blade · separationSKIN SEPARATION ON THE UPPER SURFACE NEAR THE TIP. THE SEPARATION IS NEARLY 32 INCHES SPANWISE BY 3 TO 4 INCH CHORDWISE. BLADE IS ALSO UP FOR TIME EXTENSION.SDR HEEA955190Blade · crackedNOSE AND NECK SHELL CRACKED.SDR HEEA955189Blade · crackedNOSE AND NECK SHELL CRACKED.SDR HEEA955187Blade · corrodedSEVERAL AREAS OF INNER GRANULAR CORROSION ON THE LEADING EDGE SPAR. BLADE HELD IN BLADE SHOP
Back to JASC 6210