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 ERAA078458Blade · damagedINSPECTION DUE TOP SKIN 1/3 DOWN LENGTH OF BLADE FROM ROOT, VOIDED AREA AS MARKED, EDGES OF INBOARD TAB POPPED UP. ESTANE BOOT DAMAGED, LOWER SURFACE GRIP VOID, INBOARD TRIM TAB VOID WITH GLASS DAMAGE, INBOARD ABRASION STRIP TANG VOID UPPER AND LOWER SURFACESDR HEEA078336Blade · crackedMAIN ROTOR BLADE LEADING EDGE EROSION STRIP AT INBOARD END OF TOP WEIGHT POCKET CRACKED.SDR HEEA078335Blade · crackedMAIN ROTOR BLADE IS CRACKED.SDR HEEA078334Blade · crackedMAIN ROTOR BLADE IS CRACKED.SDR HEEA078211Bolt · damagedMAIN ROTOR BLADE BOLTS HAS PLATING MISSING AT LOWER END OF BOLT SHANK.SDR R7MR34739Blade · damagedMAIN ROTOR BLADE, DAMAGED TO PITCH HORN BUSHINGS (PN L621M1010232). DAMAGED TO PITCH HORN BUSHINGS PNL621M1010232. AEC TECHNICAL SERVICES ADVISED US THAT THE WEAR IS CAUSED BY IMPROPER TORQUE OF THE UPPER HEX BOLT HARDWARD. REPLACED WITH LOANER UNIT, CORRECSDR EGR2002F00002Blade · damagedDURING MAIN ROTOR COAST DOWN, AFTER ENGINE SHUT DOWN ON THE HOSPITAL ROOF HELIPAD AT APPROX 40 PER CENT NR ONE MAIN ROTOR BLADE CONTACTED AND DAMAGED BOTH VERTICAL STABILIZER. THIS IS A DESIGN FLAW. IN HIGH AND GUSTY WINDS WITH LOW ROTOR SPEEDS, DURING STARSDR HEEA077857Blade · corrodedEROSION SHIELD WORN. BLADE CORRODED. FILLER MISSING. NEED PAINTING.SDR HEEA077856Erosion Shield · wornEROSION SHIELD WORN. CORRODED. FILLER MISSING. NEED PAINTING.SDR HEEA077855Erosion Shield · corrodedEROSION SHIELD WORN AND CORRODED. FILLER MISSING.SDR HEEA077854Erosion Shield · corrodedMAIN ROTOR BLADE EROSION SHIELD WORN AND CORRODED. FILLER MISSING. NEED PAINTING.SDR HEEA077840Doubler · separatedNR 2 LOWER DOUBLER SEPARATED APPROXIMATELY 4 1/2 INCHES LONG WHICH EXTENDS UNDERNEATH THE NR 3 FINGER.SDR CA020208003Washer · cracked(CAN) 2060101543 WASHER WAS USED ON A BLADE BOLT WITH A NAS1022A14 NUT. THE NUT IS A SMALLER NUT AND TENDS TO COVER ONLY 2/3 OF THE AREA OF THE WASHER. THE TORQUE REPETITIVE TORQUE CYCLES OVER TIME AND THE CUPPING OF THE WASHER CAUSED IT TO CRACK IN 3 PLACESDR 2002F00314Pin · wornBLADE ASSEMBLY PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M)SDR AUS20011350Blade · cracked(AUS) MAIN ROTOR BLADE CRACKED.SDR R7MR34297Blade · debondedBLADE MR 407(HIGH VISIBILITY), DEBONDING UNDER EROSION STRIP, NEAR BLADE TIP. REPLACED WITH USED BLADE CORRECTED PROBLEM.SDR JYD2002F00000Spar · crackedCRACK WAS FOUND ON THE TIP END OF MAIN ROTOR BLADE SPAR (PN 641520504102/ SN 64-65325910). DURING POST FLIGHT INSPECTION, FIELD CREW VISUALLY DETECTED A CRACK INDICATION ON TOP SIDE OF SPAR. TOTAL CRACK LENGTH IS APPROX. 2 INCHES LONG WITH 1.5 INCHES EXTENDSDR HEEA077391Blade · delaminatedLAMINATE AT STA 44 ON THE LOWER SIDE IS SEPARATED. .SDR HEEA077390Tab · splitMAIN ROTOR BLADE TRIM TAB IS SPLIT OPEN NEAR THE TIP OF THE BLADE.SDR HEEA077389Rib · debondedMAIN ROTOR BLADE TIP RIB UNBONDED.SDR HEEA077388Blade · mismanufacturedUNABLE TO INSTALL TIP CAPS - TWO DIFFERENT TIP CAPS. TIP CAP BLOCK HOLES APPEAR TO BE DRILLED 1/8 INCH TOO FAR FORWARD WHEN AFT SCREWS INSERTED.SDR AUS20011292Blade · cracked(AUS) BLUE MAIN ROTOR BLADE CRACKED AT THE ROOT END TRAILING EDGE.SDR AUS20011330Blade · cracked(AUS) MAIN ROTOR BLADES SUSPECT CRACKED.SDR ERAA077297Skin · damagedREMOVED FOR FLIGHT CHARACTERISTICS BLADE HAS CREASES UPPER AND LOWER, PAINT WORK NEEDED. L/S HAS SKIN DAMAGE WITH VOID AT STA 192-194, T/B AND CTR TRIM TABS HAVE SKIN DAMAGE WITH VOIDS, WATER FOUND IN CORE DURING BOND PREP FOR PATCHES, UPPER SURFACE SKIN DAMASDR HEEA077200Tip Cap · mismanufacturedUNABLE TO INSTALL TIP CAP, SCREW HOLES DO NOT LINE UP.SDR CA011119004Blade · cracked(CAN) DURING AIRFRAME PERIODIC INSP 3.5 INCH DIAGNAL CRACK ON LOWER SKIN OF SUBJECT BLADE FOUND AT BLADE STATION 71.0-73.0.ATTEMPTS TO DRESS OUT CRACK WITH LIGHT SANDING REVEALED SUSPECT LACK OF FIBERGLASS MATTING USED IN CONSTRUCTION OF BLADE TYPE. EVIDENCED SDR HEEA076943Blade · damagedTRAILING EDGE DAMAGE AT AREA OF P/N - S/N STENCIL. REPLACED WITH SERVICEABLE BLADE.SDR HEEA076942Blade · crackedTRAILING EDGE CRACKED JUST INBOARD OF TRIM TAB. REPLACED WITH SERVICEABLE BLADE.SDR HEEA076941Blade · crackedLEADING EDGE TITANIUM STRIP HAS A COMPLETE CHORDWISE CRACK WITH MULTIPLE BRANCH WHICH EXTENDS BEYOND LIMITS. PENDING VENDOR REPAIR.SDR HEEA076940Tip Cap · crackedFIBERGLASS SKIN NEAR THE TRAILING EDGE IS CRACKED AND HAS SOME SEPARATION NEXT TO THE ABRASION STRIP. PENDING VENDOR REPAIR.SDR HEEA076939Tip Cap · crackedOUTER DOUBLER ON LOWER SIDE CRACKED AND HAS "C" CHANNEL DEBONDED. PENDING VENDOR REPAIR.SDR CA011108001Blade · cracked(CAN) DURING INSPECTION A CRACK WAS FOUND ON THE LOWER SURFACE OF THE BLADE AT STN. 1003. CRACK LENGTH WAS APPROXIMATELY 155.52 MM STARTING 111.46 FROM THE LEADING EDGE TRAVELLING CORDWISE TO 33.02 MM FROM THE TRAILING EDGE.SDR HEEA076557Blade · crackedMAIN ROTOR BLADE CRACKED AT OUTBOUND TRIM TAB.SDR ERAA076665Blade · debondedBLADE IS DEBONDING ON LEADING EDGE. POTTING NEEDS CHANGING. ALL ABRASI9ON STRIPS VOID SCARF JOINT, NR 1 ABRASION STRIP ERROSION NOSE AND NECK SHELL CRACKED AT FITTING, SKIN AT ROOT AREA CRACKED ROVING FILLER SEPERATED, UPPER SURFACE AT TRAILING EDGE, DAMPNESDR ERAA076664Blade · debondedBLADE IS DEBONDING ON LEADING EDGE. POTTING NEEDS CHANGING NOSE AND NECK SHELLS CRACKED @ NECK DOWN AREA, SKIN CRACK AND VOIDED @ NECK AREA, TEFLON MISSING FROM MAIN BUSHING, DRAG BUSHING HAS FRAYED AND MISSING TEFLON, DAMPNER WRAP VOID LOWER SURFACE, ALL ABRSDR ERAA076663Blade · debondedM/R BLADE IS DEBONDED. LEADING EDGE DEBONDING, POTTING NEEDS CHANGING. ACTION TAKEN: ALL ABRASION STRIPS VOID, HEAVY ERROSION ON ABRASION STRIP, P.U. FILM DETERIORATION, PAINT PEELING, HARDWARE CORRODED SWEEP OUT -13.21MM, NOSE AND NECK SHELLS CRACKED SKINSDR ERAA076658Bolt · wornPRIMARY BLADE BOLTS HAS WORN PLATING. ACTION TAKEN : CLEANED & C/W VISUAL & NDT INSPECTION. SCRAPPED 3 BOLTS DUE TO MECHANICAL DAMAGE. THIS INFORMATION FOR FAA SDR.SDR HEEA076470Blade · damagedLEADING EDGE EROSION. REPLACED WITH SERVICEABLE BLADE.SDR HEEA076469Blade · damagedUNABLE TO TRACK. REPLACED WITH SERVICEABLE BLADE.SDR HEEA076394Blade · crackedMAIN ROTOR BLADE IS CRACKED.SDR IVSA076105Blade · crackedBLADE REMOVED FOR REPAIR OF LEADING EDGE ABRASION STRIP CRACKS. CUSTOMER REQUESTED EXCHANGE BLADE IN ORDER TO RESUME FLIGHTS. EXCHANGE BLADE INSTALLED, REPAIRABLE BLADE RETURNED TO AECSDR ALG2001F00031Spar · corrodedDISCOVERED DURING ROUTINE MAINTENANCE INSPECTION. SPAR EXFOLIATION WAS DETECTED ON LOWER SURFACE SKIN/SPAR SPLICE JOINT, CONSIDERED A MATERIAL DEFECT. BLADE WAS REMOVED FROM SERVICE AND SCRAPPED.SDR 2001FA0000553Blade · crackedM/R BLADE WAS RECD AT MFG FOR INSP AND EVAL. ABR STRIP CRACK WAS ID AT BLADE STAT 2305. PORTION OF ABR STRIP WAS REMOVED TO ALLOW EVAL OF UNDERLYING SURFACE. SKIN WAS CRACKED WITH DELAM SURROUNDING AREA. REVIEW OF BLADE RECORDS INDICATE MFG REPAIR ON INNERSDR 2001FA0000451Blade · delaminatedM/R BLADE WAS RECEIVED FOR INSP AND EVAL. ABRASION STRIP CRACK WAS IDENTIFIED AT BLADE STATION 2305. PORTION OF ABRASION STRIP WAS REMOVED TO ALLOW EVALUATION OF UNDERLYING SURFACE. SKIN WAS ALSO CRACKED WITH DELAMINATION SURROUNDING AREA. REVIEW OF BLADE SDR HEEA075972Blade · delaminatedDELAMINATION NEAR BLADE TIP.SDR HEEA075952Blade · crackedLARGE CRACK BY MID TRIM TAB. REPLACED WITH SERVICEABLE PART.SDR CA010913001Trim Tab · debonded(CAN) DURING SCHEDULED AIRFRAME PERIODIC INSP TRIM TAB ON PARTICULAR MAIN ROTOR BLADE FOUND TO HAVE SEVERE DEBONDING WHICH INITIALLY SHOWED UP AS CRACKS IN FILLER MATERIAL AROUND TRIM TAB EDGES. CLOSER INSP REVEALED SEVERE DEBONDING & COMPROMISE OF TRIM TAB ATSDR 2001F00558Blade · corrodedDISCOVERED DURING ROUTINE AIRFRAME INSPECTION, TRAILING EDGE EXTRUSION EXFOLIATED AT STATION 65.5. REPLACED MAIN ROTOR BLADE. TOTAL DAMAGE AREA APPROXIMATELY .5 INCH WIDE BY .75 INCH LONG. (M)SDR CA010907007Pin · sheared(CAN) WHILE CARRYING OUT HIS DAILY INSPECTION, THE PILOT NOTICED THE NUT LOOSE ON THE BLADE PIN UPON INSPECTION THE THREADED PORTION OF THE BLADE PIN WAS SHEARED.SDR CA010831010Main Rotor · cracked(CAN) 1 1/2"- 2" CHORDWISE CRACKS IN LOWER ROOT DOUBLER ADJACENT TO OUTBOARD END OF ROOT END FITTING. TWO BLADES FROM SAME SET WITH SIMILAR CRACKS S/N'S 009999-K068,-K070. *TORQUE EVENTS CALCULATED BY TSNX20 (REF: BOEING SERVICE BULLETIN SB 369D195R3)
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