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 QMLA2020022752010Blade · crackedWHILE PERFORMING THE A 1640 600 HOUR/12 MONTH HUB AND BLADE INSPECTION THE MECHANIC FOUND TWO SMALL CRACKS ON THE TOP OF THE TRIM TAB WHERE IT MEETS THE TRAILING EDGE OF THE BLADE. P/N 407-015-001-117FM1 S/N A-133. THIS IS ONLY REPAIRABLE BY AUTHORIZED MECHANISDR EVCA20201210001Blade · delaminatedDURING PERIODIC INSPECTIONS MAIN ROTOR BLADE PN: 206-015-001-115 SN: A-7245 TRAILING EDGE WAS FOUND TO BE CRACKED AND DELAMINATED. DELAMINATION SPANS FROM 142 INCHES TO 150 INCHES FROM ROOT END. THE CRACK IS WITHIN THE DELAMINATED AREA AT 146.5 INCHES FROM ROOSDR EVCA20191229002Blade · corrodedRED M/R BLADE S/N: BH468848 HAS ONE SPOT OF CORROSION ON BOTTOM SIDE TRAILING EDGE NEAR OUTBOARD TRIM TAB. REMOVED AND REPLACED MAIN ROTOR BLADE WITH SERVICEABLE.SDR EVCA20191229001Blade · corrodedWHITE M/R BLADE S/N: BH468847 HAS MULTIPLE SPOTS OF CORROSION ON TRAILING EDGE. REMOVED AND REPLACED MAIN ROTOR BLADE WITH SERVICEABLE.SDR 2019FA0000423Blade · dentedDURING A POST FLIGHT INSPECTION A MECHCANIC FOUND A 1/4 X 1/4 INCH DENT IN THE LEADING EDGE OF A MAIN ROTOR BLADE 42 INCHES IBOARD FROM THE TIP OF THE BLADE.SDR EVCA201910100003Blade · corrodedBOTH RED & WHITE MR BLADES HAVE CORROSION IN BLADE PIN RETENTION RECEPTACLES. REMOVED MR BLADE ASSY(S). PN: 206-015-001-115, SN(S) BH482876 & BH482878, AND REPLACED WITH SERVICEABLE MR BLADES PN: 20633000-101, SN(S): A074 & A075. SEE FAA FORM 337 DATED 10/8/2SDR HDNA2019080154341Blade · erodedA SMALL HOLE WAS DISCOVERED AT THE OUTBOARD EDGE OF THE TIP CAP APPROX. ONE INCH ABOVE AND ONE INCH AFT OF BLADE TIE DOWN.SDR CA190801006Blade · delaminated(CAN) WHITE MAIN ROTOR BLADE HAS DELAMINATED BONDING STRAP AT THE BLADE ROOT LEADING EDGE. BLADE REPLACED WITH SERVICEABLE UNIT. (TC# 20190801006)SDR AC2R201907149201Blade · separatedABRASION STRIP SEPARATION.SDR ALGA2019080920199Tab · debondedDURING 50HR INSP OUTBOARD TRIM TAB WAS FOUND TO BE DE-BONDED.SDR CA190611010Blade · delaminated(CAN) WHILE IN CRUISE, IN IMC ON AN IFR FLIGHT FROM AIRPORT TO CANADA, WITH THE INTENT TO BREAK-OFF ON THE APPROACH AND PROCEED HOSPITAL TO DROP OFF OUR PATIENT, THE FLIGHT CREW EXPERIENCED A NOISE THEY BELIEVED WAS LIKELY EMITTING FROM THE MAIN ROTOR. OVER THSDR QMLA2019060819054Blade · delaminatedWE DEPARTED AT NIGHT, IFR, ON AN IFT. MADE IT TO THE SENDING HOSPITAL NO ISSUES. WE TOOK OFF FROM THE HOSPITAL TO OVERFLY THE AIRPORT AND PICK UP OUR IFR CLEARANCE TO RECEIVING. I HEARD SOME WHISTLING IN THE ROTOR SO I OPTED TO DOUBLE CHECK THE EROSION STRIPS SDR 9EKA201906075003Blade · erodedDURING CRUISE, HEAVY VIBRATION FELT ON AIRCRAFT. THE AIRCRAFT MADE A PRECAUTIONARY LANDING OFF FIELD. ON INSPECTION, TIP CAP OF MAIN ROTOR BLADE SPLIT AND PEELED BACK. THERE APPEARED TO BE EROSION IN THE SANDY ENVIRONMENT.SDR CA190528020Blade · damaged(CAN) DURING A ROUTINE DAILY INSPECTION OF A BELL 206L-4 THE PILOT/ENGINEER NOTED THAT A COVER PLATE ON THE BOTTOM OUTBOARD END OF ONE OF THE MAIN ROTOR BLADES HAD BECOME DEFORMED AND BULGED AWAY FROM THE BLADE. UPON CLOSER INSPECTION IT WAS NOTED THAT IT LOOKSDR CA190506015Boot · leaking(CAN) PILOT CALLED AND REPORTED EXCESSIVE OIL ON THE MAST COVER ON THE AIRCRAFT. THE PILOT WAS INSTRUCTED TO WIPE THE BOOT AT THE BLADE AREA AND MORE DROPS CAME OUT. PILOT WAS INSTRUCTED NOT TO FLY ANYMORE. MAINTENANCE WAS DISPATCHED AND THE BLADE ASSEMBLY WASSDR CHIA201904253851Shaft · crackedDURING 100 HOUR ROTOR SHAFT IN SERVICE NDT INSPECTION, FOUND CRACK INDICATION AT THE #1 PIN HOLE IN EXCESS OF 50% FSH. THIS VERT SHAFT WAS REMOVED AND SENT TO RS CHIR823C FOR FURTHER EVALUATION ON SWO-046059-19. CRACK INDICATION HAS BEEN CONFIRMED USING BOTH NSDR CA190410019Blade · debonded(CAN) ON MARCH 25 2019, DURING AN ENGINEER WALK AROUND, WE FOUND BOTH VAN HORN MAIN ROTOR BLADE TRIM TABS DEBONDED, THE DEBONDS WERE FOUND ON THE LOWER PORTION OF THE BLADES AND EXTENDING 1.5 INCHES FROM THE INBOARD EDGE OF THE TABS. THERE IS NO INSPECTION OR SDR CHIA201904163775Shaft · crackedDURING THE 100HR AFT VERT SHAFT IN SERVICE INSPECTION OF THE UPPER PINS THE MAINTENANCE CREW GOT A READING OF A SUSPECT CRACK IN PIN 17. DUPLICATED DISCREPANCY MULTIPLE TIMES AFTER RE-CAL'ING MIZ AND USING DIFFERENT PROBES AND EVEN A SECOND MIZ TO CONFIRM. THISDR CA190409008Blade · mismanufactured(CAN) UPON INSTALLATION OF A SET OF NEW MAIN ROTOR BLADES IT WAS DISCOVERED THE ALIGNMENT PIN WAS MISSING FROM ONE OF THE NEW BLADES. PART NUMBER 206-010-200-151 AND COULD NOT BE INSTALLED ONTO THE AIRCRAFT. AFTER CONTACTING THE BELL TECHNICAL REP. HE THEN DIRSDR 2019FA0000075Blade · crackedTHE BOTTOM SKIN OF THE MAIN ROTOR BLADE HAS A 4 1/2 INCH CRACK STATING AT THE TRAILING EDGE AND PERPENDICULAR TO SPAN 57 1/4 INCHES IN FOR BLADE TIP.SDR QMLA2019012419013Abrasion Strip · debondedDURING PREFLIGHT OF AIRCRAFT, MAIN ROTOR BLADE P/N 709-0104-01-101 S/N L173 WAS FOUND WITH A 3-4 INCH SECTION OF THE LEADING EDGE ABRASION STRIP HAD BECOME UNBONDED ON THE MOST INBOARD LOWER SIDE OF THE ABRASION STRIP.SDR QMLA2018122618136Blade · contaminatedPILOT REPORTED THAT OVER THE PREVIOUS DAYS THERE WERE ICICLES FORMING ON THE YELLOW MR BLADE TIP, MORE SO THAT THE OTHER 2 BLADES. PILOT REPORTED THAT HE BECAME SUSPICIOUS AND MORE CLOSELY INSPECTED THE BLADE CAP AREA. THE PILOT REPORTS THAT HE WAS ABLE TO FORSDR 2018FA0000532Blades · corrodedDURING THE EXECUTION OF THE 100FH / IAM INSPECTION OF SAID AIRCRAFT, THE MECHANIC OBSERVED THAT THERE WAS A BUBBLE LOCATED NEAR THE LEADING EDGE OF THE MAIN ROTOR BLADE OF PN C016-7 AND SN 8048 WITH 64H SINCE NEW.....THIS PROBLEM IS OCCURRING WITH SEVERAL BLADSDR QMLA2018121118131Blade · damagedDURING PREFLIGHT OF AIRCRAFT, MAIN ROTOR BLADE P/N 709-0104-01-101 S/N A5-0111 WAS FOUND WITH A 4 INCH SECTION OF THE TIP CAP LEADING EDGE THAT IS DAMAGED/CRACKED.SDR HDNA2018070940817Blade · crackedMAIN ROTOR BLADE HAS CRACK LOCATED ON BOTTOM SIDE 15 INCHES INBOARD OF THE TIP THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.SDR HDNA2018070930817Blade · crackedMAIN ROTOR BLADE HAS CRACK LOCATED ON THE TOP SIDE 35.5 INCHES OUTBOARD OF THE CUFF THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.SDR HDNA2018070920817Blade · crackedMAIN ROTOR BLADE HAS CRACK LOCATED ON BOTTOM SIDE 48 INCHES OUTBOARD OF THE CUFF THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.SDR HDNA2018070910817Blade · crackedMAIN ROTOR BLADE HAS CRACK LOCATED ON THE TOP SIDE, 104 1/8 INCHES OUTBOARD OF THE BLADE CUFF THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.SDR HDNA201806060451Blade · crackedMAIN ROTOR BLADE HAS A 3 INCH L SHAPED CRACK ON THE TOP SIDE OF THE BLADE LOCATED 39 INCHES OUTBOARD OF THE BLADE CUFF.SDR HDNA2018050100007Cuff · crackedYELLOW MAIN ROTOR BLADE CUFF CRACKEDSDR QMLA2018040918043Blade · cracked1.5 INCH CRACK FOUND ON TRAILING EDGE OF BLADE FAIRING. CRACK STARTS AT 60MM FROM TOP OF BLADE FAIRING AND RUNS DOWN AND UNDERNEATH BLADE.SDR 2018FA0000123Tab · damagedA SEGMENT OF THE TRIM TAB OF A MAIN ROTOR BLADE WAS LOST DURING FLIGHT. THE TRIM TAB WAS REPAIRED 201FHRS BEFORE THIS WAS DETECTED. THE SITUATION WAS DETECTED DURING A 100HRS INSPECTION. REPAIRED THE MAIN ROTOR BLADE BASED ON AN ENGINEERING DISPOSITION FROMSDR QMLA2017101117106Blade · crackedCRACK IN THE INBOARD LEADING EDGE EROSION PROTECTIVE SHELL AT THE SPLICE JOINT, UNDER THE PU TAPE. THIS WAS FOUND DURING A SCHEDULED MAINTENANCE EVENT. THE AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION AWAITING REPLACEMENT MAIN ROTOR BLADES.SDR ALGA2017101143701Skin · separatedMAIN ROTOR BLADE SKIN SEPARATED IN FLIGHT. MISSING SKIN SECTION IS LOCATED 61 INCHES FROM BLADE ROOT. IT IS APPROX. 27 INCHES LONG AND 13.5 INCHES WIDE. NO OTHER COMPONENTS WERE DAMAGED.SDR ALGA2017101243723Tab · missingMISSING MAIN ROTOR BLADE TRIM TAB, DISCOVERED DURING POST FLIGHT INSPECTION.SDR QMLA2017082517084Blade · crackedDURING PREFLIGHT, AIRWORTHINESS CHECK, FOUND CRACKS ON THE MAIN ROTOR BLADES. INSTALLED IN THE BLUE & YELLOW POSITION.SDR 2017FA0000386Blade · damagedNUMBER 4 MAIN ROTOR TIP DETACHED DURING FLIGHT. ACFT LANDED SAFELY ON GROUND. TAIL ROTOR HUB, MAIN ROTOR HUB AND ALL FOUR MAIN ROTOR BLADES REMOVED AND SENT TO MANUFACTURER FOR FURTHER INSPECTION.SDR HDNA201706220001Blade · crackedDURING INSPECTION AFTER THE REMOVAL OF THE MAIN ROTOR BLADES A CRACK WAS FOUND ON BLADE P/N B621M1002103 S/N 1662,TOP SIDE OUTWARD TIP. GOING FROM THE LEADING EDGE AROUND THE CONTOUR OF THE BLADE TIP TO THE TRAILING EDGE, APPROX 6 IN IN LENGTH.SDR JYDR20170609239Blade · crackedMAIN ROTOR BLADE WAS REMOVED FOR BIM INDICATION. BLADE INSPECTED AND A 2.3 INCH CRACK WAS FOUND ON THE SPAR, ON BOTTOM OF BLADE, UNDER POCKET 17, 167.25 INCHES FROM ROOT END.SDR 9EKA20170527002Erosion Shield · debondedDURING PREVENTATIVE TOUCH UP PAINT ON MAIN ROTOR BLADE, DISCOVERED LOWER BLADE EROSION PLATE DEBONDED AT BOND LINESDR 8HBR20170317001Blade · flakingBLADE PAINT CHIPPING AND FLAKING, SPECIFICALLY AFTER AIRCRAFT HAS FLOWN DURING RAINY CONDITIONS. ROTOR BLADE BOND LINE EXPOSED AND BOND LINE SEALANT SEPARATING FROM BLADE, REQUIRING RESEALING OF ROTOR BLADE BOND LINE.SDR ALGA0104201741171Blade · crackedA NINE INCH LONG CRACK ON MAIN ROTOR BLADE BETWEEN STATIONS 166 - 173.SDR 2017F00027Blade · failedDURING CLIMB 850 FEET, LATERAL VIBRATION CAME. LANDING PROCEDURES, AFTER VISUAL INSPECTION MAIN ROTOR BLADE TIP CAME OUT. AFTER DEEP INSPECTION AT HOME BASE, TELL-TALE WEIGHT SHEARED OFF INSIDE THE SPAR. CAUSING BLADE UNSERVICEABLE AFTER THIS EVENT.SDR HEER20160801932Abrasion Strip · departedEROSION STRIP DEPARTED AIRCRAFT. PN FOR ABRASION STRIP IS FOUND IN THE SPECIAL INSTRUCTIONS NN 92-097, PAGE 5. REPLACED MAIN ROTOR BLADE.SDR 39LA20160728164Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.SDR 39LA20160728163Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.SDR 39LA20160728162Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.SDR 39LA20160728161Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.SDR DCGA2016071800332Blade · delaminatedFOUND DELAMINATION ON MAIN ROTOR BLADE STAINLESS STEEL LEADING EDGE.SDR DCGA2016FA0000261Blade · dentedDAMAGE WAS FOUND IN AREAS A AND H ON 4 OF THE 5 MAIN ROTOR BLADE BOTTOM SKINS APPROXIMATELY 6" FROM THE BLADE TIPS. MAINTENANCE DETERMINED IAW CSP HMI-2 MM THAT IT WAS REPAIRABLE DAMAGE AND NO SUDDEN STOPPAGE INSPECTION WAS REQUIRED. AFFECTED BLADES WERE REM
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