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 BAQA092751Blade · out of trackRENTAL 117-151451V001 S/N 2622 RENTAL CHARGE 36.75 HR REPLACEMENT VALVE RETURN OF RENTAL BLADE AFTER .4 HOURS OF USE, WOULD NOT TRACK REPLACED WITH ANOTHER RENTAL BLADE (S/N 2419)SDR BAQA092750Blade · out of trackRETURN OF RENTAL BLADE AFTER .4 HOURS OF USE, BLADE WOULD NOT TRACK. REPLACED WITH ANOTHER RENTAL BLADE (S/N 2413)SDR ALG2004F00011Screw · crackedON DAILY INSPECTION, FOUND THREE SCREW HEADS CRACKED ON THE MAIN ROTOR BLADE TIP CAP INSTALLED ON THE BLUE BLADE. MAINTENANCE REMOVED AND REPLACED THE THREE SCREWS. DURING REPLACEMENT OF THE SCREWS MAINTENANCE FOUND TWO MORE SCREWS WITH CRACKS IN THE WITH NESDR B3O2004F00000Blade · damagedMAIN ROTOR BLADE RECEIVED FROM AEC WITH DAMAGE TO THE TRAILING EDGE OF THE NR 3 TRIM TAB. TRIM TABS RESET AT AEC PRIOR TO RECEIPT AEC WO NR W0078958. BLADE NOT ABLE TO FLY CORRECTLY ON TWO DIFFERENT AC. REQUEST EVALUATION OF BLADE.SDR BAQA093652Bushing · unserviceableINSPECTION REVEALED DAMAGED GRIP AT BUSHINGS. TEFLON LINERS WERE REPLACED BY REP. BLADE DIMENSION TO THICK AT GRIP FOR INSTALLATION AFTER LINERS WERE INSTALLED. SUSPECT GRIP TO THICK TO BEGIN WITH, PREVIOUS LINERS WERE DAMAGED AT BLADE REMOVAL (HARD TO PUSDR BAQA093649Blade · damagedLEAD/LAG IN EXCESS OF 20MM, INSTALLED A/C TT 5145.8, REMOVED AC TT 5146.2 FOR A TOTAL .4 HOURS. RECEIVED BLADE ON EXCHANGE FROM AEC UNDER OUR PO 8-080114-36. WOULD LIKE TO HAVE THIS BLADE BACK AFTER REPAIR, SEEMS TO HAVE A GOOD HISTORY OF BEING ABLE TO STASDR BAQA093648Blade · out of trackBLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. BLADE WAS INSTALLED ON A/C N911TG/7506 FOR A TOTAL OF 2.4 HOURS. BLADE WAS RECEIVED AS AN EXCHANGE, UNDER OUR PO 8-080114-36.SDR BAQA093639Blade · out of trackBLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. BLADE WAS INSTALLED ON A/C N911TG/7506 FOR A TOTAL OF 2.4 HOURS. LAST REPAIR WAS A INSURANCE CLAIM, REF. PO 1-010199-41.SDR BAQA093638Blade · damagedBLADE DIVES IN FORWARD FLIGHT. BLADE WAS INSTALLED .2 HOURS SINCE WE HAD RECEIVED AS AN EXCHANGE UNDER OUR PO 8-080114-10. BLADE HAS ACCUMULATED 106.1 HOURS SINCE 10/23/2001 AND HAS BEEN REPAIRED THREE TIMES IN THAT TIME SPAN WITH THIS BEING THE FOURTH. AIR MESDR BAQA093636Blade · out of trackWARRANTY REPAIR/EXCHANGE : S/N 198 ; BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. SINCE FEBRUARY 21,200 BLADE HAS ACCUMULATED ONLY 279.8 HOURS BUT HAS BEEN REMOVED FROM SIX DIFFERENT AIRCRAFT FOR REPAIR WITH THIS BEING THE SEVENTH TIMSDR JJWA0055059Blade · defectiveINSTALLED 2 NEW BLADES WITH HIGH VISIBILITY PAINT FROM MFG. ABLE TO PERFORM SPAN AND LATERAL BALANCE TO LESS THAN .02IPS. UNABLE TO REDUCE VERTICAL VIBRATION TO ACCEPTABLE LEVELS IN HOVER TO 120 MPH. INSTALLED ANOTHER WARRANTY BLADE AND WAS ABLE TO TRACK TOSDR BAQA093650Blade · damagedEXCESSIVE BLADE LAG, BLADE WAS INSTALLED BUT NEVER FLOWN DUE TO EXCESSIVE LAG. RECEIVED BLADE ON EXCHANGE FROM AEC UNDER OUR PO 8-080103-07, BLADE IS UNSERVICABLE WITH ZERO HOURS ON IT. BLADE HAS ACCUMULATED ONLY 733.4 HOURS ON IT SINCE 09/15/1997 BUT HAS BEENSDR CA040213006Spar · cracked(CAN) MAIN ROTOR BLADE LEAK CHECKED AT BASE AND SPAR FOUND TO BE CRACKED.SDR ERAA095249Blade · corrodedTHIS INFO FOR FAA SDR. BLADE ASSY HAS CORROSION AT C BLOCK TO SPAR BOUND LINE. ACTION TAKEN: SENT TO CTI FOR REPAIR. INSPECTED, PERFORMED X- RAY FOR MOISTURE (FOUND APPROX 50-60 CELLS IN VIEW, E-9) REPLACED C BLOCK PER RS-008G-11, REPLACED SHIMS PER SA404SDR AUS20040010Cap · cracked(AUS) MAIN ROTOR BLADE TIP CAP TOP SKIN CRACKED IN AREA ADJACENT TO THE ATTACHMENT DOUBLER. CRACK LENGTH 270MM (10.62IN). TIP CAP HAD DISBONDED INTERNALLY FROM THE METAL DOUBLER ASSEMBLY AND THE KEVLAR SKIN HAD CRACKED AND DELAMINATED.SDR BAQA092582Blade · contaminatedWATER IN BLADE. REPLACEMENT FOR BLADE NOT RECEIVED YET. BEING REPLACED WITH SERVICABLE UNIT. 02/09/2004SDR MDR03038Spar · crackedTHE BLADE WAS INSPECTED DUE TO A BIM INDICATION IN THE FIELD. DURING THE INSPECTION, A LEAK INDICATION WAS NOTED ON THE BOTTOM SIDE OF THE SPAR BETWEEN POCKETS 5 AND 6. AFTER REMOVAL OF POCKETS 5 AND 6, AND FPI INSPECTION REVEALED A CRACK IN THE SPAR RUNNINGSDR AUS20031206Blade · delaminated(AUS) MAIN ROTOR BLADE UPPER SKIN SUSPECT DELAMINATED. DELAMINATED AREA STARTS APPROXIMATELY 381MM (15IN) IN FROM BLADE TIP TO 1295.4MM (51IN) FROM THE BLADE TIP AND 63.5MM (2.5IN) IN FROM THE LEADINGEDGE. FOUND DURING INSPECTION IAW AD/R44/18.SDR CA040217010Blade · scored(CAN) MAIN ROTOR BLADE BOLT EXTREMELY DIFFICULT TO REMOVE FROM BOTH BLADES/MAIN ROTOR HUB. BOLTS, BLADE BUSHINGS AND MAIN ROTOR GRIPS ALL HAD HEAVY SCORING. CAUSE UNKNOWN. BOLTS SCRAPPED. BUSHINGS REPLACED IN MAIN ROTOR BLADE AT APPROVED FACILITY, AND MAIN ROSDR BAQA091151Blade · will not balanceMAIN ROTOR BLADE WILL NOT BALANCE. REPLACED WITH CANNED UNIT FROM A/C.SDR BAQA091148Blade · will not balanceMAIN ROTOR BLADE WILL NOT BALANCE. INSTALLED CANNED UNITS OFF OF A/C.SDR ERAA093709Tip Cap · crackedABRASION STRIP CRACKED AND DEBONDED ON UPPER SURFACE AS INDICATED C-CHANNEL DEBONDED AS INDICATED. ACTION TAKEN: SENT FOR REPAIR. INSPECTED IAW SA 4047-76-5 REV 11; REPLACED ABRASION STRIP IAW RS-005N-III. MODIFIED EXTERNAL DOUBLERS IAW RS-017-1; INSTALLED SDR ERAA093708Cap · crackedLEADING EDGE ABRASION STRIP AND UPPER OUTER DOUBLER CRACKED. C-CHANNEL DEBONDED AND DAMAGED AS INDICATED. SENT TO FOR REPAIR. INSPECTED IAW SA4047-76-5 REV11; REPLACED ABRASION STRIP IAW RS-005N-III, MODIFIED EXTERNAL DOUBLERS IAW RS-017. INSTALLED STAINSDR CA031107004Attach Fitting · sheared(CAN) BROKEN PIN WAS FOUND ON 100 HOUR INSPECTION. LOCATION WAS AT THE JUNCTION OF SHANK AND THREADS.SDR ERAA092660Tip Cap · crackedLEADING EDGE CRACKED AWAY FROM FIBERGLASS. SENT TO CTI. INSPECTED IAW SA4047-76-5 REV 11; REPLACED ABRASION STRIP IAW RS-005N-III. REPAIRED SKIN AT LEADING EDGE AND DOUBLER JUNCTION IAW RS-005N-X111. REPLACED BOTH FORWARD INTERNAL DOUBLERS AND REB ON D C CHSDR BAQA089526Blade · contaminatedREQUEST WARRANTY REPAIR . WATER IN BLADE. PART HAS ONLY 460.0 HOURS ON IT. REPLACED WITH SERVICEABLE RENTAL.SDR AUS20031233Blade · cracked(AUS) MAIN ROTOR BLADE CRACKED IN BLADE THIMBLE RADIUS AREA. FOUND DURING REMOVAL AND INSPECTION IAW KHI KSB-117-168.SDR AUS20031232Blade · cracked(AUS) MAIN ROTOR BLADE CRACKED IN BLADE THIMBLE RADIUS AREA. FOUND DURING REMOVAL AND INSPECTION IAW KHI KSB-117-168.SDR CA030919002Pin · sheared(CAN) WHEN PIN WAS OPENED TO REMOVE MAIN ROTOR BLADE PIN FELL APART. IT WAS NOTED PIN WAS SHEARED OFF WHERE LAST THREAD WAS CUT.SDR ALGA089096Universal · bindingUNIVERSAL FOUND WORN, BINDING AND RATCHETY. REMOVED AND REPLACED BY FIELD MAINT.SDR ERAA093707Blade · pin holeDURING INSPECTION FOUND PIN HOLDS IN LEADING EDGE BEYOND LIMITS. SENT FOR REPAIR, INSPECTED PERFORMED 2500 HOUR INSPECTIONS IAW MFG 412 MM CHAPTER 5; REPLACED IB AND OB SPLICE COVERS IAW MFG 412 CR AND O PAGE 86B; TRIMMED IB ABRASION STRIP TANG IAW MFG 204-09SDR ALGA089042Blade · defectiveLOWER SURFACE GRIP FINGERS FOUND DEBONDED AT STA.38 - 43.5. DAMAGE APPEARS TO BE MANUFACTURING DEFECT. BLADE ASSY. WAS SENT TO BELL HELICOPTERS FORTWORTH. CUSTOMER PROPERTY RETURN.SDR ALGA089009Blade · defectiveDURING TRACKING PROCEDURE, TRIM TAB FAILED TO REMAIN AT SET POSITION. SHORTLY AFTER SETTING TAB TO REQUIRED POSITION,TAB WOULD RETURN TO +5 DEGREE SETTING. BLADE WILL BE SENT O.O.H FOR WARRANTY REPAIR PER B.H.T.I. P.S.E.SDR HEEA088946Blade · debondedOPEN IN BONDING BETWEEN ROOT AND VIBRATION ABSORBER.SDR CA040413004Blade · damaged(CAN) PIN FAILURE, SHEARED AT TOP THREAD OF THREADED SHANK FOR ADJUSTER NUT.SDR CA030912002Pin · failed(CAN) PIN FAILURE, SHEARED AT TOP THREAD OF THREADED SHANK FOR ADJUSTER NUT. CHIEF ENGINEERS COMMENTS: THIS IS THE SECOND PIN TO SHEAR ON THIS AIRCRAFT, SEEMS BOTH PINS WERE MANUFACTURED ATABOUT THE SAME TIME.SDR 2003FA0000846Blade · crackedCRACKS FOUND IN BOTH MAIN ROTOR BLADES IN THE AREA OF THE CONTROL CUFF/ FLEXBEAM VIEWED FROM THE INSPECTION AND DRAIN HOLES. FLEXING BLADES UP AND DOWN YOU CAN SEE THE CRACK OPEN AND CLOSE. ALSO YOU CAN HEAR AN AUDIBLE CLICKING SOUND.SDR BAQA088681Blade · damagedMAIN ROTOR BLADE HAS MINOR LEAD LAG PLAY. BLADE LASTED ONLY 421.6 HOURS SINCE LAST REPAIR. PART IS ALSO DUE LOOP INSPECTION.SDR HEEA088605Blade · crackedMAIN ROTOR BLADE CRACKED. SHOP REPAIR.SDR CHI2741Blade · crackedWHILE PERFORMING OFF AC INSPECTION OF MAIN ROTOR BLADE, UTILIZING EDDY CURRENT, DISCOVERED ONE CRACK EMANATING FROM FIRST LIGHTING HOLE AT APPROX STA 36.5 IN (C) CHANNEL. SECTION BLADE TO VERIFY EDDY CURRENT FINDINGS. CRACK EXTENDS FROM ID OF LIGHTING HOLE USDR CHI2003F00001Blade · crackedWHILE PERFORMING OFF AIRCRAFT INSPECTION OF MAIN ROTOR BLADE UTILIZING EDDY CURRENT METHOLOGY. DISCOVERED ONE CRACK EMANATING FROM FIRST LIGHTING HOLE AT APPROX. STA 36.5 IN (C) CHANNEL. SECTIONED BLADE TO VERIFY EDDY CURRENT FINDINGS. CRACK EXTENDS FROM ISDR EGR2004F00001Blade · failedMAIN ROTOR BLADE FAILED. CONTINUITY TEST BETWEEN LEADING EDGE AND GROUND STRAP BOLT.SDR AUS20030903Blade · damaged(AUS) M/R BLADE UPPER SKIN TORN IN AREA LOCATED AT BLADE TIP IMMEDIATELY INBOARD OF TIP CAP. INSP FOUND SKIN HAD LIFTED IMMEDIATELY BEHIND SPAR &TORN IN SPAN WISE DIRECTION FROM TIP TO APPROX 50.8MM INBOARD OF TIP & 25.4MM AFT OF SPAR.SKIN & ADHESIVE HAD SEPARSDR MDR03023Blade · crackedTHE BLADE WAS REMOVED FROM THE AIRCRAFT FOR BIM INDICATION. A 10-DAY LEAK CHECK WAS PERFORMED AND A CRACK WAS FOUND IN THE SPAR 117.75 INCHES FROM THE TIP END AND 4.50 INCHES FROM THE LEADING EDGE ON THE BOTTOM SIDE OF THE BLADE. CAUSE: UNKNOWNSDR MDR03022Blade · crackedTHE BLADE WAS REMOVED FROM THE AIRCRAFT FOR BIM INDICATION. A 10-DAY LEAK CHECK WAS PERFORMED AND A LEAK WAS FOUND IN A CRACK IN NR 18 POCKET. AFTER THE POCKET WAS REMOVED AND ADHESIVE WAS CHEMICALLY REMOVED, THE CRACK WAS FOUND 168.75 INCHES FROM THE ROOT ESDR HEEA088436Blade · unbondedMAIN ROTOR BLADE NICKEL ABRASION STRIP IS UNBONDED ON THE INBOARD END.SDR CA030728001Blade · cracked(CAN) ON LANDING PILOT NOTICED DEFECT IN WHITE ROTOR BLADE. BLADE FOUND CRACKED ON UNDERSIDE SKIN FROM TRAILING EDGE TO SPAR 17 INCHES FROM BLADE ROOT. REMAINING BLADES INSPECTED NO DEFECTS FOUND.SDR HEEA088437Rib · delaminatedMAIN ROTOR BLADE TIP RIB DELAMINATION.SDR HEEA088406Tip Cap · crackedMAIN ROTOR BLADE TIP CAP CRACKED. TO BE SENT TO VENDOR.SDR HEEA088405Tip Cap · crackedMAIN ROTOR BLADE TIP CAP CRACKED. TO BE SENT TO VENDOR.
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