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 HEEA084574Blade · damagedMAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES DUE TO EROSION.SDR HEEA084573Blade · damagedMAIN ROTOR BLADE LOWER TRAILING EDGE FRETTING PAD UNBONDED.SDR HEEA084572Blade · damagedMAIN ROTOR BLADE SKIN PEELING OFF TOP MIDDLE SECTION OF BLADE.SDR HEEA084571Blade · damagedMAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES DUE TO EROSION.SDR HEEA084570Blade · out of balanceMAIN ROTOR BLADE NEEDS TO BE REBALANCED ACCORDING TO SPECS.SDR HEEA084569Blade · damagedMAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES ERODED THROUGH.SDR HEEA084568Blade · damagedMAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES ERODED THROUGH.SDR HEEA084567Blade · contaminatedMAIN ROTOR BLADE HAS WATER IN THE CHORE NEAR THE MID SPAN TRIM TAB.SDR HEEA084566Blade · damagedMAIN ROTOR BLADE OUTBOARD LEADING EDGE ABRASION STRIP HAS SEVERAL EROSION HOLES. ALSO NEEDS TO BE REBALANCED. SENT TO ROTOR BLADES, INC. FOR WARRANTY REPAIR.SDR HEEA084565Blade · out of balanceMAIN ROTOR BLADE NEEDS TO BE REBALANCED ACCORDING TO SPECS.SDR HEEA084564Blade · damagedMAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS SEVERAL EROSION HOLES.SDR HEEA084563Blade · damagedMAIN ROTOR BLADE EROSION SHIELD ON THE LOWER SIDE AT THE INBOARD END IS PEELING OFF.SDR HEEA084562Blade · damagedMAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS NUMEROUS HOLES. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR.SDR HEEA084561Blade · damagedMAIN ROTOR BLADE HAS A HOLE IN TOP SKIN AT STA 93 WITH MULTIPLE BRANCHES.SDR HEEA084560Blade · damagedUNABLE TO TRACK OR BALANCE, M/R BLADE APPEARS TO BE HEAVY.SDR HEEA084559Blade · damagedMAIN ROTOR BLADE IS TOO HEAVY, WILL NOT FLY, SUSPECT WATER IN THE CORE.SDR HEEA084558Blade · damagedMAIN ROTOR BLADE UPPER AFT FRETTING PAD UNBONDED AND UPPER SKIN HAS AREA AROUND PREVIOUS REPAIR CRACKED.SDR HEEA084557Blade · damagedMAIN ROTOR BLADE EROSION SHIELD ON LOWER SIDE HAS SOME SEPARATION AND LIFTING.SDR HEEA084556Blade · damagedMAIN ROTOR BLADE TIP CAP UNBONDED, FIBERGLASS CRACKED IN SEVERAL AREAS AND TRIM TAB SEPARATED.SDR HEEA084555Blade · crackedMAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS A CRACK NEAR THE SPLICE AREA.SDR HEEA084554Blade · out of balanceMAIN ROTOR BLADE NEEDS TO BE BALANCED ACCORDING TO SPECS.SDR HEEA084553Blade · damagedMAIN ROTOR BLADE DAMAGED, UNABLE TO TRACK OR BALANCE. APPEARS TO BE HEAVY.SDR HEEA084552Blade · damagedMAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS EROSION HOLES. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR.SDR HEEA084551Blade · damagedMAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS EROSION HOLE THROUGH THE STRIP. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR.SDR ERAA085147Tip Cap · debondedWORN DOUBLER DEBONDING. R & R EXTERNAL DOUBLER, R & R FWD INT DOUBLERS AND REMOV AND REBONDED C CHANNEL REFINISH AND BALANCE.SDR ERAA085145Tip Cap · debondedWORN DOUBLER DEBONDING. KEVLAR SKIN DAMAGE IN ZONE A & D ON SN A175-03491 R & R EXTERNAL DOUBLERS, R & R FWD INT DOUBLERS AND REMOVE AND REBONDED C CHANNEL, REFINISH AND BALANCE. REPAIRED SKIN DAMAGE ON SN A175-03491.SDR ERAA085144Tip Cap · debondedDOUBLER DEBONDING, WORN. SENT TO CTI. INSPECTED PER SA 4047-76-5 REV 11; MODIFIED EXTERNAL DOUBLERS PER RS-017-1; REPLACED ABRASION STRIP PER RS-005N-III; REPAIRED KEVLAR PER PROCEDURE NR 2 AND 18 -1 PLY; REFINISHED PER DRAWING NR 76150-09043; STATIC BALANCE SDR ERAA085143Blade · lowVBIM INDICATING LOW PRESSURE . PRESSURE CHECKED AT 2.8 PSI AT 20 DEGREE C. SENT TO CTI FOR REPAIR. INSPECTED PER SRM SA 4045-31E CHAPTER / SECTION 65-10-01 REV 5. PERFORMED 2 DAY CHECK PER SER 50908. REPLACED BIM TRANSDUCER TRANSDUCER AND REINSTALLED BISDR ERAA085141Blade · damagedMAIN ROTOR BLADE HAS BLACK BIM. SENT FOR REPAIR. INSPECTED IAW SRM SA 4045-31E CHAPTER / SECTION 65-10-01 REV 5. PERFORMED 2 DAY LEAK CHECK IAW SER 50908; REPLACED BIM TRANSDUCER AND REINSTALLED BIM; RECHARGED SPAR IAW S-61N MM SA4045-80 REV MARCH 1, 1978 ASDR HEEA084171Blade · crackedMAIN ROTOR BLADE TITANIUM LEADING EDGE HAS A COMPLETE CHORDWISE CRACK WITH SEPARATION BEYOND LIMITS.SDR HEEA084170Blade · damagedMAIN ROTOR BLADE NICKEL STRIP HAS A CRACK AT THE VERY TIP AND IS STARTING TO PEEL.SDR CA030212009Blade · cracked(CAN) INBOUND FROM RIG, 'BIM' LIGHT ILLUMINATED. EMERGENCY CHECKLIST C/W. AIRCRAFT DIVERTED TO SABLE ISLAND FOR PRECAUTIONARY LANDING. COMM CENTRE ADVISED.POST S/D CHECK CONFIRMED PRESSURE BELOW LIMITS.SDR CA030305006Blade · cracked(CAN) THE BLADE WAS SENT IN FOR A HARD LANDING INSPECTION (NOT A BLADE STRIKE). UPON INSPECTION THE ROTOR BLADE WAS FOUND CRACKED ON THE UPPER SURFACE STATION 224.0 NEAR THE TIP INERTIA WEIGHT. THE CRACK ORIGINATED AT A FASTENER HOLE AND PROGRESSED THROUGH THESDR 2003FA0000138Blade · damagedONE OF THE TWO TRAILING EDGE STUDS THAT WAS HOLDING THE TIP END WEIGHT PACKAGE FRACTURED (TRAIL EDGE). THE FRACTURE OCCURED APPROX. 1/4 INCH BELOW THE LOCK RING IN THE BALANCE PLATE ASSY. THIS CAUSED THE LEADING EDGE STUD TO DEFORM, ALLOWING THE WEIGHT PACKASDR CA030125001Blade · cracked(CAN) CHORDWISE CRACK FOUND ON RED MAIN ROTOR BLADE 100MM CUFF S/N 806, 80MM OUTBOARD OF BLADE FITTING. MAIN ROTOR BLADES (4) REPLACED, MANUFACTURER NOTIFIED.SDR R7MR34599Blade · delaminatedSKIN DELAMINATION, 3 FT FROM ROOT (MAY QUALIFY FOR BLADE EXCHANGE). REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR R7MR34600Blade · crackedSKIN DELAMINATION AND CRACK, 3 FT FROM ROOT (MAY QUALIFY FOR BLADE EXCHANGE). REPLACED WITH NEW UNITS, CORRECTED PROBLEM.SDR HEEA083962Blade · separatedMAIN ROTOR BLADE HAS SEPARATION AT TIP. TO BE SENT TO VENDOR.SDR HEEA083961Blade · separatedMAIN ROTOR BLADE HAS SEPARATION ON BOTTOM OF BLADE. TO BE SENT TO VENDOR.SDR HEEA083960Blade · separatedMAIN ROTOR BLADE HAS SEPARATION ON BOTTOM OF BLADE. TO BE SENT TO VENDOR.SDR HEEA083959Blade · crackedMAIN ROTOR BLADE CRACKED AND SEPARATED NEAR THE OUTBOARD TRIM TAB.SDR HEEA083952Blade · peelingPEELING PAINT ON TAIL ROTOR BLADES AND HIGH FREQUENCY VIBRIATION. REPAIRED.SDR HEEA083814Bolt · wornMAIN ROTOR BLADE BOLT SHANK HAS TWO WORN SPOTS.SDR HEEA083812Bolt · corrodedMAIN ROTOR BLADE BOLTS HAVE CORROSION BEYOND LIMITS.SDR HEEA083563Blade · separatedTIP CAP OF BLADE IS SEPARATED AT THE OUTBOARD END.SDR HEEA083552Blade · damagedTHE UPPER GRIP PAD HAS SOME SEPARATION AND THE LOWER EROSION SHIELD HAS SEPARATION ON MAIN ROTOR BLADES.SDR HEEA083150Blade · debondedMAIN ROTOR BLADE SKIN AT THE TIP ON THE UPPER SIDE IS UNBONDED AND CORRODED.SDR ERAA082939Blade · crackedMAIN ROTOR BLADE HAS CRACK IN LEADING EDGE AND FIBERGLASS. INSPECTED, PERFORMED 2500 HOUR INSPECTION, REPAIRED SKIN AT STA 131 TO STA 153 AND STA148 TO STA 152 ON LOWER SURFACE REPLACED OUTBOARD ABRASION STRIP. REPLACED INBOARD AND OUTBOARD SPLICE COVERS RESDR HEEA082855Blade · overspeedMAIN ROTOR BLADE OVERSPEED TO 500 RPM.SDR HEEA082606Blade · damagedMAIN ROTOR BLADE WEIGHT POCKET UNBONDED AND SCREWS CORRODED.
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