Aerospatiale AS350B2
Service difficulty reports · 3,065
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'AS350B2' 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 aircraft_model_key = 'AS350B2' 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 CA050609018Nozzle · separated(CAN) FIRE EXTINGUISHER TRIGER AND NOZZLE HEAD DISLODGED AND SEPARATED FORM THE MAIN BODY.SDR CA050506006Coupling · separated(CAN) STAKED WASHER ON FLECTOR WAS FOUND TO BE SEPERATED/BROKEN. THE BRAKE WAS ON OPPOSITE SIDE WHICH HAD BEEN STAKED. THIS WAS DISCOVERED DURING MAINTENANCE OF THE TRANSISSION INPUT RE-TORQUE. REPLACEMENT PART AND HARDWARE INSTALLED.SDR KBM2005F00096Entertain Sys · failedDIGITAL MEDIA PLAYER SHOWS FAILURE, REMOVED AND REPLACED. (K)SDR KBM2005F00078Radio · distortedVHF RADIO, RECEIVES BROKEN, DISTORTED. REMOVED AND REPLACED. (K)SDR KBM2005F00201Structure · crackedHORIZONTAL STABILIZER, RT SIDE TOP IS CRACKED 5 INCHES IN LENGTH, REMOVED AND REPLACED. (K)SDR KBM2005F00048Gyro · faultyALTITUDE GYRO SHOWS 10 DEGREES RIGHT TURN DURING STRAIGHT AND LEVEL FLIGHT. REMOVED AND REPLACED. (M)SDR KBM2005F00047Gyro · faultyALTITUDE GYRO 10 DEGREES OFF DURING TURNS. REMOVED AND REPLACED. (M)SDR KBM2005F00052Chip Detector · defectiveENGINE CHIP LIGHT ON. REMOVED AND REPLACED ENGINE HORIZONTAL CHIP DETECTOR. (M)SDR KBM2005F00203Chip Detector · malfunctionedENGINE CHIP LIGHT ILLUMINATED IN FLIGHT. REMOVED, INSPECTED AND CLEANED ENG ELECTRICAL CHIP DETECTORS. NO METAL FOUND, GROUND RUN FOR 1 HOUR. CHIP LIGHT NOT ILLUMINATED, CHECK GOOD. (K)SDR KBM2005F00190Line · leakingHYDRAULIC LINE LEAKING. REMOVED AND REPLACED. (K)SDR KBM2005F00189Line · leakingHYDRAULIC LINE LEAKING, REMOVED AND REPLACED. (K)SDR KBM2005F00055Seal · damagedAIR INTAKE SEAL REQUIRED REPLACEMENT. REMOVED AND REPLACED. (M)SDR KBM2005F00054Servo · leakingSERVO LEAKING. REMOVED AND REPLACED SERVO. (M)SDR KBM2005F00205Bearing · dirtyREMOVED ENGINE ASSEMBLY FOR CHIP LIGHT EVACUATION. ENGINE REAR BEARING CLEANED, RIGGED NR1 AND N2 REPLACED WITH NEW OIL. PERFORMED GROUND RUN OPS CHECKED GOOD. (K)SDR CA050513002Spar · cracked(CAN) NOISE HEARD ON PITOT DAILY INSPECTION AS PART OF EUROCOPTERS CRITERIA. DISASSEMBLED BY ENGINEER AND FOUND CRACKED.SDR KBM2005F00056Belt · brokenFOUND COMPRESSOR BELT BROKEN. AIRCRAFT MEL. (M)SDR KBM2005F00181Igniter · wornCENTER ELECTRODE ON RT ENGINE IGNITER WORN. (K)SDR KBM2005F00053Hydraulic Line · leakingHYDRAULIC HOSE FAILED DURING CRUISE FLIGHT, 10 MINUTES IN TO FLIGHT. FOUND PIN HOLE IN LINE. REMOVED AND REPLACED HYDRAULIC LINE. (M)SDR KBM2005F00057Brushes · wornBRUSH WORN BEYOND LIMITS. (M)SDR KBM2005F00088Pump · seizedFUEL BOOST PUMP, UNIT SEIZED, BLOWS CIRCUIT FUSE W/POWER APPLIED. REMOVED AND REPLACED. (K)SDR KBM2005F00090Magnetic Seal · leakingSTARTER GENERATOR MAG SEAL LEAKING. REMOVED AND REPLACED. (K)SDR KBM2005F00064Hub · cutT/R HUB HAS CUT AROUND THE RUBBER, REMOVED AND REPLACED. (K)SDR KBM2005F00063Voltmeter · sticksVOLTMETER, NEEDLE STICKS. REMOVED AND REPLACED. (K)SDR KBM2005F00062Gyro · spinningD.G. SPINS IN FLIGHT. REMOVED AND REPLACED. (K)SDR KBM2005F00077Indicator · intermittentATTITUDE INDICATOR CAGES BUT WILL UNCAGE A FEW MINUTES LATER. REMOVED AND REPLACED. (K)SDR 2005FA0000504Case · crackedEDDY CURRENT INSPECTION IAW MFG COMPONENT MM, IDENTIFIED A CRACK FROM A PLUG HOLE.SDR KBM2005F00079Indicator · erraticN.G., GAUGE NEEDLE AND DIGITS ARE ERRATIC INTERMITTENTLY. REMOVED AND REPLACED. (K)SDR KBM2005F00061Gyro · tumblesD. G. TUMBLES IN FLIGHT. REMOVED AND REPLACED. (K)SDR CA050323011Drive Belt · cracked(CAN) DURING A DAILY INSPECTION AME DISCOVERED A CRACK IN THE HYDRAULIC PUMP DRIVE BELT. THE CRACK APPROXIMATELY 1-1.5 INCH LONG WAS LOCATED BETWEEN THE V-GROOVE SEGMENTS. (THE CRACK SEPARATES ALMOST COMPLETELY WHEN BELT IS PINCHED BY HAND IN A FOLDING MANNESDR KBM2005F00046Gyro · malfunctionedTUMBLES IN FLIGHT. REMOVED AND REPLACED. (K)SDR CA050323002Engine · out of limits(CAN) THE ENGINE HAS BEEN INSTALLED AFTER OVERHAUL, AND ON GROUND RUN HIGH VIBRATION ON THE FORWARD POINT WITHIN LIMIT BUT ABNORMALLY HIGH. AFTER CONTACTING THE OVERHAUL FACILITIES, WE DID SOME TESTS FOR RESULT. THE VIBRATION WENT UP CLOSER TO THE LIMIT. AFTESDR KBM2005F00045Gyro · failedATTITUDE GYRO UNIT TUMBLES. REMOVED AND REPLACED. (K)SDR KBM2005F00193Connector · leakingOIL PRESSURE TRANS, LEAKING FROM CONNECTOR PLUG. REMOVED AND REPLACED. (K)SDR KBM2005F00044Gyro · malfunctionedDIRECTIONAL GYRO SPINS IN FLIGHT, WILL NOT HOLD CONSTANT HEADING. REMOVED AND REPLACED. (K)SDR KBM2005F00043Gyro · malfunctionedATTITUDE INDICATOR WOULD NOT CAGE PROPERLY. REMOVED AND REPLACED. (K)SDR KBM2005F00040Sight Glass · looseNG GAUGE, COVER, GLASS LOOSE. REMOVED AND REPLACED. (K)SDR CA050321003Support · cracked(CAN) AN AME WAS PERFORMING AN INSPECTION ON A DOOR PIN IAW AD F-2005-032 AND NOTICED THAT THE LT REAR SUPPORT BRACKET HAD A CRACK FROM THE EDGE OF THE PART TO THE RADIUS NEAR THE RT UPPER ATTACHMENT HOLE. THE PART WAS REPLACED.SDR CA050314005Servo · ratcheting(CAN) WHILE IN FLIGHT THE PILOT NOTICED A RATCHETY FORE AND AFT CYCLIC MOVEMENT WHILE MOVING THE CYCLIC FORE AND AFT. SERVO SENT TO MFG FOR EVALUATION.SDR CA050310004Pin · cracked(CAN) PIN P/N 350A25-1275-20 WAS REMOVED FOR NDT IAW THE REQUIREMENTS OF AD F-2005-032 AND ALERT TELEX 05.00.47. A VISUAL INSPECTION OF THE PIN REVEALED A CRACK ON BOTH SIDES OF THE HOLE THAT IS DRILLED TO FIT UPON INSTALLATION. THE PIN WAS REPLACED.SDR KBM2005F00036Bearing · wornLAMINATED BEARINGS, WORN. REMOVED AND REPLACED. (K)SDR 2005FA0000490Gear Set · corrodedGEAR SET HAS EXCESSIVE FROSTING AND PITTING. REQUESTING WARRANTY CONSIDERATION. (K)SDR EGI2005F00000Starflex · failedSTARFLEX ARM FAILED. START PROCEEDED NORMAL UNTIL ABOUT 25-35 PERCENT NG. WHEN A SUDDEN ROTOR IMBALANCE DEVELOPED, IMMEDIATELY PULLED THE THROTTLE BACK AND APPLIED THE ROTOR BRAKE, AT THE SAME TIME, OBSERVED THAT ONE BLADE WAS TRACKING 6 INCHES LOWER THAN THSDR KBM2005F00010Gyro · intermittentDG INTERMITTENT IN FLIGHT, 2 KNOBS LOOSE, REMOVED AND REPLACED. (K)SDR CA050207004Hydraulic System · failed(CAN) THE HELICOPTER WAS ON A INTERNATIONAL JOB. THE INITIAL REPORT FROM FLIGHT OPERATIONS IS HYDRAULIC FAILURE. THE AIRCRAFT WAS IN A HOVER WHEN IT YAWED TO THE RT. THE AIRCRAFT LANDED HARD ENOUGH TO DAMAGE ONE ARM OF THE MAIN ROTOR STAR AND THE TAILBOOM HSDR CA050308014Gearbox · leaking(CAN) UPON A PREFLIGHT IT WAS NOTED THAT ALL OIL HAD EXITED THE TAIL ROTOR GEARBOX. THE INPUT SEAL WAS THE AREA WHERE THE OIL EXITED. THE GEARBOX WAS REPLACED AS A PRECAUTION.SDR 2005FA0000030Bearing · brokenBEVEL REDUCTION MODULE (PN 350A32-0300-05, SN M1899) WAS REMOVED AT TSO: 2367.5 FOR METAL CONTAMINATION. UPON TEARDOWN ANALYSIS IT WAS DISCOVERED THAT THE BEARING CAGE FOR BEARING (P/N 704A33-652-036) TSN: 2367.5, WAS BROKEN. SUBSEQUENT DETERIORATION OF BEARSDR 2005FA0000027Cage · brokenBEVEL REDUCTION MODULE P/N 350A32-0300-05 S/N M1899 WAS REMOVED AT TSO: 2367.5 FOR METAL CONTAMINATION. UPON TEARDOWN ANALYSIS IT WAS DISCOVERED THAT THE BEARING CAGE FOR BEARING P/N 704A33-652-036 TSN: 2367.5, WAS BROKEN. SUBSEQUENT DETERIORATION OF BEARINGSDR CA050114005Crossbeam · cracked(CAN) AN ENGINEER WAS DOING A 30 HOUR INSPECTION IAW AWD 96-156-071(B) R1 PART 1.1.THE ENGINEER DISCOVERED A BLACK LINE IN THE REGION THAT IS TO BE INSPECTED, A CLOSER LOOK, IT WAS DETERMINED THAT IT WAS CRACKED. THE TSO IS ACTUALLY TSI SINCE THE LAST (NDT LISDR CA050113008Window · cracked(CAN) DURING THE BLF THE MAIN WINDOW WAS FOUND TO BE CRACKED. THE OAT WAS -34 DEGREES. IT APPEARS TO HAVE BEEN INSTALLED WITH IMPROPER TORQUE AS THE CRACK ORIGINATED FROM THE TOP SCREW OF THE SLIP INDICATOR.SDR KBM2005F00008Encoder · inactiveALT DIGITIZER OFF. AOG (K)
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