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 CA040805008Bearing · worn(CAN) WHILE PERFORMING A 100 HOUR INSPECTION THE TAIL ROTOR SPIDER WAS DISCONNECTED FROM THE INPUT BELLCRANK TO CHECK THE SPIDER SWASHPLATE BEARING. NOTICED THAT THE BALL END BEARING ON THE SWASHPLATE INPUT WAS WORN OUT. ( IPC 65.20.30 FIG 1A ITEM 95 ) MEASURSDR KBM2004F00109Electrical Box · inoperativeAIR CONDITIONER BLOWS WARM. REMOVED AND REPLACED WITH SERVICEABLE UNIT.SDR CA040315012Servo Valve · unserviceable(CAN) PILOT REPORTED THAT WHEN HE TRIED TO PULL THE COLLECTIVE UP, IT FELT VERY HEAVY. IT WAS NOTED DURING TROUBLESHOOTING THAT THE SPOOL VALVE WAS VERY DIFFICULT TO MOVE AND THEN IT WOULD ONLY MOVE A SMALL AMOUNT. A SERVICEABLE SERVO WAS INSTALLED AND CONSDR KBM2004F00108Servo · leakingSERVO UNIT IS LEAKING. REMOVED AND REPLACED.SDR ULX2004F00008Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00006Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR 2004F00101Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION-USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00005Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00004Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATIONS- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00003Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00002Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE, AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00001Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION-USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00000Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR KBM2004F00107Transceiver · inoperativeREMOVED COMM, KY 196A, SN:8965 FOR TROUBLESHOOTING. REMOVED AND REPLACED.SDR HCM2004F00000Sensor · failedON MARCH 9, 2004 WHILE ON A SIGHT SEEING TRIP, THE PILOT NOTICED A HIGH ENGINE OIL TEMPERATURE INDICATION. HE MADE A PRECAUTIONARY LANDING. A MECHANIC WAS FLOWN TO THE SCENE AND REPLACED THE ENGINE OIL TEMPERATURE SENSOR. THE AIRCRAFT WAS FLOWN BACK TO BASESDR EKL2004F00000Hose · leakingAFTER START, WHILE AT FLIGHT IDLE, PRIOR TO TAKE OFF, THE PILOT RECEIVED THE HYD LIGHT ON THE WARNING PANEL. PILOT SHUT DOWN AC WITHOUT INCIDENT. UPON FURTHER INVESTIGATION, IT WAS DETERMINED THAT A SMALL PIN HOLE SIZE LEAK HAD DEVELOPED IN THE PRESSURE LINESDR KBM2004F00042Ball · excess playTAIL ROTOR PC SPIDER END BALL BEARING HAS EXCESSIVE PLAY. REMOVED AND REPLACED.SDR KBM2004F00041Drain Valve · leakingSTART DRAIN VALVE, INTERNAL LEAKING. REMOVED AND REPLACED.SDR KBM2004F00024Bearing · wornLT LAT SERVO UPPER AND LOWER ROD END BALL, WORN. REMOVED AND REPLACEDSDR ULX2004F00016Brushes · inoperativeNO OUTPUT, PROBABLE CAUSE: BRUSHES DESTROYED, BRUSH SPRINGS DAMAGED, ARMATURE GROOVED. HIGH AMPERAGE. MONITOR LOAD DURING USING.SDR ULX2004F00015Stator · shortedSTATOR SHORTED, BRUSHES DESTROYED, COMMUTATOR GROOVED. EXCESSIVE AMPERAGE. MONITOR ELECTRICAL LOAD DURING OPERATION.SDR ULX2004F00014Armature · shortedARMATURE SHORTED, BRUSHES RIVETS CAME LOOSE. PROBABLE CAUSE: EXCESSIVE AMPERAGE. MONITOR ELECTRICAL LOAD DURING OPERATION.SDR ULX2004F00013Brushes · wornBRUSHES FOUND WORN ON BRUSH CHECK.SDR ULX2004F00012Starter Gen · failedNO OUTPUT; OVERLOADED, CAUSING ARMATURE SHORTING, BRUSHES DESTROYED. MONITOR ELECTRICAL LOAD.SDR ULX2004F00011Starter Gen · failedNO OUTPUT, REPAIRED 3.1 HOURS EARLIER. UNKNOWN CAUSE OF FAILURE.SDR ULX2004F00010Shaft · shearedDRIVE SHAFT FOUND SHEARED. PROBABLE CAUSE: GENERATOR BROUGHT ON LINE WITH HIGH ELECTRICAL LOAD. RECOMMENDATION: PILOT BRING ON LINE WITH LOW LOAD AND THEN ADD LOAD.SDR ULX2004F00009Starter Gen · vibrationREMOVED FOR EXCESSIVE VIBRATION. BRUSHES DESTROYED, ENDBELL BEARING LINER WORN.SDR KBM2005F00017Blower · inoperativeAIR CONDITIONER BLOWING AMBIENT TEMP, AIR ONLY, REMOVED AND REPLACED.(K)SDR CA040308002Belt · stretched(CAN) WHILE INSPECTING THE HYDRAULIC DRIVE BELT IAW 63.00.00.601 PARA 4 FOR PROPER TENSION IT WAS FOUND TO BE LOOSE. ATTEMPTS WERE MADE TO TENSION THE BELT IAW 63.00.00.401 PARA 4.2.3. WE WERE UNABLE TO GET THE REQUIRED TENSION DUE TO NO MORE MOTION OF THE SDR 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 KBM2005F00026Bearing · crackedCRACKED .6666 THE WAY DOWN THE NUT SIDE OF FORK. REMOVED AND REPLACED. (K)SDR KBM2005F00025Bearing · crackedT/R HINGE LAMS CRACKED .6666 THE WAY AROUND ON SIDE OF FORK. REMOVED AND REPLACED. (K)SDR KBM2005F00024Pitch Link · crackedTAIL ROTOR PITCH LINK ROD HAS SILENT BLOCK HAS V-CRACK. REMOVED AND REPLACED. (K)SDR KBM2004F00176Blower · inoperativeCONDENSER BLOWER INOPERATIVE. REMOVED AND REPLACED.SDR KBM2004F00112Motor · inoperativeCONDENSOR BLOWER INOPERATIVE. QUIT DURING GROUND RUN. REMOVED AND REPLACED.SDR B30R20040226Door Frame · crackedDURING 100 HOUR INSPECTION DISCOVERED CO-PILOT DOOR POST CRACKED 14 INCHES LONG STARTING 8 INCHES ABOVE CABIN FLOOR, EXCEEDING THE LIMITS IN REPAIR MANUAL. REPAIRED CRACK IAW MM. REQUESTED FROM MFG.SDR KBM2005F00023Inertia Reel · brokenINERTIA REEL IS BROKEN, REMOVED AND REPLACED. (K)SDR KBM2005F00019Seal · leakingMAG SEAL, LEAKING, REMOVED AND REPLACED. (K)SDR CA040301005Support · cracked(CAN) A CRACK WAS DISCOVERED IN MAY ON THE NR 5 HANGER BEARING SUPPORT. THIS PART WAS REPLACED IN THE FIELD USING ALL THE APPROPIATE TOOLING. SOMETIME LATER THE PILOT COMPLAINED OF A HIGH FREQ VIBRATION. THE SHAFT WAS REBALANCED TO .2 IPS. AGAIN ABOUT 20 HOURSSDR 2004FA0000272Pipe · crackedDURING ENGINE START AFTER CHANGING THE START DRAIN VALVE, LT FUEL INJECTOR PIPE WAS SPRAYING FUEL AT INJECTOR FITTING. INSPECTION OF PIPE REVEALED A CACK AT THE TOP OF THE FLARE ON THE PIPE. CAUSE OF CRACK APPEARS TO BE FROM THE FLARE NOT BEING CENTERED ON TSDR KBM2005F00018Control Cable · bindingT/R CONTROL CABLE, CABLE IS BINDING, REMOVED AND REPLACED. (K)SDR KBM2004F00043Bracket · crackedRT SIDE TAIL ROTOR PEDAL BELLCRANK BRACKET LOCATED UNDERNEATH CABIN FLOOR HAS CRACKS. REMOVED AND REPLACED.SDR KBM2004F00111Indicator · malfunctionedINCORRECT READING DURING FLIGHT. REMOVED AND REPLACED WITH SERVICEABLE UNIT.SDR KBM2004F00058Pickup · inoperativeNR NEEDLE WENT TO ZERO IN FLIGHT. REMOVED AND REPLACED.SDR KBM2004F00110Transmitter · unreliableTORQUE GAUGE SHOWING UNRELIABLE READINGS DURING THE FLIGHT. ON GROUND IT ROTATES CLOCKWISE. REMOVED AND REPLACED.SDR KBM2004F00088Switch · inoperativeLT SIDE BAGGAGE DOOR WARNING LIGHT, INOPERATIVE. ADJUSTED MICROSWITCH FOR LT SIDE BAGGAGE DOOR. OPS CHECKED GOOD.SDR PG92004F00005Line · leakingHOSE LOST PRESSURE AND LEAKED HYDRAULIC OIL OUT, CAUSING LOSS OF FLIGHT CONTROL BOOST AND SUBSEQUENT PRECAUTIONARY LANDING. REMOVED AND REPLACED HOSE WITH NEW. (K)SDR PG92004F00000Line · leakingAC LOST ALL HYDRAULIC FLIGHT CONTROL BOOST ASSIST DURING AIR TOUR FLIGHT. PILOT PERFORMED PRECAUTIONARY LANDING IAW MFG MM. MECHANIC DISPATCHED TO REMOTE SITE TO REPAIR AIRCRAFT. FOUND ALL BUT 1 CUP OF HYDRAULIC FLUID LEFT IN RESERVOIR. FOUND SUBJECT HIGH SDR KBM2004F00018Blower · inoperativeOIL COOLER MOTOR INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE.SDR KBM2004F00017Bearing · wornTAIL ROTOR HUB LAMINATED RUBBER HINGE BEARING ARE WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW.
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