Turbomeca ARRIEL-1D1
Service difficulty reports · 933
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 engine_model_key = 'ARRIEL1D1' 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 engine_model_key = 'ARRIEL1D1' 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 KBM2005F00105Gimbal Ring · debondedGIMBAL RING DEBONDED, REMOVED AND REPLACED. (K)SDR KNK2005F00000Engine · malfunctionedENGINE WOULD NOT ROTATE FOR ENGINE DAILY RINSE. TRIED TO TURN COMPRESSOR AND IT WAS VERY HARD TO TURN. REMOVED N6 ACCY TO CHECK FOR POSSIBLE CAUSE AND COMPRESSOR WAS STILL TIGHT. BORE SCORED COMBUSTION CHAMBER AND 1ST STAGE BLADES AND FOUND NO ABNORMALLIES.SDR ILD2005F00000Manifold · damagedON THE FIRST FLIGHT, ENGINE COULDN`T START DUE TO FUEL COKING AT GENERATOR INJECTION MAINIFOLD (MODULE 3 COMBINATION) INJECTION MANIFOLD WAS REMOVED AND REPLACED WITH SERVICEABLE INJECTION MAINIFOLD. AC RETURNED TO SERVICE AFTER RUN UP LEAK CHECK AND OPERATIOSDR KBM2005F00096Entertain Sys · failedDIGITAL MEDIA PLAYER SHOWS FAILURE, REMOVED AND REPLACED. (K)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 CA050609018Nozzle · separated(CAN) FIRE EXTINGUISHER TRIGER AND NOZZLE HEAD DISLODGED AND SEPARATED FORM THE MAIN BODY.SDR CA050609017Pump · worn(CAN) PULLEY SPLINES FOUND TO BE WORN BEYOND 2/3 DURING A 100 HR INSPECTION. COUPLING S40 REPLACED 336.4 HOURS PREVIOUSLY FOR THE SAME REASON. HYDRAULIC PUMP SPLINES FOUND 2/3 WORN. A NEW PUMP HAD BEEN INSTALLED 336.4 HOURS PREVIOUSLY FOR THE SAME REASON.SDR KBM2005F00226Skid Shoe · crackedRT FWD SKID SHOE CRACKED, REMOVED AND REPLACED. (K)SDR KBM2005F00201Structure · crackedHORIZONTAL STABILIZER, RT SIDE TOP IS CRACKED 5 INCHES IN LENGTH, REMOVED AND REPLACED. (K)SDR KBM2005F00189Line · leakingHYDRAULIC LINE LEAKING, REMOVED AND REPLACED. (K)SDR KBM2005F00190Line · leakingHYDRAULIC LINE LEAKING. REMOVED AND REPLACED. (K)SDR CA050513002Spar · cracked(CAN) NOISE HEARD ON PITOT DAILY INSPECTION AS PART OF EUROCOPTERS CRITERIA. DISASSEMBLED BY ENGINEER AND FOUND CRACKED.SDR KBM2005F00181Igniter · wornCENTER ELECTRODE ON RT ENGINE IGNITER WORN. (K)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 KBM2005F00062Gyro · spinningD.G. SPINS IN FLIGHT. REMOVED AND REPLACED. (K)SDR KBM2005F00063Voltmeter · sticksVOLTMETER, NEEDLE STICKS. REMOVED AND REPLACED. (K)SDR KBM2005F00064Hub · cutT/R HUB HAS CUT AROUND THE RUBBER, REMOVED AND REPLACED. (K)SDR KBM2005F00077Indicator · intermittentATTITUDE INDICATOR CAGES BUT WILL UNCAGE A FEW MINUTES LATER. 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 KBM2005F00076Drain Valve · leakingSTART DRAIN VALVE, UNIT HAS INTERNAL LEAK. REMOVED AND REPLACED. (K)SDR 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 KBM2005F00193Connector · leakingOIL PRESSURE TRANS, LEAKING FROM CONNECTOR PLUG. 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 KBM2005F00036Bearing · wornLAMINATED BEARINGS, WORN. REMOVED AND REPLACED. (K)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 2005FA0000490Gear Set · corrodedGEAR SET HAS EXCESSIVE FROSTING AND PITTING. REQUESTING WARRANTY CONSIDERATION. (K)SDR 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 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)SDR KBM2005F00319Control Cable · bindingT/R CONTROL CABLE BINDING IN FLIGHT. REPLACED WITH SERVICEABLE CABLE. (K)SDR KBM2005F00002Bearing · wornHALF SHELLS WORN. REMOVED AND REPLACED.SDR KBM2005F00001Solenoid Valve · unserviceableFLAMED OUT DURING VIBRATION TEST. REPLACED IGNITION SOLENOID WITH SERVICEABLE UNIT AS NEEDED.SDR CA041213005Bushing · cracked(CAN) DURING ROUTINE HYDS OFF TRAINING, TAIL ROTOR INPUTS MADE THROUGH TAIL ROTOR PEDALS WERE NOT BEING TRANSFERRED TO TAIL ROTOR. PILOTS RESELECTED HYDS ON & TAIL ROTOR RESPONDED NORMALLY TO TAIL ROTOR INPUTS. AIRCRAFT RETURNED TO HANGAR FOR INSPECTION. WHEN SDR CA041203007Line · leaking(CAN) FLUID LEAK AT UPPER HOUSING SPLIT LINE.SDR KBM2005F00007Shoulder Belt · stuckPILOT SEAT SHOULDER HARNESS STUCK. REMOVED AND REPLACED. (K)SDR KBM2005F00006Bearing · wornTAIL ROTOR HALF SHELLS, BEARINGS WORN. REMOVED AND REPLACED. (K)SDR CA041117006Servo · stiff(CAN) THE PILOT WAS DOING PRE FLIGHT HYDRAULIC TEST IAW FLIGHT MANUAL REQUIREMENTS IAW AWD CF-2003-15R3 AND NOTICED A STIFFNESS IN THE FLIGHT CONTROLS. THE AIRCRAFT WAS SHUT DOWN. AN ENGINEER WAS NOTIFIED AND STARTED TO TROUBLESHOOT THE PROBLEM. THIS SERVO WASSDR 2005FA0000243Fan · mismanufacturedLOCKING SET SCREW MISSING FROM FAN, FAN DETATCHED FROM MOTOR. UPON RECEIPT OF NEW FAN, FOUND SET SCREW ALSO MISSING. (K)SDR KBM2004F00243Bearing · wornHALF SHELLS, WORN BEYOND LIMITS, REMOVED AND REPLACED.SDR KBM2004F00233Bearing · crackedBEARING HALF SHELLS CRACKED BEYOND LIMITS. REMOVED AND REPLACED.SDR PG92004F00013Blade · crackedT/R SPAR FOUND TO HAVE 5 INCH LONG SPANWISE SPAR CRACK, FOUND BY PILOT UPON TURN AROUND CHECK. THIS CONDITION PERSISTS ON THIS MODEL HELICOPTER AND PN COMPONENT. REPLACED ENTIRE T/R BLADE WITH SERVICEABLE UNIT. RETURN HELICOPTER TO SERVICE.SDR CA041025004Crossbeam · cracked(CAN) THE BI-DIRECTIONAL CROSSBEAM WAS IN FOR NDT INSPECTION IAW AD96-156-071(B)R1. THE NDT AMO FOUND THE CROSSBEAM CRACKED IN THE CUP OR AS INDICATED IN SB05-00- 28 'R' REGION.SDR KBM2004F00234Gyro · inoperativeATTITUDE GYRO WILL NOT HOLD ATTITUDE IN FLIGHT. INSTALLED GYRO FROM 350SH SERVICEABLE.SDR KBM2004F00235Gyro · inoperativeDIRECTIONAL GYRO INOPERATIVE. REMOVED AND REPLACED WITH A RECONDITIONED GYRO.
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