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 KBM2004F00226Gyro · failedARTIFICIAL HORIZON GYRO, UNIT WILL NOT CAGE. INSTALLED REPAIRED UNIT.SDR 2005FA0000661Blade · delaminatedDURING A ROUTINE ALF INSPECTION, THE MECHANIC DISCOVERED DELAMINATION ON THE TAILROTOR BLADE. THE TAILROTOR SHOWED NO SIGNS OF IMPACT. THE DELAMINATED TRIM TAB WAS APPROXIMATELY 3 INCHES LONG AND 2 INCHES IB OF THE TRIM TAB RIVET. THE TAILROTOR ASSY WAS REMSDR 2005FA0000660Blade · crackedTAIL ROTOR BLADE, FOUND CRACK APPROX 3.2500 INCH LONG, RUNNING PARALLEL TO TRIM TAB. (K)SDR HXS2004F00004Bearing · making metalPILOT REPORTED MGB CHIP LIGHT. INVESTIGATION REVEALED METALIC CHIPS ON THE BEVEL REDUCTION GEAR BOX THAT EXCEEDED SERVICABILITY STANDARDS. REMOVED GEARBOX AND FOUND EPICYCLIC HAS A BAD BEARING WHICH IS THE SOURCE OF THE METAL. SENT EPICYCLIC AND BEVEL GEAR SDR KBM2004F00225Control Cable · bindingCOLLECTIVE CABLE BINDING, REPLACED CABLE AS NEEDED.SDR KBM2004F00003Support Bracket · crackedFOUND BRACKET CRACKED UNDER FLOOR STRUCTURE THAT SUPPORTS T/R CONTROL AND BELLCRANK SYSTEM. REPLACED BACKET WITH SERVICEABLE PART.SDR KBM2004F00220Gyro · failedWILL NOT HOLDING HEADING. REMOVED AND REPLACED DIRECTIONAL GYRO.SDR CA041110017Pump · unserviceableBOOST PUMP FOUND LEAKING DURING DI. UPON FURTHER INVESTIGATION FOUND PUMP LEAKING INTERNALLY. PUMP REPLACED.SDR KBM2004F00219Motor · inoperativeA/C INOPERATIVE. REMOVED AND REPLACED 7 INCH BLOWER MOTOR.SDR KBM2004F00193Motor · inoperativeMOTOR INOPERATIVE. INSTALLED NEW MOTOR.SDR KBM2004F00217Pulley · obstructedIFS AIR CONDITIONING COMPRESSOR PULLEY CAME IN CONTACT WITH STRUT BAR. REPLACED STRUT BAR AND RESHIMMED PULLEY SO AS NOT MAKE CONTACT WITH STRUT.SDR KBM2004F00236Strut · damagedIFS AIR CONDITIONING COMPRESSOR PULLEY CAME IN CONTACT WITH STRUT BAR. REPLACED STRUT BAR AND RESHIMMED PULLEY SO AS TO NOT MAKE CONTACT WITH STRUT.SDR KBM2004F00215Gasket · debondedPILOT REPORTS ENGINE OIL PRESSURE INDICATION IS LOW AND LOW OIL PRESSURE LIGHT IS ON. FOUND RUBBER GASKET BELOW OIL FILTER HOUSING UNBONDED. REBONDED AND OPS CHECK GOOD.SDR CA040817004Spline · worn(CAN) NO LUBRICATION FOUND ON PUMP SPLINES. PUMP SPLINES WORN . NO SPLINES FOUND INSIDE THE S40 PUMP DRIVE DUE TO POOR LUBRICATION. HYDRAULIC PUMP AND S 40 DRIVE REPLACED.SDR 2005FA0000659Blade · delaminatedDURING A ROUTINE ALF INSPECTION, THE MECHANIC DISCOVERED DELAMINATION ON THE TAILROTOR BLADE. THE DELAMINATED TRIM TAB WAS APPROX 3 INCHES LONG AND 2 INCHES IB OF THE TRIM TAB RIVET. THE TAILROTOR ASSY WAS REMOVED AND SENT TO A BLADE REPAIR FACILITY FOR EVALSDR KBM2004F00214Probe · malfunctionedPROBE INDICATES 130 DEGREES ALL THE TIME. INSTALLED NEW TSN 0.0 PROBE AND OPS CHECK GOOD.SDR KBM2004F00150Belt · brokenBELT BROKEN IN FLIGHT. REPLACED BELT WITH NEW UNIT.SDR KBM2004F00184Clutch · inoperativeA/C CLUTCH INOPERATIVE. REMOVED AND REPLACED.SDR CA040804004Transmitter · erratic(CAN) ENGINE OIL PRESSURE WAS ERRATIC THEN IT WENT FULLSCALE. TRANSMITTER REPLACED WITH UNIT FROM FPBA. NEW ONE ORDERED AND INSTALLED IN PBA.SDR KBM2004F00117Control Cable · damagedRESISTANCE FELT IN COLLECTIVE AT UPPER END OF COLLECTIVE MOVEMENT. REPLACED O/S GOVE CABLE WITH NEW CABLE.SDR CA040726008Starflex · unserviceable(CAN) STARFLEX ARM END BUSHING ON YELLOW BLADE ARM BECAME LOOSE AROUND ADHESIVE JOINT OF CARBIDE BUSH AND A GAP, BEYOND SERVICEABLE LIMITATIONS, DEVELOPED. STARFLEX REPLACED WITH NEW PART IAW AS 350MWC.SDR CA040727014Spherical Stop · unserviceable(CAN) SEPARATION OF ELASTAMERIC NOTICED VISUALLY DURING (S) TYPE INSPECTION. VERY TOP MOST OB LAMINATION OF THE SHERICAL STOP WAS NOTED TO EXCEED PUBLISHED LIMITS. NO MENTION OF INFLIGHT VIBRATIONS. THE PART WAS REPLACED.SDR KBM2004F00183Magnetic Seal · leakingMAG SEAL LEAKING. REMOVED AND REPLACED.SDR B3OR20040712Evaporator · crackedPILOT WAS OPERATING AC AIR CONDTIONING SYSTEM AND HEARD A NOISE COMMING FROM THE FWD EVAPORATOR UNDER INSTRUMENT PANEL. UPON RETURN TO BASE, MECHANIC VERIFIED THAT THE NOISE WAS COMMING FROM THE FWD EVAPORATOR. THE EVAPORATOR WAS REMOVED AND IT WAS FOUND TO HASDR KBM2004F00182Belt · missingFOUND BELT MISSING AND SOME SHREADED MATERIAL IN GIMBEL AREA. REPLACED BELT WITH NEW.SDR HXS2004F2004BCompressor · fodENGINE WAS BEING INSPECTED AT THE 100 HOUR INSPECTION INTERVAL AND THE MECHANICS FOUND THAT THE ENGINE HAD BEEN DAMAGED AT THE INLET COMPRESSOR BY FOD. ENGINE WAS REMOVED FROM SERVICE AND SENT FOR EVALUATION AND REPAIR.SDR KBM2004F00181Turbine · damagedN1 TURBINE RUB. REMOVED ASSY AND INSTALLED RENTAL 9301R.SDR CA040805014Transmitter · inoperative(CAN) NO OIL PRESSURE INDICATION ON DASH GAUGE (ENGINE PRESSURE WARNING LIGHT GOES OUT).SDR KBM2004F00149Belt · failedA/C BLOWS HOT AIR. COIL, PULLEY, BELT (KIT) PULLEY/ NR 3003552, COIL/ NR 652233. REMOVED AND REPLACED.SDR KBM2004F00202Motor · inoperativeNOT BLOWING COLD AIR, REMOVED AND REPLACED 7 IN BLOWER MOTOR.SDR KBM2004F00203Motor · inoperativeNOT BLOWING COLD AIR, 7 IN BLOWER MOTOR, REMOVED AND REPLACED.SDR KBM2004F00201Magnetic Seal · leakingSEAL LEAKING, REMOVED AND REPLACED WITH RECONDITIONED UNIT.SDR KBM2004F00148Inertia Reel · mismanufacturedINERTIA REEL, HARD TO BUCKLE BELT. MANUFACTURED WITH WEBBING TOO SHORT. REMOVED AND REPLACED.SDR KBM2004F00180Probe · fluctuatesOIL TEMP GUAGE FLUCTUATES. REMOVED AND REPLACED.SDR CA040728004Servo · malfunctionedPILOT REPORTED THAT THE CYCLIC WAS STIFF IN LT QUADRANT. REPLACED THE LEFT HAND SERVO FIRST. THIS DID NOT SOLVE PROBLEM. REINSTALLED LEFT SERVO AND REPLACED RIGHT HAND SERVO. THE DEFECT WAS CORRECTED.SDR KBM2004F00179Gyro · spinningDIRECTIONAL GYRO SPINNS IN FLIGHT. REMOVED AND REPLACED.SDR KBM2004F00153Spherical Bearin · separatedT/R SPHERICAL BEARINGS HAVE SEPARATION BEYOND LIMITS. REMOVED AND REPLACED.SDR KBM2004F00154Pin · wornT/R EXPANDABLE PIN WORN. REMOVED AND REPLACED.SDR KBM2004F00152Bearing · wornT/R HALF SHELLS WORN BEYOND LIMITS. REMOVED AND REPLACED.SDR KBM2004F00151Transmitter · inoperativeNO OIL PRESSURE INDICATION. REMOVED AND REPLACED OIL PRESS TRANSMITTER.SDR CA040727013Bleed Valve · unserviceable(CAN) PILOT REPORTED BLEED VALVE APPEARED TO BE CLOSING LATE. SNAG CONFIRMED WHEN PLOTTED IN THE 1D1 MAINTENANCE MANUAL. BLEED VALVE REPLACED.SDR KBM2004F00177Seal · looseLT CABIN DOOR SEAL LOOSE AND WORN. REMOVED AND REPLACED.SDR KBM2004F00178Clock · intermittent8 DAY CLOCK, INTERMITTENT. REMOVED AND REPLACED.SDR KBM2004F00166Gauge · inoperativeFUEL AND ENGINE OIL PRESSURES READ ZERO IN FLIGHT. REMOVED AND REPLACED.SDR KBM2004F00189Magnetic Seal · leakingMO5 OUTPUT SHAFT MAGNETIC SEAL IS LEAKING. REMOVED AND REPLACED.SDR CA040805006Accumulator · unserviceable(CAN) CYCLIC OSCILLATION WHEN ACCUMULATORS BLED DOWN.SDR CA040517001Pinion Gear · worn(CAN) GEAR BOX ASSY HAD OIL SAMPLES TAKEN AFTER OVERHAUL FOR 1160.O HRS AND ALL OIL SAMPLES TAKEN WHERE NORMAL , AFTER INTERM REPAIR TO INPUT HOUSING ALL OIL SAMPLES TAKEN SHOWED SIGNS OF WEAR DUE TO ABNORMAL WEAR FOR 188.9 HOURS.SDR CA040727012Pressure Valve · unserviceable(CAN) FUEL ENTERING WHEEL EARLY, VALVE CHANGED. LIGHT OFF OCCURING NOW AT 17 PERCENT NG (NORMAL).SDR CA040805007Injector · malfunctioned(CAN) POOR STARTS REPORTED. SPRAY PATTERN ON START INJECTORS FOUND POOR. NEW INJECTORS INSTALLED AND SHIMMED.SDR HCM2004F00001Chip Detector · contaminatedON MARCH 20, 2004 WHILE ON A SIGHTSEEING FLIGHT, THE PILOT EXPERIENCED AN ENGINE CHIP LIGHT INDICATION. HE MADE A PRECAUTIONARY LANDING AT APPROXIMATELY 12:50 PM. A MECHANIC WAS DISPATCHED TO THE SITE AND INSPECTED ALL CHIP PLUGS. A SMALL SLIVER WAS FOUND A
Back to Turbomeca ARRIEL-1D1