Turbomeca ARRIEL-1C
Service difficulty reports · 48
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 = 'ARRIEL1C' 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 = 'ARRIEL1C' 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 OLJA2023060500301Bearing · failed#1 ENGINE LOSS OF OIL PRESSURE FOLLOWED BY THE #1 ENGINE FAILURE. AT APPROXIMATELY 2050L, COMPLETED AN UNEVENTFUL TAKEOFF UNDER NVGS FROM A NIGHT SCENE AT THREE SPRINGS, HUNTINGTON CO. WITH A MED CREW OF TWO AND ONE PATIENT WITH THE INTENDED DESTINATION OF UPMSDR CA120612015Bearing · failed(CAN) CHECKED CHIP PLUG AFTER 1.5 HRS OPERATING TIME, DUE TO METAL FOUND ON PLUG DURING 100 HR INSPECTION, REMOVED T/R GEARBOX AND INSTALLED SPARE. CHECKED TGB CONTROL ROD AT 100 HR INSPECTION IAW ASB 05-00-61 R1, AND FOUND MEASUREMENT TO BE CORRECT, FLUSHED SDR MHI2012F00000Turbine Blades · destroyedDURING TAXI BOTH PILOTS HEARD AN ABNORMAL WHINNING NOISE COMING FROM THE NR 1 ENGINE, IMMEDIATELY FOLLOWED BY A NR 1 ENGINE CHIP LIGHT. THEY SHUT THE ENGINES DOWN. UPON FURTHER INSPECTION THE FREE TURBINE WAS FOUND TO HAVE DESTROYED BLADES. IT WAS ALSO NOTESDR MHIA20120605001Engine · malfunctionedTHE AIRCRAFT WAS SCHEDULED FOR A CHARTER. WHILE TAXIING TO THE TAKEOFF SPOT BOTH PILOTS HEARD A LOUD NOISE COMING FROM THE NR 1 ENGINE FOLLOWED BY A CHIP LIGHT. THEY THEN SHUT THE ENGINES DOWN. THE ENGINE IS BEING FORWARDED TO THE ENGINE MANUFACTURER TO DETSDR QMLA2011072311080Connector · contaminatedTHE NR 1 GAUGE WENT TO ZERO WITH NO ASSOCIATED WARNING LIGHT WHILE IN CRUISE FLIGHT. THE PILOT IMMEDIATELY LANDED AT THE CLOSEST AIRPORT AND CALLED THE MECHANIC. THE MECHANIC INSPECTED THE ACFT AND FOUND SOME WATER IN THE 9 ALPHA CONNECTOR FOR THE INDICATOR.SDR QMLA2011061411064Cable · brokenPILOT NOTED ON ENGINE START, THAT THE NR 2 ENGINE NG INDICATION WAS 15 PERCENT LOWER THAN THE NR 1 ENGINE NG INDICATION. PERFORMED A NORMAL ENGINE SHUTDOWN AND CALLED MX. FOUND THE ANTICIPATOR CABLE BROKEN APPROX 5" FROM THE RT FWD SERVO. REPLACED THE ANTICSDR QMLA2011052011058Connector · looseAFTER LANDING AT A SCENE TO PICK UP A PATIENT, THE PILOT NOTICED THE NR 1 ENGINE OIL PRESSURE INDICATION DROP TO 0 PSI. THE PILOT IMMEDIATELY SHUTDOWN ACFT, AND CALLED MX. MX VERIFIED THE DISCREPANCY. INSPECTED THE ASSOCIATED WIRING AND ALSO REMOVED, CLEANESDR KY1R2011072510012Chip Detector · brokenON PREFLIGHT INSPECTION, PILOT FOUND M04 MAGNETIC DETECTOR TIP BROKEN FROM BASE. TIP OF THE DETECTOR WAS RETAINED BY THE MAGNETIC BASE, AND SUBSEQUENTLY REMOVED.SDR BAQA200700023Wire Harness · defectiveDURING LEVEL FLIGHT NR 1 ENGINE FIRE LIGHT ILLUMINATED. AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. AFTER MECHANIC INVESTIGATED FOR CAUSE FOUND ENGINE WIRING HARNESS TO BE DEFECTIVE.SDR BAQ2006F00003Engine · making metalENGINE CHIP DETECTOR ILLUMINATED ON GROUND. REAR BEARING ELECTRICAL DETECTOR AND ACCESSORY GEARBOX AND REDUCTION GEARBOX WERE INSPECTED WITH METAL FOUND ON REAR BEARING AND REDUCTION GEARBOX DETECTORS. PARTICULE ORIGINATION UNKNOWN AT THIS TIME. (K)SDR BAQ2006F00004Gearbox · making metalENGINE CHIP DETECTOR ILLUMINATED ON GROUND. REAR BEARING ELECTRICAL DETECTOR AND ACCESSORY GEARBOX AND REDUCTION GEARBOX WERE INSPECTED WITH METAL FOUND ON REAR BEARING AND REDUCTION GEARBOX DETECTORS. PARTICULE ORIGINATION UNKNOWN AT THIS TIME. (K)SDR AU510001643Coupling · cracked(AUS) TAIL ROTOR DRIVESHAFT FORWARD FLEXIBLE COUPLING CRACKED. INVESTIGATION FOUND MECHANICAL DAMAGE ON THE EDGE OF THE COUPLING AT ONE END OF THE CRACK. (OTHER CAUSE: MATERIAL - IMPACT DAMAGE ) (CASA NR 510001643)SDR AU510001872Probe · failed(AUS) NR 1 ENGINE T4 TEMPERATURE PROBE SEPARATED FROM ENGINE. LOCKING NUT STILL FIRMLY ATTACHED TO MOUNTING POINT. (CASA NR 510001872)SDR BAQ2005F00000Blade · crackedFOUND CRACK ON 1 SIDE OF T/R BLADE AT STA 540.00, CRACK EXTEND FROM DOUBLER BACK 4 INCHES ALONG STA 540. CORDWISE REF FIG. 1 OF AD 2002-25-51 AIRCRAFT WAS POST MOD. (K)SDR KBM2005F00014Indicator · intermittentATTITUDE INDICATOR, WILL NOT HOLD ATT, REMOVED AND REPLACED. (K)SDR BAQA088195Metering Valve · malfunctionedFUEL FLOW METER COULD NOT SET. WOULD NOT GIVE CORRECT BURN RATE. REPLACED WITH SERVICEABLE UNIT.SDR EGR2004F00001Blade · failedMAIN ROTOR BLADE FAILED. CONTINUITY TEST BETWEEN LEADING EDGE AND GROUND STRAP BOLT.SDR AUS20021401Windshield · bird strike(AUS) LT WINDSHIELD STRUCK BY SEAGULL IN THE LOWER RIGHT CORNER. WINDSHIELD CRACKED.SDR ZYW2002F00000Bleed Valve · leakingBLEED VALVE, AIR LEAKING OUT BODY. REMOVED AND REPLACED.SDR OLJ2001F00002Pump · malfunctionedPILOT DETECTED AN ODOR OF SMOKE IN CABIN OF AIRCRAFT AND PERFORMED A PRECAUTIONARY LANDING. MAINTENANCE WAS DISPATCHED TO AIRCRAFT. A MEDICAL PUMP WAS FOUND TO BE THE ORIGIN OF THE SMOKE. THE SYSTEM WAS DE-ACTIVATED AND THE DISCREPANCY WAS DEFERED TOTHE MELSDR OU1R01003Pressure Switch · failedAUX HYDRAULIC LIGHT ILLUMINATED INFLIGHT. AIRCRAFT MADE PRECAUTIONARY UNSCHEDULED LANDING TO VACANT PARKING LOT. CAUSED BY UNIT FAILURE.SDR OLJ2001F00001Pressure Switch · inoperativeAUX HYDRAULIC ILLUMINATED DURING CRUISE FLIGHT. PILOT PERFORMED A PRECAUTIONARY LANDING. MAINTENANCE WAS DISPATCHED TO THE SITE. MAINTENANCE FOUND PRESSURE SWITCH INOPERATIVE. THE SWITCH WAS REMOVED AND REPLACED AND THE SYSTEM WAS OPERATIONAL TESTED AND AISDR 20010130CW009Gearbox · failedINITIAL GRND RUN-UP, AFTER MJR INSP, A T/R GBX FAILURE WAS EXPERIENCED AFTER APPROX 15-20 MINUTES. AC JERKED SEVERAL TIMES ALONG THE YAW AXIS, WITH NR1 ENG RUNNING AT 68%NG AND NR2 AT 65%NG AN UNUSUAL NOISE WAS HEARD FRM TAIL ROTOR, SHUT DOWN WAS INITIATED,SDR OLJA574U001Hose · leakingFOUND ON DAILY INSPECTION, HYDRAULIC FLUID LEAKING FROM PRESSURE LINE TO NOSE LANDING GEAR ACTUATOR. PRESSURE LINE HOSE REPLACED IN NOSE LANDING GEAR ACTUATOR.SDR OLJA574U002Hose · leakingLT HYDRAULIC SYSTEM LEAK DURING AC RUN UP. TROUBLESHOOTING FOUND HYDRAULIC HOSE BETWEEN DISTRIBUTION MANIFOLD AND T FITTING IN HYDRAULIC BAY RUPTURED. REPLACED HOSE.SDR 20001016SH025Transmitter · intermittentFUEL PRESSURE INTERMITTENT. REMOVED AND REPLACED TRANSMITTER. (X)SDR 20000406SH006Drain Valve · leakingVALVE LEAKING AROUND SPLIT LINE OF CASING. (X)SDR 20000605SH008Generator · inoperativeHE GENERATOR INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 99ZZZX226Diffuser · damagedTEC TECH REP AT FACILITY TO C/W TU 202. SECOND STAGE NOZZLE INSTALLATION AFTER REMOVAL OF MODULES 2 AND 3 HEARD PIECES INSIDE ENGINE. UPON TEAR-DOWN OR SEPARATION OF MODULES 2 AND 3 FOUND DIFFUSER TO HAVE HOLE IN IT, 2 INCHES BY 6 INCHES. PARTS HAD LIBERATESDR MVH0064158Fcu · malfunctionedFUEL CONTROL INOPERATIVE. SLOW STARTS AND FLUCTUATING RPM.SDR MVH0064159Transmitter · not calibratedTRANSMITTER CALIBRATED IMPROPERLY.SDR MVH0064160Engine · making metalENGINE MAKING METAL AND MODULE 3 DUE TBO.SDR MVH0064153Sensor · malfunctionedOVERSPEED FAIL LIGHT ILLUMINATES INTERMITTENTLY.SDR MVH0064152Fcu · malfunctionedFUEL CONTROL INOPERABLE. HARD STARTS AND HOT STARTS FIRST START OF THE DAY.SDR MVH0064143Check Valve · leakingREPLACED VALVE FOR EXTERNAL LEAKING SN P171B. REMOVED VALVE SN P171B AND INSTALLED SERVICABLE VALVE , SN K575B.SDR MVH0064141Magnetic Seal · leakingMAG SEAL REMOVED FOR LEAKING.SDR MVH0064119Chip Detector · leakingCHIP PLUG LEAKS THROUGH BODY AND ELECTRODE IS LOOSE.SDR MVH0064099Transmitter · failedTORQUE TRANSMITTER SHORTED INTERNALLY.SDR MVH0064096Transmitter · reads lowTORQUE TRANSMITTER READS LOW.SDR 96ZZZX3174Igniter · tip wornIGNITER TIPS WORN. REPLACED 3 EACH. REMOVED AND REPLACED IGNITERS.SDR 96ZZZX3175Igniter · tip wornIGNITER TIPS WORN. REPLACED 3 EACH. REMOVED AND REPLACED IGNITERS.SDR 96ZZZX3176Igniter · tip wornIGNITER TIPS WORN. REPLACED 3 EACH. REMOVED AND REPLACED IGNITERS.SDR 96ZZZX2799Electrovalve · failedNR 2 ENGINE WOULD NOT HAVE T4 CLIMB UNTIL NG SHOWED 30 PERCENT, THEN RAPID RISE ONCE IGNITION OCCURRED. REPLACED START FUEL ELECTROVALVE.SDR 95ZZZX6499H. E. Generator · defectiveINTERMITTENT OPERATION OF H.E. GENERATOR.SDR EGRA95101Generator · inopHE GENERATOR INOPERATIVE . REPLACEDSDR HEEA955042He Generator · inoperativeHE GENERATOR INOPERATIVE.SDR HEEA954673Ignitor · defectiveDURING ROUTINE INSPECTION NOTED LH IGNITER DID NOT FIRE.SDR 96ZZZX562Fuel Control · fail testFCU FAILED MAXIMUM NG CHECK BY MINIMUM OF .8 PERCENT. MINIMUM CHECK OF 101.8 PERCENT MINUS NG EQUALS 101.0 PERCENT. REMOVED FCU FOR REPAIR.
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