Turbomeca ARRIEL-1D
Service difficulty reports · 252
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 = 'ARRIEL1D' 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 = 'ARRIEL1D' 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 98ZZZX4351Cover · crackedDURING ROUTINE 100 HOUR INSPECTION, THE COMPRESSOR IMPELLER WAS INSPECTED DUE TO THE RECENT PROBLEMS WITH COMPRESSOR COVER CRACKING. THE IMPELLER WAS FOUND UNSERVICEABLE DUE TO THE COMPRESSOR COVER BEING CRACKED AND HAD TO BE REMOVED FROM SERVICE. SUBMITTER SDR HCMA0000227Igniter · wornIGNITER IS WORN BEYOND LIMITS. (X)SDR 98ZZZX3997Manifold · failedMECHANIC WAS PERFORMING A DAILY INSPECTION AFTER A FLIGHT AND FOUND THE COMPRESSOR WOULD NOT ROTATE, THE ENGINE WAS SEIZED. AFTER THE ENGINE COOLED, COMPRESSOR TURNED FREELY, BUT THE REPAIR IS TO CHANGE THE GAS GENERATOR AND THE COMPRESSOR AS AN ASSY. SUBMITSDR 98ZZZX4352Cover · crackedAFTER ROUTINE 100-HOUR INSPECTION, THE SUBSEQUENT GROUND RUN REVEALED AN ODD NOISE COMING FROM THE ENGINE. A THOROUGH INSPECTION WITH BORESCOPE THROUGH THE COMPRESSOR BLEED VALVE OEPNING OF MODULE MO3 REVEALED A PIECE OF THE COMPRESSOR COVER IN FRONT OF THE CSDR HEEA0015987Screen · damagedINTAKE SCREEN HAS SEVERAL BROKEN WIRES AND CHAFING.SDR HCMA062001Bearing · crackedBEARING CRACKED BEYOND LIMITS.SDR 98ZZZX4084Manifold · failedDURING A DAILY INSPECTION, MECHANIC COULD NOT TURN THE COMPRESSOR FREELY. THIS ACFT JUST RETURNED FROM A FLIGHT. IT HAD BEEN SHUT DOWN APPROX 45 MINUTES. THE ENGINE WAS SEIZED. THE REPAIR IS THE REPLACEMENT OF THE COMPRESSOR AND THE GAS GENERATOR ASSY. AFSDR 98ZZZX4080Blower · inoperativeAIR CONDITIONING SYSTEM DOES NOT COOL AIRCRAFT. BLOWS HOT AIR. FOUND 1 OF 2 CONDENSOR BLOWER MOTOR ASSEMBLIES INOPERATIVE. THE 2-BLOWER MOTOR ASSEMBLIES WERE INSTALLED AT THE SAME TIME. THEY BOTH HAVE 14.1 HOURS OF USE SINCE OVERHAUL. THE REPORTED MOTOR ASSDR CA980811014Line · cracked(CAN) DURING INSPECTION, A FUEL LEAK WAS FOUND ON THE FUEL INJECTOR LINE AT THE FLAIRED AREA NEAR THE B-NUT. THE LINE WAS REPLACED.SDR 98ZZZX2586Detector · failedDURING 500-HOUR T INSP' INSPECTION OF 3 OF THE 6 ENGINE FIRE DETECTORS WERE FOUND DEFECTED PER TURBOMECA MM CHAP 26-11-00 PARA 1 INSPECTION PROCEDURES. TWO WERE OVERHEATED AND ON ONE THE OHMS WERE TOO LOW. SUBMITTER STATED THE OPERATOR BELIEVES THEY SHOULD HSDR 98ZZZX2587Detector · failedDURING 500-HOUR T INSP' INSPECTION OF 3 OF THE 6 ENGINE FIRE DETECTORS WERE FOUND DEFECTED PER TURBOMECA MM CHAP 26-11-00 PARA 1 INSPECTION PROCEDURES. TWO WERE OVERHEATED AND ON ONE THE OHMS WERE TOO LOW. SUBMITTER STATED THE OPERATOR BELIEVES THEY SHOULD HSDR HCMA061987Pin · wornEXPANSION PIN PART HAS EXCESSIVE PLAY.SDR HCMA061984Rod · wornPC LINK BALL JOINT WORN BEYOND LIMITS.SDR 98ZZZX3090Exciter · failedEXCITER INOPERATIVE. WILL NOT SPARK AT PROPER FREQUENCY. UNIT HAS CONTINUOUS SPARK MOST OF THE TIME. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 98ZZZX2349Line · crackedNOTICED FUEL ON ENGINE DECK. FUEL WAS RUNNING DOWN FROM TOP OVER ENGINE DURING START. FOUND LEFT FUEL INJECTOR LINE CRACKED AT TOP FLARE. SUBMITTER STATED THIS IS THE THIRD ONE OF THESE THEY HAVE HEARD ABOUT IN THE SAME AREA AND SUGGESTED MANUFACTURE FLARE SDR HEEA0013614Magnetic Seal · leakingMAGNETIC LEAKING.SDR HEEA0012970Engine · making metalRECURRING METAL ON UPPER ELECTRICAL PLUG AND ON ELECTRICAL PLUG AT ENGINE OIL TANK. CHROME FLAKES IN OIL FILTER.SDR HEEA0011825Engine · making metalS.O.A.P SAMPLE SHOWED HIGH IRON AND OTHER METAL CONTENT.SDR HEEA0011836Bearing · crackedREAR BEARING P.T. NGV CRACKED AT 6:00 POSITION BEYOND LIMITS. DURING BORESCOPE INSPECTION OF COMB. CHAMBER SWIRL PLATE, FOUND CRACK OF ABOUT 90 DEGREES.SDR HEEA0011117Bleed Valve · malfunctionBLEED VALVE FLAGGING TOO SOON, POPPING AT LOW RPM.SDR 97ZZZX4348Circlip · missingDURING CLEANING OF REAR BEARING SUPPORT ASSEMBLY, INSPECTION FOUND THE CIRCLIP THAT HOLDS REAR BEARING POWER TURBINE GUIDE VANE MISSING. SUSPECT CAUSE: DURING LAST MAINTENANCE PROCEDURES BY TURBOMECA CO., CIRCLIP WAS NOT INSTALLED. A/C TT: 1,699.5 HOURS. ESDR 97ZZZX3769Bearing · failed15.9 AIRCRAFT FLIGHT HOURS AFTER CHANGING 2-3 MODULES. ALL ENGINE CHIP PLUGS HAD METAL ON THEM. ENGINE REPAIRED AND NOTIFIED THAT FREE TURBINE BEARING HAD FAILED. PART TOTAL CYCLES, 8,080.SDR CA970630001Seat Belt · frayed(CAN) EDGES OF SEAT BELT WERE FOUND FRAYED - DUE TO THE BELT GUIDE ON THE REEL BEING BROKEN AND MISSING.SDR 97ZZZX2723Compressor · damagePICKED UP HIGH FREQUENCY VIBRATION WHILE HOVERING TO MAINTENANCE HANGAR. UPON INSPECTION, FOUND FOD DAMAGE TO COMPRESSOR. SUSPECTED CAUSE IS ROTOR WASH KICKED UP FOD.SDR HAIHEEA9753Fuel Control · defectiveENG WOULD NOT START AFTER FIRST SHUTDOWN. FUEL CONTROL FAULT.SDR HEEA978966Igniter Plug · defectiveINTERMITTENT SPARKLE.SDR HEEA978967Igniter Plug · defectiveINTERMITTENT SPARKLE.SDR HEEA978845Grid Valve · inoperativeENG VALVE GRID INOPERATIVE.SDR CA970121010Inlet Duct · lost in flight(CAN) STARTER GENERATOR AIR INLET DUCT WAS LOST IN FLIGHT. SUSPECT CAUSE OF SEPARATION IS LOOSENING OF SECURING CLAMP.SDR 97ZZZX4138Module · cokingAFTER NORMAL SHUT DOWN OF ENGINE, THEN NORMAL START OF ENGINE, HEARD GRINDING NOISE IN ENGINE 15-20 PERCENT NG; AT ABOUT 25 PERCENT NG, ENGINE SLOWED WITH NORMAL BATTERY VOLTAGE. START ABORTED. FOUND BY MANUAL TURNING OF GAS GENERATOR AND AT HOT TEMP OF ENGISDR 97ZZZX2374Compressor · cover brokenENGINE WAS PRODUCING AN ODD NOISE AND HAD A HIGH FREQUENCY VIBRATION. PREVIOUS VIBRATION CHECK WITH BRUEL AND KSAER VIB METER 64.4 HRS EARLIER WAS WITHIN LIMITS. INSPECTED COMPRESSOR WITH BORESCOPE THROUGH BLEED VALVE HOLE AND FOUND TAB ON CENTRIFUGAL COMPRESDR 97ZZZX2375He Generator · failedACFT TT 5,043.8 HOURS. HELICOPTER FAILED TO START. AFTER TROUBLESHOOTING, FOUND BOTH IGNITERS DEFECTIVE AND H.E. GENERATOR (EXECUTER BOX) INOPERATIVE. H.E. GENERATOR HAD 399.0 HRS SINCE NEW. PAPERWORK WAS SUBMITTED TO MANUFACTURE FOR WARRANTY.SDR HEEA968167Engine · making metalLOW OIL PRESSURE, STARTING TO MAKE METAL ON UPPER ELECTRIC PLUG.SDR HEEA968168Engine · making metalMAKING METAL IN OIL AND FILTER.SDR 97ZZZX94Bearing · port blockedIN-FLIGHT OIL PRESSURE FLUCTUATED UP TO 8 BARS, PILOT LANDED AND MAINT CALLED, PERFORMED OIL FLOW CHECK. RESULT, 18 CC. REMOVED ENG AND DISASSEMBLED, FOUND REAR BEARING OIL DELIVERY PORT IN BEARING CAGE COMPLETELY BLOCKED BY COKING. SUBMITTER RECOMMENDS ENLSDR CA960910041Vent Pipe · plugged(CAN) PILOT REPORTED SMOKE COMING FROM ENGINE REAR BEARING AREA.OIL LEAKAGE AT VENT PIPE ATTACH FLANGE. VENT PIPE REMOVED AND FOUND PLUGGED WITH CARBON DEPOSITS. CLEANED AND REINSTALLED.SDR HCMA9655Ignitor · defectiveIGNITOR INOP.SDR 97ZZZX121Module · bearing roughDURING ENG COAST DOWN, UNUSUAL NOISE WAS HEARD. ROTATION OF FREE TURBINE WAS NORMAL, COMPRESSOR ROTATION WAS ROUGH. SUSPECTED REAR BEARING, BUT DID A BORESCOPE TO CHECK TURBINE WHEELS AND NOZZLES. FOUND CRACK IN 2ND STAGE GAS GEN STATOR/NOZZLE OUTER RING. SDR HCMA9644Spider · bindingT/R P/C SPIDER BINDING WHEN RIGHT PEDAL IS APPLIED.SDR HCMA9645Spherical Stop · crackedSPHERICAL STOPS ARE CRACKING.S/N 9528,9529,&9527SDR HCMA9646Servo · defectiveSERVO IS SEEPING BEYOND LIMITS. REPLACEMENT PART IS ON ORDERSDR HCMA9651Gyro · defectiveINOP. SEE JUDY SMITH FOR REPLACEMENT PART DATA.SDR HCMA9622Lamification · rubber tornLAMIFICATION RUBBER IS TORN BEYOND LIMITS.SDR HEEA966801Engine · oil lossLOSS OF OIL OUT OF TAIL PIPE, BLEED VALVE AND COMPRESSOR.SDR HCMA9612Seal · defectiveSEAL IS DEFECTIVE. SEAL IS LEAKING.SDR CA960212102Engine · flamed out(CAN)ENGINE FLAMED OUT ON APPROACH AT 8,000 FEET ALTITUDE. OAT 20 DEGREES. ENGINE WAS RUNNING NORMAL PRIOR TO LANDING. PILOT PULLED ON COLLECTIVE TO CHECK HIS DESCENT WHEN THE LIGHTS AND HORN CAME ON AND E NGINE FLAMED OUT. FUEL INSPECTED FOR ICE AND WATER, BUSDR 96ZZZX523Fuel Control · defectiveOCCASIONAL SMOKE AND FUEL SMELL EMITTING FROM HEATER OUTLET. REPLACED WITH NEW FCU, CORRECTED PROBLEM.SDR HEEA956049Engine · malfunctionDURING ENGINE START, WHEN THE START BUTTON IS PRESSED AND FFC LEVER WAS ADVANCED, NORMAL IGNITION AND ACCELERATION WOULD OCCUR UNTIL REACHING 25 TO 30% NG. AT THAT TIME ACCELERATION WOULD ALMOST STOP. THE ENGINE WOULD NOT ACCELERATE UNLESS THE T4 WAS KEPT ATSDR HEEA956050Engine · making metalENGINE CHIP LIGHT. FOUND TINY AMOUNT FERROUS SHINY FUZZ ON LOWER CHIP PLUG. FILTER HAD SMALLER AMOUNT OF SAME TYPE OF FUZZ. CLEANED AND COMPLIED WITH 30 MINUTE PENALTY RUN. ON REAR BEARING ELEC. PLUG FOUND TINY FERROUS SPECKS (ABOUT 15 EA)REINSTALLED ALL CSDR HEEA955717Engine · making metalENGINE MAKING METAL.
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