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 HEEA073516Exciter · inoperativeINOPERATIVE.SDR HEEA073518Magnetic Seal · leakingLEAKING.SDR HEEA073519Magnetic Seal · leakingLEAKING.SDR CA010711006Valve · seized(CAN) FAILED TO OPERATE WHEN TESTED (PARTICLE SEPARATOR ACTUATOR).ENGINE INTAKE.SDR HEEA073011Blade · crackedCRACKED COMPRESSOR BLADE.SDR HEEA073012Blade · crackedCRACKED COMPRESSOR BLADE.SDR HEEA072890Turbine · failedHIGH OIL CONSUMPTION. SENT TO TURBOMECA FOR CREDIT AGAINST REPLACEMENT PART PURCHASED.SDR HEEA072891Turbine · failedHIGH OIL CONSUMPTION. SENT TO TURBOMECA FOR CREDIT AGAINST REPLACEMENT PART PURCHASED.SDR CA010518003Pump · failed(CAN) NR 2 FUEL BOOST PUMP WAS FOUND TO BE EXCESSIVELY NOISY DURING POST FLIGHT INSPECTION. PUMP WAS REMOVED FOR REPAIR AS THIS NOISE IS A SIGN OF IMPENDING FAILURE. REPLACEMENT PUMP INSTALLED.SDR CA010529020Spacer · corroded(CAN) WHEN THE HOOK ARRIVED AT E.C.L., THE SCREW AND NUT WHICH TIGHTEN THE SPACER (P/N S1609-19) HAD BEEN LOOSENED. IT WAS TIGHTENED TO PERFORM INCOMING TESTS. THE CAM WHICH RELEASES THE LOAD BEAM WOULD NOT FUNCTION UNDER LIGHT LOAD (12 LBS). AS THE LOAD WAS ISDR WPO12001B2579Sleeve · wornSB CALLS FOR THE INSTALLATION OF A SLEEVE IN THE BLEED VALVE BOSS. THIS SLEEVE DEVELOPED ROTATIONAL MOVEMENT AND CAUSED WEAR DAMAGE TO ITSELF, THE BOS ON M02, AND TO THE BLEED VALVE. THIS SLEEVE WAS INSTALLED AT TIME OF MANUFACTURE.SDR CA010504020Bracket · cracked(CAN) UPON INSPECTION, THE EIGINEER NOTICED A CRACK ON THE NR 5 T/R HANGAR BEARING SUPPORT BRACKET.SDR CA010504021Bracket · cracked(CAN) UPON INSPECTION THE ENGINEER NOTICED A CRACK ON THE HYDRAULIC PUMP MOUNTING BRACKET. THE CRACK SEEMS TO ORIGINATE FROM TOOL MARKS CAUSED BY MAINTENANCE.SDR CA010323002Control Cable · broken(CAN) MANUAL / EMERGENCY RELEASE CABLE SHEATH BROKEN AWAY FROM FERRULE / SLEEVE WHERE CABLE ASSEMBLY ATTACHES TO THE CARGO HOOK.THE CARGO SUSPENSION SYSTEM (SWING) ALLOWS FOR A LOT OF MOVEMENT OF THE CARGO HOOK. THERE APPEARS TO BE A LOT OF FLEXING OF THE CABLSDR CA010302007Filter · clogged(CAN) - UPON HOVERING IN AERIAL LONG LINE WORK. THE PILOT NOTICED SOME FEEDBACK IN CYCLIC CONTROLS WHEN INPUTING AGGRESSIVE MOVEMENTS (I.E. WINDY CONDITIONS). HE IMMEDIATELY ABORTED THE TASK AT HAND AND LANDED.- ON INSPECTION OF HYDRAULIC FILTER FOUND A BLACK SDR KBMA9743410Strut · damagedSTRUT DAMAGED DUE TO COMPRESSOR CLUTCH.SDR 20010208CW004Chip Detector · contaminatedJAN 9, 2001 WHILE ON A SIGHTSEEING FLIGHT, THE PILOT EXPERIENCED AN ENGINE CHIP WARNING. HE MADE A PRECAUTIONARY LANDING. A MECHANIC WAS FLOWN TO THE SCENE AND A SMALL HAIRLIKE SLIVER WAS FOUND ON THE MAGNETIC PLUG. THE CHIP PLUG WAS CLEANED AND THE AIRCRAFSDR 20010122CW015Connector · looseDURING A TOUR FLIGHT WITH 4 PASSENGERS ON BOARD, PILOT NOTICED A HIGH ENGINE OIL TEMPERATURE READING. HE ELECTED TO PERFORM A PRECAUTIONARY LANDING. UPON INSPECTION, THE MECHANIC FOUND THE SPADE CONNECTION LOOSE AND IT HAD MOISTURE ON IT. CONNECTION WAS TISDR CA010518004Servo · leaking(CAN) ROUTINE DAILY INSPECTION REVEALED EXCESSIVE LEAKAGE FROM MAIN ROTOR SERVO. SERVO REMOVED FOR REPAIR.SDR R8RR010147Gas Generator · cokedAFTER LANDING AND SHUT DOWN, THE MECHANIC CHECKED THE COMPRESSOR FOR FREEDOM OF ROTATION. THE COMPRESSOR WAS SEIZED. SUSPECT FUEL INJECTION WHEEL COKING. (X)SDR 20001018SH030Servo · bindingSERVO CONTROL REMOVED DUE TO CYCLIC BINDING. (X)SDR 20000918SH030Fuel Control · leakingFUEL CONTROL ASSY LEAKING FUEL BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR CA000726003Wheel · coked(CAN) THIRD OCCASION THAT THE COMPRESSOR SECTION HAD BECOME DIFFICULT TO TURN DUE TO COKING AROUND LABYRINTH SEAL AT INJECTION WHEEL. ONLY SOLUTION IS TO REMOVE ENGINE M.O.2 SECTION SENT TO OVERHAUL FACILITY FOR REPAIR. TURBOMECA IS NOW LOOKING INTO THIS PROBSDR CA000731017Nut · flaking(CAN) THERE WERE 2 REPORTED ENGINE CHIP LIGHTS BOTH FROM THE NR 2 CHIP PLUG. THE FIRST OCCURED AT A/F TIME 6540 MINOR AMOUNT OF METAL OR FUZZ. THE SECOND (10 HOURS LATER) FOUND THE GAP ON CHIP DETECTOR 50 PERCENT FULL OF METAL. THE BOTTOM AND REAR CHIP DETECTOSDR 20000510SH021Chip Detector · defectiveWHILE PILOT FLYING ON TOUR FLIGHT, NOTICED AN ENGINECHIP LIGHT ILLUMINATED. PILOT IMMEDIATELY MADE PRECAUTIONARY LANDING. INSPECTED AIRCRAFT AND FOUND THAT ENGINE CHIP PLUG HAD A DEFECT. CLEANED CHIP PLUGS AND C/W OPERATIONAL CHECK AND FUNCTIONALLY CHECKESDR CA000412004Vent Line · broken(CAN) ENGINE REAR BEARING VENT LINE SNAPPED OFF DURING FLIGHT AND WAS LATER DISCOVERED THAT THE VENT LINE WENT INTO THE TAIL ROTOR. THE PREVIOUS DAY THE VENT LINE CLAMP HAD BROKE AND IT WAS THEN NOTED THAT THE VENT LINE HAD CHAFE WEAR MARKS CAUSED BY THIS CLASDR 20000407SH008Bolt · backed outPOST-FLIGHT DAILY INSPECTION REVEALED ENGINE FREEWHEEL AT FLANGE ATTACH BOLT UNSCREWED FROM THE TORQUED AND SAFTIED POSITION. DAMAGED PIECES INCLUDE FREEWHEEL SHAFT, T/R SHORT SHAFT ASSY, AND FLANGES, AFT FREEWHEEL BEARING, AFT MAG SEAL, T/R LONGSHAFT SPLINESSDR CA000301002Engine · making metal(CAN) ENGINE MAKING METAL; PARTICLES TYPE 111 FOUND ON TU 208 CHIP DETECTOR,AWAITING OPERATOR TEARDOWN REPORT FROM TURBOMECA GRAND PRAIRIE TEXAS.SDR CA000301001Compressor · chafed(CAN) AXIAL COMPRESSOR AND GAS GENERATOR REMOVED FOR INTERNAL RUBBING NOISE. MOD TU202 COMPLIED WITH.SDR 2000ZZZX746Fcu · leakingFCU LEAKING FUEL BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 2000ZZZX119P2 Line · failedDURING FLIGHT, PILOT EXPERIENCED LOW MAIN ROTOR SPEED CONDITION WITH AURAL WARNING. PILOT THEN LOWERED COLLECTIVE CONTROL AND MAINTAINED OPERATING SPEED OF ROTOR SYSTEM. AT THAT TIME, HE ELECTED TO TAKE GOVERNOR OUT OF THE AUTO POSITION AND INTO MANUAL OVERRISDR 20000406SH044Pump · failedBOOST PUMP FAILED DURING CRUISE FLIGHT. REMOVED AND REPLACED. (X)SDR CA991028031Bearing · rough(CAN) DURING COMPLIANCE WITH DGAC AD 99-085-076(A)R1, FOUND T/R PITCH CHANGE SPIDER BEARING WAS VERY ROUGH/DRY. BEARING REPLACED.SDR 99ZZZX3969Blade · failedHELICOPTER WAS ON A FINAL APPROACH TO LANDING SITE ON ISLAND OF KAHOOLAWE, HAWAII. PILOT EXPERIENCED A YAW TO THE ACFT. HE MADE A NORMAL LANDING ON THE HELIPAD AND SHUT DOWN ENGINE. POST-FLIGHT CHECK REVEALED THE POWER TURBINE BLADES WERE DAMAGED. UPON DISSDR 99ZZZX4167Bleed Valve · inoperativeBLEED VALVE INOPERATIVE. CLOSES AT 98 PERCENT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR QKLA0000032Gear · damagedGEAR SET REPLACED AT THE FIRST OVERHAUL. SECOND GEAR SET REPLACED AT THE FIRST OVERHAUL WITH NEW PART. PART TOTAL CYCLES: 5,975.SDR 99ZZZX3557Bearing · failedDURING SIGHTSEEING FLIGHT, PILOT EXPERIENCED AN ENGINE CHIP WARNING ILLUMINATION AND MADE PRECAUTIONARY LANDING. UPON FURTHER EXAMINATION, MECHANIC DETERMINED THERE WAS SUFFICIENT METAL CONTENT ON MAGNETIC PLUG TO CEASE FURTHER FLIGHT UNTIL CORRECTIVE ACTION SDR CA990907024Line · cracked(CAN) DURING POST-FLIGHT INSPECTION, EVIDENCE OF FIRE DAMAGE WAS NOTED ON THE COMPRESSOR CASING WHICH WAS ATTRIBUTED TO A CRACKED FLARE ON THE FUEL FITTING LINE AT THE BOTTOM OF THE B-NUT. THE SOURCE OF IGNITION IS THOUGHT TO BE EITHER TO STARTER/GENERATOR ORSDR HEEA063410Igniter Plug · wornIGNITER SHOWS WEAR, BURNED, AND SIGNS OF ARCING. REPLACED WITH SERVICEABLE PART.SDR HEEA063411Igniter · wornTIP OF IGNITER WORN. REPLACED WITH SERVICEABLE PART.SDR 99ZZZX3771Fcu · malfunctionedNG FLUCTUATING 1 PERCENT TO 2.5 PERCENT.SDR 99ZZZX4165Fcu · leakingFCU LEAKING FUEL BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR HCMA066323Servo · defectiveSERVO CAUSED HARD OVER IN CYCLIC. REPLACEMENT PART WAS OFF SHELF IN O/H CONDITION.SDR CA990420008Bell Assy · wrong part(CAN) STARTER/GENERATOR REC'D FOR REPAIR AT 1056 HOURS TSO (1600 HOURS TBO) WITH WORN COMMUTATOR. UPON DISASSY/INSPECTION, LUCAS P/N 23032-1423 (A.D.E) END BELL ASSY WAS FOUND. THIS PART IS NOT APPROVED FOR INSTALLATION AND WAS FOUND WORN BEYOND LIMITS AT THSDR CA990219026Regulator · leaking(CAN) A FUEL LEAK WAS NOTICED UNDER AN ENGINE. CLOSER INSPECTION FOUND THAT WITH THE FUEL BOOSTER PUMPS ON, THERE WAS A FUEL LEAK FROM THE REGULATOR UNIT WHICH IS CONNECTED DIRECTLY TO A DRAIN ASSEMBLY. THIS FUEL LEAK IS NOT NORMAL. TURBOMECA ADVISED THE PASDR 99ZZZX1220Fcu · leakingFUEL COMING OUT OF P-2 SENSING LINE. FUEL SMELL IN COCKPIT HEATING SYSTEM.SDR CA990209001Line · cracked(CAN) FUEL LEAK DURING START. INSPECTION FOUND LEFT HAND FUEL INJECTOR LINE CRACKED. THIS LINE HAD NOT BEEN REMOVED SINCE INITIAL INSTALLATION AND THE ALIGNMENT WAS CORRECT.SDR CA990423012Engine · failed(CAN) ENGINE FAILURE ON TAKEOFF AT APPROXIMATELY 50 FEET. FLAME AND DEBRIS OBSERVED COMING FROM TAILPIPE, BY GROUND PERSONNEL. SUCCESSFUL AUTOROTATION EXECUTED. NO FURTHER DAMAGE. FAILURE APPEARS TO BE IN THE GAS PRODUCER SECTION. NO FURTHER INFO AT THISDR HCMA062017Bearing · wornBEARING IS DISTORTED OUT OF LIMITS.SDR CA990203009Turbine Wheel · failed(CAN) ENGINE FAILED IN-FLIGHT. POSSIBLE CAUSE WAS THE UNCONTAINED FAILURE OF THE TURBINE WHEEL. PART TC: 5,164.
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