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 KBM2005F00026Bearing · crackedCRACKED .6666 THE WAY DOWN THE NUT SIDE OF FORK. REMOVED AND REPLACED. (K)SDR AUS20040113Servo · faulty(AUS) TAIL ROTOR SERVO FAULTY. INVESTIGATION FOUND ALTHOUGH FULL TAIL ROTOR PEDAL CONTROL WAS AVAILABLE, THE ACTUATOR GAVE LIMITED OUTPUT.SDR KBM2005F00023Inertia Reel · brokenINERTIA REEL IS BROKEN, REMOVED AND REPLACED. (K)SDR KBM2005F00035Power Supply · burned outSMOKED POWER SUPPLY INTERNAL INPUT, REMOVED AND REPLACED. (K)SDR KBM2005F00030Light · inoperativeEXTERIOR LIGHT INOPERATIVE, REMOVED AND REPLACED. (K)SDR KBM2005F00028Gyro · malfunctionedDG ROTATES 180 DEGREES IN STRAIGHT AND LEVEL FLT. REMOVED AND REPLACED. (K)SDR CA030910010Flex Coupling · cracked(CAN) DURING ROUTINE INSPECTION, A SMALL MARK, SLITE DENT WAS FOUND ON THE OUTER DISC OF THE FLEX COUPLING FURTHER INVESTIGATION FOUND THAT THIS DENT HAD SET UP A STRESS RISER IN WHICH HAD CAUSED THE DISC TO CRACK THE COUPLING WAS REPLACED WITH NEW PARTS AND SDR BAQA088146Compressor · wornMODULE 2 DUE CHANGE FOR WEAR AT BLEED AIR DUCT. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT.SDR KBMA088331Bleed Valve · stuckBLEED VALVE FLAG SHOWING, SUSPECT BLEED VALVE WONT CLOSE. INSTALLED SERVICEABLE BLEED VALVE .SDR KBM2003F00011Pump · leakingNO NR 1 BOOST PUMP LEAKING (1 DROP IAW SECOND). DEFUELED, REMOVED AND REPLACED GASKET (PN 350A55-1103-22). ORINGS (PN 81811050) REFUELED AIRCRAFT. OPS CHECK GOOD.(K)SDR CDBR084854Belt · failedAIR CONDITIONING BELT FAILED CAUSING DAMAGE TO THE HYDRAULIC BELT.SDR CA030317006Cable · broken(CAN) CARGO HOOK SWING SUSPENSION SYSTEM: WHILE SLING THE LOAD WAS RELEASED DUE TO THE DAMAGE OF THE MANUAL HOOK RELEASE CABLE. IN THE INVESTIGATION IT WAS FOUND THAT WITH THE ONBOARD CARGO HOOK ASSEMBLY HOOK RELEASE CABLE CONTACTS THE SUSPENSION FRAME IN THE SDR HEEA083533Engine · making metalNR 2 ENGINE FAILED CHIP CHECK. TO BE SENT TO VENDOR FOR REPAIR.SDR CA030319002Pressure Switch · inoperative(CAN) PILOT WAS LONG LINING, DIRECTING ATTENTION TO VERT REF WINDOW. A/C SUDDENLY PITCHED UP, CONTROLS BECAME STIFF. THERE WAS NO HORN OF ANY KIND, NOR WAS HYD PRESS DROP WARNING LIGHT (HYD LIGHT)ON WARNING CAUTION ADVIS PNL. PILOT CONTINUED TO EVALUATE PROBLSDR AC2A081172Seal · leakingENGINE STARTED LEAKING OIL AFTER OIL FLOW CHECK. REPLACED SEALSDR CA021125006Bell Assy · cracked(CAN) WHILE COMPETING A DAILY INSPECTION ON THE AIRCRAFT THE ENGINEER NOTICED A CRACK ON THE DRIVE END BELL ON THE STARTER GEN.SDR KBMA115449Fuel Control · leakingDECEL LEAKING CONTINUOUSLY. REPLACED FUEL CONTROL.SDR FF6R112443Gear · dentedPINION HAS DENT ON END OF SHAFT. BEVEL RING GEAR HAS CHATTER MARKS IN 7 HOLES.SDR 3W2324Blade · crackedTAIL ROTOR BLADE ASSEMBLY HAS CRACK IN SKIN. ORDER NEW TAIL ROTOR BLADE.SDR CA020827007Bearing · spalled(CAN) DURING FLIGHT AN ENGINE CHIP LIGHT OCCURRED. PILOT LANDED AS SOON AS PRACTICAL. ENGINEER FOUND THAT ALL THE ENGINE CHIP PLUGS HAD METAL. ENGINE CHIP PLUGS WERE CLEANED AND THE ENGINE WAS RUNUP AGAIN. ENGINE WAS RUN AND SHUT DOWN TO INSPECT THE CHIP PLUSDR KBMA117643Pump · inoperativeFUEL PRESSURE CAUTION LIGHT INDICATION IS ON. FUEL PUMP IS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT.SDR AUS20020632Pump · fod(AUS) ENGINE OIL PUMP INLET FOD. INVESTIGATION FOUND A SMALL PIECE OF RUBBER TUBING LODGED IN THE OIL PUMP INLET, RESTRICTING OIL FLOWTO THE PUMP. ENGINE WAS BEING GROUND RUN FOR INSTALLATION FOLLOWING REPAIR. PERSONNEL/MAINTENANCE ERROR.SDR CA020627001Bellcrank · cracked(CAN) CRACK FOUND AFTER INSPECTION ON T/R BELLCRANK. THE CRACK IS ON THE WEB OF THE SHORT ARM OF THE BELLCRANK. THE TSN OF THE BELLCRANK IS FROM THE AIRFRAME TIME.SDR HEEA079285Inlet Screen · brokenENGINE INLET SCREEN HAS BROKEN STRANDS.SDR AUS20020343Pipe · loose(AUS) P2 REGULATOR PIPE FROM THE COMPRESSOR SCROLL TO THE FCU LOOSE.PERSONNEL/MAINTENANCE ERROR.SDR HEEA078002Engine · damagedNO N1 INDICATION NOISE WHEN TURNING ENGINE.SDR HEEA077705Valve · failedENGINE WOULD START INTERMITTENTLY.SDR ULX2002F00000Fuel Control · leakingDURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, DIRECTLY UNDER THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS NECESSARY TO CORRECT THIS PROBLEM. MFG HAS NOT OFFERED A SDR ULX2002F00001Fuel Control · leakingDURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, DIRECTLY UNDER THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FUEL CONTROL UNIT WAS LEAKING FROM THE FUEL CONTROL UNIT DRAIN. SDR ULX2002F00002Fuel Control · leakingDURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, DIRECTLY UNDER THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FUEL CONTROL UNIT WAS LEAKING FROM THE FUEL CONTROL UNIT DRAIN. RSDR HEEA077553Metering Valve · leakingFUEL CONTROL METERING VALVE HAS INTERNAL FUEL LEAK.SDR HEEA077552Fuel Control · malfunctionedENGINE SLOW START DURING COLD WEATHER.SDR CA020104004Wire · burned(CAN) JUST PRIOR TO LDG PILOT SMELLED SOMETHING LIKE PLASTIC OR RATHER BURNING BUT NOT SMOKE. AFTER SHUTTING DOWN, PILOT COULD SEE SMOKE INSIDE TAILBOOM & STRONG SMOKE OF SOMETHING ELECTICAL SMOKING IN MAIN CARGO BAY, PILOT INVESTIGATED FURTHER TO FIND SOURSDR VE32002F00000Fuel Control · leakingDATE: 12-3-2001, AFTER INSTALLATION, WITH BOOST PUMPS ON, FUEL WAS NOTICED LEAKING FROM THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FCU WAS SDR VE32002F00001Fuel Control · leakingDATE: 11-20-2001, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FSDR VE32002F00002Fuel Control · leakingDATE: 11-28-2000, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. FURTHER ON THE GROUND, UNDER THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU SDR VE32002F00003Fuel Control · leakingDATE: 11-27-2001, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FSDR VE32002F00004Fuel Control · leakingDATE: 11-30-2001, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. FURTHER INSPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FSDR VE32002F00005Fuel Control · leakingDATE: 2-9-2001, DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, UNDER THE ENGINE DECK DRAIN. FURTHER INSPECTION IFENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS LEAKING FROM THE FCU DRAIN. REPLACEMENT OF THE FCUSDR CA011116010Bellcrank · cracked(CAN) AS PER A COMPANY MEMO TO CHECK THIS LEVER/BELLCRANK FOUND ANOTHER ONE CRACKED IN THE SAME REGION (SEE ATTACHED DOCUMENT). NOTE: THE FIRST SDR SUBMITTED THE ARROWS WERE POINTING IN THE WRONG REGION. THE ARROWS SHOULD BE MORE OUTBOARD FROM WHERE THEY WERE SDR HEEA076956Engine · making metalENGINE MAKING METAL.SDR CA011017002Bellcrank · worn(CAN) TAIL ROTOR PITCH CONTROL PUSH-PULL TUBE ROD END BEARING STAKING SLEEVE WORE A CIRCULAR GROOVE INTO THE EAR / CLEVIS OF THE BELLCRANK THAT IS MOUNTED ON THE T/R GEARBOX.SDR HEEA076249Valve · malfunctionedNG AND TORQUE FLUCTUATIONS. PENDING VENDOR RETURN.SDR VE32001F00000Module · failedMO2 AND MO3 WERE REPLACED ON ENG. GRND RUNS WERE PERFORMED. VIBR TESTS AT FRONT AND RR PNTS WERE NML. OIL PRESS TESTS WERE NML. OIL FLOW AT RR BRG WAS MEAS AT 180 ML. NO FUEL OR OIL LKS NOTED ON ANY OF GRND RUNS. AT APPROX. 1000 FT AGL, AND ENG CHIP LISDR CA010827008Chip Detector · activated(CAN) ENGINE CHIP LIGHT IN FLIGHT. CHIPS FOUND ON UPPER ELECTRICAL CHIP PLUG, MO5 AND ENGINE OIL TANK PLUGS. ENGINE REMOVED FOR EVALUATION.SDR JPB2001F00000Solenoid Valve · damagedPILOT AND CREW SMELLED JET FUEL, SOON AFTER THE AIRCRAFT LOST PARTIAL POWER. MAINTENANCE FOUND THAT THE THREADS ON THE IGNITION SOLENOID VALVE/PURGE VALVE WERE DISTORTED AND LETTING FUEL PASS AROUND THE PACKING. UNIT WAS REPLACED WITH NEW PART.SDR 1Transmitter · inoperativeNO ENGINE OIL PRESSURE INDICATION DURIN ENGINE START SEQUENCE.THE OIO PRESSURE TRANSMITTER WAS REPLACED ON MORE THAN ONE TIME, BUT THE NEW TRANSMITTER WERE BAD FROM OVERHAULED FACILITY.SDR CA011116009Bushing · debonded(CAN) BOLT P/N 22208BC10001GL BACKED OUT ALLOWING DEBONDED BUSHING P/N 704A33-633-160 TO MOVE OUTWARD APPROXIMATELY 1/4 INCH ON THE OUTBOARD END OF THE RED ARM. DAMAGE WAS DISCOVERED ON A DAILY INSPECTION. PILOT HAD COMPLAINED OF VIBRATION ON GROUND WHILE RUNNSDR B3OR20010004Thermocouple · out of toleranceAIRCRAFT HAD SUFFERED A SERIES OF HUNG STARTS, ENGINE WOULD HANG UP AT 30%. IF THE ENGINE WOULD START, IT WOULD BE A SLOW START. USUALLY, THE PILOT WOULD REACH THE STARTER TIME LIMIT OF 45 SEC'S BEFORE THE ENGINE WOULD START AND BE SELF-SUSTAINING,AND HE WOULDSDR HEEA073515Fire Detector · intermittentINTERMITTENT.
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