Turbomeca ARRIEL-1S
Service difficulty reports · 93
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 = 'ARRIEL1S' 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 = 'ARRIEL1S' 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 AU510002121Connector · contaminatedNR 1 ENGINE FIRE WARNING SYSTEM GAVE FALSE INDICATIONS. SUSPECT CONNECTOR CONTAMINATED.SDR AU510001909Module · seized(AUS) NR 1 ENGINE, NR 2 AND NR 3 MODULES SEIZED. INVESTIGATION CONTINUING. (CASA NR 510001909).SDR AUS20040511Engine · making metal(AUS) ENGINE CHIP DETECTORS AND OIL FILTER CONTAMINATED WITH METAL. ENGINE WAS REPLACED.SDR AUS20040334Fitting · cracked(AUS) LT MAIN LANDING GEAR DOOR HINGE FITTING FAILED.SDR AUS20040263Fire Detector · faulty(AUS) NR 2 ENGINE FLAME DETECTOR FAULTY.SDR AUS20040130Drain Valve · leaking(AUS) ENGINE START DRAIN VALVE LEAKING DUE TO ORING SEAL FAILURE.SDR AUS20040008Bearing Race · cracked(AUS) LANDING GEAR INTERCONNECT ROD SPHERICAL BEARING INNER RACE CRACKED. FOUND DURING INSPECTION IAW AD/S-76/66 PT4.SDR AUS20040010Cap · cracked(AUS) MAIN ROTOR BLADE TIP CAP TOP SKIN CRACKED IN AREA ADJACENT TO THE ATTACHMENT DOUBLER. CRACK LENGTH 270MM (10.62IN). TIP CAP HAD DISBONDED INTERNALLY FROM THE METAL DOUBLER ASSEMBLY AND THE KEVLAR SKIN HAD CRACKED AND DELAMINATED.SDR AUS20031292Fire Detector · faulty(AUS) NR 2 ENGINE BAY FIRE DETECTOR FAULTY.SDR AUS20030898Line · cracked(AUS) NR 1 ENGINE FUEL INJECTOR FUEL SUPPLY PIPE CRACKED IN FLARE.SDR AUS20030627Pipe · cracked(AUS) ENGINE START FUEL INJECTOR PIPE FRACTURED AT FLARE UNDER (B NUT).SDR AUS20030527Pump · faulty(AUS) NR 1 HYDRAULIC SYSTEM PUMP FAULTY. HYDRAULIC FLUID LOST THROUGH PUMP CASE DRAIN.SDR AUS20030499Servo · leaking(AUS) TAIL ROTOR SERVO PISTON SEALS LEAKING. LOSS OF NO1 HYDRAULICSYSTEM FLUID.SDR AUS20030352Seat Back · cracked(AUS) PASSENGER SEAT BACK ASSEMBLY CRACKED ACROSS ENTIRE WIDTH. SUSPECT CAUSED BY PASSENGERS PUSHING/PULLING BACK ON SEAT. SEAT BACK IS MANUFACTURED FROM COMPOSITE MATERIAL.SDR AUS20030329Wheel · cracked(AUS) NOSE WHEEL HALF CRACKED AT INSIDE BEAD AREA. CRACK LENGTH 85MM(3.34IN). CRACK HAD NOT PROPAGATED COMPLETELY THROUGH THE WHEEL AND WAS NOT VISIBLE FROM THE OUTSIDE AND WAS FOUND WHEN THE WHEEL WAS DISASSEMBLED FOR A TYRE CHANGE.SDR AUS20030256Gearbox · contaminated(AUS) MAIN TRANSMISSION CHIP DETECTORS CONTAINED A SMALL AMOUNT OFFERROUS PARTICLES. THE PARTICLES WERE WITHIN LIMITS AS PER THEMAINTENANCE MANUAL. AFTER CHANGING THE OIL AND OIL FILTER A FURTHER CHECK FOUND NO EVIDENCE OF METAL PARTICLES AND THEAIRCRAFT WAS RSDR AUS20030251Angle · cracked(AUS) FUSELAGE TEE SECTION CRACKED. CRACK LENGTH APPROXIMATELY 25.4MM (1IN). CRACK IS LOCATED IN AREA IMMEDIATELY ABOVE THE TOP LT TAIL BOOM ATTACHMENT FITTING AND APPEARS TO HAVE INITIATED FROM THE RADIUS CUT AT THE END OF THE STRINGER.SDR HEEA084157Fuel Control · leakingFUEL CONTROL LEAKING.SDR HEEA084181Ignition Lead · chafedIGNITION LEAD CHAFED.SDR HEEA084182Igniter · wornIGNITER WORN.SDR HEEA084183Generator · inoperativeHIGH ENERGY GENERATOR IS INOPERATIVE.SDR HEEA084149Bellows · rupturedDOES NOT OPEN ON TEST RUN. REPLACED BELLOWS PN 6893483 DUE TO RUPTURED AND PITTED. REPAIRED BLEED VALVE.SDR EGR2003F00002Wire · chafedNR 2 ENGINE DECU FAULT, T 1 FAILURE IN FLIGHT, ENROUTE. FOUND CHAFED WIRE. REPLACED HARNESS.SDR HEEA082984Generator · malfunctionedHIGH ENERGY GENERATOR POPS START CONTROL CIRCUIT BREAKER.SDR AUS20021038Swivel · fractured(AUS) LH UNDERCARRIAGE DOOR LINK SWIVEL BROKEN. INVESTIGATION FOUND THAT THERE WAS AN INDICATION OF A PRE-EXISTING CRACK IN THE RADIUS THROUGH APPROXIMATELY ONE THIRD OF THE DIAMETER.SDR AUS20020962Pressure Switch · failed(AUS) ROTOR BRAKE PRESSURE SWITCH FAILED INTERNALLY.SDR AUS20020903Wire · worn(AUS) NO2 ENGINE FIRE WARNING. PRIMARY AND SECONDARY FIRE EXTINGUISHERS DISCHARGED. INVESTIGATION COULD FIND NO EVIDENCE OF FIRE. CAUSEDBY CHAFING OF FIRE WARNING SYSTEM WIRE.SDR AUS20020510Sensor · faulty(AUS) NO2 ENGINE OVERSPEED SENSOR FAULTY.SDR HEEA078710Exhaust Stack · crackedLT ENGINE EXHAUST STACK IS CRACKED.SDR AUS20020459Starter Gen · malfunctioned(AUS) DC GENERATING SYSTEM FAULTY. INVESTIGATION COULD FIND NO CAUSE FOR THE PROBLEM BUT THE FOLLOWING ITEMS WERE REPLACED; NR 2 ENGINE STARTER-GENERATOR NR 2 GENERATOR CONTROL UNIT NR 2 TRIPLE TACHO INDICATOR NR 2 ENGINE T5 GAUGE. SUSPECT CAUSED BY A VOLTASDR AUS20020420Servo · unserviceable(AUS) TAIL ROTOR CONTROL SYSTEM SERVO FAULTY.SDR AUS20020419Hose · leaking(AUS) RT MAIN LANDING GEAR DOWN' HYDRAULIC HOSE LEAKING. LOSS OF HYDRAULIC FLUID.SDR AUS20020284Gearbox · making metal(AUS) MAIN TRANSMISSION CHIP DETECTOR CONTAMINATED WITH METAL. AMOUNT OF METAL ON DETECTORS WAS BEYOND MANUFACTURERS LIMITS AND THE TRANSMISSION WAS CHANGED.SDR AUS20020020Float · faulty(AUS) AIRCRAFT SUFFERED AN UNCOMMANDED INFLATION OF THE REAR CELLS OF THE NOSE FLOATATION BAGS. THE FLOAT SYSTEM WAS NOT ARMED AT THE TIME.SDR HEEA077387Engine · malfunctionedENGINE WOULD NOT START.SDR AUS20011272Wire · broken(AUS) RH MAIN LANDING GEAR DOWNLOCK SENSOR HARNESS WIRE BROKEN.SDR AUS20010981Swivel · loose(AUS) NR 1 ENGINE COMBUSTION CHAMBER P2 AIR TAP SWIVEL UNION ASSEMBLY CONE LOOSE.SDR AUS20010731Engine · failed(AUS) ENGINE SUFFERED SEVERE INTERNAL FAILURE. COMPRESSOR AND TURBINE SEIZED. GAS GENERATOR AND POWER TURBINE BLADES BADLY DAMAGED. EXTERNAL DAMAGE ALSO EVIDENT.SDR HEEA073520Engine · malfunctionedHIGH OIL CONSUMPTION.SDR HEED073497Fuel Control · malfunctionedN2 LAGS CREATING A 20 PERCENT TORQUE SPLIT. REPLACED UNIT.SDR HEED073498Check Valve · stuckCHECK VALVE STICKING. REPLACED UNIT.SDR CA011105005Labyrinth Seal · failed(CAN) TEARDOWN REPORTS - SEVERE FAILURE OF LABYRINTH SEAL. SMALL DIAMETER ROTATING LABYRINTH SEAL ALMOST COMPLETELY DISINTEGRATED. SMALL PIECES RECOVERED. OUTER TWO ROTAING SEALS SEPERATED FROM LABYRINTH SHAFT. ACRO AEROSPACE W/O 21-8077PARTS SHIPPED TO TURBOMSDR AU010369Spar Cap · cracked(AUS) VERTICAL STABILISER FORWARD RH SPAR CAP ANGLE LOCATED AT VS117.25 CRACKED IN THE AREA WHERE THE RIVETS ATTACH THE TOP RIB TO THEANGLE.SDR HEED072254Magnetic Seal · leakingTHIS SEAL LEAKED SINCE THE ENGINE S/N 15529 WAS INSTALLED ON 9/7/2000. REPLACED UNIT.SDR HEED072203Igniter · weakWEAK- WILL NOT START AIRCRAFT. FOUND BAD ON 150 HOURS INSPECTION. REPLACED UNIT.SDR HEED072204Magnetic Seal · leakingTHIS SEAL LEAKED SINCE THE ENGINE 15529 WAS INSTALLED ON 9/7/2000 AT ATT: 4867.15 REPLACED UNIT.SDR HEED072212Igniter · erodedERODED CENTER ELECTRODE. REPLACED UNIT.SDR AU010108Engine · seized(AUS) NR 1 ENGINE INTERNAL FAILURE. INSPECTION FOUND COMPRESSOR SEIZED AND SEVERAL TURBINE BLADES MISSING/BROKEN.SDR AU000013Valve · failed(AUS) PILOT''S LIFE RAFT EXPERIENCED AN UNCOMMANDED INFLATION DUE TO A RUPTURED SEAL AND WASHER IN THE INFLATION HEAD. DAMAGE TO THE RIGHT PILOT''S DOOR WITH DOOR LATCH TORN FROM DOOR FRAME CAUSING A HOLE IN THE DOOR FRAME AND SURROUNDING STRUCTURE.SDR AU990761Cyclic Stick · jammed(AUS) CYCLIC CONTROL STICK JAMMED BY FOD. INVESTIGATION FOUND THAT A SCREW BECAME TRAPPED BETWEEN THE CYCLIC TORQUE TUBE FITTING AND THE TORQUE TUBE SUPPORT BRACKET PREVENTING FULL AFT CYCLIC MOVEMENT. THE ORIGIN OF THE SCREW COULD NOT BE CONFIRMED.
Back to Turbomeca ARRIEL-1S