Turbomeca ARRIEL-2S2
Service difficulty reports · 52
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 = 'ARRIEL2S2' 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 = 'ARRIEL2S2' 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 VE7A2024091700001Pump · failedON CLIMB OUT WHEN AC WAS TURNED ON ODOR FILLED THE COCKPIT AREA. FLIGHT CANCELED AND RETURNED TO BASE. AIR PUMP MFG BY IMPACT INSTRUMENTATION FAILED AND CAUSED ODOR TO FILL THE COCK PIT AREA PUMP PN E-428K SN 0609003 WAS THE PROBLEM, AND IT FAILED.SDR U0GA202311150001Control Rod · damagedBRISTOW RECENTLY DISCOVERED A LOOSE JAM NUT ON AFT M/R SERVO INPUT ROD END DURING A SCHEDULED INSPECTION. THE JAM NUT IS THE SUBJECT OF FAA AD 2015-19-51, AD 2017-19-01 AND SIK AWL 300 HOUR INSPECTION ITEM 30A. THE INTENT OF THESE INSPECTIONS IS ‘. TO DETECT SDR U0GA ASR11041Unknown · unknownHOLDING SOUTH OF 92LA AT 500' AGL FOR COMPANY TO CLEAR HOSPITAL HELIPAD, #2 ENGINE FIRE WARNING TONE SOUNDED, #2 ENGINE FIRE LIGHT ILLUMINATED, MASTER CAUTION LIGHT ILLUMINATED, AND #2 FIRE T-HANDLE LIGHT ILLUMINATED. AFTER ASSESSING THE SITUATION, CREW DECIDSDR 2023FA0000387Transducer · abnormalMOMENTARY PARTIAL POWER LOSS WITH YAW KICK AND LOSS OF TORQUESDR 2023FA0000392Transducer · abnormalMOMENTARY ENGINE ROLL BACK WITH TORQUE SPLIT AND YAWING MOTIONSDR 2023FA0000391Transducer · abnormalMOMENTARY ENGINE ROLL BACK WITH TORQUE SPLIT AND YAWING MOTIONSDR 2023FA0000386Transducer · abnormalMOMENTARY PARTIAL POWER LOSS WITH YAW KICK AND LOSS OF TORQUESDR 2023FA0000390Transducer · abnormalMOMENTARY ENGINE ROLL BACK WITH TORQUE SPLIT AND YAWING MOTIONSDR 2023FA0000389Transducer · abnormalMOMENTARY ENGINE ROLL BACK WITH TORQUE SPLIT AND YAWING MOTION.SDR 2023FA0000385Transducer · abnormalMOMENTARY PARTIAL POWER LOSS WITH YAW KICK AND LOSS OF TORQUESDR 2023FA0000213Transducer · defectivePILOT REPORT: WHEN DEPARTING PN44 IN 431MK WITH TWO PAX ONBOARD, WE EXPERIENCED A MOMENTARY LOSS OF POWER WITH ENGINE OSCILLATIONS. ON TAKEOFF WE PULLED APPROXIMATELY 95% TQ, AFTER ABOUT 5 SECONDS THE LEFT ENGINE ROLLED BACK TO ABOUT 70% TQ AND THE RIGHT SPIKSDR 2023FA0000384Transducer · abnormalMOMENTARY PARTIAL POWER LOSS WITH YAW KICK AND LOSS OF TORQUESDR 2023FA0000388Transducer · abnormalENGINE OUT INDICATION WITH A TORQUE SPLIT AND YAWING MOTION MOMENTARILYSDR 2023FA0000383Transducer · abnormalMOMENTARY PARTIAL POWER LOSS WITH YAW KICK AND LOSS OF TORQUESDR 2022FA0000220None · leakingON CLIMB OUT FROM ARA THERE WAS A STRONG SMELL OF FUEL. ALL CREW MEMBERS
SMELLED IT. RTB AND SHUT DOWN.SDR 2023FA0000381Transducer · abnormalINFLIGHT MOMENTARY ENGINE ROLLBACK WITH YAW KICK AND TORQUE LOSSSDR 2023FA0000382Transducer · abnormalAIRCRAFT HAS A MOMENTARY POWER LOSS WITH ENGINE OUT INDICATION AND TORQUE SPLIT WITH A YAWING MOTION,SDR ALGA020190828087Magnetic Seal · leakingOIL PRESSURE ON #2 ENGINE FLUCTUATING BETWEEN 30-45PSI , OIL TEMP BEGAN TO DECREASE FROM 74 DEG C - 67 DEG C . OIL PRESSURE LIGHT ILLUMINATED . ENGINE WAS SECURED. CREW DIVERTED TO 2LS0.SDR CA190221013Fire Bottle · cracked(CAN) ON THE DAILY INSPECTION OF THE NUMBER ONE ENGINE FIRE BOTTLE IT WAS FOUND TO BE LOW ON PRESSURE. FIRE BOTTLE WAS REPLACED AND WHEN IT WAS SENT FOR SERVICING IT WAS FOUND TO HAVE A HAIRLINE CRACK. (TC# 20190221013)SDR HEER20160809030Warning Light · false activationDURING CLIMB AT 600 FEET AND COUPLED, NR 1 ENGINE OUT LIGHT AND TONE WITH YAW AND MASTER CAUTION, ENGINE T&PS NORMAL. GROUND RUN, OPS CHECK FLIGHT, FCPM DAFCS COUPLED-AUTO PILOT MODES PARA. 2.26-2.31. NO DEFECTS NOTED.SDR HEER20160121123Line · leakingIN CRUISE FLIGHT, NOTICED NR 2 ENGINE OIL PRESSURE FLUCTUATION FOLLOWED BY STEADILY DECREASING OIL PRESSURE OVER A PERIOD OF SEVERAL MINUTES. ELECTED TO ABORT FLIGHT AND RETURN TO DEPARTURE. PRESSURE CONTINUED TO DECREASE AND EVENTUALLY WENT BELOW RED LINE. SDR HEER20150522285Hmu · failedNR 2 ENGINE DECU FAILED WITH STEPPER LEVEL 3 FAULT. TROUBLESHOOTING WITH LEAD TO HMU STEPPER FAILURE.SDR HEER20150325925O-Ring · cutDURING CRUISE FLIGHT NOTICED MASTER CAUTION BEGIN TO FLICKER. OBSERVED NR 2 ENGINE OIL PRESSURE BEGIN TO FLUCTUATE AND DROP. EVENTUALLY PRESSURE DROPPED BELOW RED LINE AND ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. ON INSPECTION FOUND CUT O-RING ON OIL SDR HEER20141213581Valve · out of adjustFUEL ODOR IN CABIN DURING CRUISE FLIGHT WITH HEATER ON. MAINTENANCE REPLACED THE ADJUSTED VALVE ASSY ON THE NR 1 ENGINE.SDR ALGA2014082433384Bearing · wornUPON PICKUP TO A HOVER BINDING WAS FELT IN THE CYCLIC FLIGHT CONTROL SYS. ACFT WAS LANDED & THE BINDING CONDITION WAS CONFIRMED BY THE COPILOT. ACFT WAS GND TAXIED TO PARKING. IDLER LINK IN FLIGHT CONTROL SYS WAS FOUND TO HAVE WORN BEARING. IDLER LINK WAS SDR BTEA2014F00047Starter Gen · failedNR 1 STARTER/GENERATOR FAILED. DURING START, THE ENGINE TOOK AN UNUSUALLY LONG TIME TO REACH LIGHT OFF AND IDLE SPEED. AFTER ENGINE START, THE GENERATOR WOULD NOT COME ON LINE. AFTER THE ACFT RETURNED TO THE MAINTENANCE FACILITY, THE STARTER WAS EXAMINED ANSDR BTEA201306250001Brushes · brokenNR 2 DC GENERATOR FAILED IN FLIGHT. AFTER THE ACFT RETURNED TO THE MX FACILITY, THE STARTER GENERATOR WAS REMOVED FOR INSPECTION. THE BRUSHES WERE FOUND WORN EXCESSIVELY AND BROKEN. REPLACED WITH AN O/H UNIT, ALL SYS CHECKED GOOD.SDR BTEA20121130001Hmu · malfunctionedTHE FUEL CONTROL FAILED ON START CAUSING THE ENGINE TO EXCEED TEMPERATURE LIMITS. THE HMU WAS FOUND TO BE AT FAULT. (SUSPECT THE CONSTANT DELTA "P" VALVE FAILED). THE ENGINE ASSEMBLY AND HMU WERE REPLACED. THIS FAILURE COULD HAVE OCCURRED IN FLIGHT CAUSINGSDR ALGA201210126705Drag Brace · corrodedFOUND WORN ROD END BEARING. ALSO FOUND CORROSION ON UPPER BRACE AND RETRACTION BRACE.SDR BTEA2012F00158Engine · vibrationINTEGRATED INFORMATION DISPLAY SYSTEM, (IIDS), DISPLAYED A "MINOR" ENGINE FAULT "TQ TRIM LVL L" FOR THE NR 1 ENGINE FROM THE DIGITAL ENGINE CONTROL UNIT (DECU). PILOTS CHECK FOR FAULTS FROM THE DECU AND THE IIDS. A MINOR FAULT WAS NOTED ON THE NR 1 ENG; "TQSDR ALGA2012052501Oil System · fluctuatesENROUTE, NR 2 ENGINE OIL PRESSURE DROPPED TO LOWER SIDE OF GREEN RANGE. THE ACFT IS RETURNING TO DEPARTURE NR 2 ENGINE OIL PRESSURE FLUCTUATING BETWEEN 27 AND 30 PSI IN THE CAUTION RANGE. ENGINE WAS MANUALLY SECURED. ENGINE CHANGED QUARANTINED FOR EVALUATION.SDR CA120309006Wire · shorted(CAN) 10 MILES TO LANDING, BURNING ODOR WAS NOTED AND SHORTLY THEREAFTER SMOKE WAS SEEN COMING FROM THE AREA OF A RIVET ON THE FORWARD PART OF THE DOOR FRAME NEAR THE LOWER AFT CORNER OF THE PORT SIDE WINDSHIELD. LAST ELECTRICAL ITEM TURNED ON WAS THE VENT BLSDR ALGA20110916001AEngine · faultyNR 2 ENGINE OUT LIGHT FLASHED DURING CRUISE WITH N1 OSCILLATIONS FOR ABOUT 2 SECONDS. DETECTED FAULT CODES WERE 2 DECU A FAULT MINOR - COLL POSITION LVL-1. MX REPLACED FAULTY COLLECTIVE TRANSDUCER. OPS CHECKED GOOD.SDR CA110916009Gas Generator · overheated(CAN) EXCESSIVE HEAT. DISCOLORING OF TURBINE CASING, DAMAGED WIRING HARNESS. FUEL IN P-3 AREA OF ENGINE. ACFT IS ON THE GROUND FOR FURTHER INVESTIGATION BY TECH SERVICES. PLEASE SEE PRELIMINARY COMMENTS FROM MFG ON SITE. NR 1 ENGINE AFTER DISASSEMBLY OF THSDR HEEA131581Coupling · wornHIGH IRON CONTENT IN SOAP SAMPLE - EXCESSIVE WEAR IN MO5 MUFF COUPLING AND DRIVE SPLINES. REPLACED MO5 AND MUFF COUPLING.SDR HEEA131582Module · damagedHIGH IRON CONTENT IN SOAP SAMPLE - EXCESSIVE WEAR IN MO5 MUFF COUPLING AND DRIVE SPLINES. REPLACED MO5 AND MUFF COUPLING.SDR HEEA129640Transducer · warning lightIN CRUISE FLIGHT ENGINE OUT LIGHT MOMENTARY ILLUMINATED WITH AUDIO WARNING. MOMENTARY YAW TO LEFT. COLLECTIVE TRANSDUCER FAULT CHANNEL 1. REPLACED TRANSDUCER.SDR HEEA129628Starter Gen · surgesWHILE IN CRUISE FLIGHT ALL DAFCS SYS DISENGAGED. COPILOT EFIS WENT OFF. ELECTRICAL SURGES IN SYS FOLLOWED BY NR1 ADC FAILURE. MX REPLACED THE NR 2 STARTER GENERATOR.SDR 7KFA775L001Engine · shutdownUPON TAKEOFF, ACFT EXPERIENCED A LOSS OF POWER IN THE NR 2 ENGINE AT APPROX 100 FT AGL. PILOT REJECTED THE TAKEOFF AND SAFELY LANDED IN A HOSPITAL PARKING LOT. NO INJURIES, NO DAMAGE TO THE HELICOPTER AND NO PROPERTY DAMAGE. PATIENT WAS TRANSPORTED BY GROUNDSDR ALGA09290900861Spar · crackedIN AN ATTEMPT TO TRACK AND BALANCE 2 EACH NEWLY INSTALLED T/R BLADE ASSEMBLIES, A VERY HIGH VIBRATION WAS NOTED AND IMMEDIATE SHUTDOWN OCCURRED. THE T/R BLADE ASSEMBLIES WERE REMOVED AND RETURNED TO OUR BLADE SHOP. UPON PERFORMING A PRELIMINARY INSP ON THE BLASDR HEEA123787Transducer · inoperativeDURING CRUISE FLIGHT, AFTER CLIMBOUT, ACFT YAWED 2 OR 3 TIMES, NR 2 ENGINE OUT LIGHT ILLUMINATED AND AUDIO SOUNDED FOR ABOUT 2 SECONDS THEN RETURNED TO NORMAL. RETURNED TO BASE AND NOTIFIED MX. MX REPLACED THE DECU COLLECTIVE POSITION TRANSDUCER.SDR U0GA2009122580145Autopilot Sys · malfunctionedWHILE ON A FULLY COUPLED ILS 15, ON THE PILOT SIDE (NR 1 SIDE), SEVERAL SECONDS BEFORE THE OCCURRENCE, ACFT WAS HUNTING FOR THE GLIDE SLOPE. WHILE COUPLED THE AFCS WAS MAKING CORRECTION FOR THE GLIDE SLOPE THEN MADE AN ABRUPT NOSE UP OF ABUT 40-60 DEGREES NOSSDR HEEA119764Shaft · shearedNR 1 ENGINE OIL TEMPERATURE WENT TO 120 DEGREES C, IN THE RED ZONE. COMPLIED WITH CHECKLIST AND SHUTDOWN NR1 ENGINE AND PERFORMED RUN-ON LANDING. FOUND OIL COOLER BLOWER SHAFT SHEARED.SDR HEER118259Control Unit · unknownNR 1 DC GENERATOR DROPS OFF LINE.SDR HEER117364Life Raft · unbondedOB ATTACHMENT EDGE OF LT LIFE RAFT POD FOUND TO BE DISBONDED FROM CENTER FILLET. REPLACED WITH SERVICEABLE PART.SDR HEEA116982Actuator · malfunctionedDURING CLIMB, AIRCRAFT YAWED NOTICEABLY AND WAS ACCOMPANIED BY AN IE27 YAW FAILURE CAUTION LIGHT. RESET BOTH AP1 AND AP2 SWITCHES AND CAUTION LIGHT EXTINGUISHED. COLLECTIVE YAW CIRCUIT BREAKER WAS THEN FOUND TO BE TRIPPED. RESET CIRCUIT BREAKER. DURING DESDR CA070823002Jettison System · failed(CAN) EXTERNAL LIFERAFT JETTISON SYS FAILED TO OPERATE. WHEN LEVER ACTUATED, CABLE BROKE AND PULLEY BRACKET ON LT SIDE OF CENTER PEDESTAL DETACHED. (2) BRACKETS UNDER FLOOR FOUND TO BE LOCATED INCORRECTLY. INSTALLATION WAS CARRIED OUT IAW ASI-500-100 REV.G. (SDR HEEA116970Detector · malfunctionedIN CRUISE, NR 1 CRT LIGHT ILLUMINATED. MAINTENANCE REPLACED THE LOW SPEED DETECTOR.SDR HEEA116826Pressure Switch · malfunctionedNR 1 ENGINE OIL PRESSURE LIGHT CAME ON IN FLIGHT. MAINTENANCE REPLACED THE OIL PRESSURE SWITCH.SDR HEEA117030Bearing · failedMGB CHIP PLUGS INDICATED A METAL IN OIL CONDITION. THE MGB WAS REMOVED AND SENT TO COMPONENT OVERHAUL SHOP TO DETERMINE CAUSE OF METAL. OHS COMPLETELY DISASSEMBLED THE MGB AND DETERMINED THE BEARING CUP IN THE LEFT HAND BEVEL SPUR GEAR ASSY WAS THE PRIMARY
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