Turbomeca ARRIUS-2B2
Service difficulty reports · 89
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 = 'ARRIUS2B2' 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 = 'ARRIUS2B2' 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 2A6D2015092501Turbine · damagedDURING DISASSEMBLY OF MODULE 2 FOR REAR BEARING SCAVENGE OIL LEAK INVESTIGATION, FOUND METALLIC SEAL PN 9560160210 CUTTING INTO THE BACK SIDE OF THE PT NOZZLE GUIDE VANE PN 0319412140 & THE FRONT SIDE OF THE REAR BEARING SUPPORT PN 0319250420. WE WILL BE REPLSDR QMLA2015090115080Warning System · false activationTHE PILOT RECEIVED A SYS 2 DEGRADE CAUTION LIGHT ILLUMINATION DURING FLIGHT WITH A PATIENT ON BOARD. IMMEDIATELY ABORTED THE FLIGHT & RETURNED TO THE HOSPITAL FOR LANDING AS THE EMER PROCEDURE WAS LAND AS SOON AS PRACTICAL. THE MECHANIC ARRIVED TO TROUBLESHOSDR QMLA2015082115075Valve · leakingTHE PILOT & MEDICAL CREW WERE ON FINAL APPROACH TO THE HOSPITAL LZ, THE MEDIC IN THE CABIN SMELLED FUEL. THE PILOT CONTINUED THE APPROACH & LANDED AT THE HOSPITAL. UPON SHUTDOWN, FUEL WAS OBSERVED TO BE ALL OVER THE CLAMSHELL DOORS, EXTERIOR. FUEL WAS OBSERSDR E3MA20150821001Engine · leakingDURING FLIGHT THE PILOT HEARD A NOISE FROM THE ENG WITH AN ASSOCIATED ACFT YAW. THE TORQUE OF THE ENG FELL BELOW THE OPPOSING ENG FOLLOWED BY A CHIP CAUTION ON THE CAD. THE ENG THEN TORQUE INDICATION CAME BACK TO MATCH THE OPPOSING ENG. UPON POST FLIGHT WALSDR QMLA2015071515058Electrical Box · faultyDURING NORMAL PREFLIGHT INSPECTION, IT WAS DISCOVERED WE HAD A NR 1 BUS TIE CAUTION LIGHT. THE ACFT WAS NEVER FLOWN ON THAT DATE. UPON FURTHER INSPECTION OF THE MASTER ELEC BOX, WE FOUND THE BOX WAS CLICKING CONSTANTLY WHENEVER POWER WAS APPLIED & WE SMELLEDSDR E3MA20150715001Engine · flamed outENGINE FLAMEOUT DURING TRAINING FLIGHT WHILE NR 1 ENG WAS IN MANUAL MODE.SDR CA150713023Chip Detector · weak(CAN) MGB CHIP DETECTOR MAGNETISM IS WEAK.SDR QMLA2015050715036Chip Detector · contaminatedDURING CRUISE FLIGHT, THE PILOT WAS ALERTED TO A MAIN TRANSMISSION CHIP LIGHT. HE IMMEDIATELY DIVERTED BACK TO THE BASE OF OPERATIONS APPROX 3NM AWAY WITH NO ISSUES. INSPECTED THE CHIP DETECTORS. A CLASS C CHIP WAS FOUND. THE DETECTOR WAS CLEANED, SYS OIL SDR QMLA2015011615004Engine · contaminatedDURING THE FIRST FLIGHT SINCE ENG FLUSH, THE COCKPIT & CABIN FILLED WITH SMOKE. THE SMOKE WAS CONSISTENT WITH THE SMELL FROM RUNNING THE HEATER AFTER AN ENG FLUSH. INSPECTED BOTH ENGS FOR LEAKS & BURNED WIRING WITH NO DEFECTS NOTED. THIS WAS THE FIRST FLIGHSDR CA141110011Search Light · smoke(CAN) DURING A FLIGHT AFTER USING THE SEARCH LIGHT THE PILOTS SMELLED SMOKE IN THE CABIN. FOLLOWING AN IMMEDIATE LANDING THEY NOTICED THE LIGHT WAS AT A 90 WHILE BEING IN ITS STOWED POSITION WHICH CAUSED THE INSIDE OF THE FIBERGLASS HOUSING TO MELT. TRIED TO SDR QMLA2014092714117Valve · leakingDEPARTED FOR SCENE FLIGHT MEETING EMS ON HOSPITAL PAD. THIS IS AN 18 MINUTE FLIGHT, ABOUT 15 MINUTES INTO THE FLIGHT THE CREW MEMBER IN THE BACK STARTED SMELLING OIL & FUEL TYPE FUMES. THE PILOT COULD AS WELL AS THE OTHER CREW MEMBER IN THE FRONT. ABOUT 1 -SDR QMLA2014091214109Unknown · odorTHE PILOT SMELT WHAT APPEARED TO BE BURNING RUBBER IN THE ACFT RETURNING TO BASE FOLLOWING A PATIENT TRANSFER. THE PILOT TURNED OFF THE AIR CONDITIONING & OPENED UP THE FRESH AIR VENTS. HE THEN DIVERTED TO & LANDED. AT NO TIME WAS THERE EVER SMOKE IN THE COCSDR QMLA2014051914058Hmu · leakingON POST FLIGHT WALK AROUND, FUEL WAS DISCOVERED LEAKING FROM A DRAIN COMING FROM THE NR 2 ENG DECK. TROUBLE SHOT THE LEAK, THE FUEL ADJUSTED PUMP & METERING VLV, HMU, WAS LEAKING AT APPROXIMATELY 10 DROPS PER MINUTE DURING A GND RUN. UPON SHUTDOWN FROM THE GSDR QMLA2014021114014Bearing · wornTHE PILOT REPORTED WHILE IN CRUISE FLIGHT THE NR 1 ENG CHIP LIGHT ILLUMINATED ON A RETURN FLIGHT TO BASE. THE PILOT IMMEDIATELY PLACED THE NR 1 ENG INTO IDLE & NOTIFIED TOWER OF HIS INTENT TO PERFORM A RUN ON LANDING. THE LANDING WAS ACCOMPLISHED WITHOUT INCSDR QMLA2013102613150Bottle · looseTHE FLIGHT CREW DETECTED A STRONG FUEL SMELL UPON LANDING AT THE HOSPITAL HELIPAD FOR A PATIENT PICKUP. THE MECHANIC ARRIVED AT THE HELICOPTER AND INSPECTED THE ACFT. HE FOUND THAT THE NR1 ENGINE FUEL COMPARTMENT HAD FUEL RESIDUE COLLECTING ON THE AFT FIREWASDR QMLA2013080613113Control Unit · failedIN-FLIGHT, NR 1 FADEC FAILURE. SWITCHED NR 1 ENGINE FROM "NORMAL" TO "MANUAL" AND RETURNED SWITCH TO THE "NORMAL" POSITION. USING MANUAL CONTROL OF NR 1 ENGINE VIA TWIST-GRIP, A PRECAUTIONARY UNSCHEDULED LANDING WAS MADE. PILOT REPORTED THE NR 1 ENGINE HAD SDR QMLA2013032013041Magnetic Seal · wornDURING FLIGHT, NOTICED THE NR 1 ENGINE CHIP LIGHT. RESET THE MASTER CAUTION AND BURNED CHIP. CHIP LIGHT WENT OUT. NR 1 ENGINE CHIP CAUTION RETURNED. RESET MASTER CAUTION AND BURNED CHIP. CHIP LIGHT WENT OUT. RETURNED TO BASE. NR 1 ENGINE CHIP RETURNED SDR E3MA20121220004Engine · shutdownDURING APPROACH INTO A LANDING ZONE, THE NR 2 ENGINE SHUTDOWN. INDICATIONS ON THE CAD WERE A "FLI DEGRADE" AND A DELTA N1. THERE WAS NO TORQUE INDICATION ON THE VEMD.SDR E3MA201210180001Bolt · wornDURING FLIGHT, THE PILOTS WERE COMPLAINING OF A VIBRATION IN THE MAIN ROTOR. THE MAIN ROTOR TRACK AND BALANCE WAS CHECKED AND NECESSARY ADJUSTMENTS WERE MADE TO BRING IT WITHIN ACCEPTABLE LIMITS. THE VIBRATION REMAINED DURING FLIGHT. AFTER FURTHER INSPECTIOSDR QMLA2012083012145Fire Detector · false activationON LANDING ON FINAL LEG TO RETURN TO HOME BASE PILOT INDICATED A FIRE WARNING LIGHT AND DING IN THE HEADSET. INDICATED THAT THERE WAS NO FIRE AND CONFIRMED AFTER LANDING. TROUBLESHOOT THE FIRE DETECTION SYS IAW MM AND FOUND ON A FUNCTION TEST THE TURBINE HEASDR QMLA2012082512138Valve · leakingDURING CRUISE FLIGHT AT 1,000 FT AGL, PILOT NOTICED AN ODOR OF FUEL IN COCKPIT. COULD SEE A CLEAR LIQUID RUNNING DOWN THE REAR CLAM SHELL DOOR. TURNED BACK TO THE AIRPORT AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION FOUND THE ADJUSTED FUEL VALVE ASSSDR QMLA2012070812114Warning Light · illuminatedNR 1 ENGINE CHIP INDICATION MODULE 1, NR 1 ENGINE.SDR QMLA2012052012086Magnetic Seal · wornNR 2 ENGINE CHIP LIGHT ILLUMINATED IN FLIGHT. ATTEMPTED TO BURN IAW RFM WITH NO SUCCESS. LANDED IAW RFM. MX INSPECTED CHIP DETECTORS AND FOUND CLASS B CARBON LIKE PARTICLES AND WIRE LIKE FILAMENTS ON REDUCTION GEARBOX CHIP PLUG. REMOVED AND INSPECTED STARTSDR QMLD201203232842Combustion Liner · crackedDURING INSPECTION OF ENGINE, FOUND THE COMBUSTION LINER CRACKED. REPLACING THE COMBUSTION LINER.SDR QMLA2012012912013Unknown · odorFUEL ODOR IN CABIN. THE PILOT IMMEDIATELY RETURNED TO THE BASE, AND SHUTDOWN. NO DEFECTS WERE NOTED AND THE ACFT WAS RETURNED TO SERVICE.SDR QMLD201201255951Guide Vane · crackedWHILE PERFORMING DISASSEMBLY OF ENGINE SN 32072 FOR A REAR BEARING OIL PIPE LEAK, FOUND DAMAGE TO THE FOLLOWING COMPONENTS INCLUDING THE PT NOZZLE GUIDE VANE: HP SEGMENT ASSY PN 0319217910, SN 653B FOUND CRACKED. FLAME TUBE PN 031917850, SN 664 CRACKED. HP NSDR E3MA20110606Terminal · looseDURING HOVER OPERATION, THE PILOT NOTICED SMOKE COMING FROM THE BOOT AROUND THE CYCLIC. AFTER LANDING A VISUAL INSP IN THE AREA BELOW THE CYCLIC BOOT COVER REVEALED LOOSE RING TERMINALS (ON WIRES 2006N AND 2008N) FOR THE MOVEABLE SEARCH LIGHT.SDR QMLDMG2301Fcu · brokenDURING PRELIMINARY INSP OF THE ACFT FOR INDUCTION INTO THE REPAIR STATION FOUND A SCREW HEAD ON THE NR 2 ENGINE DECK. AFTER FURTHER INVESTIGATION FOUND THAT THE SCREW HEAD WAS FROM A BLANKING PLATE ON THE FUEL CONTROL UNIT.SDR E3MA20110602Blade · wornPILOT COMPLAINED OF A VIBRATION THAT WAS MOST NOTICEABLE IN THE TAIL ROTOR PEDALS. UPON INSPECTION OF THE TAIL ROTOR A BLADE WAS DICOVERED TO HAVE EXCESSIVE LEAD-LAG MOVEMENT.SDR QMLA2011052611059Hmu · leakingAFTER RETURNING FROM A FLIGHT, THE PILOT REFUELED THE ACFT. WHEN FUELING WAS DONE THE PILOT RETURNED THE FUELING NOZZLE TO THE TANK. WALKING BACK TO THE AIRCRAFT THE PILOT THEN NOTICED FLUID UNDERNEATH THE ACFT. THE MECHANIC WAS CALLED IN AND UPON FURTHER ISDR QMLDMG2162Turbine Wheel · failedWHILE PERFORMING A BORESCOPE INSPECTION AND ROTATING THE ENGINE, A NOISE WAS HEARD AND THE N1 SECTION OF THE ENGINE LOCKED UP. REMOVED THE ENGINE AND DISASSEMBLED MODULE 1 FROM MODULE 2 AND AWAITED MFG SUPPORT TO COME AND DISASSEMBLE MODULE 2. UPON DISASSEMBSDR QMLA2011040211043Switch Panel · defectiveTHE CAD DISPLAYED "IDLE" WHEN FADEC SWITCH WAS TURNED ON. THE ENG WAS NOT RUNNING AT THIS POINT. THE 20VE SWITCH PANEL WAS FOUND TO BE THE CAUSE. THE PANEL WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE.SDR QMLDMG2011Diffuser · crackedWHILE PERFORMING SB SB319722830, VER B CENTRIFUGUAL DIFFUSER VANE BORESCOPE, FOUND A PIECE OF THE DIFFUSER VANE MISSING AND CRACKED. AWAITING MFG TEC TO COME REPLACE THE DIFFUSER.SDR QMLA2010121310078Hmu · leakingUPON LANDING ACFT WENT TO FLAT PITCH PILOT DETECTED A STRONG ODOR OF FUEL AND COCKPIT FILLED WITH VISIBLE EXHAUST THAT SMELLED STRONGLY OF FUEL. PRIMARY TROUBLESHOOTING WITH MFG REP POINTED TO AN INTERNAL LEAK IN BOTH NR1 AND NR2 ENGINE HMU'S ALLOWING FUEL INSDR QMLA2010121310079Hmu · leakingUPON LANDING, ACFT WENT TO FLAT PITCH PILOT DETECTED A STRONG ODOR OF FUEL AND COCKPIT FILLED WITH VISIBLE EXHAUST THAT SMELLED STRONGLY OF FUEL. PRIMARY TROUBLESHOOTING WITH REP POINTED TO AN INTERNAL LEAK IN BOTH NR1 AND NR2 ENGINE HMU'S ALLOWING FUEL IN THSDR QMLA2010101310067Transmission · misalignedMAIN TRANSMISSION CHIP LIGHT. SLIGHT ABRASION ON CHIP DETECTOR. CLEANED CHIP DETECTOR INSTALLED CLEAN FILTER ALL IAW EC135-63A-012 REV 4 STAGE A PROCEDURES. ACFT RETURNED TO SERVICE.SDR E3M2010F00001Bulkhead · crackedA 4 INCH CRACK WAS DISCOVERED ON THE BULKHEAD SKIN ADJACENT TO FRAME 5 (FR5), RT SIDE NEAR THE NR 2 ENGINE FACEC COMPUTER. THE CRACK WAS DISCOVERED WHEN THE PELICAN RACK WAS LOWERED DURING INSPECTION.SDR QMLA2010090310059Connector · burnedON A FINAL APPROACH, THE PILOT REPORTED SMELLING AN ELECTRICAL TYPE SMELL IN THE COCKPIT. HE SHUT OFF THE AIR CONDITIONING AND THE SMELL WENT AWAY. UPON LANDING, THE MX INSPECTED THE ACFT AND FOUND THAT A CONNECTOR FOR THE AFT EVAPORATOR ASSY HAD BURNED. THSDR QMLA2009122209051Heater · fumesSTRONG ODOR OF JET FUEL IN COCKPIT AND CABIN WHEN HEATER TURNED ON IN FLIGHT ON 12/22, WHILE IN FLIGHT AND CABIN HEATER IS ENGAGED, EXHAUST FUMES ODOR ENTER THE CABIN ON 12/26. MX IS CURRENTLY TROUBLESHOOTING.
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