Turbomeca ARRIEL-2B1

Service difficulty reports · 757

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 = 'ARRIEL2B1'
  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.

SDR CA150224021O-Ring · leaking(CAN) DURING PERFORMANCE OF P-CHECK, DAILY INSPECTION/AFTER LAST FLIGHT, HYDRAULIC FLUID FOUND LEAKING AT LOAD SENSOR AREA, FROM UNDER CUP ASSY, PN 801540 OF RT MAIN ROTOR SERVO. SERVO MFG COMPONENT MM WITH ILLUSTRATED PARTS BREAKDOWN, 67-39-13, DOES NOT BREAFeb 2, 2015 · Urocop EC130B4 · Rotorcraft Servo SystemSDR QMLA2014120214135Wire · meltedON STARTUP SMOKE OBSERVED ON RT SIDE OF AVIONICS PANEL FROM BOTTOM OF PANEL.Dec 2, 2014 · N118LN · Snias AS350B3 · Light System WiringSDR QMLA2014110414129Fire Detector · intermittentINTERMITTENT FIRE LIGHT ON FINAL APPROACH. PILOT REPORTED THAT AS HE WAS LANDING THE FIRE LIGHT WOULD FLICKER. AT NO TIME DID THE LIGHT COME ON & STAY ON.Nov 4, 2014 · N3866 · Urocop AS365N3 · Fire DetectionSDR QMLA2014102914128Unknown · smokeDURING CRUISE FLIGHT A CREW MEMBER REPORTED SEEING SMOKE IN THE CABIN FWD OF THE STRETCHER WITH A STRANGE SMELL IN THE CABIN. THE PILOT DID NOT WITNESS THIS SMOKE, BUT RETURNED TO BASE FOLLOWING A DISCUSSION WITH THE MEDICAL CREW. ONCE ON THE GND, THE PILOT Oct 29, 2014 · N209LF · Urocop EC130B4 · Air Distribution SystemSDR QMLA2014102014125Adapter · crackedFREQUENCY ADAPTER IS CRACKED ON THE RED BLADE.Oct 20, 2014 · N108LN · Snias AS350B3 · Main Rotor HeadSDR QMLA2014091814112Compressor Blade · damagedDURING THE FIRST 600 HOUR ENG INSPECTION, PERFORMED AXIAL COMPRESSOR BLADE INSPECTION CHECK FOR DAMAGE & SERVICEABILITY, DISCOVERED ONE BLADE HAD FOD DAMAGE AT THE TIP THAT EXCEEDED THE REPAIR LIMITS FOR LEVEL 2 TECHNICIANS. FURTHER DAMAGE TO THE ENG IS UNKNOSep 18, 2014 · N328CH · Urocop EC130B4 · Turbine Engine Compressor SectionSDR QMLA2014091514110Crossbeam · corrodedUPON REMOVAL OF MGB FOR REPLACEMENT, CROSSBEAM MEMBER WAS FOUND TO BE CRACKED AT TRANSMISSION TO CROSSBEAM FITTING HOLE.Sep 15, 2014 · N335AM · Urocop EC130B4 · Main Rotor GearboxSDR CA141020008Shoulder Belt · frayed(CAN) THE EDGE OF THE SHOULDER HARNESS PORTION OF THE SAFETY BELT WAS FOUND FRAYED. LOCATION OF THE FRAYING IS WHERE THE SINGLE BELT SPLITS INTO A DOUBLE BELT FOR EITHER SIDE OF THE SHOULDER.Sep 10, 2014 · Snias AS350B3 · Emergency EquipmentSDR CA140912005Windshield · cracked(CAN) CRACK IN WINDSHEILD RT, UPPER RT CORNER . ORIGINATING FROM SCREW AREA THAT HOLDS SIDE FAIRING.Sep 8, 2014 · Urocop EC130B4 · Flight Compartment WindowsSDR QMLA2014081214100Unknown · odorSTRONG ODOR OF FUEL PROMPTED PRECAUTIONARY LANDING. POST FLIGHT INSPECTION DID NOT REVEAL ANY FUEL LEAKS.Aug 12, 2014 · N108LN · Snias AS350B3 · Air Distribution SystemSDR CA140813002Pressure Switch · leaking(CAN) HYDRAULIC PRESSURE SWITCH FOUND LEAKING ON NR 2 HYD SYSTEM. PRESSURE SWITCH REPLACED WITH NEW UNIT. AFTER 83.1 HOURS OF OPERATION, REPLACED PRESSURE SWITCH, WHICH WAS FOUND TO BE LEAKING AGAIN. IT WAS REPLACED WITH A WARRANTY REPLACEMENT. THE SECOND HYAug 8, 2014 · Snias AS350B3 · Hydraulic Quantity SensorSDR QMLA2014072914093Connector · contaminatedFLIGHT ABORTED DUE TO NOISE COMING FROM OIL COOLER FAN. DETERMINED WATER WAS PRESENT IN THE CONNECTOR.Jul 29, 2014 · N209LF · Urocop EC130B4 · Engine Oil System WiringSDR CA140724010Engine · power loss(CAN) POWER LOSS DURING TAKEOFF RESULTING IN HARD LANDING. ENGINE WAS RUNNING AT THE TIME OF THE HARD LANDING.Jul 23, 2014 · Snias AS350B3 · Engine (Turbine/Turboprop)SDR QMLA2014071714087Pressure Switch · faultyUPON DEPARTURE FROM A SCENE LOCATION, THE HYD LIGHT ILLUMINATED WHILE EN ROUTE TO THE HOSPITAL. DIVERTED TO & HAD A GND AMBULANCE MEET THE ACFT AT THE AIRPORT TO COMPLETE THE PATIENT TRANSPORT. FOUND THAT THE HYD PRESS SWITCH HAD FAILED. THIS SWITCH WAS REPJul 17, 2014 · N306LF · Urocop EC130B4 · Hydraulic Pressure SensorSDR QMLA2014071614086Duct · contaminatedAPPROXIMATELY 5 MILES FROM LANDING THE DEFOG SYS & NOTICED A STRANGE SMELL, NOT BURNING ELEC, RUBBER, ETC. WHEN CLOSER TO LANDING HE COULD NOTICE A FAINT WISPS OF SMOKE IN THE NVG LIGHTING. THE DEFOG SYS WAS TURNED OFF & THE ACFT WAS RETURNED TO THE BASE. AJul 16, 2014 · N132HN · Urocop EC130B4 · Heating SystemSDR CA140704003Hinge · cracked(CAN) ENGINE COWLING HALF HINGE FOUND CRACKED DURING A VISUAL INSPECTION AND REPLACED WITH A NEW HINGE. FOLLOWING 84.5 FLIGHT HOURS, THE SECOND REPLACMENT HINGE WAS FOUND CRACKED DURING A VISUAL INSPECTION. THE TECH HAS BEEN NOTIFIED AND THE HINGE HAS AGAIN BJul 3, 2014 · Urocop EC130B4 · Engine Cowling SystemSDR QMLA2014061114072Attach Fitting · crackedWHILE COMPLYING WITH EAD 2014-12-51, THE RT SIDE HORIZONTAL ATTACHMENT FITTING CRACKED UPON REMOVAL. THIS STABILIZER HAD BEEN DETERMINED TO BE FAIRLY DIFFICULT TO REMOVE & REINSTALL ON PREVIOUS MX EVENTS INVOLVING THIS TASK. MOBILE SUPPORT REPAIR TEAM TO BE Jun 11, 2014 · N133LN · Urocop EC130B4 · Rotorcraft Tail BoomSDR QMLA2014061114073Skin · crackedCRACK FOUND IN THE TAIL BOOM SKIN WHILE PERFORMING A DYE PENETRANT INSPECTION OF THE AREA DESCRIBED IN SDR QMLA2014061114072. THE CRACK IN THE TAIL BOOM SKIN IS CURRENTLY BEING EVALUATED FOR AN APPROVED REPAIR. THE REPAIR TEAM THEY WILL BE SENDING TO ACCOMPLJun 11, 2014 · N133LN · Urocop EC130B4 · Rotorcraft Tail BoomSDR QMLA2014060914069Attach Fitting · crackedDURING REMOVAL OF HORIZONTAL STABILIZER FOR COMPLETION OF EASB 05A017 IT WAS DISCOVERED THAT THE UPPER RT STABILIZER ATTACHMENT FITTING WAS CRACKED.Jun 9, 2014 · N335AM · Urocop EC130B4 · Rotorcraft Tail BoomSDR QMLA2014060714066Drive Belt · brokenPRIOR TO TAKE OFF, TURNED ON THE ACFT`S AIR CONDITIONER. DURING CLIMB OUT WE SMELLED AN ELEC BURNING SMELL & ASSOCIATED GREY SMOKE COMING FROM THE NOSE OF THE ACFT. TURNED OFF THE THE AIR CONDITIONER, PERFORMED THE EMERGENCY PROCEDURE FOR SMOKE IN THE COCKPIJun 7, 2014 · N3817 · Urocop AS365N3 · Cabin Cooling SystemSDR QMLA2014060614065Drive Belt · brokenDURING A PATIENT TRANSFER, THERE WAS A BURNT RUBBER ODOR IN THE CABIN & LOSS OF AIR CONDITIONING. AFTER LANDING AT GOOD SAM & OPENING THE TRANSMISSION COWLING, RUBBER DEBRIS COVERED THE DECKS & SEPARATED BELT WAS DISCOVERED. NO DAMAGE TO ROTATING COMPONENTS Jun 6, 2014 · N44925 · Urocop AS365N3 · Cabin Cooling SystemSDR QMLA2014042614042Pump · seizedTHE PILOT REPORTED ON THE RETURN LEG OF A PATIENT TRANSPORT THAT SMOKE BEGAN TO FILL THE COCKPIT FROM AN UNKNOWN SOURCE. THE PILOT & MEDICAL CREW ON BOARD BEGAN OPENING WINDOWS & TURNING THE AIR CONDITIONING OFF. THE PILOT THEN NOTICED THE HYD & SERVO CAUTIOApr 26, 2014 · N47HN · Urocop EC130B4 · Hydraulic Pump (Electric/Engine), MainSDR QMLA2014041514036Connector · not seatedBEFORE TAKEOFF PILOT NOTED 81 GALLONS OF FUEL. SHORTLY AFTER TAKEOFF PILOT NOTICED FUEL 0. PILOT DECLARED A PRECAUTIONARY LANDING. TROUBLE SHOT VEMD SYS TO INCLUDE THE CONNECTIONS FOR MISSING OR BENT PINS. REMOVED BELLY PANEL & VISUALLY CHECKED ALL CONNECTApr 15, 2014 · N920U · Urocop EC130B4 · Fuel System WiringSDR CA140410002Fitting · cracked(CAN) ONGOING REPEAT INSPECTION FOR THIS ITEM FOUND UPPER HORIZONTAL STABILIZER CRACKED FITTINGS: 350A23-4222-20 RT AND 350A23-4222-21 LT. REPLACED BOTH FITTINGS NEW W/SAME PN`S. LT FITTING HAD 268 HRS, PREVIOUSLY REPLACED AND RT FITTING WAS ORIGINAL AND HADApr 9, 2014 · Urocop EC130B4 · Rotorcraft Tail BoomSDR QMLA2014032114027Door Frame · cracked2 INCH CRACK FOUND ON TAIL BOOM, BATTERY DOOR FRAME, UPPER RT CORNER. BATTERY TRAY WAS REPLACED ON 021914 BY QUALIFIED SHEET METAL TECHNICIAN FROM AMC DENVER.Mar 21, 2014 · N325AM · Urocop EC130B4 · Rotorcraft Tail BoomSDR QMLA201403214028Web · crackedFOUND CRACK 2 1/2 LONG AT RT SIDE PICKUP WEB OF CANOPY FOUND IN AMM 53-21-00, 6-1 DURING INSPECTION.Mar 21, 2014 · N506LF · Urocop EC130B4 · Fuselage Miscellaneous StructureSDR CA140217026Cable · failed(CAN) DURING 36 MONTH INSPECTION HANDLE WAS PULLED TO DEPLOY EMERGENCY FLOAT SYSTEM. SYS DID NOT DEPLOY. CABLE WAS REMOVED AND FOUND UNSERVICEABLE.Feb 11, 2014 · Snias AS350B3 · Emergency Flotation SectionSDR CA140217014Eec · malfunctioned(CAN) YELLOW GOV LIGHT ILLUMINATED IN CRUISE FLIGHT WITH THE SMELL OF "ELECTRICAL BURNING" CREW ALSO REPORT THE AFT BAGGAGE COMPARTMENT, EECU LOCATION, SMELT OF BURNED ELECTRONICS. TROUBLESHOOTING CONFIRMED FAULTY EECU. SERVICEABLE EECU INSTALLED. ACFT HASFeb 1, 2014 · Snias AS350B3 · Fuel Controlling SystemSDR QMLA2014013114013Search Light · inoperativeTHE PILOT REPORTED THAT HE & THE MEDICAL CREW WERE ON CLIMB OUT JUST FOLLOWING A REFUEL OF THE ACFT WHEN THEY EXPERIENCED AN ELEC SMELL COME THROUGH THE CABIN. THE PILOT IMMEDIATELY PERFORMED AN EMERGENCY LANDING INTO A VACANT PARKING LOT. THE MECHANIC DID AJan 31, 2014 · N425AM · Urocop EC130B4 · Exterior LightingSDR QMLA2014013014012Engine · making metalTHE PILOT & MEDICAL CREW WERE ON THEIR WAY TO A SCENE LOCATION TO PICK UP A PATIENT WHEN APPROXIMATELY 4 MILES FROM THEIR DESTINATION, THE ENG CHIP LIGHT ILLUMINATED. THE PILOT NOTIFIED THE CREW THAT THEY WOULD NOT BE ABLE TO CONTINUE & PROCEEDED TO FIND A SUJan 30, 2014 · N137HN · Urocop EC130B4 · Engine (Turbine/Turboprop)SDR CA140125004Crosstube · damaged(CAN) BOUGHT NEW CROSS TUBES FWD AND AFT UPON ASSY FOUND THAT TUBE WIDTH WAS NOT TRUE ROUND AND PARTIALLY FLAT AND DART STEPS WON`T CLAMP ON TO TUBES BECAUSE OF OUT OF ROUND CLAMPS WON`T FIT PROPERLY DUE TO THE OUT OF ROUND DIAMETER.Jan 24, 2014 · Snias AS350B3 · Main Landing Gear Attach SectionSDR QMLA2014011714006Structure · crackedDURING A0560 100 HR 12 MONTH AIRFRAME INSPECTION, TWO CRACKS WERE DISCOVERED. ONE ON LT SIDE OF ACFT BETWEEN SLIDING DOOR & BAGGAGE DOOR, EXTENDING 115MM DOWN THE SIDE OF THE AIRCRAFT & UPWARD TO FRONT OF THE DOOR TRACK. THE OTHER CRACK IS ON THE RT SIDE OF Jan 16, 2014 · N382AM · Urocop EC130B4 · Fuselage Miscellaneous StructureSDR QMLA2014011314005Unknown · odorDURING THE RETURN FLIGHT FROM UMC, THE PILOT SWITCHED ON THE CABIN VENT BLOWER. THE MEDICAL CREW IMMEDIATELY SMELLED A BURNING SMELL COMING FROM THE VENTS. THE PILOT TURNED THE VENT BLOWER OFF & THE SMELL DISSIPATED. THE PILOT PERFORMED A PRECAUTIONARY LANDJan 13, 2014 · N4497Y · Snias AS350B3 · Air Distribution SystemSDR QMLA2014011214003Pump · seizedTHE PILOT REPORTED THAT WHILE DURING A TRAINING FLIGHT DURING CRUISE APPROXIMATELY 10 MINUTES INTO THE FLIGHT, THE PILOT NOTICED A SMELL OF SMOKE FILL THE CABIN. THIS WAS IMMEDIATELY FOLLOWED BY THE HYD & SERVO AMBER CAUTION LIGHTS INDICATING A RT HYD SYS FAIJan 12, 2014 · N130HN · Urocop EC130B4 · Hydraulic Pump (Electric/Engine), MainSDR QMLA2014011214009Pump · seizedDURING CRUISE FLIGHT, CREW NOTICED THE ODOR OF SMOKE IN COCKPIT, FOLLOWED SHORTLY BY THE HYD & SERVO AMBER CAUTION LIGHT, RT HYD SYS FAILURE. THERE WAS NO LOSS OF ACFT CONTROLLABILITY, RETURNED TO DEPARTURE WITHOUT FURTHER DAMAGE OR INCIDENT. AFTER SHUTDOWNJan 12, 2014 · N130HN · Urocop EC130B4 · Hydraulic Pump (Electric/Engine), MainSDR CA140113007Hose · leaking(CAN) HYDRAULIC HOSE LEAKING IN STATIC AND DYNAMIC MODE. THE HOSE WAS REPLACED IN DEC 08, 2013 AND THE ACTUAL A/F TIME IS 1812.2. WHEN THE HOSE WAS INSTALLED THERE WERE NO LEAKS DISCOVERED. AFTER 2.2 HRS, THE HOSE STARTED LEAKING WHERE THE HOSE IS CRIMPED INJan 10, 2014 · Snias AS350B3 · Hydraulic System, MainSDR 2014FA0000036Friction Cup · wornPILOT REPORTED HARD POINTS IN THE CYCLIC CONTROL SYS DURING GROUND OPERATION AND IN FLIGHT. THE CYCLIC CONTROL WAS FOUND TO HAVE ABNORMAL WEAR BETWEEN THE CYCLIC FRICTION BOX AND THE FRICTION CUP, THIS WAS DUE TO 2 FACTORS. DIRT AND DUST ACCUMULATION. THE FDec 23, 2013 · N3972A · Snias AS350B3 · Main Rotor ControlSDR 2014FA0000037Friction Cup · misinstalledPILOT REPORTED HARD POINTS IN THE CYCLIC CONTROL SYS DURING GROUND OPERATION AND IN FLIGHT. CYCLIC CONTROL FOUND TO HAVE ABNORMAL WEAR BETWEEN CYCLIC FRICTION BOX AND THE FRICTION CUP, THIS WAS DUE TO DIRT AND DUST ACCUMULATION. FRICTION CUP AND FRICTION BOXDec 23, 2013 · N3972A · Snias AS350B3 · Main Rotor ControlSDR QMLA2013122113176Attach Fitting · crackedDURING AAIP A1040 300 HOUR, 12 MONTH INSPECTION, STEP A1040 2.4, A CRACK WAS FOUND IN THE LT UPPER STABILIZER MOUNT DURING THE VISUAL INSPECTION. THE CRACK RAN FROM THE FWD EDGE OF THE MOUNT THROUGH THE FWD OTBD BOLT HOLE & TO THE MIDLINE OF THE MOUNT.Dec 21, 2013 · N382AM · Urocop EC130B4 · Rotorcraft Tail BoomSDR QMLA2013121813175Duct · missingSTARTER GEN COOLING DUCT FOUND MISSING DURING AIRWORTHINESS CHECK.Dec 18, 2013 · N903CF · Snias AS350B3 · Starter-GeneratorSDR CA131218022Window · cracked(CAN) CRACKED WINDOW WAS BEING REMOVED, LT EDGE BONDING AT UPPER CABIN DOOR POST JUNCTION FOUND NON-EXISTANT FOR 26 CM. REMOVED WINDOW PIECES AVAILABLE.Dec 18, 2013 · Urocop EC130B4 · Flight Compartment WindowsSDR QMLA2013121713174Engine · making metalON INVESTIGATION OF ENG CHIP LIGHT, FOUND THE ELEC CHIP DETECTOR HAD AN EXCESSIVE AMOUNT OF GROUND CHIPS. CHECKED THE OIL FILTER BUT DID NOT SEE MUCH METAL UNTIL CLEANED THE FILTER. THERE WAS A GOOD AMOUNT OF SEDIMENT. CHECKED THE MO5 CHIP DETECTOR & FOUND Dec 17, 2013 · N497AE · Snias AS350B3 · Engine (Turbine/Turboprop)SDR CA131205006Windshield · cracked(CAN) CENTER WINDSHIELD CRACK WAS VISUALLY OBSERVED PROPAGATING FROM THE RT LOWER RADIUS DURING CRUISE FLIGHT ENROUTE TO THE MAIN BASE. PILOT FOLLOWED PROPER PROCEDURES AND ACFT LANDED WITHOUT INCIDENT AT THE MAIN BASE. THE CRACK MEASURED APPROXIMATELY 3" ANDDec 4, 2013 · Urocop EC130B4 · Flight Compartment WindowsSDR QMLA2013120213171Engine · making metalTHE PILOT STARTED THE ACFT ENG WITH THE INTENTION OF TAKEOFF, WHEN JUST BEFORE, HE OBTAINED AN ENG CHIP LIGHT. THE MISSION WAS ABORTED & THE ACFT WAS SHUT DOWN. TROUBLESHOOT THE PROBLEM, FOUND THE ENG CHIP DETECTOR FULL OF METALLIC MATERIAL. HE REFERRED TO Dec 2, 2013 · N131LN · Urocop EC130B4 · Engine (Turbine/Turboprop)SDR CA131202021Filter · dislodged(CAN) DURING MAINTENANCE RUNS WITH THE AIRCRAFT RUNNING AT GROUND IDLE, THE ENGINEER LEAK CHECKING THE ENGINE. WITNESSED THE M/R BLADES CONTACTING THE SAND FILTER DISCHARGE TUBE. THE ENGINE COWL WAS LATCHED WITH THE PROP ROD ON THE ENGINE DECK FITTING. THISNov 29, 2013 · Snias AS350B3 · Engine (Turbine/Turboprop)SDR QMLA2013112013168Attach Fitting · crackedDURING THE SCHEDULED MAINTENANCE AMC EC130B4 AAIP A 1040 300 HOUR - 12 MONTH AIRFRAME INSPECTION, FOUND RT LOWER HORIZONTAL STABILIZER ATTACH FITTING CRACKED. THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION AWAITING A MOBILE REPAIR TEAM FRNov 20, 2013 · N47HN · Urocop EC130B4 · Fuselage, Stabilizer Attach FittingsSDR QMLA2013111413166Drive Assy · seizedAT CRUISE ALTITUDE 2500 FT MSL, COCKPIT BEGAN TO FILL WITH SMOKE. HYD AND SERVO LIGHTS ON CAUTION PANEL ILLUMINATED. REDUCED AIRSPEED AND MADE EMERGENCY LANDING. AFTER LANDING AND ENGINE SHUTDOWN THE PRIMARY HYD BELT WAS FOUND BROKE AND MISSING. NO OTHER ANov 14, 2013 · N137HN · Urocop EC130B4 · Hydraulic System, MainSDR QMLA2013110413158Seal · separatedDURING TROUBLESHOOTING OF THE ENGINE ELECTRICAL INDICATION SYSTEMS FOR POSSIBLE CAUSE OF ENGINE POWER CHECK FAILURE, FOUND THAT THE INTAKE COMPRESSOR BLADES SUSTAINED DAMAGE. ON FURTHER INSPECTION AND REMOVAL OF THE INTAKE SHROUD AND THE INLET BARRIER FILTER Nov 4, 2013 · N329AM · Urocop EC130B4 · Engine (Turbine/Turboprop)SDR QMLA2013110213154Display · failedDISCOVERED BURNED ODOR IN CABIN WHILE RETURNING TO BASE. VERIFIED THAT HEATING AND DEMISTER WAS STILL OFF. FAILED MESSAGE AND PUSHED RESET AND FAILED AGAIN. ODOR HAD DISSIPATED AT THIS POINT, OVER AIRPORT AND LANDED UNEVENTFULLY. ON SHUTDOWN, FAILURE MESSAGENov 2, 2013 · N329AM · Urocop EC130B4 · Central ComputersSDR QMLA2013110113155Starter Gen · failedDURING APPROACH, GENERATOR INDICATED ZERO AMPS AND BATTERY VOLTAGE WAS DROPPING RAPIDLY. PILOT PERFORMED NORMAL LANDING AT AIRPORT. MECHANIC REPLACED STARTER GENERATOR.Nov 1, 2013 · N533AM · Snias AS350B3 · Starter-Generator
Back to Turbomeca ARRIEL-2B1