Turbomeca ARRIEL-1D1
Service difficulty reports · 933
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 = 'ARRIEL1D1' 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 = 'ARRIEL1D1' 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 QMLA2014062114077Warning System · false activationON TAKEOFF, THE PILOT RECEIVED AN EXCEEDANCE INDICATION ON THE VEMD. THE PILOT LANDED THE ACFT WITHOUT INCIDENT. THE MECHANIC ARRIVED TO INSPECT THE ACFT & FOUND NO STORED EXCEEDANCES IN THE VEMD. HE THEN ASKED THE PILOT TO PERFORM A GND RUN WHICH AFTER SHUSDR QMLA2014061914076Chip Detector · contaminatedAFTER TAKEOFF, ENG CHIP DETECTOR CAUTION CAPSULE FLICKERED. RETURNED TO BASE & SHUT DOWN. BY SHUT DOWN, CHIP LIGHT WAS STEADY. THE MECHANIC ARRIVED & INSPECTED THE SYS, HE COULD NOT IDENTIFY ANY ANOMALIES IN THE SYS. HE CLEANED THE CHIP PLUGS OF SOME CARBSDR QMLA2014060814067Drive Belt · tornJUST AFTER TAKEOFF DURING CLIMB THE CREW DETECTED THE SMELL OF BURNING RUBBER IN THE CABIN & HEARD A SQUEALING SOUND. SECURED THE AIR CONDITIONING SYS & OPENED THE CABIN VENT. THE ACFT WAS RETURNED TO THE HELIPAD & SHUT DOWN NORMALLY. UPON POST FLIGHT THE DSDR CA140604003Housing · corroded(CAN) DEEP PITTING CORROSION IN A VERY SMALL LOCAL AREA. NO OTHER CORROSION ON THE COMPONENT. SUSPECT FOREIGN OBJECT IMPREGNATED INTO MATERIAL OR DEFECTIVE CASTING. DAMAGE IS WELL BEYOND LIMITS.SDR CA140603009Magnetic Plug · damaged(CAN) AT A SM EVENT, SIGNIFICANT METAL WAS NOTED ON THE M05 MAG PLUG AND THE MAG PLUG. NO CHIP LIGHT ILLUMINATION HAD OCCURRED DURING OPERATION, HOWEVER IT APPEARED TO BE IMMINENT. FILTERS AND OIL WERE CHANGED AND A 20 MIN GROUND RUN WAS CARRIED OUT IAW THE SDR ULXR2014050900059Structure · crackedUPPER WIRE STRIKE CUTTER MOUNTING FLANGE CRACKED.SDR QMLA2014042314039Frame · corrodedMOUNTING SCREW NUTPLATE & FRAME AT STATION X1790.15 & Y400.0 HAS DAMAGE & HAS SURFACE CORROSION JUST FWD OF RT LANDING LIGHT ASSEMBLY.SDR QMLA2014042314041Starter Gen · faultyGENERATOR CAUTION LIGHT ILLUMINATED APPROXIMATELY 10 MINUTES AFTER DEPARTURE. RESET OF GENERATOR EXTINGUISHED THE CAUTION LIGHT. FLIGHT CONTINUED NORMALLY TO HOME BASE. THE STARTER GENERATOR WAS REPLACED & THIS ACFT WAS RETURNED TO SERVICE.SDR ULXR201405090005Structure · crackedUPPER WIRE STRIKE CUTTER MOUNTING FLANGE CRACKED.SDR QMLA2014042114040Duct · contaminatedAFTER STARTING THE ENG FOR A SCENE FLIGHT, THE NURSE & MEDIC DETECTED AN UNIDENTIFIED ODOR. ATTEMPTS TO LOCALIZE & IDENTIFY THE ODOR WERE UNSUCCESSFUL & WE ELECTED TO SHUT DOWN WITH NO FURTHER INCIDENT. AFTER ADDITIONAL GND RUN, THE ODOR WAS DETERMINED TO BESDR QMLA2014041614038Planetary Gear · unserviceableDURING A6031RT, MAST INSPECTION, UPON SEPARATION OF THE MAST & MGB, SEVERAL METALLIC FERROUS FLAKES WAS LOCATED ON & AROUND THE EPICYCLICAL REDUCTION GEAR. AFTER FURTHER INVESTIGATION, 1 OF 5 SATELLITE PLANETARY GEARS PN 350A32-1082-03, SN L31442 OF THE EPICSDR 2A6R2014041195301Structure · corrodedDURING INSPECTION PROCESS, FOUND CORROSION LOCATED INSIDE UPPER RT SIDE BAGGAGE COMPARTMENT, UNDER ENG DECK. AFTER REMOVAL OF CORROSION A FULL PENETRATION AREA OF APPROXIMATE 3/4 TO 1 INCH DIAMETER HOLE WAS FOUND, MANUFACTURE IS BEING CONTACTED FOR POTENTIAL SDR MHIA20140408001Pump · seizedON APPROACH TO 65NJ PILOT NOTED HYD LIGHT ON WARNING CAUTION PANEL INDICATING HYD FAILURE. ABORTED LANDING AT 65NJ TO CHANGE COURSE TO EWR FOR A RUN ON LANDING. MADE A MAYDAY CALL TO EWR SIGHTING INFLIGHT EMERGENCY. EWR CLEARED RUNWAY 29 FOR EMERGENCY LANDISDR CA140404002Frame · cracked(CAN) CRACK DEVELOPED ON MAIN FRAME AT THE REAR LT UPPER ATTACHMENT OF FUEL TANK SUPPORT.SDR CA140222004Hose · leaking(CAN) DURING DAILY INSPECTION, OIL WAS FOUND ON TRANSMISSION DECK, AFTER INVESTIGATION, THE HOSE GOES TO THE MGB FILTER HAS BEEN SUSPECTED TO LEAK. FINALLY AFTER INSPECTION THE HOSE WAS LEAKING AT THE PART WHERE THE HOSE IS CRIMP AT THE UPPER FITTING. HOSE WSDR MHIA20140325001Seal · damagedDURING FLIGHT THE RT PILOT DOOR UPPER WINDOW DEPARTED THE ACFT. THE SEAL WAS DRY ROTTED.SDR 2014FA0000050Impeller · failedAIR CONDITIONING BLOWER FAN IMPELLER FAILED. CAUSED HIGH VIBRATION LEVEL THAT LED TO PRECAUTIONARY LANDING.SDR CA140204011Stop · delaminated(CAN) SPHERICAL STOP ASSY FOUND DELAMINATED BEYOND LIMITS. THREE SPHERICAL STOP ASSEMBLIES REPLACED.SDR CA140110004Gearbox · leaking(CAN) DURING THE ALF CHECK, IT WAS NOTICED THAT THE OIL LEVEL IN T/R GEAR BOX WAS TOO LOW, AND THE FIN WAS COVERED IN OIL. THE INPUT MAG SEAL WAS REPLACED AT 3105.4 HRS. THE ACFT FLEW FOR 3.4 HRS AND NO DEFECT WAS REPORTED. THE DAY AFTER THE ACFT FLEW FOR 1.SDR DCGA2013FA0000717Seal · leakingDURING PREFLIGHT CHECKS, PILOT TURNED ON FUEL BOOST PUMPS. NOTICE FUEL COMING FROM THE ENGINE DECK DRAINS. MAINTENANCE DETERMINED THAT THE ENGINE FUEL CONTROL GOVERNOR DRIVE FUEL SEAL WAS LEAKING. THE FUEL CONTROL UNIT WAS REPLACED.SDR QMLA2013112713169Unknown · odorTHE PILOT DEPARTED THE BASE EN ROUTE FOR A PATIENT. OUTSIDE AIR TEMP WAS 3 3DEG F. THE HEATING & DEMISTING SYS WAS SWITCHED ON. AS THE AIRCRAFT STARTED TO HEAT UP WE NOTICED A STRONG ODOR, IT WAS NOT THE NORMAL SMELL OF THE HEATING SYS WARMING UP BUT A STROSDR CA131121003Servo · frozen(CAN) DURING ENGINE START, THE PILOT IN COMMAND WAS UNABLE TO MOVE THE CYCLIC FORWARD. AFTER A VISUAL INSPECTION BY THE MAINTENANCE PERSONNEL, ICE BUILDUP WAS FOUND UNDER THE SERVO VALVE PROTECTION COVER. PRIOR TO THAT DAY, HEAVY RAIN WENT THROUGH THE AREA FSDR CA131204006Fcu · failed(CAN) FUEL CONTROL UNIT WAS ACQUIRED OVERHAULED FROM MFG AND INSTALLED ON ACFT. REMOVED DUE TO SLOW START AND UNABLE TO ACCELERATE PAST 30 PERCENT DURING START SEQUENCE.SDR QMLA2013111413167Sense Line · crackedIN CRUISE FLIGHT WHILE ON A SCENE STANDBY, THE ENG OIL PRESS LIGHT ILLUMINATED WITH CORRESPONDING OIL PRESS GAGE INDICATION OF ABOUT 1.2 BAR. WE ANNOUNCED A PRECAUTIONARY LANDING, SIMULTANEOUSLY COMMENCED AN IMMEDIATE POWER ON LANDING, TOUCHING DOWN APPROXIMASDR QMLA2013111113164Warning Light · illuminatedENGINE CHIP SEGMENT ILLUMINATED IN FLIGHT AND POWER WAS REDUCED TO LAND. LANDED WITHOUT FURTHER INCIDENT.SDR QMLA2013110913163Housing · crackedDURING INSPECTION OF THE FDC INLET BARRIER FILTER SEAL, DISCOVERED LARGE CRACK IN THE FIBERGLASS FILTER HOUSING JUST BELOW SEAL.SDR CA131107006Reservoir · contaminated(CAN) WATER AND ICE CONTAMINATION WAS FOUND IN THE HYDRAULIC RESERVOIR FILLER NECK.SDR QMLA2013102913152Blower · burned outDURING A RETURN FLIGHT, CREW DETECTED AN ELECTRICAL ODORL. AT SAME TIME CABIN VENTILATION FAN STOPPED WORKING. PILOT IMMEDIATELY NOTICED THAT THE FRONT FAN WAS WORKING, SHUT THE SYS OFF AND OPENED THE OUTSIDE AIR VENT. ODOR DISSAPATED AS SOON AS THE VENT WSDR QMLA2013100613139Controller · bindingPILOT FELT RESISTANCE IN THE FORE AND AFT CYCLIC PITCH CONTROL ON APPROACH. TROUBLESHOOTING AND TALKING TO TECH REP, DETERMINED THAT THE PITCH MAIN ROTOR SERVO IS FAILING INTERNALLY. THIS SERVO CONTROL WAS R & R, WITH THE SUBSEQUENT OPERATIONAL GROUND AND FLSDR XSFA201310170001Gyro · failedPILOT REPORTED AN ELECTRICAL TYPE BURNING ODOR FOLLOWED BY LIGHT WISPS OF SMOKE FROM UNDER THE INSTRUMENT PANEL HOOD. FLIGHT WAS ABORTED, AND A PRECAUTIONARY LANDING WAS MADE, WHERE THE ACFT WAS SHUTDOWN AND REMOVED FROM SERVICE. UPON FURTHER INSPECTION BY SDR QMLA2013092913138Fuel Control · leakingSHORTLY AFTER TAKEOFF, CREW SMELLED FUEL IN CABIN. PILOT RETURNED TO BASE AND LANDED WITHOUT INCIDENT. ARRIVED AT BASE HAD PILOT TURN MASTER AND FUEL BOOST PUMP ON TO VERIFY THAT THE LEAK WAS COMING FROM FUEL CONTROL . GROUND RAN ACFT. LEAK STOPPED AND WAS SDR 2013FA0000559Leaf Pad · looseBEFORE FIRST FLIGHT CHECK, WHILE HELICOPTER WAS ON TRANSPORT WHEELS, MECHANIC NOTICED THE LT SKID T/E LEAF PAD, LEAF SPRING, WAS LOOSE. REPLACED BOTH LEAF PADS WITH NEW AND REPLACED ALL ATTACHING HARDWARE.SDR QMLA2013092113137Lamp · burned outON CLIMBOUT FROM BASE HELIPAD, INSTRUMENT LIGHTS FAILED. ATTEMPTED TO RESET SWITCHES AND DIMMERS WITH NO RESULTS. RETURNED TO BASE HELIPAD AND LANDED WITHOUT INCIDENT. CONTACTED THE BASE MECHANIC WITH NOTIFICATION OF MX ISSUE.SDR CA130918007Servo · failed(CAN) AFTER INSTALLATION AND DURING A FREEDOM OF MOVEMENT CHECK IT WAS NOTED THAT THE RT LATERAL SERVO CONTROL INPUT LEVER LOCK WOULD POP OUT OF THE LOCKED POSITION. THIS COULD INTRODUCE A DANGEROUS INFLIGHT CONTROL CONDITION IN THE EVENT OF A HYDRAULIC FAILURSDR CA130916011Sight Gauge · cracked(CAN) AIRFRAME FUEL FILTER SIGHT GLASS DOME FOUND CRACKED. DOME REPLACED NEW WITH UNIT REMOVED FROM A NEW FILTER ASSY PURCHASED AUG 8/13. NEW DOME CRACKED AND WAS REPLACED AGAIN WITH A USED SERVICABLE PART AND FOUND SERVICABLE AFTER BLEEDING.SDR CA130925003Oil Cooler · leaking(CAN) ENGINE OIL COOLER SPRUNG A LEAK, PILOT DISCOVERED DURING A DI. MAINTENANCE DISPATCHED, COOLER CHANGED, ACFT RETURNED TO SERVICE. COOLER TO BE SENT OUT TO SEE IF IT`S REPAIRABLE.SDR QMLA2013082013119Unknown · odorDURING FLIGHT, PILOT SMELLED A STRONG ODOR OF SMOKE FROM THE CABIN AREA. CAUSE IS UNKNOWN AT REPORT DATE. MX COULD NOT DUPLICATE.SDR CA140707001Hose · leaking(CAN) HYDRAULIC HOSE LEAKING.SDR CA130813005Bearing · cracked(CAN) TAIL ROTOR HALF SHELL BEARINGS CONSIST OF 4 SEPARATE BEARINGS TO MAKE 1 SET. 2 OF THE 4 BEARINGS WERE FOUND WITH CRACKS THAT EXTENDED AROUND A CORNER OF THE RUBBER AND CONTINUED ALONG THE OTHER EDGE AND THE CRACKS WERE BEYOND ALLOWABLE LIMITS. THE HALFSDR 2013FA0000426Drive Belt · brokenAIR CONDITIONER COMPRESSOR SEIZED IN FLIGHT. AIR CONDITIONER DRIVE BELT BROKE WAS TANGLED IN THE HYD. PUMP DRIVE BELT WHICH CAUSED THE HYD. DRIVE TO DISINGAGE AND PILOT LANDED WITH HYD. OFF. NO DAMAGE TO ACFT.SDR QMLA2013070213088Engine · making metalENG CHP SEGMENT ILLUMINATED IN FLIGHT AND POWER WAS REDUCED TO LAND AS SOON AS POSSIBLE WHERE AARF RESCUE WAS ON STANDBY. LANDED AT HOME PAD WITHOUT FURTHER INCIDENT AND NOTIFIED MX. MX FOUND SMALL FLAKE ON CHIP DETECTOR AND SEVERAL FLAKES IN OIL FILTER BOWLSDR CA140707002Transducer · malfunctioned(CAN) WRONG INDICATION WHEN THE TORQUE TRANSDUCER GETS WARM.SDR CA130715014Hose · cracked(CAN) THE PILOT NOTICED SOME DROPLETS OF OIL. THE PILOT LANDED AT STAGING SITE TO INVESTIGATE. THE ENGINE OIL COOLER OUTLET HOSE HAD A LENGTHWISE CRACK DEVELOP ALLOWING THE OIL TO LEAK. THE FLEX HOSE HAD STAMPED ON IT THE YEAR 2007 WAS CUE TO BE REPLACED IN SDR CA130618011Seal · leaking(CAN) THE STARTER GEN SEAL FOUND LEAKING.SDR QMLA2013060913080Gearbox · making metalTAIL ROTOR GEARBOX CHIP LIGHT, NON TAKEOFF FOR SCENE FLIGHT, LANDED AT AIRPORT AFTER TRGB CHIP LIGHT CAME ON. FOUND LARGE SHAVINGS ON CHIP DETECTOR. REPLACED TRGB.SDR QMLA2013060313073Skin · crackedDURING PREFLIGHT, FOUND CRACK ON RT UPPER HORIZONTAL STABILIZER. MEASURED CRACK AT 70MM. AEC CRITERIA FOR BEYOND REPAIR IS 60MM.SDR CA130618012Bearing · worn(CAN) THE TAIL ROTOR LAMINATED BEARING FOUND WORN.SDR 2013FA0000323Switch · inoperativeDURING FLIGHT, THE "HYD POWER" ANNUNICATOR AND WARNING HORNS WERE ACTIVATED. THE PILOT FOLLOWED THE PUBLISHED EMERGENCY PROCEDURE AND DEACTIVATED THE HYD POWER. AN EMERGENCY WAS DECLARED AND THE PILOT EXECUTED A RUN-ON LANDING. DURING THE MX INVESTIGATION, ISDR CA130424003Hose · leaking(CAN) NEW STYLE LINES WERE INSTALLED LESS THAN 3 HRS PRIOR TO FAILURE. PILOT NOTICED HYD FLUID UNDER THE ACFT AND FOUND A MASSIVE LEAK ON THE MGB DECK. THERE HAVE BEEN REPORTED ISSUES WITH THESE "NEW" LINES AND WE ARE AWARE OF SEVERAL OPERATORS WHO HAVE HAD SDR CA130424009Magnetic Seal · leaking(CAN) WHEN ACFT LANDED AT OUR BASE FOR MAINTENANCE, IT WAS NOTICED THAT THE TGB INPUT SEAL WAS LEAKING OIL.
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