Turbomeca ARRIEL-1E2
Service difficulty reports · 163
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 = 'ARRIEL1E2' 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 = 'ARRIEL1E2' 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 O84A2014101400161Unknown · odorON LEVEL OFF AND INTO CRUISE FLIGHT, MED CREW DETECTED A STRONG FUEL ODOR IN CABIN. ODOR THEN SPREAD TO COCKPIT. FLIGHT ABORTED AND RETURNED TO PAD. ACFT INSPECTED FOR FUEL LEAKS NONE FOUND. TOOK TWO ATTEMPTS TO START NR 2 ENGINE AND ODOR IS BELIEVED TO BESDR HDNA2014092600160Actuator · failedDUPLEX CYCLIC TRIM ACTUATOR FAILED INFLIGHT CAUSING UNWANTED FORCE TO CONTROLS.SDR QMLA2014091014108Shaft · damagedUPON REMOVAL OF TAIL ROTOR SHAFT FROM GEAR BOX, FOUND METAL PARTICLES INSIDE CASING & EXCESSIVE WEAR ON END SHAFT SPLINES. EROSION IS APPROX .090 FORM END INWARD & .030 DEEP.SDR QMLA2014090414105Gearbox · crackedPILOT REPORTED OIL RESIDUE ON TAIL ROTOR GEARBOX & SCRATCH ON LEADING SIDE NEAR LT BOLT AFTER FLIGHT. MECHANIC INSPECTED & FOUND CRACK AFT OF LT AFT BOLT & TAIL ROTOR GEARBOX 1/4 QT LOW ON OIL.SDR O84A2014082700149Engine · power lossBRIEFLY BEFORE ENTERING CRUISE FLIGHT, BOTH ENGINE CAD DISPLAYS SHOWED ENG PA DIS. ALSO ROTOR RPM DROPPED TO THE POINT OF WP LIGHT AND HORN. PILOT LOWERD POWER AND ATTEMPTED TO BEEP UP RPM. LOWERING POWER BROUGHT UP ROTOR RPM. AFTER CONSULTING CHECKLIST FOSDR QMLA2014043014048Transmitter · defectiveDURING TAKEOFF FROM LANDING ZONE THE NR 1 SYS MGB OIL PRESS DROPPED TO .4 BAR, BELOW NORMAL RANGE. THERE WERE NO CHIPS DETECTED OR TEMP RISE ASSOCIATED WITH THIS INDICATION. SYS NR 2 PRESS REMAINED WITHIN NORMAL LIMITS. THE FLIGHT WAS ABORTED & CONTINUED TSDR QMLA2014042914045Actuator · leakingTHE TAIL ROTOR ACTUATOR WAS FOUND SEEPING. THIS ACTUATOR WAS IN SERVICE FOR 146 HOURS, ABOUT THE AVERAGE TIME FOR REPLACEMENT EXPERIENCED AT THIS FACILITY WITH THIS ACFT. THE LEAKAGE RATE EXCEEDS THE LIMITS SPECIFIED IN THE MBB BK117C-2 AMM IAW CH 67-34-00, SDR 3GMA20140212002Unknown · malfunctionedTEN MINUTES INTO 1 LEG OF FLIGHT, NOTICED NR 1 & NR 2 OIL PRESS SLIGHTLY OFF. NOTED DECREASE IN OIL PRESS OF THE NR 2 ENG. AFTER 10 MINUTES PILOT ELECTED TO DIVERT FOR RUN ON LANDING. PILOT BROUGHT NR 2 ENG TO IDLE & SET UP FOR RUN ON LANDING.SDR 3GMA20140212001Connector · dirtyEXPERIENCED LOSS OF OIL PRESS INDICATION ON NR 2 ENG IN-FLIGHT. FOLLOWED RFM FOR LOSS OF OIL PRESS INDICATION SINGLE ENG ID, SINGLE ENG EMERGENCY SHUTDOWN PERFORMED, LANDED AS SOON AS PRACTICAL AT NEAREST IMPROVED AREA FOR RUN ON LANDING. NO LIMITS EXCEEDED,SDR QMLA2013101013141Valve · failedFOUND FUEL PRESSURIZING VALVE ON NR 2 ENGINE INOPERATIVE, ALLOWING TOO MUCH FUEL TO ENTER ENGINE AT START. RAW FUEL WAS BEING PUSHED THROUGH THE ENGINE ON START AND FLOWING INTO THE COWLINGS OF ACFT. IN FLIGHT THE TRAPPED FUEL WAS SEEPING OUT OF THE COWLINGSSDR 3GMA20130706006Gearbox · chippedTAIL ROTOR CHIP LIGHT IN FLIGHT. MADE A PRECAUTIONARY LANDING IN BASEBALL FIELD. ENROUTE TO MEDICAL SCENE CALL AND HAD TO ABORT.SDR QMLA2013070513093Engine · making metalDURING A SCHEDULED ZONE INSPECTION, THE MECHANIC FOUND THE CHIP DETECTORS FOR THE NR 2 ENGINE WITH SMALL AMOUNTS OF METAL CHIPS ON ALL DETECTORS. HE THEN REMOVED THE OIL FILTER TO FIND METAL CHIPS AS WELL. AN OIL SAMPLE AND CHIPS WERE SENT TO LAB FOR TESTINGSDR GVNA201306180001Drain Valve · failedSTART DRAIN VALVE FAILED INTERNALLY ALLOWING FUEL TO FLOW INTO THE COMPRESSOR THROUGH THE P2 AIR LINE. FUEL BLEW OUT OF THE COMPRESSOR CASE SPLIT LINE AND IGNITED ON TOP OF THE ENGINE CAUSING THE FIRE WARNING LIGHT TO FLICKER ON AND OFF SEVERAL TIMES. PILOT SDR 3GMA20130515004Tachometer · inoperativeDURING SYSTEM CHECK, AFTER STARTING NR 1 ENGINE, NO ROTOR TACH WAS INDICATED WITH ROTORS TURNING.SDR QMLA2013032313042O-Ring · leakingAN ODOR OF FUEL IN THE NR 2 ENGINE COMPARTMENT, AND NOTICED THE ENGINE DECK HAD FUEL ON IT. DRIP FROM THE STARTING DRAIN VALVE DRAIN LINE. FOUND LEAK COMING FROM THE UNION BETWEEN THE STARTING DRAIN VALVE, AND IGNITION SOLENOID VALVE. FOUND O-RING HAD NOSDR 2013FA0000127Bolt · crackedDURING A 100HR ANNUAL INSPECTION, IT WAS NOTED ON THE VEMD THAT THERE WERE MAST MOMENT EXCEEDANCES TRAPPED. DURING A DIE PENETRANT INSPECTION OF THE SECONDARY BOLTS 3 OF 4 INSTALLED SECONDARY BOLTS HAD CRACKING IN THE THREADED PORTION OF THE BOLT.SDR 3GMA20130215001Blade · damagedON APPROACH, ROTOR TIP IMPACTED FLAG & FLAG HOLDER MOUNTED ON INDUSTRIAL CRANE. CREW FELT MINOR LOW FREQUENCY VIBRATION. PILOT LANDED ACFT IMMEDIATELY. ON PRELIMINARY INSPECTION, MINOR DAMAGE TO ONE MAIN ROTOR BLADE END CAP WAS DISCOVERED. PILOT NOTED NO LSDR QMLA2013012613013Unknown · unknownPILOT REPORTED AFTER TAKEOFF, GOING THROUGH TRANSITIONAL LIFT, TRIM (YAW) TRIED TO MAKE NOSE YAW RIGHT, PILOT HAD TO EXCESSIVELY FIGHT TRIM. MECHANICS HAVE CHECKED THE TAIL ROTOR CONTROL SYS, INSPECTED AND CLEANED T/R BLADE GRIPS AND PERFORMED AUTOPILOT CHECKSDR QMLA2013012413010O-Ring · pinchedPILOT REPORTED FUEL SEEPING FROM ENGINE NR 2 COWLING AND MIGRATING BACK TO RT CLAMSHELL DOOR: UPON TROUBLESHOOTING, FOUND DAMAGED O-RING AT ENGINE 2 DRAIN VALVE. THE MECHANIC R & R THE O-RING AND PERFORMED LEAK CHECK WITH NO DISCREPANCIES NOTED. THE ACFT WASDR 2013FA0000076Mount Bracket · crackedON VISUAL INSPECTION FOUND CRACKED MOUNTING BRACKET.SDR QMLA2013011013004Fan · shortedCREW AND PILOT SMELLED ELECTRICAL BURNING ODOR DURING FLIGHT. NORMAL LANDING COMPLETED WITHOUT INCIDENT, AND WITHOUT ANY FURTHER EMERGENCY ACTION TAKEN. MX INSPECTED ACFT, FOUND COCKPIT VENTILATION FAN SHORTING.SDR QMLA2012121012189Switch · shortedDURING TAKEOFF, SMELLED ELECTRICAL BURNING, NO SMOKE IN AIRCRAFT. RETURNED TO BASE. FOUND ODOR TO BE COMING FROM SWITCH FOR CONTROLLABLE IR SEARCHLIGHT. SWITCH IS MOUNTED IN COLLECTIVE.SDR QMLA2012112612187Structure · crackedTWO CRACKS NOTED DURING PREFLIGHT INSPECTION ON THE LT HORIZONTAL STABILIZER LOWER SIDE. NO OTHER VISUAL INDICATION OF DAMAGE.SDR QMLA2012111212180Blade · crackedAFTER REMOVAL OF BLADE FITTINGS FOR NDT, CRACK DETECTED IN GRIP AREA.SDR QMLA2012111212181Blade · crackedAFTER REMOVAL OF BLADE FITTINGS FOR NDT, CRACK DETECTED IN GRIP AREA.SDR QMLA2012111212182Blade · crackedAFTER REMOVAL OF BLADE FITTINGS FOR NDT, CRACK DETECTED IN GRIP AREA. TSDR QMLA2012100912170Attach Fitting · cracked90 DEG, TAIL ROTOR GEAR BOX ATTACHMENT FITTING, CRACKED ABOUT 1 CM AT OTBD TOP MOUNTING BOLT.SDR QMLA2012100112160Belt · brokenIN FLIGHT, PILOT AND PASSENGERS DETECTED THE ODOR OF SMOKE. NO SMOKE OR EVIDENCE OF FIRE WAS VISIBLE INSIDE OR OUTSIDE THE ACFT. PILOT SHUTOFF BOTH GENERATORS AND AIR CONDITIONER IAW CHECKLIST. ACFT MADE A PRECAUTIONARY LANDING AND PERFORMED AN EMERGENCY SHUSDR QMLA2012092012157Frame · crackedDURING PREFLIGHT, FOUND A CRACK APPROX ONE INCH LONG IN THE LT FRAME OF THE TAIL FIN NEAR THE CAMLOCK FASTENER RECEPTACLE BELOW THE SERVO MOUNT.SDR QMLA2012083012143Starter Gen · malfunctionedGENERATOR DISCONNECT LIGHT CAME ON FOR THE NR 1 GENERATOR. LANDED WITHOUT INCIDENT UNDER POWER FROM BOTH ENGINES. SWAPED STARTER/GENERATOR FROM SIDE TO SIDE. FOUND ISSUED FOLLOWED GENERATOR.SDR QMLA2012081112132Engine · making metal20 MINUTES INTO FLIGHT, THE NR 2 ENGINE CHIP LIGHT ILLUMINATED. ACTIVATED THE FUZZ BURNER FOR APPROX 1 SECOND AND THE LIGHT EXTINGUISHED. APPROX 1 SECOND LATER THE CHIP LIGHT ILLUMINATED AGAIN. ACTIVATED THE FUZZ BURNER AGAIN AND LIGHT EXTINGUISHED. APPROSDR QMLA2012081012128Unknown · odorIN LEVEL FLIGHT, CREW DETECTED ODOR IN AFT CABIN SPREADING FORWARD TO COCKPIT. NOT ELECTRICAL, BUT MORE OF SOMETHING GETTING VERY HOT BUT NOT QUITE BURNING. AIR CONDITIONING UNIT WAS SHUTOFF AND THE ODOR DISSIPATED. ACFT RETURNED TO BASE. MECHANIC NOTHINSDR QMLA2012070112110Chip Detector · dirtyDURING CRUISE FLIGHT, 4 MINUTES AFTER DEPARTURE TAIL ROTOR CHIP CAUTION SEGMENT ILLUMINATED. PILOT PERFORMED EMERGENCY PROCEDURE IAW FMS 9.2-15-5. TAIL ROTOR CHIP REMAINED ILLUMINATED. PILOT LANDED WITHOUT FURTHER INCIDENT, ACFT SHUTDOWN. MECHANIC REMOVED SDR QMLA2012060512090Disk · damagedWHILE PERFORMING TU360 UPGRADE TO ENGINE SN 18789 FOUND THE SECOND STAGE TURBINE DISK BLADE LOCKS DISPLACED LEADING TO BLADE SHIFT. R & R MODULE 3.SDR QMLA2012060112092Fcu · out of tolerancePERFORMED ENGINE ZONE 8 INSPECTION, RUN UP AND LEAK CHECKED, AND STARTED POWER CHECK PROCEDURE. N1, N2 AND TORQUE FLUCTUATING, 1-2 PERCENT ON N1, 2-3 PERCENT ON THE TORQUE. INSPECTED P2 LINE, PERFORMED LEAK CHECKS, AS DIRECTED BY THE TECH REP AND RAN UP AGASDR QMLA2012051812083Fcu · unserviceableFUEL LEAKING FROM OVERBOARD DRAIN DETECTED AFTER ENGINE SHUTDOWN FROM GROUND RUN LEAK CHECK FOR PERFORMED MX NOT ASSOCIATED WITH THIS FAILURE. TROUBLESHOOTING IAW MM REVEALED THAT THE FCU HAD FAILED, LEAKING FUEL AT A RATE WELL ABOVE THAT ALLOTED BY MFG. CONFESDR QMLA2012051412081Fcu · leakingCREW MEMBER SMELLED FUEL. COULD SEE LIQUID ON THE RT REAR CLAM SHELL GLASS WINDOW. CONTINUED FLIGHT AND LANDED WITHOUT INCIDENT. AFTER LANDING, FOUND THE FUEL CAP SECURE, BUT FUEL ON NR 1 ENGINE DECK AND ON THE ACFT SKIN BELOW AND AFT OF THE ENGINE DECK. SDR QMLA2012041212059Throttle · roughPILOT WAS PERFORMING PRE-START CHECKLIST FOR 2ND FLIGHT OF THE DAY. WHILE OPERATING NR 2 TWIST GRIP FROM "0" TO "F" NOTICED EXTREME FRICTION FROM BETWEEN "30" AND "F". MADE SEVERAL ATTEMPTS TO GO TO "F" BUT WAS CONCERNED THAT SOMETHING MAY BREAK. ACFT REMOVSDR QMLA2012032112034Engine · malfunctionedINBOUND TO THE MAIN HELIPAD WHEN THE LOW ROTOR HORN ACTIVATED WHILE AIRSPEED WAS ABOVE 55 KNOTS. DUE TO THE DECREASING AIRSPEED DURING APPROACH AND AFT CYCLIC STICK APPLICATION, AIRSPEED DROPPED BELOW 55 KNOTS & ROTOR RPM INSCREASED TO 101 PERCENT. ABORTED SDR QMLA2012030312023Unknown · odorTHE PILOT DETECTED THE ODOR OF FUEL IN THE CABIN AND COCKPIT, APPROXIMATELY FOUR MINUTES INTO FLIGHT. RETURNED TO BASE. MX INSPECTED ACFT IAW THE MM 60. NO DEFECTS WERE NOTED. A MX CHECK FLIGHT WAS PERFORMED WITH NO ODOR DUPLICATED. THE ACFT WAS RETURNED SDR QMLA2012012712014Fuel Control · leakingAFTER TAKEOFF, NOTICED FLUID ON THE HELIPAD WHERE THE HELICOPTER WAS SITTING. WHILE SETTING UP FOR FINAL APPROACH BACK TO BASE, RECEIVED COMMUNICATION THAT FLUID WAS IDENTIFIED AS JET FUEL. AFTER LANDING, NOTED FLUID COMING OUT OF NR 2 ENGINE DRAIN PORT. SDR QMLA2012010412001O-Ring · tornTHE PILOT REPORTED AFTER LANDING, THE NURSE IN THE AFT CABIN STATED HE SMELLED GAS FUMES. AS THE CREW WAS EXITING THE ACFT, THEY VISUALLY CONFIRMED FUEL LEAKING FROM THE NR 1 ENGINE COWLING. THE PILOT IMMEDIATELY COMPLIED WITH AN EMERGENCY SHUTDOWN OF THE ENSDR QMLA2011101811102Fuel Tank · leakingTHE MEDICAL CREW REPORTED TO THE PILOT THAT THEY SMELLED FUEL IN THE CABIN SHORTLY AFTER TAKEOFF. THE PILOT IMMEDIATELY RETURNED TO THE HELIPAD. THE MECHANIC PERFORMED AN INPSECTION OF THE FUEL SYS AND FOUND THAT THE LOWER FITTING OF THE EXPANSION TANK WAS LSDR QMLA2011090711104Control Tube · crackedDURING AN AIRWORTHINESS CHECK, A CRACK WAS DISCOVERED IN THE MAIN ROTOR ROTATING CONTROL TUBE ATTACHED TO THE GREEN MAIN ROTOR BLADE. THE CRACK WAS LOCATED IN THE COLLAR OF THE TUBE POSITIONED NEAREST THE BLADE, AND WAS PARALLEL TO THE LENGTH OF THE TUBE. ONCSDR QMLA2011052411060Fuel Control · defectiveABOUT 4 MINUTES INTO FLIGHT STRAIGHT AND LEVEL NR 1 ENGINE ROLLED BACK TO 74 PERCENT N1 UNCOMMANDED. NR1 ENGINE LOW LIGHT ILLUMINATED. PILOT CONFIRMED PCL WAS IN FULL FORWARD FLY POSITION AND ATTEMPTED TO BEEP NR1 ENGINE UP USING ENGINE TRIM SWITCH, ENGINE RESDR QMLA2011050611054Blade · damagedDURING THE PILOTS PRE FLIGHT, FOUND THAT THE TRIMMING SURFACE ON THE YELLOW BLADE WAS MISSING. UPON INSPECTION FOUND THE TWO RIVET HOLES, WHERE THE RIVETS HELP HOLD THE TRIMMING SURFACE TO THE BLADE, WAS IN ALMOST PERFECT CONDITION. SENT MAIN ROTOR BLADE TO AMSDR QMLA2011033011042Bearing · making metalTHE NR 2 ENGINE CHIP LIGHT ILLUMINATED ENROUTE TO A SCENE CALL. THE PILOT IMMEDIATELY ABORTED THE FLIGHT AND RETURNED TO BASE LESS THAN 3 MILES AWAY. UPON ARRIVING AT THE BASE, THE MECHANIC INSPECTED THE CHIP PLUGS AND FOUND METAL ON THE M05 MAGNETIC PLUG ANSDR 7KFA775LWire · chafedELECTRICAL FIRE IN FLIGHT IN THE VICINITY OF SUCTION CONTROLS AND LIQUID OXYGEN GAUGE, FLAMES, SMOKE AND FUMES IN ACFT. WHEN DISCOVERED: IN FLIGHT, CAUSE OF INCIDENT COME FROM THE 120 VOLT AC OUTLET WIRE NR XMO10B12, PN M22759/16/12 WHICH IS LOCATED ON THE LTSDR UIEA201000233Skin · puncturedDURING JACKING OF ACFT, MX PUNCTURED AN EXISTING REPAIR DOUBLER THROUGH THE UNDERLYING SKIN, LOCATED AT SECTION 48, BS 2594 ABOVE STRINGER 42R TAIL JACK PAD AREA. PUNCTURE MEASURING 5.0 IN. LENGTH X 1.750 WIDTH. DISPOSITION WAS MADE TO PERFORM PERMANENT REPASDR QMLA2010091810061Chip Detector · contaminatedTHE TRANSMISSION CHIP LIGHT ILLUMINATED IN CRUISE FLIGHT ON RETURN FLIGHT TO BASE. THE MECHANIC INSPECTED THE CHIP PLUGS AND FILTERS, AND FOUND A SMALL PARTICLE ON THE PLUG, AND FUZZ ON BOTH THE FILTER HOUSING AND THE FILTERS. THE MECHANIC PROCEEDED TO DRAIN
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