Safran 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 QMLA2021082020042Engine · power lossAPPROXIMATELY 5 MIN INTO THE RETURN FLIGHT I NOTICED THE TQ NEEDLES STARTING TO SPLIT AND I RECEIVED THE ENG PA DIS LIGHT WITH TQ DISPLAYED IN YELLOW, APPROX. 20SEC LATER I RECEIVED THE ENG SPLIT CAUTION AND HEARD THE LOW ROTOR WARNING SOUND. I IMMEDIATELY LOWSDR QR9R20210624002Fuel Control · fluctuatesUNABLE TO HOVER WITH VARTOMS IN NORM MODE BECAUSE FLI NEEDLES WOULD FLUCTUATE EXCESSIVELY WITH SPREADS GREATER THAN 20% DIFFERENCE BETWEEN BOTH TORQUES, HAD TO HOVER IN THE MAN MODE NOT TO EXCEED ANY LIMITS. NOTICED THAT FLI #2 NEEDLE WAS VERY SLOW TO REACT TOSDR 2021FA0000171Oil System · leakingIN CRUISE FLIGHT #1 ENGINE OIL PRESSURE LIGHT CAME ON ENGINE OIL TEMP STARTED TO RISE FOLLOWED BY DEC4REASING ENGINE TORQUE INDICATION. PILOT SHUTDOWN #1 ENGINE AND PERFORMED A RUNNING LANDING AT KYVS. INVESTIGATION SHOWED LOSS OF OIL IN ENGINE RESERVOIR AND ASDR 2021FA0000094Motor · inoperativeDURING FLIGHT, THE CREW SMELLED A BURNING SMELL IN THE CABIN. THE PILOT DEACTIVATED THE A/C SYSTEM AND PERFORMED AND UNSCHEDULED LANDING. UPON MAINTENANCE ARRIVAL, IT WAS FOUND THAT THE EVAPORATOR MOTOR WAS INOPERATIVE. THE SYSTEM WAS DEFERRED AND THE BLOWER WSDR QMLA2021030820011Drain Valve · leakingPILOT REPOTS THAT " UPON LIFT HAD A LARGE TORQUE SPLIT. ENGINE WENT FROM CATA TO MAUAL. FUEL SMELL IMMEDIATELY AFTER SPLIT." BASE MECHANIC RESPONDED TO BASE. MECHAIC VISUALLY INSPECTED #1 & #2 ENGINE FUEL CONTROL ANTISIPATORS FOR EVIDENCE OF BINDING AND PRSDR QMLA2021012220001None · noneAFTER PICKING UP FROM THE BASE HELIPAD THE MEDIC WHO WAS SEATED IN THE CO-PILOT SEAT NOTED THAT SHE COULD SMELL FUEL. I DIDN'T SMELL ANYTHING AND NEITHER DID THE NURSE WHO WAS SEATED IN THE BACK. I CHECKED ALL GUAGES AND CAUTION AND WARNING LIGHTS FOR ANY ABSDR HDNA20201029001Wire · brokenPIC REPORTED SPARKS AND SMALL AMOUNTS OF SMOKE EMITTING FROM OVERHEAD C/B PANEL DURING THE APPROACH PHASE OF THE FLIGHT. SUBSEQUENT TROUBLESHOOTING REVEALED A BROKEN GROUND WIRE MAKING INTERMITTENT CONTACT WITH A 28V BUS BAR. NO SECONDARY INDICATIONS OR FAILSDR 2020F00313Wire · brokenNR 1 GENERATOR DISCONNECT. WAS ABLE TO RESET. INSPECTION REVEALED A BROKEN WIRE AT THE NR 1 GENERATOR. REPAIRED THE WIRE. GROUND RUN. OPS CHECKED GOOD.SDR GVNA2020061000001Fcu · failedNR 2 ENGINE UNDERSPEED IN-FLIGHT. SUSPECT INTERNAL FAILURE OF FUEL CONTROL. REM'D FUEL CONTROL. INSTALLED SERVICEABLE FUEL CONTROL. PERFORMED GROUND RUN/LK CHK. PERFORMED OPERATIONAL CHK FLIGHT. CHK'D GOOD. NO ANOMALIES. ACFT RETURNED TO SERVICE.SDR 2020F00312Pressure Switch · failedNR 1 FUEL PRESSURE LIGHT INTERMITTENTLY ILLUMINATES. REMOVED THE FUEL PRESSURE SWITCH. INSTALLED SERVICEABLE FUEL PRESSURE SWITCH. PERFORMED GROUND RUN, LEAK CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.SDR HDNA2020031300000Fire Detector · failed3/11/2020 AT 2035 - ON FINAL APPROACH TO REFERRING HOSPITAL #2 ENGINE FIRE CAUTION INDICATION ILLUMINATED ON AIRCRAFT WARNING UNIT. NO SECONDARY INDICATIONS WERE NOTED. POST FLIGHT INSPECTION CONFIRMED FALSE INDICATION.SDR HDNA2020030500000Fire Detector · corroded3/4/2020 AT 1408 - ON SHORT FINAL TO KOAJ ILS RWY05... THE #2 ENGINE "FIRE" LIGHT ILLUMINATED FOR ABOUT 15 SECONDS. NO VISIBLE SMOKE OR SECONDARY INDICATIONS WAS NOTED BY THE CREW. AIRCRAFT LANDED SAFELY AT THE BASE OF OPERATION WITH SUBSEQUENT INSPECTION CONFSDR HDNA2019120900233Warning Light · false activation#2 ENGINE FIRE LIGHT WAS ILLUMINATED 3-4 MILES FROM DESTINATION. ONCE THE ENGINE WAS SHUTDOWN THE LIGHT EXTINGUISHED. THE FAULT WAS TROUBLESHOT AND COULD NOT BE DUPLICATED.SDR HDNA201911189494Actuator · faultyPILOT REPORTED AN ACTUATOR WARNING LIGHT ILLUMINATED ON THE CENTRAL PANEL DISPLAY SYSTEM WITH NO SECONDARY INDICATIONS OR SUBSEQUENT DEGRADATION OF CONTROL-ABILITY. SYSTEM WAS DEFERRED I/A/W WITH THE APPROVED MEL AND RETURNED TO SERVICE. DURING THE REPAIR PHASSDR 2019FA0000360Unknown · odorSTRONG RUBBER/ELECTRICAL SMELL COMING FROM REAR CABIN AC VENTS. SMELL DISAPPEARED WITH AC TURNED OFF.SDR QMLA2019071119058Fire Detector · faultyPILOT REPORTED #1 ENGINE FIRE WARNING LIGHT DURING FLIGHT. THIS LIGHT INITIALLY BEGAN TO FLICKER, THEN WENT ON SOLID WITH AURAL TONE. THE PILOT CHECKED ALL ENGINE INSTRUMENTATION, AND THEY ALL WERE ALL IN NORMAL RANGE. HE THEN PERFORMED A VISUAL WITH THE ASSISDR GVNA2019F00211Thermocouple · failedIN CRUISE FLIGHT, THE ENG PA DIS LIGHTS ILLUMINATED IN BOTH LANES OF THE CAD. PERFORMED ENGRUN, TO REVEAL #2 ENG TEMP DIFFERENCE OF APPROX. 200DEG. REM'D ALL 3 THERMOCOUPLES. INSTALLED 3EA SERVICEABLE THERMOCOUPLES. PERFORMED GROUND RUN, FUNCTION CHK'D GOOD. PSDR 2019FA0000131Vent Line · looseFUEL SMELL NOTICEABLE IN CABIN, DURING FLIGHT. INSPECTED, FOUND EXPANSION TANK VENT LINE LEAKING AT FITTING. INSPECTED AND REPAIRED LINE, AS REQUIRED. NO OTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE.SDR QMLA20190419719Starter Gen · arcedDURING ATTEMPTED ENGINE START, PILOT OBSERVED THE NR 2 ENGINE N1 FAILURE TO INCREASE, AND SUBSEQUEENT FAILURE OF ENGINE TO START. AFTER ABORTING ENGINE START PILOT INSPECTED ENGINE AREA AND FOUND SEVERE ARCING ON POST 'C' OF STARTER GENERATOR. ARCING CAUSED TSDR GVNA201904230179Pressure Switch · failedNR 1 ENG FUEL PRESSURE LIGHT ILLUMINATED DURING FLIGHT/APPROACH. REPLACED LOW FUEL PRESSURE SWITCH WITH SERVICEABLE PART. PERFORMED GROUND RUN/LK CHK. CHK'D GOOD.SDR QMLA2019030519026Wire · burnedSUPPLEMENTAL INFORMATION: THE PILOT REPORTED THAT THE STANDBY ATTITUDE INDICATOR BACKLIGHTING AND THE SUPER NIGHT SCANNER SEARCHLIGHT REMAINED ILLUMINATED IN THE OFF POSITION. THE MECHANIC BEGAN TROUBLESHOOTING THIS PILOT REPORTED SQUAWK (FOUND ON THE GROUND).SDR QMLA2019030419024Magnetic Seal · leakingWHILE CONDUCTING A MAINTENANCE TEST FLIGHT, WITH TWO MECHANICS ABOARD, AIRCRAFT WAS RETURNING TO AIRPORT (KUKT) AFTER HAVING REFUELED AT AIRPORT (KLOM). AIRCRAFT WAS IN CRUISE FLIGHT WITH AUTOPILOT ENGAGED, 1500FT MSL AND 120KIAS. THREE MINUTES INTO THE FLIGHTSDR QMLA2019021299018Union · loosePILOT REPORTED SMOKE AND OIL SEEPING FROM # 1 ENGINE LUBRICATION PIPE OF THE REAR BEARING. INSPECTED LUBRICATION PIPE OF THE REAR BEARING IAW MM 70-40-02-801. FOUND UNION LOOSE AT LUBRICATION PIPE. TORQUED UNION IAW MM 79-29-00-900-802-A01. PERFORMED GROUND RUSDR HDNA2019013100002Wire Harness · intermittentDURING CRUISE FLIGHT NR 2 ENG FIRE WARNING LIGHT ILLUMINATED, APPROPRIATE EMERGENCY PROCEDURES WERE EXECUTED, LANDED SAFELY, AFTER LANDING ACFT INSPECTED, NO INDICATIONS OF A FIRE NOTED, THIS IS THE SECOND TIME IN 25 HRS OF FLIGHT TIME. FOUND ENG HARNESS TO BESDR GYNA20190410153Packing · failedON SCENE, ACFT RUNNING, AFTER PATIENT LOADING, MED CREW PERFORMING FINAL WALK AROUND, NOTICED FUEL LEAKING FROM #2 ENGINE COWLING. ACFT SHUTDOWN. MECHANIC PERFORMED FURTHER INSP, REVEALING FUEL FILTER BOWL SHUT OFF VALVE LEAKING. REM'D & REPLACED PACKING. FUNCSDR GVNA201904170170Packing · failedAFTER PATIENT LOADING, DURING FINAL WALK AROUND, MED CREW NOTICED FUEL LEAKING FROM #2 ENGINE. MECHANIC, UPON FURTHER INSPECTION, FOUND FUEL SHUTOFF VALVE LEAKING AT FILTER BOWL. REPLACED PACKING. LEAK CHK GOOD. NO OTHER DEFECTS NOTED.SDR HDNA2018082700072Seal · leakingFUEL LEAK FROM THE L/H ENGINE DECK OVERBOARD DRAIN BY PILOT DURING POST FLIGHT CHECK. TROUBLESHOOTING REVEALED AN OUT OF LIMITS FUEL LEAK OF THE F.C.U (FUEL CONTROL UNIT) NFT SEAL.SDR QMLA201808178096Engine · making metalENGINE CHIP LIGHT ILLUMINATED DURING AIRCRAFT STARTING. NO METAL FOUND ON CHIP PLUG. ENGINE OIL FILTER WAS REMOVED AND FLUSHED. NUMEROUS SHINNY METAL PARTICLES FOUND IN OIL ALONG WITH CARBON PARTICLES. OIL SAMPLE AND FILTER WERE SENT FOR ANAYSIS.SDR XU5A2018052400001Engine · making metalTHE AIRCRAFT EXPERIENCED AN ENGINE CHIP INDICATION ON THE NR 2 ENGINE. THE FUZZ BURNER SYSTEM WAS UNSUCCESSFUL IN EXTINGUISHING THE INDICATION. AFTER AN UNEVENTFUL LANDING AT THE AIRPORT, THE CHIP INDICATORS WERE INSPECTED AND SUBSEQUENTLY A SMALL MACHINE CURLSDR QMLA2017092417097Engine · making metalDURING ROC FLIGHT FOR MAX N1 (TOPPOING CHECK), AT 13,000 FEET, NR 1 ENGINE WAS IN THE IDLE POSITION, WHEN THE NR 2 ENGINE CHIP LIGHT ILLUMINATED CONSTANTLY. THREE ATTEMPTS WERE MADE TO "BURN" THE CHIPS WITH NO SUCCESS. NR 1 ENGINE WAS MOVED TO THE FLIGHT POSSDR QMLA2017092117098Drain · cloggedDURING ZONE INSPECTIONS, PULLED OFF THE VENT LINE GOING FROM RIGHT SIDE OF THE NR 1 ENGINE TO THE ENGINE DECK. FOUND THAT THE DRAIN COLLECTOR WAS CLOGGED WITH DEBRIS ON THE RIGHT SIDE OF THE Y-FITTING.SDR QMLA2017071017065Switch · failedWHILE ENROUTE, AIRCRAFT HAD A VARNR LIGHT ILLUMINATE AND EXPERIENCED AN APPROXIMATE 30% ENGINE SPLIT WITH NR 2 ENGINE GOING LOW. AIRCRAFT VARTOM’S SYSTEM WENT INTO MANUAL MODE. PILOT ATTEMPTED TO BEEP UP THE NR 2 ENGINE WITH COLLECTIVE TRIM SWITCH WITH NEGATIVSDR QMLA2017070317063Warning Light · false activationUPON ARRIVING AT A SCENE JUST AS WE BEGAN THE OVERHEAD RECON THE TAIL ROTOR CHIP LIGHT ILLUMINATED. EXECUTED THE EP IAW THE AIRCRAFT EMERGENCY PROCEDURE, THE LIGHT CAME ON AGAIN AFTER THE SECOND ATTEMPT TO BURN OFF. THE FLIGHT WAS ABORTED, AIRCOM AND GROUND SDR QMLA2017041617034Unknown · odorPILOT REPORTED, CREW MEMBER SMELLED A FUEL ODOR IN THE CABIN AREA. FLIGHT WAS ABORTED. AIRCRAFT RETURNED TO BASE. MAINTENANCE NOTIFIED. AIRCRAFT AND ENGINES INSPECTED FOR FUEL LEAKS. NONE FOUND. A 22 MINUTE OPS CHECK FLIGHT WAS CONDUCTED WITH NO FUEL ODOSDR 2M7A201702020001Oil System · pluggedTHE PROBLEM APPEARS TO BE A PLUGGED SCAVENGE LINE DUE TO INTERNAL ENGINE COKING. THE RESULT COULD BE EXCESSIVE INTERNAL OIL PRESSURES CAUSING EXTERNAL DISCHARGE OF THE OIL,
IN THIS CASE OUT THROUGH A VENT LINE. ALONG WITH THAT THERE WOULD BE A BYPASS OF OIL ISDR HDNA2016F00191Gearbox · brokenDURING REMOVAL OF THE TAIL ROTOR GEARBOX FOR TBO CHANGE, WE FOUND THAT THE ATTACHING STUD WAS SHEARED OFF AT THE TAIL BOOM ATTACHMENT POINT.SDR HDNA0917201600001Warning Unit · faultyON APPROACH, FUEL VALVE CLOSED CAUTION NOTED ON NR 1 CAD SIDE FOLLOWED SHORTLY BY NR 1 ENGINE FAILURE. ACFT LANDED WITHOUT INCIDENT. THE EMERGENCY OFF SWITCH 1 WAS NOTED WITH ACTIVE ILLUMINATED. EMERGENCY OFF SWITCH 1 ENGAGED AGAIN, ACTIVE ANNUNCIATOR EXTINSDR 2016F00179Ovrspeed Limiter · activatedNR 2 ENGINE SHUTDOWN IN FLIGHT DURING TRAINING DUE TO A TRIPPING OF THE NR 2 OVER SPEED PROTECTION BOX. PILOTS VERIFIED VISUALLY THAT THERE WAS NO OVERSPEED THAT OCCURRED AND PROCEEDED WITH A RUN ON LANDING. AFTER TROUBLESHOOTING WE FOUND THE OVERSPEED PROTESDR QMLA2016082316096Gearbox · making metalTAIL ROTOR CHIP INSPECTION REQUIRED AFTER 10HR SHOWED FUZZ PRESENT. AMM REQUIRES GEARBOX TO BE CHANGED IF ANY IS PRESENT DURING INSPECTION. THIS ACFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION WHILE THE TAIL ROTOR GEAR IS REPLACED.SDR E3MA20160506001Engine · making metalDURING FLIGHT THE OVER SPEED CAUTION ILLUMINATED FOLLOWED BY CHIP A CHIP CAUTION FOR THE NR 2 ENG. THE PILOT TRIED TO BURN THE CHIP & WAS UNSUCCESSFUL. THE PILOT LANDED SAFELY AT THE NEAREST AIRPORT & DURING SHUTDOWN OF THE ENG THERE WAS A LOUD BANG. DISCOVSDR HDNA2016031100002Abrasion Strip · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LE ABRASION STRIP, 132 INCHES FROM THE CTR OF THE PRIMARY BOLT HOLE.SDR QMLA2015101515098Drain Line · cloggedDURING TAKEOFF, THE CREW NOTICED A STRONG FUEL SMELL IN CABIN. FOUND THE COMMON DRAIN LINE ON THE NR 2 ENG DECK TO BE CLOGGED. THIS ALLOWED AN ACCUMULATION OF FUEL AFTER MULTIPLE STARTS, WHICH RESULTED IN THE FUEL SMELL IN THE CABIN. CLEANED DRAIN WITH AIR SDR GVN2015F00000Fcu · leakingWITH PRIME PUMP ON, FUEL WAS LEAKING FROM THE OVERBOARD DRAIN IN A STEADY STREAM. WITH ENGINE RUNNING, FUEL WAS LEAKING FROM THE OVERBOARD DRAIN AT A RATE OF 1 DROP EVERY 2 TO 4 SECONDS.SDR QMLA2015053001504Blade · crackedCRACK FOUND IN MAIN ROTOR BLADE BY PILOT DURING PRE-FLIGHT. CRACK IS ON THE RED MAIN ROTOR BLADE, APPROX 3/4 INCHES LONG, CHORDWISE. BEGINNING APPROX 4 INCHES OTBD OF THE ROOT END OF THE BLADE. ACFT PLACED IN AOG STATUS IMMEDIATELY. CONTACTED SUPPORT FOR GSDR O84A2015F00029Wire · brokenON FINAL APPROACH, NR 1 GEN DISCONNECT APPEARED ON CAD. AFTER SEVERAL ATTEMPTS TO RESET GENERATOR, IT REMAINED OFFLINE. THE ACFT LANDED AND MAINTENACE WAS CONTACTED. A MECHANIC WENT TO ACFT AND DEFERRED THE DISCREPANCY AND THE ACFT WAS FLOWN TO THE MAIN MAISDR E3MA20150204001Clamp · missingDURING A PREFLIGHT INSPECTION, DAMAGE WAS DISCOVERED ON THE MAIN ROTOR DRIVE LINK. IT WAS DETERMINED THAT THE DAMAGE WAS MOST LIKELY CAUSED BY THE LOWER SWASH PLATE HOSE CLAMP, DUE TO THE FACT THAT THE CLAMP WAS MISSING.SDR HDNA201501230002Torque Sensor · unknownUPON APPROACH TO DESTINATION HELIPAD & AS POWER REDUCED BELOW 80% N1, NR 2 ENG WAS NOTED TO DROP TO 0% TORQUE WITH ASSOCIATED, ENG SPLIT, CAUTION. ATTEMPTS TO REJOIN FLI NEEDLES WITH COLLECTIVE N2 TRIM SWITCH MET WITH NEGATIVE RESULTS. OEI FLIGHT CONDITIONS SDR QMLA2015010515002Blade · crackedPERFORMING PREFLIGHT INSPECTION & SAW A TRANSVERSE CRACK AT THE MAIN ROTOR BLADE FITTING ZONE NR 1 AREA. THIS IS ACCEPTABLE IN ZONE NR 1. AT APPROX THE CTR OF THE BLADE, THERE IS ANOTHER CRACK THAT GOES OUT FROM THIS TRANSVERSE CRACK, TOWARD THE END OF THE BSDR QMLA2014121314141Warning System · activatedEVENT OCCURRED WHILE INFLIGHT AT 8000'. ON BOARD THE ACFT WERE 3 MX PERSONNEL. THE NR 2 ENG CHIP ANNUNCIATOR LIGHT ILLUMINATED. ACTIVATED THE CHIP PULSE SYS ONCE & THE WARNING LIGHT DID NOT EXTINGUISH. SHUTDOWN NR 2 ENG & DIVERTED. DECLARED AN EMER & PROCSDR QMLA2014120914138Trim Tab · crackedPILOT PERFORMING AIRWORTHINESS INSPECTION FOUND A CRACK AT THE UPPER INBD TAB ATTACHMENT OF THE TRIM TAB ON THE YELLOW MAIN ROTOR BLADE. INSPECTED THE TRIM TAP & FOUND 10 MM CRACK AT TRIM TAB RIVET ATTACHMENT, 7 MM WAS ALLOWABLE & THE ACFT WAS TAKEN OUT OF SE
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