Turbomeca ARRIEL-1S1
Service difficulty reports · 78
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 = 'ARRIEL1S1' 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 = 'ARRIEL1S1' 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 CA141121006Blade · cracked(CAN) SEVERAL CRACKS FOUND AFTER LAST FLIGHT OF THE DAY ON TAIL ROTOR BLADE BOND ASSY 76101-05020-045, PART OF TAIL ROTOR BLADE ASSY 76101-05101-041.SDR CA130322001Fire Detector · failed(CAN) WHILE ENROUTE, WE HEARD NR 2 ENGINE FIRE TONE. THE FIRE CAUTION LIGHT INDICATOR WAS LIT AS WELL. WE THEN PROCEEDED WITH THE IMMEDIATE ACTION PRESCRIBED IN THE EMERGENCY PROCEDURE. THE FIRE INDICATOR C/L WAS STILL ON AFTER MAIN BOTTLE WAS DISCHARGED. SDR CA120822005Linkage · failed(CAN) PILOT REPORTED A SLIGHT JERK 10 MIN BEFORE LANDING ON DECK. AN INSPECTION WAS DONE ON DECK AND REPORTED THE DOOR FITTING BROKEN. ACFT WAS SHUTDOWN, DOOR TIED DOWN AND ACFT FLEW BACK TO BASE WITH LANDING GEAR EXTENDED AND WITHOUT ANY PASSENGERS ONBOARD.SDR CA120312021Exciter · failed(CAN) NR 1 ENGINE START CONTROL CIRCUIT BREAKER POPPED ON START. MAINTENANCE REPLACED THE IGNITION EXCITER BOX.SDR CA100413011Landing Gear · misrigged(CAN) DURING THE 12 MONTH TEST OF THE EMERGENCY LANDING GEAR BLOWDOWN SYSTEM, THE LANDING GEAR FAILED TO OPERATE DUE TO THE CABLE NOT BEING RIGGED CORRECTLY. CABLE RE-RIGGED, TESTED AND FOUND TO OPERATE CORRECTLY.SDR CA110105010Spar · cracked(CAN) DURING A SCHEDULED 500 HR TAIL ROTOR BOROSCOPE, MRS 35974, FOUND FWD AND AFT L/E OF SPAR CRACKED FROM BS 9.6 TO 13.25. TAIL ROTOR PADDLE ASSY REPLACED. CONTINUE 500 HR INSPECTIONS.SDR HEEA116943Control Switch · malfunctionedDURING TAKEOFF, AFTER RELEASING THE FORCE TRIM BUTTON AT (4), CYCLIC WOULD COME AFT. MAINTENANCE INSPECTED THE AIRCRAFT, CONNECTED A HYDRAULIC MULE AND WORKED ALL CONTROLS. THEY WERE UNABLE TO DUPLICATE THE DISCREPANCY.SDR HEEA116155Inverter · inoperativeAPPROX 7 MILES EAST, AIRCRAFT HAD A COLLECTIVE TRIM FAILURE, THE FUEL ON THE NR 1 SIDE WENT TO ZERO AND THE IDS DISPLAY ON THE NR 1 SIDE FAILED, ALONG WITH A YELLOW FUEL LIGHT INDICATING ONLY 210 POUNDS OF FUEL ON BOARD. THE OAT GAUGE ON THE NR 2 IIDS DISPLAYSDR HEEA115976Line · chafedDURING SHORT FINAL LANDING AT VK989, NR 1 HYDRAULIC LIGHT CAME ON. COMPLETED LANDING SAFELY ON DECK, SHUTDOWN. MAINTENANCE FOUND HYDRAULIC TUBE BELOW TAIL ROTOR GEARBOX TO HAVE A HOLE CHAFED IN IT. REPLACED TUBE ASSY.SDR HEEA109087Metering Valve · out of adjustIN FLIGHT FROM EI314 TO LAFAYETTE MINOR FCU RSOLV FAULT DISPLAYED. COMPLETED FLIGHT AND MAINTENANCE REPLACED THE NR 1 ENGINE ADJUSTED METERING VALVE - FUEL CONTROL UNIT.SDR U0GA108035Smoke Detector · illuminatedTHE BAGGAGE SMOKE DETECTOR LIGHT ILLUMINATED INTERMITTENTLY SHORTLY AFTER DEPARTURE. RETURNED AND FOUND PAX BAGGAGE DISCHARGED AN AEROSOL (DEODERANT) POSSIBLY CAUSING LIGHT TO ILLUMINATE.SDR HEEA107320Actuator · inoperativeDURING CRUISE FLIGHT, THE AIRCRAFT STARTED FISH TAILING. RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE NR 1 AFCS YAW ACTUATOR.SDR ALG2005F00038Chip Detector · inoperativePRIOR TO REACHING DESTINATION, NR 1 ENGINE CHIP LIGHT CAME ON. AC LANDED AND MAINTENANCE CHECKED NR 1 ENGINE CHIP PLUG AND NO DEFECTS WERE NOTED. THE AC WAS RETURNED TO SERVICE AFTER OPERATIONAL CHECKS WERE COMPLETED. (K)SDR HEEA107333Hmu · malfunctionedMASTER CAUTION 5-PACK ILLUMINATED. CHECKED CAUTION PANEL AND NR 2 LOW FUEL PRESSURE SEGMENT WAS DIMLY ILLUMINATED. MASTER CAUTION WOULD NOT RESET. SUSEQUENTLY NR 2 DECU DEGRADE LIGHT ILLUMINATED. CHECKED DDR FAULT. P3 DRIFT WAS THE DEGRADE. THEN FUEL PRSDR ALG2005F00034Amplifier · unserviceableBEFORE ENGINE START CHECK OF THE FIRE DETECTION SYSTEM, TEST HAD NO TONE. MAINTENANCE REMOVED FIRE CONTROL AMPLIFIER SN 11595 AND INSTALLED SERVICEABLE CONTROL AMPLIFIER 2329. ALL WORK WAS DONE IAW MM. OPS CHECK WAS GOOD. (K)SDR 2005FA0000636Wire · burnedENGINE ANTI-ICE SYSTEM, ENGINE HEATED INTAKE BELLMOUTH AND SNOW BLANKET. MAINT FOUND BURNED WIRE AT PLUG J701 AND P701 (PIN A) 16 GAGE WIRE. THEY ALSO FOUND THIS WIRE WAS FED BY A 35 AMP COCKPIT DC PRIMARY BUSS CIRCUIT BREAKER THROUGH A 10 GAGE WIRE TO PLUG SDR 2005FA0000637Wire · burnedENGINE ANTI-ICE SYSTEM, HEATED INTAKE BELLMOUTH, HEATED SNOW BLANKET. MAINT FOUND BURNED WIRE AT PLUG J701 AND P701 (PIN A) 16 GAGE WIRE. THEY ALSO FOUND THIS WIRE WAS FED BY A 35 AMP COCKPIT DC PRIMARY BUSS CIRCUIT BREAKER THROUGH A 10 GAGE WIRE TO PLUG J30SDR ALG2005F00021Chip Detector · contaminatedDURING FLIGHT THE NR 1 ENGINE ILLUMINATED TEN MINUTES AFTER DEPARTURE. THE NR 1 ENGINE WAS PLACED IN GROUND IDLE IAW EMERGENCY CHECK LIST AND THE FLIGHT CONTINUED. AT ARRIVAL, THE NR 1 ENGINE WAS PLACED IN FLY POSITION IAW CHECK LIST FOR NORMAL LANDING. THESDR RG82005F00000Fastener · looseAFTER LANDING, PILOT PERFORMING POST-FLIGHT CHECK NOTICED LARGE AMOUNT OF OIL ON GROUND. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT A FASTENER, PN 9550158060 ON LT SIDE OF OIL COOLER DUCTING PANEL PN 0401272790 HAD COME LOOSE AND WORN A HOLE ON THE IB SIDSDR ALG2004F00055Circuit Board · corrodedRECURRING INCIDENT, MORE THAN FOUR SEPARATE INCIDENTS SPANNING LESS THAN A FIVE MONTH PERIOD AND ON DIFFERENT AC. CIRCUIT BOARD CORROSION CAUSED DECU T4.5 TRIM FAULTS UPON SHUT DOWN, CONFORMATION BOX WIRES CORROSION RESULTED IN DECU T4.5 TRIM FAULT UPON SHUTDSDR ALG2004F00066Engine · malfunctionedON TAKEOFF, T-5 WAS IN THE YELLOW AND 51 DEGREES HOTTER THAN THE NR 2 ENGINE, RETURNED TO DEPARTURE AND DID POWER CHECK AND THE NR 1 ENGINE FAILED CHECK. MAINTENANCE REMOVED NR 1 ENGINE ASSY, SN 2055TEC, AND INSTALLED SERVICEABLE ENGINE ASSY SN 20537TEC. (SWSDR Z1RA096970Torque Box · intermittentREPLACED TORQUE TRIM CONFORMATION BOX. NO FURTHER DEFECTSSDR 2004F00380Bellows · contaminatedON TAKEOFF, THE NR 1 ENGINE STARTED TO SURGE. MAINTENANCE REMOVED FUEL CONTROL, FOUND WATER IN THE P1 BELLOWS REMOVED WATER AND REINSTALLED FUEL CONTROL, OPS CHECK WAS GOOD. (M)SDR ALG2004F00024Bracket · out of adjustWHEN RETRACTING LANDING GEAR AFTER TAKEOFF THE RED GEAR UNLOCKED LIGHT CAME ON. RECYCLED GEAR WITH SAME AFFECT. RETURNED TO GNO WITH GEAR LOCKED IN THE DOWN POSITION. MAINTENANCE INSPECTED LANDING GEAR FOUND WEIGHT ON WHEEL SWITCH BRACKET SLIGHTLY OUT OF AFSDR ALG2004F00030Bulkhead · crackedBULKHEAD CRACKED FROM RT HAND STIFFNER BL18 TO EDGE OF CUT OUT FOR BAGGAGE DOOR. CRACKS FORM RIVET HOLE TO EDGE. DOOR ASSEMBLY ALSO CRACKS AROUND UPPER ATTACHMENT RIVETS.SDR ALG2004F00005Switch · dirtyDURING APPROACH TO CM243, WHILE CHECKING DECU FAULTS PRIOR TO LANDING, NOTICED A NR 2 DECU (FLY GATE FAULT). PROCEED TO ICY AND SHUTDOWN NR 2 ENGINE IN MIXED MODE. MAINTENANCE CLEANED SWITCHES ON NR 2 THROTTLE IN QUADRANT AND CLEANED AND INSPECTED CONNECTORSSDR HEEA093480Fuel Control · failedNR 2 ENGINE HIGH SIDE FAILURE. MAINTENANCE REPLACED FUEL CONTROL.SDR CA031120008Duct · separated(CAN) DURING NORMAL DAILY TREND CHECK, PILOT NOTICED GRADUAL INCREASE IN ENG OIL TEMP ON NR 2 AND REPORTED TO THE ENGINEER. INSPECTION CARRIED OUT ON THE NR 2 OIL COOLER DUCT INSTALLATION IN WHICH THE FLEXIBLE DUCT LOCATED BELOW THE BLOWER ON THE INSIDE OF THSDR CA030918012Generator · out of adjust(CAN) DURING TRAINING, INFLIGHT ENGINE SHUTDOWN AND RESTART PROCEDURES WERE BEING DEMONSTRATED. WHEN START WAS ATTEMPTED THE THE OVERSPEED SYSTEM TRIPPED AND PREVENTED THE RESTART. TROUBLESHOOTING INDICATES THAT A OUTPUT VOLTAGE OF 28.55 VDC FROM THE OPERATINGSDR HEEA088386Fuel Control · malfunctionedFUEL CONTROL PRODUCING TORQUE SPLITS. TO BE SENT TO VENDOR.SDR HEEA087122Check Valve · leakingENGINE LEAKS OIL STATICLY FROM BURNER CAN.SDR HEEA086531Fuel Control · malfunctionedNR 2 ENGINE LIGHTS OFF BUT WILL NOT ACCELERATE PAST 30 PERCENT N1.SDR HEEA086532Fuel Control · failedENGINE WON'T START - TROUBLESHOOTING.SDR HEEA086533Valve · interferenceVALVE HAS INTERMITTENT OPERATION DURING ENGINE STARTS.SDR HEEA086546Connector · damagedENGINE VALVE CONNECTOR DAMAGED. REPLACED CONNECTOR V5032-135 DUE TO DAMAGED. REPAIRED.SDR ALG2003F00024Sensor · failedDURING GROUND RUN, WITH NR 1 ENGINE RUNNING AT GROUND IDLE (70 PERCENT NR1) AND ROTOR BRAKE ENGAGED, THE ENGINE SHUT ITSELF OFF AFTER RUNNING ABOUT 3-5 MINUTES. THE MECHANIC REMOVED AND REPLACED THE MAG OVERSPEED SENSOR AND THE AIRCRAFT RETURNED TO SERVICE.SDR HEEA082537Thermocouple · damagedTHERMOCOUPLE LEAD HAS OPEN IN THERMOCOUPLE END.SDR CA021218006Brake Disc · cracked(CAN) DURING PREFLIGHT INSPECTION AND TO COMPLY WITH ASB76-66-36 THE ROTOR BRAKE DISC WAS FOUND TO BE CRACKED. NO OTHER DEFECTS FOUND. PART REPLACED. REPORTED FINDING TO SIKORSKY.SDR ALG2003F00036Sensor · inoperativeON TAKEOFF, NR 2 ENGINE DROPPED OFF LINE AND WOULD NOT RESTART. THE MECHANIC TROUBLESHOT AND FOUND NR 2 OVERSPEED SENSOR NOT OPERATIONAL.SDR HEEA078715Ecu · faultyECU FAULT. TO BE SENT TO VENDOR FOR REPAIR.SDR HEEA078701Ecu · failedRECEIVED MAJOR FAULT ON NR 2 ENGINE. FOUND NR 2 ENGINE ECU FAILED.SDR CA011219009Line · chafed(CAN) DURING POST FLIGHT WALK AROUND FLIGHT CREW NOTICED HYD FLUID LEAKING OUT OF COWLING. COWL WAS REMOVED. HYD RESEVOIR WAS 1/2 FULL AND A/C GROUND RUN A LEAK WAS DETECTED UNDER A CLAMP OF NR 2 SYSTEM PRESSURE LINE. THE LINE WAS REPLACED WITH A NEW PART, NR SDR CA011114018Bearing · failed(CAN) SUBJECT: ESN 15051- PARTICLES ANALYSIS. WE HAVE RECEIVED THE ANALYSIS RESULTS OF THE PARTICLES FOUND ON THE MODULE 05 S/N¦ 03199¦ MAGNETIC PLUG . THE PARTICLES¦ ARE 100 C6 MATERIAL AND HAVE AS THE ORIGIN ONE OF THE HYDRAULIC TORQUEMETER BEARINGS ("TRIPSDR HEEA073538Engine · making metalFOUND OIL SAMPLE HAS HIGH IRON.SDR HEEA073539Ecu · malfunctionedREVERSION LIGHT ON NR 1 THROTTLE STAYS ON.SDR HEEA073517Valve · leakingFUEL SMELL IN COCKPIT DURING START.SDR HEED073506Control Unit · failedNR 1 ENGINE RUN UP FAULT. REPLACED UNIT.SDR CA010810001Bulkhead · cracked(CAN) CRACKED FOUND AT ST.215 L/H SIDE BULKHEAD 7.5 INCHES BELOW WATERLINE 121. EXTENDING FROM M6B SUPPORT TO MAIN BULKHEAD ELECTRICAL PLUG.SDR HEED072213Pump · fluctuatesFLUCTUATING OIL PRESSURE . REPLACED UNIT.SDR HEED072216Engine · making metalGENERATING METAL AT THE ACCESSORY MAG PLUG. REPLACED UNIT.
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