Turbomeca ARRIEL-2S1
Service difficulty reports · 45
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 = 'ARRIEL2S1' 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 = 'ARRIEL2S1' 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 HC7A201801230001Resistor · inoperativeAIRCRAFT WAS IN CRUISE FLIGHT, THE AIR CONDITIONING WAS TURNED ON, A BURNING SMELL WAS SOON NOTICED, THE A/C WAS THEN TURNED OFF, THE SMELL IMMEDIATELY DISSIPATED. THE AIRCRAFT RETURNED TO BASE. TECHNICIAN INSPECTED THE A/C SYSTEM TO INCLUDE THE EVAP BLOWER, ISDR Z1RA030062017001Relay · inoperativeDURING CRUISE FLIGHT, THE NR 2 HYDRAULIC SERVO SYSTEM WARNING CAUTION LIGHT ILLUMINATED. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. REPLACED THE NR 2 SERVO RELAY AND AS A PRECAUTION, REPLACED THE NR 2 HYDRAULIC MODULE PRESSURE SWITCH.SDR HC7A201606120001Fire Detector · intermittentAFTER AIRCRAFT LANDED AND DURING THROTTLE REDUCTION TO IDLE, THE NR 1 ENGINE FLAME DETECTOR FLICKERED ON AND OFF TWICE, APPROXIMATELY 1 SECOND EACH TIME. ACFT WAS SHUTDOWN, AND MAINTENANCE VISUALLY INSPECTED THE ENGINE AREA, NO EVIDENCE OF A FIRE WAS NOTED. SDR ALGA2015122137489Duct · disconnectedAT CRUISE CHECK PILOT NOTICED NR 2 ENG TEMP AT 92 DEG, OIL PRESS 52 PSI. DURING DESCENT TEMP ROSE TO 100 DEG & PRESS DROPPED TO 42 PSI. FLIGHT DIVERTED, RECONNECTED NR 2 ENG OIL COOLER DUCT.SDR CA150921012Drive Shaft · broken(CAN) WHILE 4 MILES FINAL FOR AIRPORT THE OIL PRESSURE LIGHT ILLUMINATED FOLLOWED A LOW PRESSURE INDICATION ON THE PRESSURE GAUGE, 4 PSI AND DECREASING RAPIDLY. POWER REDUCED, ENGINE SHUTDOWN, PAN DECLARED WITH THE TOWER. PRIORITY CLEARANCE WAS GIVEN TO LANDSDR CA141124001Pushrod · chafed(CAN) DURING 36 MONTH INSPECTION, COLLECTIVE PUSH ROD FOUND CHAFED. CHAFING WAS CAUSED BY BLIND RIVETS INSTALLED DURING POST MFG OF ACFT. PUSH ROD REMOVED, AND RIVETS ARE TO BE REPLACED WITH SOLID RIVETS TO ALLOW FOR ADDITIONAL CLEARANCE.SDR Z1RA2014081900145Warning Light · illuminatedMAIN GEAR BOX CHIP LIGHT ILLUMINATED ON RUNUP.SDR ALGA0820201433330Line · misinstalledAIRCRAFT SHUTDOWN AFTER OIL COOLER RUPTURED DUE TO INCORRECT INSTALLATION OF OIL LINES. NR 1 ENG COMPRESSOR WAS FOUND TO BE DAMAGED, DAMAGE WAS DETERMINED TO BE OUT OF LIMITS & REQUIRED ENG TO BE CHANGED.SDR ZR1A2014081200144Igniter Box · weakENGINE FAILED TO START. IGNITER BOX REPLACED.SDR ALGA2014051232593Firewall · damagedON DESCENT, CRUISE REPO FLIGHT FROM HUM TO GNO WITH NO PAX, MANEUVERED TO AVOID SEAGULL, WHICH IMPACTED ABOVE LT WINDSHIELD WITH AUDIBLE THUMP. ENG OUT AUDIO & LIGHT ACTIVATED MOMENTARILY BUT NO UNUSUAL NOISE OR VIBRATIONS OCCURRED. INSTRUMENTS DISPLAYED 10%SDR CA140422002Line · ruptured(CAN) HYDRAULIC "UP" HOSE RUPTURED. FLUID LOSS. NR 2 SERVO LIGHT AND ZERO PRESSURE WITH RED UNLOCKED LIGHT. EMERGENCY GEAR EXTENSION SYS ACTUATED WITH NO EFFECT. PILOT REPORTED THAT WHEN MAINS TOUCHED DOWN NOSE GEAR THEN LOCKED INTO PLACE. LANDING COMPLETED.SDR Z1RA2014F00052Transducer · intermittentMINOR DECU FAULT, COLLECTIVE POSITION FAULT.SDR 2013FA0000288Starter Gen · malfunctionedDURING CRUISE FLIGHT CENTER IIDS DISPLAY BEGAN FLASHING. DC ELECTRICAL POWER PULSING ON NR 2 SYSTEM FROM 0 TO 11 AMPS OUTPUT ONLY (NORMALLY 140AMPS). ESS VOLTS LOW LIGHT ILLUMINATED ON SHORT FINAL. RADIOS WERE SWITCHED TO EMERGENCY SETTING SO COMMUNICATION WSDR CA130503003Rod End · sheared(CAN) UPON TAXIING OUT FOR OFFSHORE FLIGHT, PILOTS NOTICED A `THUMP` COMING FROM REAR OF ACFT. PILOTS ELECTED TO TAXI BACK TO THE STAND TO ALLOW ENGINEERS TO INSPECT LANDING GEAR. CROSS TUBE BRACE ROD END ON RT SIDE MAIN GEAR WAS FOUND SHEARED. GROUND OCCURSDR CA130321011Cover · missing(CAN) ENGINE OIL COVER FOUND MISSING DURING POST FLIGHT INSPECTION ON COMPLETION OF FLIGHT. ACFT WAS INSPECTED AND NO OTHER DAMAGE WAS FOUND. INVESTIGATION STARTED TO DETERMINE ROOT CAUSE.SDR CA130312001Blade · delaminated(CAN) DURING 300 HR MAIN ROTOR BLADE INSPECTION 3 OF 4 BLADES WERE FOUND DELAMINATED BEYOND LIMIT, ALL IN THE SAME AREA OF THE BLADE.SDR ALGA201210116700Housing · corrodedMAIN GEARBOX HOUSING HAS CORROSION.SDR ALGA201210116704Landing Gear · corrodedFOUND AXLE FITTING, AXLE FITTING STUD, LOWER BEARING, AND TORQUE ARM PIN WITH CORROSION PITTING.SDR CA120418006Hub · cracked(CAN) DURING THE 3 YR HUB VISUAL INSPECTION, A CRACK WAS NOTICED ON DAMPER LUG. EDDY CURRENT INSPECTION WAS USED TO CONFIRM THE CRACK. MAIN ROTOR HUB REPLACED.SDR CA121102005Line · chafed(CAN) APPROXIMATELY 10 NM S/E OF THE FINAL DISTINATION THE CREW REALIZED A PRESSURE DROP IN NR 2 HYDR SYSTEM. FOLLOWING THE EMERGENCY CHECKLIST WE SECURED THE NR 2 SYSTEM, PRESSURE WAS ALREADY "0", INFORMED ATC ABOUT OUR SITUATION AND REQUESTED PRIORITY FOR LSDR ALGAR91311A245005Blade · crackedTAIL ROTOR BLADE FOUND TO BE SPLINTERED AND CRACKED AT INBD EDGE RT STA 11.00SDR CA110830019Pump · failed(CAN) OIL PRESSURE LIGHT ILLUMINATED FOLLOWED A LOW PRSSURE INDICATION ON THE PRESSURE GUAGE (4 PSI AND DECREASING RAPIDLY). POWER REDUCED, ENGINE SHUTDOWN. PRIORITY CLEARANCE WAS GIVEN TO LAND. A RUN ON LANDING WAS MADE AT A LOW POWER SETTING. ACFT TAXIEDSDR ALGA07302011Transducer · failedDURING DESCENT, ACFT YAWED LT, NR 2 ENGINE OUT LIGHTS AND AUDIO CAME ON AND THEN EXTINGUISHED. ALL INDICATIONS RETURNED TO NORMAL. THIS WAS A QUICK FLAMEOUT AND THEN RELIT.SDR ALGA062211864ALOil System · overheatedSHORTLY AFTER TAKEOFF, NOTICED THE NR 2 ENGINE OIL TEMP HAD CLIMBED ABOVE THE RED LINE ALL THE WAY TO 118 C. IMMEDIATELY REDUCED THE ENGINE TO IDLE, AS IT APPROACHED IDLE THE ENGINE OIL PRESSURE WENT TO 0. SECURED THE ENGINE AND RETURNED TO DEPARTURE.SDR ALGA1101103333Skin · debondedLOWER SURFACE SKIN/CORE HAS A 5" LONG DEBOND AT STA 80.00 TO STA 85.00, 3" X .75" DEBOND AT STA 70.5 TO 73.5 AND 1.5" DIA DEBOND AT STA 69.00SDR HEEA129840Pitch Horn · crackedON DAILY INSPECTION FOUND TAIL ROTOR PITCH HORN CRACKED. REPLACED T/R ASSEMBLY.SDR ALGA072710A117306Bearing · frozenUPON INSP OF BELLCRANK ASSY, FOUND BEARING FROZEN AND UNABLE TO MOVE.SDR CA100526008Fire Detector · failed(CAN) DURING THE BEFORE TAKEOFF CHECKS PILOTS NOTICED THAT NR 2 ENGINE FIRE WARNING LIGHT CAME ON INTERMITTENTLY. PILOTS DID NOT NOTICED ANY SECONDARY INDICATIONS FOR ENGINE FIRE. THEY IMMEDIATELY SHUT DOWN BOTH ENGINES AND CHECKED THE ENGINES FOR SIGNS OF FSDR ALGA1351021200986Engine · flamed outNR 2 FUEL LEVER MOVED TO CROSSFEED POSITION, LOW PRESSURE LIGHT CAME-ON AND NR 2 ENG FLAMED OUT. PILOT TOOK C/A, LOWERED COLLECTIVE, BACK ON AIR SPEED, STABILIZED. CONCLUDED A PROBLEM IN CROSSFEED SYS. CONDUCTED ENG RESTART. NO INCURSIONS OR ACCIDENCES. UPOSDR ALGA081709863ALO-Ring · cutIN CRUISE FLIGHT,NR 2 ENG OIL PRESSURE LIGHT ILLUMINATED. CREW SHUTDOWN ENG AND PERFORMED SINGLE ENG LANDING. INSP BY MX REVEALED LEAKING OIL COOLER BLOWER TO GEARBOX ADAPTER O-RING.SDR CA090529006Housing · damaged(CAN) MGB UPPER HOUSING BEARING SUPPORT STUDS MISSING LOCK RINGS. MAIN GEAR BOX PN 76351-09600-044, SN A231-00295 DISASSEMBLED FOR OVERHAUL AT 3226:35 TSN. UPPER HSG (PN 76351-09002-053, SN A001-00566) DISSASEMBLED AND FOUND BEARING SUPPORT ATTACHMENT STUDS (SDR ALGR050609865ALConnector · contaminatedNR 2 ENGINE FIRE T-HANDLE ILLUMINATED WITH AUDIBLE TONE. RESET CIRCUIT BREAKER. INDICATIONS REAPPEARED WITHIN 5 MINUTES. NO OTHER INDICATIONS OF FIRE. CREW DIVERTED TO OPERATING BASE. MX INSPECTED NR 2 ENGINE AND FOUND NO EVIDENCE OF FIRE. MX CLEANED OIL FROM SDR HEEA123694Engine · warning lightCRUISING AT 2500 FEET THE NR 1 ENGINE CHIP LIGHT ILLUMINATED AND APPROX 5 SECONDS THEREAFTER THE ENGINE SHUTDOWN.SDR EGRR119591Motor · failedSTEP MOTOR FAILED, REPLACED STEP MOTOR P/N M102M660.SDR HEEA118383Pump · failedENROUTE , TLP NR 1 HYD PRESS WENT TO ZERO AND NR 1 SERVO LIGHT ILLUMINATED. FOLLOWED RFM PROCEDURE AND LANDED ON THE BEACH. MAINTENANCE REPLACED NR 1 HYD PUMP.SDR 2007F00055Engine · power lossDURING CLIMB OUT FROM CONFINED AREA, ENGINE AND ROTOR RPM FLUCTUATED. ROTOR RPM DROOPED, COLLECTIVE APPLIED, ACTIVATED NR 2 ENGINE OEI LIGHT.SDR HEEA116985Ecu · inoperativeON LANDING, NR 1 DECU CIRCUIT BREAKER POPPED. ON TURNING ON THE BATTERY, CIRCUIT BREAKER POPPED AGAIN. MAINTENANCE REPLACED THE ELECTRONIC CONTROL UNIT.SDR HEEA116983Autopilot Sys · unknownDURING HOVER FOR TAKEOFF, AFCS KICKED HARD. LANDED AIRCRAFT GROUND TAXIED TO PARKING. MAINTENANCE INSPECTED THE AIRCRAFT, CONNECTED A HYDRAULIC MULE AND WORKED ALL CONTROLS. THEY WERE UNABLE TO DUPLICATE THE DISCREPANCY.SDR HEEA116744Wire Harness · damagedON CRUISE CHECK, NOTED RT MAIN GEAR GREEN LIGHT ILLUMINATED. LOWERED GEAR TO 3 GREEN INDICATION. RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE RT LANDING GEAR SENSOR HARNESS.SDR 2007FA0000716Lamp · burned outPOSSIBLE MFG PARTS NOT TO SPECIFICATIONS. MFG OF ORIG UNKNOWN. (GENERIC) LESS THAN 7 FLT HOURS IAW LAMP (AVERAGE) FROM INSTALLATION TO REPLACEMENT. HAVE REPLACED AT LEAST 5 LAMPS IAW AIRCRAFT IN LESS THAN 30 FLIGHT HOURS EACH. NO CIRCUIT BREAKERS POPPING. SDR 2007FA0000717Lamp · burned outPOSSIBLE MFG PARTS NOT TO SPECIFICATIONS. MFG OF ORIGIN UNKNOWN. (GENERIC) LESS THAN 7 FLT HOURS PER LAMP (AVERAGE) FROM INSTALLATION TO REPLACEMENT. HAVE REPLACED AT LEAST 5 LAMPS PER AC IN LESS THAN 30 FLIGHT HOURS EACH. NO CIRCUIT BREAKERS POPPING. TROUSDR HEEA116823Transducer · fluctuatesIN CRUISE FLIGHT AT 5000 FT IFR NR 2 ENGINE DECELLED THEN CAME BACK TO NORMAL. ENGINE OUT LIGHT, AUDIO BOTH CAME ON FOR ABOUT 1 SECOND DURATION. ENGINE RECOVERED. AFTER DESCENDING TO 2000 FT TO START APPROACH, AFTER ABOUT 20 SEC LEVEL AT 2000 FT. N1 ON NRSDR HEEA116160Wire · chafedTRIM FAIL AND MASTER CAUTION LIGHT BLINK IN HOVER. SYSTEM OPERATES NORMALLY. MAINTENANCE REPAIRED CHAFED WIRING IN CENTER CONSOLE TO CONTROL PANEL.SDR HEEA116157Wire Harness · damagedRAISED GEAR. ALL (3) GREEN LIGHTS AND RED LIGHTS WENT OUT. RT MAIN GREEN LIGHT THEN CAME ON. LOWERED GEAR. RETURNED TO BASE. MAINTENANCE REPLACED RT MAIN PROXIMITY SWITCH HARNESS.SDR HEEA114545Hmu · inoperativeDURING ENROUTE DESCENT NR 2 FUEL PRESSURE LIGHT ILLUMINATED. NO SECONDARY NOTED. DIVERTED AND LANDED WITHOUT INCIDENT. DURING SUBSEQUENT START ATTEMPT FOR TROUBLESHOOTING, ENGINE WOULD NOT START. MAINTENANCE FOUND THE HMU TO BE AT FAULT. REPLACED HMU.
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