Safran ARRIEL-2D
Service difficulty reports · 138
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 = 'ARRIEL2D' 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 = 'ARRIEL2D' 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 7AJA20220329004None · noneDURING THE RETURN FLIGHT AFTER THE PATIENT HAD BEEN DROPPED OFF, THE MGB CHIP LIGHT ILLUMINATED IN FLIGHT.
I IMMEDIATELY REDUCED POWER AND LOOKED FOR A SUITABLE LANDING SPOTSDR QMLA2022032920021Skin · unserviceableHORZ. STAB IS UNSERVICABLE UPPER SKIN RH SIDE HAS 24 WORKING RIVITS WITH SKIN MOVEMENT (WARRANTY ISSUE)SDR 2A6D20220208001Skin Panel · chafedCHAFING WAS DISCOVERED ON THE ENGINE DECK (AIRBUS PN 350A21-1239.21) JUST NEAR LH PASS THROUGH. THERE ARE SEVERAL CHAFE DAMAGES AT THE PASS-THROUGH, WITH THE LARGEST CHAFE MEASURED TO BE APPROXIMATELY 0.229” AND 0.007” DEEP. THERE IS ALSO AN ENLARGED ANCHOR NSDR 2A6D20220208002Skin Panel · dentedDENT DAMAGE TO ENGINE DECK. THE DAMAGE IS LOCATED AT STA 4387 WL 1780 RBL 254. AND MEASURES APPROXIMATELY 0.048” IN DEPTH AND 1.4” IN DIAMETER.SDR QMLA2021102220053Handle · noneCREW HEARD A SINGLE BANG NOISE. DECIDED TO CONDUCT PRECAUTIONARY LANDING. WAS LATER FOUND BY MECHANICS TO BE A LATCH FOR THE SLIDING DOOR THAT WAS NOT SEATED PROPERLY, THAT DUE TO AIRCRAFT VIBRATION RETURNED ITSELF TO IT'S SPRING-LOADED REST POSITION, CAUSINSDR 2021FA0000291Sleeve · crackedDURING ROTINE M/R BLADE INSTALLION, TECNICIAN FOUND LOWER SLEEVE BLADE PIN BUSH CRACKED.SDR QMLA2021855320041Elastomer · crackedTAIL ROTOR PITCH CONTROL LINKS (P/N LB6-1231-3-2) ARE IN HIGH DEMAND DUE TO A VERY SHORT LIFE SPAN BEFORE THE LAMINATED BEARINGS SHOW CRACKS BEYOND LIMITS OUTLINED IN AMC EO 33-6520-EO-2481P2 AND AD 2021-05-09. THE LIFE SPAN RANGES GREATLY BETWEEN DIFFERENT LSDR 2A6D20210413001Floor Support · corrodedCORROSION WAS NOTED ON THE RH SIDE OF THE CABIN FLOOR EDGE.SDR QMLA2021020820004Unknown · odorBURNING SMELL NOTICED IN CABIN UPON TAKEOFF BY PILOT AND MED CREW. PILOT RETURN TO AIRPORT WHERE HE HAD JUST TAKEN OFF FROM. MAINTENANCE: PERFORMED GROUND RUN AND 20 MINUTE MAINTENANCE FLIGHT. NO CAUTION OR WARNING LIGHTS NOTED. OPERATED HEATER WITH NO ISSUESSDR 7AJA20200115Thermoswitch · failedAIRCRAFT CABIN HEAT P2 OVHT LIGHT IN FLIGHT. PILOT DEACTIVEATED SYSTEM AND CONTINUED FLIGHT, PER RFM. REPLACE DEFECTIVE THERMAL SWITCH P/N 704A32135018 AND RETURNED AIRCRAFT TO SERVICE.SDR 7AJA20201106Warning Light · false activation"ENGINE CHIP" ILLUMINATION DURING FLIGHT. LIGHT FLICKERED ABOUT 5-8 SECONDS THEN WENT SOLID. ENGINE CHIP PROCEDURE INITIATED. MADE PRECAUTIONARY LANDING AND CONTACTED MAINTENANCE. TECHNICIAN COMPLIED WITH ENGINE CHIP LIGHT PROCEDURES, IAW SAFRAN EMM 71-00-SDR 7AJA20201006Chip Detector · activatedENGINE CHIP WARNING LIGHT ILLUMINATED DURING FLIGHT. PILOT MADE A PRECAUTIONARY LANDING. MAINTENANCE COMPLETED LEVEL A PROCEDURE, IAW THE ENGINE MM. CHANGED OIL AND FILTERS, AIRCRAFT RETURNED TO SERVICE.SDR 2A6D20200430001Deck Plate · chafedR/H SIDE TRANSMISSION DECK INBOARD OF ENGINE OIL TANK AT THE EDGE OF TRANSMISSION DOUBLER. THE CHAFF DAMAGE MEASURES .009 IN. DEEP AND .2955 IN WIDE X .5335 LONG. LOCATED AT STATION IS 3440.58 WL 15.18, BL/R 373.13.SDR 2A6D20200430002Bulkhead · chafedFORWARD L/H SIDE BAGGAGE AREA FORWARD BULKHEAD HAS MULTIPLE CHAFF MARKS. 31 IN TOTAL; THE TOTAL SIZE OF THE AREA IS 10.5 IN X 11 IN. THE DEEPEST CHAFF MEASURES OUT AT .008 IN.SDR 2A6D20200423001Door Frame · crackedFOUND A CRACK UNDER THE FORWARD LOWER R/H SIDE DOOR LATCH, THE CRACK MEASURES 5.7345 IN. LONG AND HAVE 2 EA. SPIDERS CRACKS EMITTING FROM MAIN CRACK. STA.1633.6 WL 2544.9 BL/R 863.6SDR 2A6R2020013055301Bearing Support · crackedFOUND NUMBER 5 BEARING SUPPORT CRACKED.SDR 7AJA202001160001Warning Light · illuminatedPILOT REPORTED SHORTLY AFTER DEPARTING YUMA MEDICAL CENTER THE "MGB CHIP" LIGHT ILLUMINATED. PILOT LANDED AT KNYL.SDR 7AJA2020010600006Relay · contaminated#2 GTN650 COMM, SKY CONNECT SAT PHONE AND STANDBY ATTITUDE INDICATOR CUTTING ON AND OFF. AIRCRAFT RETURNED TO BASE. FOUND AVIONICS RELAY AND CONNECTOR WERE WET. CLEANED AND DRIED RELAY AND CONNECTOR. OPS CHECK NORMAL.SDR QMLA2019100819078Structure · crackedDURING SCHEDULED HEAVY MAINTENANCE EVENT, TWO CRACKS WERE FOUND UNDER THE STRAKE OF THE VERTICAL STABILIZER TRAILING EDGE. ONE CRACK IS 3.5" IN LENGTH, AND THE OTHER IS 1.5" IN LENGTH. THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION AWAITINSDR 7AJA2019040200001Gearbox · warning lightTGB CHIP LIGHT ILLUMINATED IN LEVEL FLIGHT EN ROUTE. LIGHT FLICKERED AND THEN EXTINGUISHED AND REMAINED OFF FOR THE REST OF THE FLIGHT FOLLOWING POWER REDUCTION PER RFM. MAINTENANCE PERFORMED PROCEDURES IAW EC130T2 AMM 05-50-00, 6-1. NO CHIPS OR DEFECTS FOUSDR JBZA20190305001Starter Gen · failedCREW DETECTED A STRONG ELECTRICAL BURNING SMELL DURING FLIGHT BACK TO BASE. NO SMOKE MADE A PRECAUTIONARY LANDING AT KCIC.SDR QMLA2018112918127Unknown · odorUPON DEPARTURE FROM BASE I TURNED ON THE ENVIRONMENTAL CONTROL SYSTEM (ECS) TO WARM THE COCKPIT. ALMOST IMMEDIATELY THE ENTIRE CREW SMELLED A BURNING SMELL AND THE MEDICAL CREW IN BACK REPORTED SEEING SMOKE IN THE COCKPIT. THE ECS WAS IMMEDIATELY SECURED ANDSDR QMLA2018092818105Cover · crackedUPON PREFLIGHT THE PILOT DOOR WAS OPENED AND THE JETTISON HANDLE COVER WAS FOUND TO BE CRACKED. IT WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR QMLA2018090718100Cover · brokenCREW JETTISON HANDLE COVER WAS BROKEN. FOUND ON POST FLIGHT. THE MECHANIC REPLACED JETTISON DOOR HANDLE COVER. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 7AJA2018082001Friction Cup · dirtyPILOT EXPERIENCED LIMITED CONTROL MOVEMENT IN THE AFT-LEFT QUADRANT OF TRAVEL. A PRECAUTIONARY LANDING WAS MADE. MAINTENANCE DETERMINED THE CYCLIC FRICTION CUPS WERE DIRTY AND CAUSING RESISTANCE TO MOVEMENT. CUPS WERE CLEANED AND THE AIRCRAFT WAS RETURNED TSDR QMLA201808038092Cover · crackedFOUND DOOR JETTISON COVER CRACKED AT ONE OF THE MOUNTING HOLES DURING AIRWORTHINESS CHECK.SDR 7AJA2018082002Rivet · shearedFOUND THREE SHEARED RIVETS ON ANTI-VIBRATION ASSEMBLY. DURING REMOVAL FOR 600HR INSPECTION. ALL PARTS ARE CAPTURED AND THERE WAS NO RISK OF DEPARTURE IN FLIGHT BUT THE FAILURE HAS NOT BEEN OBSERVED AND IS UNCOMMON. AVA BASE WAS REPLACED WITH A NEW PART AND SDR 7MNA2019F00024Shaft · shearedON THE FIRST ENGINE START OF THE DAY THE STARTER WOULD NOT ENGAGE THE ENGINE. FOUND THE STARTER GENERATOR SHAFT HAD SHEARED.SDR QMLA2018051728059Engine · making metalDURING ENGINE START AND PRE TAKEOFF CHECK, THE PILOT NOTICED AN AMBER ENG CHIP LIGHT WAS SOLID. ABORTED TAKEOFF. AIRCRAFT WAS TAKEN OUT OF SERVICE. THE MECHANIC EXAIMED THE CHIP PLUGS AND FOUND METAL PARTICLES ON ENGINE ELECTRICAL CHIP PLUG AND ON MOD 1 SUMP SDR QMLA2018010118001Wire · damagedPILOT REPORTED DURING COLD WEATHER EVENT (<20 DEGREES F) THAT ECS WOULD NOT BLOW HOT AIR INTO THE CABIN. ECS CONTROL HEAD WOULD POWER UP MOMENTARILY THEN SHUT DOWN. DUE TO THE LIMITATION ON EC130T2 AIRCRAFT, IF THE HEATER IS NOT WORKING, IT CAN'T FLY BELOW 41 SDR 9SZA2017111600001Fire Warning · false activationENGINE FIRE ILLUMINATED TWICE DURING FLIGHT THEN EXTINGUISHED. GONG SOUNDED BOTH TIMES.SDR 2018FA0000096Bushing · backed outDURING PREFLIGHT INSPECTION, NOTICED THAT THE TAIL ROTOR GEARBOX CONTROL LEVER LOWER BUSHING HAD BACK OUT OF ITS HOLE A FEW THOUSANDTHS OF AN INCH. THE LEVER HAD BEEN REPLACED 86.9 HOURS PREVIOUSLY FOR THE SAME PROBLEM. THIS IS A RECURRING PROBLEM.SDR 2018FA0000094Bushing · backed outDURING A PREFLIGHT INSPECTION, NOTICED THAT THE TAIL ROTOR GEARBOX CONTROL LEVER LOWER BUSHING HAD BACKED OUT OF ITS HOLE A FEW THOUSANDTHS OF AN INCH. THIS LEVER HAD BEEN REPLACED 82.5 HOURS PREVIOUSLY FOR THE SAME PROBLEM.SDR 2018FA0000095Bushing · backed outDURING A PREFLIGHT INSPECTION, NOTICED THAT THE TAIL ROTOR GEARBOX CONTROL LEVER LOWER BUSHING HAD BACKED OUT OF ITS HOLE A FEW THOUSANDTHS OF AN INCH.SDR QMLA2017072717072Hopper · crackedDURING AAIP A0740 INSPECTION, FOUND THE OIL COOLER FAN HOPPER CRACKED AT FAN ATTACHMENT LOWER RIGHT BOLT LOCATION.SDR 2018FA0000092Bushing · backed outDURING DAILY PREFLIGHT INSPECTION, NOTICED THAT THE TAIL ROTOR GEARBOX CONTROL LEVER LOWER BUSHING HAD BACKED OUT OF ITS HOLE A FEW THOUSANDTHS OF AN INCH. THIS IS A RECURRING PROBLEM.SDR H44R2017051700003Bearing · seizedSMELLED AND SAW LIGHT SMOKE IN THE COCKPIT WHILE INBOUND. ASSUMED ELECTRICAL FIRE, SWITCHED BATTERY TO EMER SHED AND NOTICED SMOKE STOPPED. DID NOT NOTICE A LIGHT ON THE CWP BEFORE EMER SHED. LANDED AND SHUTDOWN. A WALKAROUND SHOWED NO CIRCUIT BREAKERS WERESDR JRUR201702270001Buckle · brokenCO-PILOT SEAT BELT BUCKLE ASSEMBLY PLASTIC ROTARY GUARD CRACKED CAUSING THE INABILITY TO RELEASE THE BELTS FROM THE BUCKLESDR 2017F00021Air Filter · saturatedAPPROXIMATELY 25 MINUTES AFTER TAKEOFF, THE MED CREW NOTICED SMOKE IN THE CABIN. THEY WERE UNAIDED AT THE TIME AND COULD SEE A LIGHT SMOKE BETWEEN THEM & THE LIGHTING THEY WERE USING FOR PATIENT CARE. THE PILOT WAS UNABLE TO SEE IT UP FRONT UNTIL HE TURNED ONSDR M7KA201702081592Bearing · making metalAFTER COMPLETION OF A .6 HOUR FLIGHT AND WHILE HOVER TAXIING TO HELIPAD, THE CENTRAL WARNING PANEL ENGINE CHIP LIGHT ILLUMINATED. PILOT IMMEDIATELY DIVERTED TO THE CLOSEST ALTERNATE DESIGNATED HELIPAD AND LANDED, UNDER NORMAL ENGINE POWER AND A NORMAL AIRCRAFTSDR 7AJA2017020601Air Filter · odor25 MINUTES AFTER TAKE-OFF, MEDICAL CREW NOTICED LIGHT SMOKE IN THE CABIN. PILOT REMARKED THAT THE ODOR WAS IDENTICAL TO A PREVIOUS INCIDENT WHERE ENGINE INLET FILTER OIL ENTERED THE COMPRESSOR AFTER SERVICING. MAINTENANCE CLEANED INLET AND PERFORMED A VISUASDR 9SZA20170124001Doubler · crackedCRACK WAS FOUND ON THE BATTERY DOOR DOUBLER AND SKIN UNDERNEATH APPROX 2 1/2 INCHES LONG DURING THRU-FLIGHT.SDR 7AJA201612201Duct · debondedDURING CRUISE, WITH CABIN BLEED AIR HEATER AND DEMISTER SYSTEMS OPERATING. NOTICED A CHANGE IN THE SOUND OF THE HEATER SYSTEM AND AN INCREASE IN AIRFLOW FROM BOTH SYSTEMS. AROUND 10 SECONDS LATER NOTICED AN ODOR DESCRIBED AS HOT PLASTIC. THE HEATER AND DEMSDR 7AJA2016121401Filter · contaminatedAFTER TAKEOFF AFTER TURNING ON THE BLEED AIR HEATER AND DEMISTER A BURNING ODOR AND LIGHT SMOKE WAS VISIBLE IN THE COCKPIT. SMOKE AND FUMES WENT AWAY AFTER TURNING OFF HEATER AND DEMISTER AND VENTED THE CABIN. MAINTENANCE FOUND EXCESS ENGINE INLET BARRIER FISDR 7AJA2016100600002Door · openDOOR WARNING LIGHT ILLUMINATED DURING FLIGHT. ON APPROACH, THE LEFT HAND BAGGAGE DOOR OPENED IN FLIGHT. AN UNEVENTFUL LANDING WAS MADE AND MAINTENANCE WAS DISPATCHED TO INSPECT THE DAMAGE TO THE HELICOPTER. MAINTENANCE FOUND THE LEFT FORWARD DOOR HINGE BENTSDR QMLA2016090316101Bearing · seizedENROUTE, THE NR 2 HYDRAULIC LIGHT ILLUMINATED AND SHORTLY AFTER THE CABIN FILLED WITH SMOKE. THE AIR CONDITIONER WAS TURNED OFF. THE LANDING WAS MADE IN A PASTURE. AFTER SHUTDOWN THE HYDRAULIC BELT WAS DISCOVERED IN THE TRANSMISSION AREA. IT WAS TWISTED AND CHSDR 7AJA20160901001Air Duct · dirtySMOKE IN CABIN WITH HEATING AND DEMISTING ON AFTER TAKEOFF. DIVERSION TO SUITABLE LANDING AREA WAS MADE. PRECAUTIONARY LANDING WAS PERFORMED. HEATING AND DEMISTING WERE TURNED OFF IMMEDIATELY WHEN STRONG BURNING ODOR AND POSSIBLE SMOKE WAS OBSERVED. MECHANSDR M7KA20160822001Turbine · making metalDURING CRUISE FLIGHT THE CENTRAL WARNING PANEL, ENGINE CHIP, SEGMENT ILLUMINATED. PILOT PROCEEDED TO PERFORM A NORMAL POWERED PRECAUTIONARY LANDING. MAINTENANCE PERSONNEL DISPATCHED TO THE ACFT DETERMINED METAL FOUND ON THE AIRCRAFT'S ENGINE ELECTRIC CHIP DESDR QMLA2016060316059Warning System · false activationTHE AVCS FAIL LIGHT ILLUMINATED IN FLIGHT. THE PILOT ABORTED THE FLIGHT ENROUTE TO THE SENDING HOSPITAL & RETURNED TO BASE. COMPLIED WITH THE PROCEDURE IN THE RFM & THE SYS RETURNED TO NORMAL OPERATION. UPON LANDING, THE MECHANIC REINITIALIZED THE AVCS SYS SDR 7AJA20160608003Control Servo · unreliableUPON APPROACH, THE AMBER SERVO CAUTION ANNUNCIATOR ILLUMINATED. NO LOSS OF FLIGHT CONTROL WAS OBSERVED. IT WAS FOUND THAT THE RT LATERAL SERVO HAD EXPERIENCE AN INTERNAL FAILURE.
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