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 2016FA0000193Transponder · malfunctionedTHE TRANSPONDER BECAME VERY DIFFICULT TO ENTER SQUAWK CODES. THE UNIT WAS SENT INTO THE MFG FOR REPAIR WHERE THEY HAD TO REPLACE THE ENTIRE FACEPLATE WITH NEW. THE EXPLANATION IS THAT THE HELICOPTER OPERATIONS HAVE A HIGHER VIBRATION RATE AS WELL AS PERFORMEDSDR 7AJA2016FA0000169Packing · cut5.7 HOURS AFTER COMPLETING AN ENGINE INSPECTION, WHICH INCLUDED CHANGING THE HMU FILTER AND PACKINGS, THE PILOT UPON HIS POST FLIGHT WALK AROUND NOTICED FUEL ON THE UNDERSIDE OF THE FUSELAGE. TO ASSIST IN TROUBLESHOOTING THE PROBLEM, THE PILOT THEN PROCEEDED SDR 7AJA20160415002Packing · cutFUEL WAS DISCOVERED DRAINING OUT OF THE ENG OVERBOARD DRAIN SYS. FOUND THE FUEL CONTROL, HYDRO MECHANICAL UNIT, PUMP FILTER INTERNAL PACKING CUT.SDR 7AJA20160407001Packing · cutAFTER SHUTDOWN, THE PILOT WAS COMPLETING HIS WALK AROUND & NOTICED FUEL DRIPPING FROM THE ENG OVERBOARD DRAIN TUBE. HE ALSO NOTICED THAT THE FUEL LEAKED ONTO THE BELLY & WAS DRIPPING THERE ALSO. AFTER THE MECHANIC ARRIVED, THEY TURNED ON THE ACFT BOOST PUMP SDR CA151120006Bracket · misinstalled(CAN) DURING INSTALLATION OF FWD BRACKET ASSY IT WAS FOUND THAT IF NOT CORRECTLY INSTALLED, A CHAIN DESIGNED TO PREVENT LOSS OF PIP PIN, CAN BE WRAPPED AROUND THE CO-PILOT TAIL ROTOR CONTROL STUBS AND CAUSE RESTRICTION OF MOVEMENT. THIS CAN HAPPEN ON BOTH SISDR CA151117010Starflex · overheated(CAN) UPON DISASSEMBLY AS PART OF SCHEDULED 600 HR INSPECTION, IT WAS DISCOVERED THAT 1 OF 3 STARFLEX ARM BUSHINGS HAD HEAT DISCOLORATION AND TURNED BLUE IN PLACES. THE ACFT INCORPORATES MFG MODIFICATION DESIGNED TO PREVENT OVERHEATING IN THIS AREA. ASSY WILLSDR QMLA2015091915083Fire Warning · false activationTHE PILOT HAD JUST COMPLETED A FLIGHT & LANDED AT RECEIVING HOSPITAL, NORMAL SHUTDOWN & UNLOADED PATIENT. THE PILOT THEN POWERED UP THE ACFT TO CRANK FOR THE RETURN FLIGHT TO BASE & WHEN BATTERY POWER WAS APPLIED NOTICED THAT THE ENG FIRE LIGHT WAS ILLUMINATESDR CA150724001Duct · cracked(CAN) DURING DISASSEMBLY OF AIRCRAFT FOR PAINT THE OIL COOLER INLET AIR DUCT WAS FOUND CRACKED.THE SAME DISCREPANCY WAS FOUND ON AIRCRAFT .PARTS REPLACED WITH SERVICEABLE UNITS. MFG HAS INTRODUCED A DAILY INSPECT BY MEANS OF ASB 05A020 AND HAS ISSUED EMERGENCYSDR CA150615024Nut · damaged(CAN) WHEN DISASSEMBLING PITCH LINK ON SWASH PLATE, ENGINEER WAS LOOSENING NUT & NOTICED THAT THE NUT WAS HOT & UPON FINAL INVESTIGATION THE THREADS HAD BEEN DAMAGED.SDR CA150331013Cap · leaking(CAN) AFTER COMPLETION OF FLIGHT NOTICED CAP AT TOP OF SERVO LEAKING. CLEANED UP, DID 20 MIN GROUND RUN AND TEST FLIGHT. SERVO LEAKED AGAIN.SDR CA150211005Fitting · leaking(CAN) HYDRAULIC HOSE LEAKING SEVERELY FROM SWAGGED FITTING ON END. FOUND DURING POST FLIGHT CHECK. HYDRAULIC FLUID AT MIN QTY LINE, SIGNIFICANT FLUID LOSS OBSERVED.SDR CA150202011Spring · damaged(CAN) DURING AIRFRAME 1200 HR INSPECTION, ENG CONTROL TWIST GRIP LOAD COULD NOT BE ADJUSTED DUE TO OUTSIDE TIGHTENER SPRING NOTCH WAS OUT OF THE RECEIVER, INSIDE THE TWIST BOX ASSEMBLY. THIS LEADS TO THE TWIST GRIP LOAD COULD NOT BE TIGHTENED IAW MM SINCE THESDR CA150211006Fitting · leaking(CAN) LEAKING FOUND AT SWAGED FITTING ON HYDRAULIC MANIFOLD END. SIGNIFICANT FLUID LOSS. FOUND ON POST FLIGHT INSPECTION. FLUID SLIGHTLY BELOW MIN LEVEL.SDR CA150211007Hose · leaking(CAN) HYDRAULIC HOSE LEAKING AT SWAGED END. SIGNIFICANT FLUID LOSS. FOUND DURING POST FLIGHT CHECK.SDR CA141212007Bearing Race · out of alignment(CAN) UPON DISASSEMBLY MAINTENANCE ENGINEER NOTICED WITNESS MARK MOVED. THE OUTER RACE MOVED ON MAST .1250" APPROXIMATELY WHERE ALIGNMENT MARK IS RACE TURNED ON MAST.SDR CA150224032Bushing · damaged(CAN) TAIL ROTOR ASSY, WAS REMOVED TO FACILITATE REPLACEMENT OF PITCH HORN ASSY, PN 355A12-5102-00 X 2. UPON REMOVAL, THE ANTI-ROTATION BUSHING WAS FOUND DEFORMED AT THE TIP, PREVENTING ITS REMOVAL FROM THE PITCH HORN. A REQUEST HAS BEEN SUBMITTED WITH MFG HELSDR CA141120016Washer · failed(CAN) UPON DISASSEMBLY FOR SCHEDULED INSPECTION, FOUND 2 OF THE 4 ROTATING SWASHPLATE DRIVE LINKAGE FRICTION WASHERS SHATTERED.SDR CA141109002Scissor Link · scored(CAN) SCORING ON DRIVE LINK AND BUSHING.SDR CA141104003Elt · power loss(CAN) ON MONTHLY CHECK, IT HAD 3+2 LIGHTS LOW RF POWER.SDR HCMA201407170001Bolt · looseTHE DIGITAL NR READING WAS FLUCTUATING IN FLIGHT. AFTER TROUBLESHOOTING OF THE NR PICKUP ON THE NR GAUGE, IT WAS DECIDED TO INSPECT THE PHONIC WHEEL FOR SECURITY. UPON REMOVAL OF THE EPICYCLIC, IT WAS FOUND THAT SIX ATTACHMENT BOLTS, 2 WERE TORQUED TO 100 INSDR 2014F00133Release Mech · brokenWHILE ADJUSTING THE PASSENGER SEAT BELTS BETWEEN FLIGHTS, THE SEAT BELT RELEASE MECHANISM BROKE OFF WHILE RELEASING THE HARNESS FROM THE BUCKLE.SDR CA140428001Hose · leaking(CAN) ON A DAILY INSPECTION THE HYDRAULIC OIL LEVEL WAS FOUND TO BE LOW. IT WAS FOUND THAT THE TAIL ROTOR PRESSURE HOSE TO THE T/R SERVO HAD A SMALL LEAK IN IT. CHANGED THE HOSE OUT OUT AT THIS TIME WHICH FIXED THIS PROBLEM.SDR CA140417009O-Ring · failed(CAN) ON PLACING FUEL FILTER IN FUEL BOWL O-RING BROKE CAUSING PIECE OF O-RING TO CONTAMINATE HIGH PRESSURE PUMP AND HMU ASSY. THE TOP OF THE SHORT STANDPIPE IN THE FILTER BOWL IS VERY SHARP NOT CHAMFERED, MAKING THE ASSY HARD WHEN YOU PUSH THE FILTER WITH THSDR CA140417011Spacer · scored(CAN) AFTER AROUND 100 HOURS THE DRIVE LINK SCORES THE SPACER ON THE ROTATING SCISSORS AND THE SPACER AND THE DRIVE LINK HAVE TO BE CHANGED THE SPACER IS BASICALLY SCRAP BUT THE BUSHINGS ON THE DRIVE LINK CAN BE PRESSED OUT AND CHANGED. WE THINK THAT THIS IS SDR CA140307002Wheel · loose(CAN) DURING POWER APPLICATION, PILOT NOTICED AN ERRATIC READING ON THE MAIN ROTOR RPM GAUGE. ON FINAL APPROACH THE LOW ROTOR WARNING SYS ACTIVATED, ALARM IN HEADSET, HOWEVER, THE ROTOR RPM WHERE CORRECT. INVESTIGATION IN CONJUNCTION WITH MFG REVEALED THAT TSDR CA140218008Spacer · loose(CAN) ACFT WAS HAVING ROTOR RPM FLUCTUATION INDICATION TROUBLES IN FLIGHT. TROUBLESHOOTING THIS PROBLEM LED TO AN INDICATION ISSUE. REPLACED THE NR/N2 INDICATOR. WENT FOR A TEST FLIGHT AND FOUND THIS, RPM IS GOOD ON THE GROUND, BUT WHEN YOU PULL IN POWER FORSDR CA140125003Warning Light · activated(CAN) WHEN TURNED ON PITOT HEAT LIGHT WON`T EXTINGUISH IN DASH.SDR CA140125002Shoulder Belt · malfunctioned(CAN) SEAT SHOULDER HARNESS WON`T RETRACT.SDR CA131220005Bearing · seized(CAN) PUMP DRIVE BEARING SEIZED CAUSING HYDRAULIC BELT TO DISINTEGRATE WITH LOSS OF 1 HYDRAULIC SYSTEM. PLEASE NOTE REASON THIS HAS BEEN SUBMITTED LATE AUDIT FINDING.SDR CA130321010Filter · clogged(CAN) HYDRAULIC FILTER BYPASS INDICATOR POPPING DURING GROUND RUN/FLIGHT. FILTERS INSPECTED AND FLUID CHANGED NUMEROUS TIMES AND INDICATOR CONTINUED TO POP. NEW BYPASS INDICATOR INSTALLED.SDR CA130214024Eec · malfunctioned(CAN) AFTER TAKEOFF AROUND 09:40 AM, HAD THE GOVERNOR YELLOW LIGHT ON ON MY CAUTION PANEL, FOLLOW BY RPM DECREASING TO AROUND 369, WITH THE LOWER VEMD SCREEN LOOSING THE GAUGES IN SAME TIME. TURN BACK FOR AND IMMEDIATELY AFTER THIS TURN, HAD THE TOP SCREEN OFSDR CA121012016Bearing · cracked(CAN) ON INSPECTION IAW ASB 01-00-65 TAIL ROTOR HALF SHELLS FOUND WORN AND CRACKED. REPLACED ALL 4 BEARING.SDR CA120926009Bearing · worn(CAN) PREMATURE WEAR OF THE LAMINATED BEARING.SDR CA120801016Bearing · seized(CAN) ON THE ACFT SHUTDOWN, NOTICED THAT THE MAIN ROTOR WAS SLOWING FASTER THAN USUAL. THE DRIVE LINE, ROTORS, WERE HARD TO TURN BY HAND. THE HYDRAULIC PRESSURE WARNING LIGHT NEVER WENT ON. INVESTIGATION REVEALED THAT THE BELT DRIVEN HYDRAULIC PUMP DRIVE BESDR CA120723020Bearing · cracked(CAN) AFTER INSTALLING A NEW SET OF TAIL ROTOR BLADES AND TGB ASSY AFTER THE LAST HALF SHELL FAILURE. WE FLEW THE ACFT HOME. ON INSPECTION OF THE HALF SHELL, WEAR WAS NOTICED. IAW ACFT MFG SAFETY INFORMATION NOTICE NR 2482-S-64. WE WILL BE REPLACING THE BESDR CA120716023Bearing · cracked(CAN) AIRCRAFT WAS FLYING FROM A TO B WHEN THE PILOT AND AME HERD A LOAD NOISE COMING FROM THE TAIL ROTOR FOLLOWED BY HIGH LEVELS OF VIBRATION. THIS VIBRATION INCREASED AS THE FLIGHT UNTIL THEY BOTH THOUGHT IT WAS TOO MUCH AND LANDED THE ACFT TO INSPECT THE TSDR CA120716024Bearing · cracked(CAN) ON INSPECTION OF THE TAIL ROTOR BLADE IT WAS FOUND THAT THESE HALF SHELLS OR LAMINATED BEARING WHERE WEARING OUT AT A VERY HIGH RATE AND WOULD NOT LAST FOR MORE THAN 100 HRS. THESE BEARING WHERE REMOVED AND A NEW SET INSTALLED. ACFT BALANCED AND PUT BASDR CA120615006Exciter · failed(CAN) DURING ENG START, THE ENG FAILED TO LIGHT OFF & FAILED TO CLIMB PAST 12% N1. DURING START, THE START CB TRIPPED. UPON TROUBLESHOOTING THE IGNITOR BOX WAS FOUND TO HAVE FAILED INTERNALLY. THE TIME OF THE FAILURE THE ACFT & ENG BOTH HAD A TOTAL TIME OF
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