Turbomeca ARRIEL-1D1
Service difficulty reports · 933
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 = 'ARRIEL1D1' 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 = 'ARRIEL1D1' 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 KBM2003F00047Gyro · precessesDIRECTIONAL GYRO PRECESSES AND SPINS. INSTALLED NEW DIRECTIONAL GYRO.SDR KBM2003F00048Gyro · fluctuatesATTITUDE INDICATOR FLUCTUATES AND SITS NOSE HIGH ABOUT 12 DEGREES IN FLIGHT.SDR KBM2003F00036Pitch Link · wornTAIL ROTOR PC BEARING, PLAY BEYOND LIMIT. REPLACED WITH 2 OVERHAULED PITCH LINKS.(K)SDR KBM2003F00037Bearing · crackedHALF SHELL BEARINGS HAVE CRACKED. REPLACED WITH NEW HALF SHELL BEARINGS.SDR 2003FA0001076Module · damagedPILOT REPORTED ENGINE WOULD NOT START AFTER FUEL STOP. AFTER 45 MINUTES ANOTHER ATTEMPT WAS MADE. ENGINE STARTED AND RAN NORMALLY. AIRCRAFT RETURNED THE FOLLOWING DAY. DURING OTHER SCHEDULED MAINTENANCE THE AXIAL COMPRESSOR WAS TURNED BY HAND. A NOTICEABLSDR CA031015013Gearbox · making metal(CAN) PILOT HAD AN TGB CHIP LIGHT INFLIGHT. LANDED AT HIS BASE FOR THE ENGINEER TO CHECK IT OUT. THEY FOUND A LOT OF A DARK GRAY SLUDGY SUBSTANCE WHICH PUT THE CHIP LIGHT ON. THEY DRAINED THE GEARBOX ANDDID A GROUND RUN FOR ABOUT .5 HOUR AND FOUND NOTHING (NOSDR CA030918011Starflex · worn(CAN) DURING THE BEFORE THE FRIST FLIGHT (BFF) INSPECTION, THE PILOT FOUND THE STARFLEX ARM END BUSHING DEBONDED AND DISPLACED OUTBOARD BY APPROXIMATELY 3/8 OF AN INCH. UPON DISASSEMBLY OF THE M/R HEAD THE FREQUENCY ADAPTER PN EIT-3023-01 INNERBORE WAS FOUND TSDR CA030911002Servo · damaged(CAN) PILOT CONDUCTED PREFLIGHT CHECK AND ON AIRCRAFT RUN UP COMPLIED WITH THE INTENT OF AD CF 200315R1. DURING THE TEST UPON DEPLETION OF THE HYDRAULIC SYSTEM ACCUMULATORS, CYCLIC MOVED TO THE LT FWD QUADRANT UNCOMMANDED. THE TEST WAS REPEATED 12 TIMES AT BOTSDR KBM2003F00030Switch · failedRT SIDE BAGGAGE DOOR WARNING LIGHT IS INOPERATIVE. REPLACED SWITCH WITH NEW.(K)SDR KBM2003F00015Battery · inoperativeBATTERY LIGHT ILLUMINATES IN FLIGHT FOUND NR 19 CELL REVERSE POLARITY. REMOVED AND REPLACED WITH SERVICEABLE CELL. REPLACED WITH SERVICE BATTERY.SDR CA030910007Servo · unserviceable(CAN) DURING GRD CHECKS AT IDLE & FLIGHT IDLE, CYCLIC CONTROL MOVING UNCOMMANDED LT & FORWARD. CYCLIC CONTROL WOULD CONTACT STOP, AFTER 1-2 SECONDS IT COULD BE BROUGHT BACK TO CENTER POSITION & APPEARED NORMAL. MOVEMENT COULD BE DUPLICATED ON SUBSEQUENT RUSDR CA030910008Module · making metal(CAN) ENGINE MAKING METAL INVESTICATION LED US TO BELIEVE METAL COMING FROM MO5 MODULE. REPLACED MODULE AND NO LONGER MAKING METAL.SDR CA030805011Wire · damaged(CAN) JUST AFTER TAKE OFF THE PILOT & PASSENGERS NOTICED SMOKE COMING IN THE CABIN OF AIRCRAFT. PILOT OPENED DOOR TO VENT SMOKE OUT OF CABIN. PILOT LANDED AS SOON AS PRATICAL. AFTER LANDING INSTRUCTED PASSENGERS TO EXIT A/C, SHUT DOWN THE ENGINE , CLOSED THE FSDR HEEA088655Coupling · looseDURING 1500 HOUR ENGINE INSPECTION FOUND RETAINING RING P/N 9745008005 LOOSE IN MOUNT GROOVE IN COUPLING. REPLACED RING WITH NEW RING WITH NO CHANGE (RING SHOULD BE TIGHT WITHIN GROOVE WITH NO MOVEMENT). DETERMINED COUPLING TO BE WORN AT RING GROOVE. TO BE SDR 2003FA0000826Bearing · roughCYCLIC CONTROLS PIVOT ON THIS BEARING DURING PITCH INPUTS. BEARING WAS (CATCHING) OR (RATCHETING) CAUSING DIFFICULTY CONTROLLING AIRCRAFT IN PITCH.SDR 3998Coupling · overheatedDURING FLT, AIRCREW NOTED BURNING RUBBER ODOR. DURING UNEVENTFULL, UN-PLANNED LANDING AIRCREW NOTED THE AIR-CONDITIONING BELT HAD BURNED UP AND MELTED TO AIR-CONDITIONING COMPRESSOR. THIS WAS DUE TO AN SEIZED AIR-CONDITIONING COMPRESSOR. IT IS OUR EXPERIENCE SDR HEEA088651Igniter · wornENGINE RIGHT SIDE IGNITER WORN. TO BE SENT TO VENDOR.SDR HEEA088433Bleed Valve · malfunctionedBLEED VALVE CLOSING AT TOO HIGH AN INDICATED NG RPM.SDR 2904071503Bleed Valve · defectiveBLEED AIR VALVE FLAG NOT GOING OFF.SDR KBM2003F00008Bleed Valve · failedBLEED VALVE DOES NOT CLOSE, FLAG CONTINOUS TO SHOW. REPLACED BLEED VALVE WITH SERVICEABLE UNIT.SDR KBM2003F00009Bleed Valve · failedBLEED VALVE FLAG SHOWING, SUSPECTED BLEED VALVE WILL NOT CLOSE. REMOVED AND REPLACED WITH SERVICEABLE BLEED VALVE.(K)SDR KBM2003F00010Bleed Valve · failedBLEED VALVE DOES NOT REMAIN CLOSED. REMOVED AND BENCH TSTED AND LUBRICATED NO DEFECTS NOTICE AND INSTALLED SAME BLEED VALVE.(K)SDR KBM2003F00013Blower · stoppedA/C STOPPED BLOWING COLD AIR. REMOVED SQUIRREL CAGE AND REPLACED WITH SERVICEABLE UNIT.(K)SDR 2904070703Indicator · defectiveHSI WILL NOT SAVE TO GPS.SDR 2904062803Bleed Valve · defectiveBLEED VALVE WILL NOT CLOSE UNTIL 101 PERCENT NG.SDR 2904062403Light · inoperativePULSLITE INOP.SDR 2904061103Light · inoperativePULSLITE INOP.SDR CA030610008Igniter · broken(CAN) ON INSPECTION IT WAS DISCOVERED THE INSULATOR HAD BROKEN FREE AND HAD SLID DOWN THE CENTER ELECTRODE ABOUT .3750. COULD POSSIBLY HAVE GONE THROUGH THE GAS PATH OF ENGINE HAD IT NOT BEEN DISCOVERED.SDR CA030612004Transducer · inoperative(CAN) DURING CRUISE FLIGHT THE PILOT NOTICED ENG OIL PRESSURE DROP OFF TO ZERO THEN INDICATED 9 BARS ON THE PRESSURE GAUGE. PILOT RETURNED TO POINT OF DEPARTURE. TROUBLE SHOOTING FOUND THE TRANSDUCER TO BE UNSERVICEABLE.SDR CA030527008Servo · failed(CAN) RESISTANCE IN CYCLIC STICK LT INPUT. FLIGHT CONTROL SYSTEM INSPECTED. CYCLIC STICK FRICTION STACK UP CHECKED OK. ALL FLIGHT CONTROLS UP TO THE SERVOS CHECK OK. M/R PITCH LINKS DISCONNECTED OK. SERVO AC 67244 SWAPPED AND PROBLEM WENT TO OPPOSITE SIDE RT. SDR HEEA086742Pump · failedFUEL PUMP DOES NOT RUN. TO BE SENT TO VENDOR.SDR HEEA086507Harness · failedPROBE BECAME UNSOLDERED AT PROBE ATTACH NUT AND CAME OUT OF ENGINE.SDR HEEA086525Magnetic Seal · leakingENGINE MAGNETIC SEAL LEAKING.SDR 2004FA0000174Buckle · brokenLT OB SEATBELT BUCKLE BROKEN.SDR CA030530013Bolt · sheared(CAN) UPON REINSTALLING THE LANDING GEAR SHOCK ABSORBERS, THE LOWER BOLT HOLDING THE FORWARD CROSSTUBE SHOCK CLAMPS IN PLACE SHEARED WHEN BEING TORQUED TO MANUFACTURERS RECOMMENDATIONS. THE BOLT SHEARED JUST BEFORE REACHING THE 132.7 IN LBS OF TORQUE LISTED ISDR CA030528014Igniter · failed(CAN) GENERAL INFORMATION LETTER NR 02-01 (FEB18, 2002), SERVICE LETTER 2171/02/ARL1/66 (FEB12, 2002), AND SERVICE LETTER 2223/03/ARL/173 (APRIL02, 2003), THESE PART NUMBER IGNITERS ARE FAILING IN SERVICE, USUALLY CAUSING EXTENSIVE ENGINE DAMAGE (WITH FIRST HASDR 2004FA0000175Coupler · seizedP2 HEATER HOSE SEIZED ONTO THE FITTING AT THE ENGINE.SDR 2904050203Bleed Valve · defectiveBLEED VALVE OPENING AT 71 PERCENT NG.SDR HCM2003F00001Warning Light · illuminated1.4 HOURS INTO A SIGHT SEEING FLIGHT, THE (FUEL FILTER) LIGHT ILLUMINATED ON THE CAUTION PANEL. THE PILOT MADE A PRECAUTIONARY LANDING AS SOON AS POSSIBLE. A MECHANIC WAS SENT TO THE HELICOPTER AND CHANGED THE FUEL CONTROL AND THE AIRFRAME FUEL FILTER. THE SDR CA030424003Turbine · damaged(CAN) THE ENGINEERS WERE CARRYING OUT THE ALERT SERVICE BULLETIN A292-72-0263.SUBJECT: CHECK OF RELATIVE POSITION OF 2ND STAGE TURBINE BLADES.THIS CHECK OF THE POSITION OF 2ND STAGE TURBINE BLADES CAN BE CARRIED OUT BY TWO METHODS WITHOUT DISASSEMBLY AND WITH SDR AL05200301779Module · inoperativeTHE PILOT CALLED IN LOW OIL PRESSURE AND DECLARED AN EMERGENCY. LANDED THE HELICOPTER SAFELY. PRELIMINARY INVESTIGATION SHOWED THAT THE OIL EVACUATED OUT THE EXHAUST PIPE INDICATING LOSS OF LABYRINTH SEAL PRESSURIZATION. THE RETURN OIL STRUT TUBE HAD ALSO CSDR CA030409010Hose · cracked(CAN) UPON INITIAL INSTALLATION OF HYDRAULIC HOSE (TAIL ROTOR CONTROL SERVO) THE FLARE FITTING SPLIT ALONG LENGTH OF FLARE NUT/FERRULE (ONE PIECE). HOSE RETURNED TO MFG FOR WARRANTY REPLACEMENT.SDR XSF2003F00000Coupling · wornPILOT EXPERIENCED HYDRAULIC FAILURE IN FLIGHT. SPLINES BETWEEN HYDRAULIC PUMP AND DRIVING PULLEY FOUND WORN. SPLINES ARE GREASED EVERY 500 HOURS. TT 409.5 HOURS. SPLINE MAY NOT HAVE BEEN GREASED SUFFICIENTLY. WHEN AIRCRAFT WAS ASSEMBLED.SDR 2003F00157Switch · intermittentDURING CRUISE FLIGHT THE PILOT FELT THE CONTROLS GET "HARD" LIKE A HYDRAULIC SYSTEM FAILURE, BUT AIRCRAFT STILL FLYABLE. PILOT OPTED TO DO PRECAUTIONARY LANDING IN AN OFF-AIRPORT AREA WITH NO INCIDENT REGARDING PERSONNEL OR AIRCRAFT. AFTER INSPECTING SYSTEM SDR 2004FA0000176Shim · missingHYDRAULIC FILTER BYPASS BUTTON POPPED (NO SHIMS INSTALLED).SDR S88R554JSeal Ring · distortedENGINE OIL PRESSURE LOSS RESULTED FROM DISTORTION OF THE DRAIN VALVE SEALING RING WITHIN THE OIL FILTER ASSEMBLY. INDENTATIONS ON THE SEALING RING CORRESPONDING TO HOLES IN THE FILTER BASE BECAME MISALIGNED DURING FILTER ELEMENT INSPECTION AND FAILED TO PRESENSDR M7K2003F00000Engine · making metalUPON ENGINE START ENGINE CHIP LIGHT ILLUMINATED ON THE CENTRAL WARNING PANEL. ENGINE IMMEDIATELY SHUT DOWN. CHIP DETECTORS AND OIL FILTER FOUND WITH METAL CONTAMINATION. ENGINE REMOVED. UNUSUAL NOISE EMINATES FROM THE FREE TURBINE WHEN ROTATED BY HAND. ENSDR HEEA082801Start Valve · failedENGINE DOES NOT START. START VALVE SUSPECTED.SDR HEEA082854Intake · crackedENGINE AIR INTAKE CRACKED AND CORRODED. TO BE SENT TO VENDOR.SDR B3OR20020021Bearing · failedDURING POST FLIGHT INSPECTION TECHNICAN ROTATED MAIN ROTOR TO INSPECT. WHILE TURNING HE NOTED THAT IT WAS VERY HARD TO TURN. FURTHER TROUBLESHOOTING REVEALED THE AIR CONDITIONER COMPRESSOR BELT SLIPPING ON THE COMPRESSOR DRIVE PULLEY. THE AIR CONDITIONER COMP
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