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 CA021028003Fuel Control · leaking(CAN) FUEL LEAKING FROM OVERBOARD DRAIN WHEN BOOST PUMP TURNED ON TO DRAIN FUEL FILTERS.SDR CA021029005Cable · worn(CAN) THE PRIMARY FUNCTION OF THIS IS TO ADD FRICTION TO THE INERTIA REEL PORTION OF THE SHOULDER HARNESSES. THE RUBBER SHEATH THAT COVERS THE CABLE HAD SEPARATED AT BOTH ENDS OF THE CABLE ASSEMBLY DUE TO THE LACK OF SUPPORT. THE PREVIOUS ASSEMBLIES THAT WERE SDR CA021016028Door Frame · cracked(CAN) 32.5 INCH CRACK FOUND ALONG ENTIRE LT DOOR POST.SDR B3OR20020019Evaporator · brokenCRACKED HOUSINGS THAT CAUSE BLOWER MOTORS TO BECOME DISLODGED IN THE HOUSING, CAUSING BLOWER CAGES TO RUB ON THE HOUSING AND HOUSINGS TO BREAK APART. EVENTUAL FAILURE OF ENTIRE ASSEMBLY AND BLOWER MOTOR RENDERING THE AIRCONDITIONING SYSTEM INOPERATIVE. ONE OFSDR EHA2003F00000Bearing · failedDURING RETURN FLIGHT, THE GENERATOR MASTER CAUTION LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO BASE. UPON INSPECTION IT WAS FOUND THAT THE STARTER GENERATOR FORWARD BEARINGS HAD FAILED. THE BEARINGS ON THIS STARTER/GEN ARE ADDRESSED UNDER SB. THIS SB HAD SDR 2002FA0001003Transistor · inoperativePILOT REPORTED AIRCRAFTS RADIOS BEGAN TO SHUT DOWN FOLLOWED BY THE INDICATORS BECOMING ERRATIC. PILOT BEGAN TO SHUT DOWN NON ESSENTIAL ELECTRICAL LOADS. ELECTRICAL SYSTEM BEGAN TO OPERATE NORMALLY. PILOT RETURNED TO MAINTENANCE FACILITY AND LANDED WITH NO SDR 2002FA0001004Brushes · failedPILOT REPORTED ELECTRICAL SYSTEM FAILURE AND ACCOMPLISHED AN EMERGENCY LANDING AT AIRPORT. REMOVED STARTER/ GENERATOR, SUBSEQUEANT INSPECTION REVEALED ONE SET OF BRUSHES HAD FAILED. THE SESULT OF THIS WAS A GRADUAL DROP OF OUTPUT COMPENSATED FOR BY THE AIRCRSDR HXS2002F00000Labyrinth Seal · damagedIT WAS NOTICED THAT AIRCRAFT WAS TRAILING OIL & SMOKE FROM THE EXHAUST IN FLIGHT AND DID A LANDING AND INVESTIGATED. FOUND OIL ON TAIL BOOM AND EXHAUST TURBINE. GROUNDED AIRCRAFT. PREFORMED ENGINE CHANGE UP, AT LANDING SITE. SENT ENGINE FOR INVESTIGATION.SDR CA020801012Bevel Gear · failed(CAN) TAILROTOR GEARBOX BEVEL GEAR - LOSS OF TORQUE ATTACHING IT TO THE OUTPUT DRIVE SHAFT - ALL THE BOLTS WERE LOOSE CAUSING EXTREME BACKLASH IN GEAR SET. FOUND DURING GEARBOX REMOVAL/INSTALLATION. THE INPUT PINION, OUTPUT BEVEL GEAR, OUTPUT SHAFT ALL SCRAPESDR RX8R2002001Starter Gen · failedDURING FLIGHT AT 2500 FT. ONE SET OF BRUSHES IN THE STARTER GENERATOR FAILED. THE GENERATOR WAS STILL PUTTING OUT 28 VDC THROUGH THE REMAINING BRUSHES SO THE GENERATOR WARNING LIGHT DID NOT ILLUMINATE. THE GENERATOR WAS NOT PUTTING OUT ENOUGH CURRENT IN ITS DASDR HCM2002F00001Warning Light · illuminatedWHILE ON A SIGHTSEEING FLIGHT, PILOT EXPERIENCED A MAIN GEARBOX CHIP LIGHT INDICATION. THE PILOT MADE A PRECAUTIONARY LANDING. UPON INSPECTION OF THE MAIN GEARBOX CHIP PLUGS BY MAINTENANCE PERSONNEL, NO METAL WAS FOUND. CLEANED MAGNETIC CHIP PLUGS AND CONNESDR HCM2002F00002Relay · failedWHILE ON ROUTINE SIGHTSEEING TRIP, THE PILOT EXPERIENCED A FLICKERING GENERATOR FAILURE WARNING LIGHT WHILE TAKING OFF FROM THE AIRPORT. CONTINUED FLIGHT UNTIL RECEIVED A STEADY GENERATOR FAILURE WARNING LIGHT. RETURN TOT AIRPORT. UPON INSPECTION BY MAINTENSDR EHA2002F00007Indicator · inoperativeTORQUE METER FOUND INOPERATIVE ON START UP. REPLACED TORQUE METER.SDR CA020726009Control Cable · broken(CAN) PILOT MAKES NORMAL LDG AT FIRE BASE CAMP IN PELICAN NARROWS, SASK. PILOT PULLS / RETARDS THROTTLE LEVER & HEARS CLUNK. THROTTLE LEVER IS VERY LOOSE & ENGINE DOES NOT SHUTDOWN, IDLES AT 55 PERCENT NG. THROTTLE LEVER IS UNRESPONSIVE TO ANY POSITIIONS . PILSDR 3144060302Compressor · defectiveA/C COMPRESSOR DEFECTIVE.SDR B3OR20020008Coupler · wornDURING 1000 HOUR INSPECTION, THE ENGINE TO TRANSMISSION MOUNT TUBE WAS FOUND TO HAVE EXCESSIVE PLAY. THE GIMBAL RING MOUNT BUSHINGS ON THE TUBE WERE MEASURED, AND FOUND TO BE OUT OF LIMITS. UPON FURTHER INVESTIGATION, AND A PHONE CALL TO AMERICAN EUROCOPTER, WSDR B3OR20020009Isolator · delaminatedDURING A 1000 HOUR INSPECTION, THE FORWARD LATTERAL LAMINATED ISOLATOR MEMBER WAS FOUND TO BE DELAMINATED. THERE WAS NO OIL OR HYDRAULIC FLUID PRESENT IN THE AREA OR ON THE LAMINATED ISOLATOR MEMBER ITSELF. WE SUSPECT THAT THE AFT ISOLATOR MEMBER LOSS OF TORSDR B3OR20020006Crossbeam · groovedDURING A 1000 HOUR INSPECTION, THE CROSS BEAM WAS FOUND TO HAVE ONE DELAMINATED FWD. RUBBER ISOLATOR, AND DAMAGE TO THE AFT LATERAL LAMINATED RUBBER ISOLATER MOUNTING AREA. THE DAMAGE WAS CAUSED BY THE RUBBER ISOLATOR LOSING TORQUE, AND ROTATING ON ITS MOUNTINSDR B3OR20020007Gimbal Ring · wornDURING A 1000 HOUR INSPECTION, THE GIMBAL RING ON THE ENGINE TO MAIN GEARBOX MOUNT HAD EXCESSIVE PLAY IN THE BUSHINGS THAT WAS OUT OF LIMITS. THE BUSHINGS ARE NOT REPLACEABLE, AND THE GIMBAL RING HAD TO BE SCRAPPED.SDR HEEA078707Engine · malfunctionedENGINE TAKES SEVERAL ATTEMPTS TO START AFTER THE ENGINE IS RUN AND GETS WARMED UP. STARTS OK WHEN COLD.SDR HEEA078708Transducer · failedINTERMITTENT P3 FAILURES WITH AMBER GOVERNOR CAUTION LIGHT COMING ON.SDR HEEA078709Igniter · wornENGINE IGNITER WORN.SDR 2002FA0000557Bolt · brokenAFTER A MAINT FLIGHT, FOLLOWING THE CLEANING OF THE NR 4 BEARING, THE MAINT TECH FOUND THE OUTSIDE OF THE ENGINE COWLING DELAMINATED. DURING INSPECTION TO DETERMINE THE CAUSE, THE MECHANIC NOTICED THE ENGINE SPLIT LINE BETWEEN MO3 AND MO4 DEVELOPED A BLEED AIRSDR CA020507011Vent Line · clogged(CAN) REMOVED VENT TUBE FOR MORE DETAILED INSPECTION AND FOUND THAT THE TUBE WAS PLUGGED SOLID WITH WHAT APPEARED TO BE CARBON. THIS CAUSED THE REAR BEARING NOT VENT PROPERLY.THE COMPANY WILL ADD REMOVAL & INSPECTION OF THIS TUBE TO THE SCHEDULED 500 HOUR ENGISDR CA021016005Pump · failed(CAN) NR 2 FUEL BOOST PUMP LIGHT ILLUMINATED. FAULTY (NO PRESSURE) BOOST PUMP REPLACED WITH AIRWORTHY PART.SDR CA020501001Strut · failed(CAN) GAS STRUTS FAIL TO HOLD DOOR OPEN.SDR HEEA078471Lead · chafedIGNITER LEAD CHAFED.SDR HEEA078472Igniter · wornIGNITER HAS EXCESSIVE WEAR.SDR HEEA078473Igniter · wornIGNITER HAS EXCESSIVE WEAR.SDR CA020326001Belt · debonded(CAN) HYDRAULIC BELT WAS STARTING TO DEBOND NEAR THE DIRECTION OF ROTATION ARROW NEAR THE BONDED JOINT. THE TTSN OF THE BELT BY THE MANUFACTURE IS 600 HOURS. WE HAVE FOUND THAT THE OCCURRENCE OF DEBONDING IS HAPPENING TOO OFTEN, SO OUR INSPECTION OF THE BELT ISDR PG92002F00000Engine · failedENGINE CHIP LIGHT ILLUMINATED DURING PART 135 FLIGHT. PILOT MADE PRECAUTIONARY LANDING ON IMPROVED PRIVATE HELIPAD. MECHANIC DISPATCHED TO SIDE. FOUND EXCESSIVE METAL SLIVERS ON ALL ENGINE OIL SYSTEM MAGNETIC AND INDICATOR CHIP DETECTORS. AIRCRAFT GROUNDEDSDR CA020507006Control Cable · binding(CAN) . THE PILOT WAS ON APPROACH TO AN ISOLATED LANDING SIGHT. DID NOT HAVE FULL TAILROTOR AUTHORITY. HE ABORTED THE LANDING APPROACH SINCE IT WAS IN A CONFINED AREA & RETURNED BACK TO BASE. LANDED AT THE BASE WITH NO INCIDENT. THE HELICOPTER WAS BROUGHT INSSDR CA020313002Blade · will not balance(CAN) THE TAIL ROTOR HAS HAD A PROBLEM OF GOING OUT OF BALANCE. THE FIRST TIME IT WENT OUT OF BALANCE HAD TO REMOVE WEIGHT FROM ONE OF THE TIPS OF THE BLADE. THE SECOND TIME HAD TO ADD WEIGHT TO THE BLADE OUT OF BALANCE. THE THIRD TIME THE T/R WENT OUT OF BA
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