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 QMLA2012052012084Switch · burnedON STARTUP, SMELLED ELECTRICAL BURNING AND NOTICED LOWER FUEL PUMP SWITCH LIGHT TO NOT BE ON AND THE ENGINE FIRE WARNING LIGHT TO BE ON IN THE WARNING CAUTION PANEL. FOUND WARNING BREAKER TO BE TRIPPED AND LOWER FUEL PUMP SWITCH TO BE BURN AND STUCK IN THE ON SDR CA120507014Seal · leaking(CAN) INPUT SEAL LEAKING SO SEAL WAS REPLACED AND GROUND RUN TO CONFIRM NO LEAKS.SDR CA120507015Seal · leaking(CAN) INPUT SEAL LEAKING. TGB REMOVED FOR REPAIR.SDR QMLA2012050112072Bar · damagedDURING PREFLIGHT INSPECTION, NOTICE LT FWD MGB SUPPORT BAR EXTREMELY EASY TO TWIST AND HAD A POPPING SOUND WHEN CHECKING BEARING PLAY. INSPECTED THE OTHER SUPPORT BARS AND FOUND THE RT FWD SUPPORT BAR LOWER CRIMPED COLLAR SHOWED MARKING THAT LOOKED LIKE IT HASDR CA120502008Battery · weak(CAN) COULD NOT START THE ACFT BECAUSE THE BATTERY WAS WEAK. REMOVED THE BATTERY TO FIND IT LEAKING. REPLACED THE BATTERY WITH A NEW RG355. THIS BATTERY WAS INSTALLED NEW IN SEPTEMBER 2011.SDR CA120501006Connector · intermittent(CAN) AT EACH 100 HR INSPECTION, WHEN YOU DISCONNECT THE CONNECTOR PLUG, OR WHEN IT`S DISCONNECTED TO REMOVE THE ENGINE COWL, THE ELECTRICAL PINS INSIDE THE CONNECTOR PLUG PUSH AWAY FROM EACH OTHER, CAUSING A FAULTY CONNECTION, LEADING TO EITHER A LACK OF POWSDR QMLA2012042612068Pump · inoperativeSHORTLY AFTER TAKEOFF, FOR A REPOSITION MISSION, PILOT OBSERVED THE ILLUMINATION OF THE FUEL PRESSURE CAUTION LIGHT WHILE IN LEVEL CRUISE FLIGHT. ALL OTHER INSTRUMENT INDICATIONS APPEARED NORMAL ALONG WITH ENGINE PERFORMANCE. PILOT ALERTED BOTH AIRCREW AND ASDR QMLA2012042512065Unknown · odorPILOT AND CREW DETECTED A BURNING ODOR IN CABIN. RETURNED TO BASE AND LANDED WITHOUT INCIDENT. INSPECTED THE ENGINE BAY, MAIN GEARBOX AREA, UNDER CABIN FLOOR, BEHIND INSTRUMENT PANEL, IN BOTH SIDE CARGO BAYS, INSIDE THE AFT BAGGAGE BAY. NO DEFECTS NOTED. SDR QMLA2012041112057Wire · looseENROUTE, PILOT NOTICED CLIMBING OIL TEMPERATURE. ALL OTHER INSTRUMENTS NORMAL. SLOWLY REDUCED POWER AND MAINTAINED AIRSPEED FOR COOLING IAW FLIGHT MANUAL INSTRUCTIONS. AFTER CONTINUING WITH SUFFICIENT AIRSPEED AND REDUCED POWER, TEMPERATURE STILL HIGH. PERSDR CA120413007Control Cable · worn(CAN) PILOT REPORTED "TAIL ROTOR PEDALS FEEL STIFF" -TAIL ROTOR CONTROL FLEXIBLE CONTROL CABLE FOUND WORN ON FORWARD END DUE TO MOVABLE PORTION OF CABLE CHAFING ON FIXED PORTION OF CABLE.SDR QMLA2012040212041Pressure Switch · intermittentINTERMITTENT FUEL FILTER CAUTION LIGHT ILLUMINATED, CONTINUED FROM CRUISE THROUGH PRECAUTIONARY LANDING WITH NO DECREASE OF FUEL PRESSURE INDICATED BELOW .4 BAR ON THE COCKPIT GUAGE.SDR QMLA2012032612037Tube · shearedPILOT ATTEMTED START PROCEDURE WITH NO SUCCESSFUL LIGHT OFF. FUEL WAS FOUND ON THE ENGINE DECK, DOWN THE DECK DRAIN TUBES, AND ON PORTIONS OF THE LT SIDE OF THE ENGINE. FOUND THAT THE LT INJECTOR TUBE WAS SHEARD FLUSH WITH THE END OF THE FLARE SUPPORT, .125SDR QMLA2012032412035Blower Motor · failedCREW SMELLED SMOKE IN THE CABIN FOLLOWED BY A CYCLING "GRUMBLING" NOISE WHILE AT CRUISE FLIGHT. MADE A PRECAUTIONARY LANDING WITHOUT INCIDENT. MX INSPECTED AND FOUND THAT THE AFT EVAPORATOR BLOWER MOTOR FOR THE AIR CONDITIONING SYSTEM TO BE THE CAUSE OF THE SDR 2012FA0000243Skin · chafedDURING A SCHEDULED 600 HR INSPECTION, MECHANIC PERFORMED A CMD-AS350-09-22 CONCERNING CHAFING OF THE CONDUIT CLAMPS AND CONDUIT ON THE UPPER AND LOWER VERTICAL STABILIZER SPAR AND SKIN. FOUND CHAFE DAMAGE TO THE UPPER VERTICAL STABILIZER SKIN, IN THE AREA OF SDR QMLA2012031712028Unknown · odorCREW HEARD A LOUD "POP" NOISE FOLLOWED BY AN ACRID ODOR IN THE CABIN . PILOT DID NOT NOTICED ODOR OR HEARD THE POP. PILOT CHECKED THE AIR CONDITIONING, HEATER, CHECKED ALL OF THE INSTRUMENTS. EVERYTHING APPEARED TO BE WORKING NORMALLY. MADE A PRECAUTIONARY SDR QMLA2012031612033Engine · failedON START UP, ENGINE FLAMMED OUT THEN COUGHT AGAIN ABOUT FOUR TIMES IN ABOUT 6 SECONDS. EACH TIME IN FLAMMED OUT TEMP DROPPED ABOUT 25 TO 50 DEGREES AND THEN WOULD RELIGHT. ABORTED START. MAX TEMP ABOUT 710.SDR QMLA2012030812053Cyclic Stick · loosePLAY IS FELT IN THE CYCLIC STICK - FORE AND AFT AXIS: DISCOVERED THE CYCLIC PITCH STICK STAND WAS SLIDING BACK AND FORTH ON THE BUSHING THAT WAS SUPPOSE TO BE PRESS FITTED TO THE CYCLIC PITCH STICK STAND.SDR CA120213008Skin Panel · detached(CAN) DURING NORMAL OPERATIONS, THE FORWARD BELLY PANEL DEPARTED IN FLIGHT. THE PILOT HAD DROPPED OFF A GROUP OF SKIERS AND WAS ON HIS DECENT HEADING TO THE PICK-UP. AT THIS TIME HE HEARD A LOUD BANG AND AS A RESULT BROUGHT THE ACFT TO A LEVEL ATTITUDE AND RESDR CA120204001Turbine · failed(CAN) PILOT WAS PERFORMING SLING OPERATIONS AND LANDED FOR FUEL. ACFT WAS SHUTDOWN FOR APPROXIMATELY 10 MINUTES AND PILOT THEN STARTED ACFT WITH NO DEFECTS AND CARRIED ON OPERATIONS. AT THE NEXT FUEL STOP, PILOT LANDED AND SHUTDOWN ACFT FOR APPROXIMATELY 10 SDR CA111222001Nozzle · failed(CAN) FOLLOWING REMOVAL OF FORWARD BELLY COWLING IN PREPARATION FOR 600 HRS INSPECTION, WE FOUND THAT THE VENTILATION DUCT, WAS COMPLETLY TORN AT AIR INTAKE END AND AT OUTLET END BELOW CO-PILOT SEAT. SINCE THERE IS A PLASTIC "Y" UNION PART OF THAT DUCT AND THSDR CA111208012Drain Valve · leaking(CAN) ENGINE START DRAIN VALVE LEAKING FUEL FROM SPLITLINE DURING ENGINE SHUT DOWN.SDR HCMA2012F00018Wire · shortedACFT DEPARTED. APPROX 10 MINUTE INTO FLIGHT, PILOT NOTICED SMALL ELECTRICAL PROBLEMS SUCH AS A SCRATCHY INTERCOM AND VOLUME CHANGING. NOTICED RADIO, GPS, VIDEO SCREEN AND AIR CONDITIONING SYS GO OFF LINE. DID NOT NOTICE A GENERATOR LIGHT AT THIS TIME. RETURSDR QMLA2011102711107Unknown · odorCREW SMELLED FUEL IN THE CABIN ON A FLIGHT TO PICK UP A PATIENT. MADE A PRECAUTIONARY LANDING. INSPECTED ENTIRE FUEL SYS AND COULD NOT LOCATE ANY LEAKS. RAN BOTH BOOST PUMPS AND RE-CHECKED FUEL SYS. NO LEAKS NOTED. PERFORMED A GROUND RUN, & COULD NOT FINDSDR RMXA2011101788168Connector · contaminatedOIL PRESSURE INDICATOR FLUCTUATION DURING FLIGHT WITH NO CAWS PANEL INDICATION OF FAILURE. FOUND CONNECTOR PLUG TO OIL PRESSURE TRANSDUCER CONTAMINATED. REMOVED, CLEANED, AND REINSTALLED CONNECTOR PLUG FOR TRANSDUCER. PERFROMED GROUND RUNS AND OPS CHECK FLIGSDR 2011FA0000629Structure · crackedCRACK IN TAIL BOOM.SDR 2011FA0000612Indicator · damagedNG INDICATOR DIGITAL READOUT IS DIFFICULT TO READ IN DAYLIGHT CONDITIONS.SDR QMLA2011091911093Starter Gen · burned outTHE PILOT AND MEDICAL CREW NOTICED THE ODOR OF SMOKE IN THE CABIN SHORTLY AFTER TAKEOFF. THE PILOT IMMEDIATELY LANDED THE ACFT AND PERFORMED A SHUTDOWN. MECHANIC INSPECTED THE ACFT. MECHANIC OPENED THE ENGINE COWLING, THE BURNED/ELECTRICAL TYPE ODOR WAS EXTSDR RMXA20110915001Boot · tornMAST BOOT CAME FREE FROM ROTATING SWASH PLATE. A PIECE OF THE BOOT LOWER FLANGE TORE OFF AND DEPARTED THE ACFT MOST LIKELY HITTING THE P/C LINKS THAT CAUSED A VIBRATION FELT IN THE CYCLIC CONTROL STICK.SDR QMLA2011091411095Connector · looseIN CRUISE, DURING FERRY FLIGHT FIRE LIGHT ILLUMINATED. STARTED AUTHORITATIVE TYPE DECENT DOING NOTHING WITH FUEL CONTROL. ONCE IN DECENT LOOKED OVER THE REST OF THE INSTRUMENTS AND EVERYTHING LOOKED NORMAL. DID SLIGHT S TURN TO SEE IF I WAS TRAILING ANY SMOKE SDR CA110909013Hydraulic System · failed(CAN) HYD FAILURE IN FLIGHT. HELICOPTER SEVERELY DAMAGED UPON LANDING. HYD FAILURE ROOT CAUSE WILL BE BASED ON TSB`S INVESTIGATION.SDR RMXA390549Compressor · failedAIR CONDITIONER COMPRESSOR FAILED, PILOT REPORTED ODORS IN COCKPIT.SDR QMLA2011082411089Belt · frayedWHILE ON A SHORT FINAL, THE PILOT DETECTED AN ODOR THAT SMELLED LIKE BURNING RUBBER WITH NO ASSOCIATED SMOKE. UPON THE POST FLIGHT INSP THE PILOT NOTICED THAT THE AIR CONDITIONING BELT SOME NOTICEABLE SHREDDING, BUT STILL HAD TENSION. THE MECHANIC WAS CALLEDSDR CA110829005Nut · backed out(CAN) DURING SLINGING OPERATIONS WITH THE PILOT REDUCED DOOR REMOVED AND RT SLIDING DOOR IN THE OPEN AND LOCKED POSITION. THE RETAINING NUT PN, ASN 52320BH060N BECAME LOOSE AND BACKED OFF OF RETAINMENT PIN 350A25-1348-21. THE SLIDING DOOR SWUNG DOWN AND TO TSDR CA110909009Engine · seized(CAN) WHILE STARTING THE ENGINE, AS THE TEMPERATURE WENT THROUGH 650 OR APPROX 20 PERCENT NG IT STARTED TO DEACCELERATE. THE THROTTLE WAS PULLED BACK AND THE STARTER BUTTON WAS ENGAGED TO COOL THE ENGINE. WHEN THE START BUTTON WAS RELEASED A SQUEALING NOISE WSDR CA110822010Probe · wrong part(CAN) ERRATIC OPERATION OF LOW FUEL LIGHT DURING 500 HR INSPECTION, ACFT HAD OLD TYPE FLOAT SENSOR, NOW MODIFIED VERSION IAW SB 28-12 (MOD 07-2484, CAPACITOR GAGING SYSTEM).SDR PG92011F00003Switch · defectiveA MALFUNCTION OCCURRED BETWEEN THE 30 ALPHA PANEL AND STROBE LIGHT SWITCH CAUSING THE STROBE LIGHTS NOT TO WORK. THE 30 ALPHA PRINTED CIRCUIT BOARD AND STROBE LIGHT SWITCH BOTH SUSTAINED BURN MARKS AND MELTED SOLDER POINTS. THE CIRCUIT BRAKER FOR THE STROBE SDR PG92011F00004Panel · defectiveA MALFUNCTION OCCURRED BETWEEN THE 30 ALPHA PANEL AND STROBE LIGHT SWITCH CAUSING THE STROBE LIGHTS NOT TO WORK. THE 30 ALPHA PRINTED CIRCUIT BOARD AND STROBE LIGHT SWITCH BOTH SUSTAINED BURN MARKS AND MELTED SOLDER POINTS. THE CIRCUIT BREAKER FOR THE STROBESDR PG92011F00006Switch · malfunctionedA MALFUNCTION OCCURRED BETWEEN THE 30 ALPHA PANEL AND STROBE LIGHT SWITCH CAUSING THE STROBE LIGHTS NOT TO WORK. THE 30 ALPHA PRINTED CIRCUIT BOARD AND STROBE LIGHT SWITCH BOTH SUSTAINTED BURN MARKS AND MELTED SOLDER POINTS. THE CIRCUIT BREAKER FOR THE STROBSDR PG92011F00007Panel · malfunctionedA MALFUNCTION OCCURRED BETWEEN THE 30 ALPHA PANEL AND STROBE LIGHT SWITCH CAUSING THE STROBE LIGHTS NOT TO WORK. THE 30 ALPHA PRINTED CIRCUIT BOARD AND STROBE LIGHT SWITCH BOTH SUSTAINED BURN MARKS AND MELTED SOLDER POINTS. THE CIRCUIT BREAKER FOR THE STROBESDR PG92011F00008Switch · malfunctionedA MALFUNCTION OCCURRED BETWEEN THE 30 ALPHA PANEL AND STROBE LIGHT SWITCH CAUSING THE STROBE LIGHTS NOT TO WORK. THE 30 ALPHA PRINTED CIRCUIT BOARD AND STROBE LIGHT SWITCH BOTH SUSTAINED BURN MARKS AND MELTED SOLDER POINTS. THE CIRCUIT BREAKER FOR THE STROBESDR CA110902003Seal · leaking(CAN) HYD PUMP PULLEY BEARING FOUND OUTER SEAL SPINNING ON OUTER RACE, CAUSING WEAR ON SEAL LIP. BEARING LEAKING GREASE FROM SEAL. BEARING REPLACED.SDR QMLDMG2541Guide Vane · crackedWHILE PERFORMING MODIFICATION TU347 TO MODULE 3, DISCOVERED THE SECOND STAGE NOZZLE GUIDE VANE ERRODED AND CRACKED. REASSEMBLED MODULE 3 QND ARE SENDING IT TO A LEVEL 4 REPAIR CENTER FOR REPAIR.SDR CA110801004Drain Valve · failedENGINE START IS NORMAL AT THE BEGINNING, BUT T4 DROPS SUDDENLY AROUND 35 TO 47 PERCENT, AND THE START FAILS (INTERMITTENT PROBLEM WHEN ACFT IS STARTED MORE THAN 1.5 TO 2 HRS AFTER LAST SHUTDOWN). DURING 30 SECOND BOOST-PUMP ON, BEFORE START, IT IS DISCOVEREDSDR CA110803031Mount · crackedMOUNT WAS CHANGED, DURING REGULAR INSPECTION THERE WAS A CRACK COMING OUT FROM UNDER THE HYD PUMP MOUNTING FACE.SDR CA110712006Line · crackedTROUBLESHOOTING START SOLENOID VALVE AND WHEN RE-INSTALLING LINE IT WAS FOUND TO HAVE A CRACK AND CORROSION BEHIND THE FERRULE. PART WAS REPLACED. OTHER LINE WAS INSPECTED AND FOUND SERVICEABLE.SDR CA110714002Module · contaminatedAFTER SECOND START OF THE DAY, ENGINE CHIP WARNING LIGHT COMES ON ON WARNING PANEL. ENGINE SHUTDOWN. PILOT VERIFIES CHIP DETECTORS AND FINDS HEAVY CONTAMINATION ON MODULE 5, ENGINE OIL TANK OUTLET AND OIL FULL FLOW CHIP DETECTORS. NO CONTAMINATION ON MODULESDR 2011FA0000442Engine · warning lightPILOT HAD AN ENGINE CHIP LIGHT ILLUMINATION DURING FLIGHT. HE PERFORMED AN UNEVENTFUL UNSCHEDULED LANDING. MX FOUND A 1MM WIRE (FILIMENT) ON THE LOWER ENGINE ELECTRICAL DETECTOR. MX PERFORMED A DRAIN AND RINSE OF THE OIL SYS AND FOUND ALL PLUGS CLEAN AND RESDR QMLA2011070311075Compressor · failedTHE PILOT SMELLED A BURNING ODOR IN THE CABIN ALONG WITH A HEAT/TEMPERATURE RISE. IMMEDIATELY LANDED AND NOTIFIED MX. MECHANIC FOUND THAT THE AIR CONDITIONING COMPRESSOR APPEARED TO HAVE LOST OIL RETENTION THROUGH THE DRIVE PULLEY SEAL. THE COMPRESSOR AND CSDR QMLA2011070711073Bonding Strap · brokenARRIVED AT HELICOPTER, THE FUEL QUANTITY INDICATION WENT FROM 50 PERCENT TO 0 PERCENT. AN UNUSUAL ODOR FOLLOWED DURING FLIGHT. TROUBLESHOT SYS, FOUND WITH A/C ELECTRIC POWER ON, AND BOOST PUMPS ON. FLUCTUATING FUEL INDICATION, LOW FUEL PRESSURE, AND INOP FUSDR 2011FA0000436Indicator · failedLOSS OF ENGINE TORQUE INDICATION.
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