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 CA160129002Pump · unserviceable(CAN) FUEL PRESSURE LIGHT ILLUMINATED IN CRUISE FLIGHT. FUEL PRESSURE CONFIRMED NORMAL, FLIGHT CONTINUED IAW PMV AND PILOT RETURNED TO BASE. MAINTENANCE TROUBLESHOOTING CONFIRMED FAILURE OF NR 2 BOOST PUMP. PUMP MOTOR WAS RECEIVING POWER AND RUNNING BUT NO SDR QMLA2016010216001Accumulator · low pressureTHE PILOT & MEDICAL CREW WERE ENROUTE TO AN ACCIDENT SCENE WHEN THE PILOT FELT SOME FEEDBACK IN THE TAIL ROTOR PEDALS. ABORTED THE FLIGHT & PROCEEDED TO THE NEAREST AIRPORT FOR A PRECAUTIONARY LANDING. MADE AN APPROACH TO A RUNWAY TO ENSURE CONTROLLABILITY, SDR 9SZA2015122802Fire Detector · erraticENGINE FIRE LIGHT FLICKERING DURING FINAL APPROACH. (UNDER 100KT.)SDR QMLA2015120915109Setscrew · looseDURING CLIMB OUT WITH PATIENT ONBOARD, THE PILOT & MEDICAL CREW SMELLED & SAW SMOKE ENTERING THE CABIN FROM BELOW THE PILOTS SEAT AREA. IT SHOULD BE NOTED THAT JUST BEFORE TAKEOFF, THE PILOT HAD TRIED TO FULLY OPEN THE DEMISTER VLV TO CLEAR SOME CONDENSATION SDR CA151208007Bearing · dislodged(CAN) WHEN CONDUCTING A 600 HR INSPECTION, WHICH REQUIRES THE VISUAL INSPECTION OF THE MAIN ROTOR SHAFT INNER BEARING, SLEEVE, PN 704A33-653-109 FOR ALIGNMENT, WITNESS MARK AND MAST SEAL FOR CONDITION, THE AME DISCOVERED THE BONDING SEALANT, PRC WAS CRACK ALL SDR CA151127012Pump · failed(CAN) PILOT NOTICED LOSS OF FUEL PRESSURE ON 1 FUEL PUMP, 2 IN SYSTEM. FLIGHT BACK TO BASE WITH NORMAL LANDING. FUEL BOOST PUMP WAS FOUND NOT OPERATING, FAILED.SDR CA151127010Cable · shorted(CAN) INTERMITTENT INDICATION OF POSITION AND FLIGHT DATA. TROUBLESHOOTING INDICATED GPS ANTENNA SYSTEM, FOUND SECTION OF GPS ANTENNA CABLE SHORTED TO CABLE SHIELD AT TRANSCEIVER BOX, CONNECTOR. SUSPECT GPS ANTENNA CABLE CONNECTOR TERMINAL IS INTERNALLY SHORTSDR HDNA20151012005Window · blew outDURING CRUISE FLIGHT LT PAX SLIDING DOOR WINDOW FELL OUT & WAS HIT BY TWO MAIN ROTOR BLADES. TEC TOOLS COMFORT WINDOW STC SH8966SW.SDR 9SZA2015111601Fire Detector · saturatedFALSE FIRE WARNING LIGHT CAUSED BY SATURATED FIRE DETECTOR LOCATED UNDERNEATH THE STARTER GENERATOR ON THE RIGHT HAND SIDE.SDR QMLA2015111115105Attach Fitting · improper partDURING CRUISE FLIGHT, MEDICAL CREW REPORTED A BURNING ELEC TYPE SMELL IN THE REAR CABIN. THE PILOT IMMEDIATELY ABORTED THE FLIGHT & RETURNED TO THEIR BASE APPROX 4 MINUTES AWAY. NO MECHANICAL ANOMALIES WERE NOTED & EVERYTHING ELSE WAS NORMAL THE REMAINDER OFSDR QMLA2015103115101Chip Detector · carbonedWHILE EN-ROUTE TO A LOCAL HOSPITAL FOR A PATIENT TRANSFER, THE TAIL ROTOR GEARBOX CHIP LIGHT ILLUMINATED INFLIGHT WITHOUT SECONDARY’S. THE PILOT IMMEDIATELY INFORMED THE CREW & AIR COM THAT THEY WERE ABORTING THE FLIGHT FOR MX & PROCEEDING BACK TO BASE. THE SDR QMLA2015101315099Starter Gen · failedAPPROX 25 MINUTES INTO A 35 MINUTE FLIGHT, THE MASTER CAUTION FUEL PRESS LIGHT ILLUMINATED. CROSS CHECKED THE INSTRUMENTS & ALL OTHER INDICATIONS WERE NORMAL. BRIEFED CREW THAT WE HAD LOST A FUEL BOOST PUMP. ALMOST IMMEDIATELY THE ACFT INTERIOR LIGHTING BEGSDR CA151014002Bearing · cracked(CAN) DURING AN INSPECTION IT WAS NOTICED THE THE ELASTOMERIC BEARINGS HAD CRACKS THAT EXCEEDED LIMITS AND WERE REMOVED.SDR CA151212001Fuel Control · damaged(CAN) AFTER LANDING, PILOT RETARDED THROTTLE CONTROL TO IDLE, WITH ENGINE NOT RESPONDING. ATTENDING AME DISCOVERED THE THROTTLE CONTROL LEVER ON FCU WAS DISCONNECTED, PIN & CIRCLIP ARRANGEMENT. THE PIN, FOUND ON ENGINE DECK WAS RE-INSERTED AND DECELERATION, SDR CA150901010Power Supply · inoperative(CAN) POWER SUPPLY WOULD STOP WORKING AFTER 15-20 MINUTES INTO FLIGHT, THE PULSE WOULD STOP BEING GENERATED AND THE ANTI COLLISION LIGHT WOULD STAY DIMLY LIT. REPLICATED SCENARIO IN HANGAR WITH GROUND POWER ON FOR 15 MINUTES, LIGHTLY TAPPED POWER SUPPLY BOX ANSDR CA150819002Chip Detector · inactive(CAN) IT WAS DISCOVERED THAT DURING TROUBLINGSHOOTING AND TESTING. THE CHIP PLUG WOULD ACTIVATE THE CAUTION LIGHT WHEN ENGINE OIL TEMP. REACHED 80 DEGREES, HOVERING, APPROXIMATELY AND DEACTIVATE WHEN TEMP DROPPED BELOW 80 FWD FLIGHT.SDR QMLA2015070815055Structure · crackedCRACKS FOUND ON THE STRUCTURE WHERE THE NIGHT SCANNER IS MOUNTED. THE FWD CRACK IS APPROX 6 INCHES LONG, AT APPROX STATION 655, STARTING AT LBL 4" & ENDING AT RBL 2". THE CTR CRACK IS 0.5 INCHES LONG, ABOUT AN INCH AFT OF THE FWD CRACK, AT LBL 6". THE AFT TSDR CA150629011Tail Boom · cracked(CAN) CRACK FOUND AROUND RIVET ON LT SIDE OF TAIL BOOM ON HORIZONTAL STABILIZER SUPPORT STRUCTURE. CRACK IS ON REINFORCEMENT RIB FWD OF HORIZONTAL STABILIZER.SDR CA150623006Pump · faulty(CAN) DURING CRUISE FLIGHT FUEL WARNING LIGHT ILLUMINATED. FUEL PRESS DROPPED SLIGHTLY BUT REMAINED IN GREEN. UPON INSPECTION IT WAS NOTED THAT THE PUMP WAS RUNNING BUT NO PRESS. PUMP REPLACED.SDR CA150615023Spider · seized(CAN) PERFORMING 100HR INSPECTION ON ACFT. REMOVED T/R PITCH LINKS & SPIDER LINK. CHECKED SPIDER ASSEMBLY FOR FREEDOM OF MOVEMENT & PLAY ON THE TAIL ROTOR GEARBOX OUTPUT SHAFT. FOUND T/R SPIDER ASSEMBLY TO BE EXCESSIVELY TIGHT ON THE OUTPUT SHAFT. GROUNDED SDR CA150602025Engine · making metal(CAN) WHILE AT CRUISING ALTITUDE THE PILOT OBSERVED THE RED ENG CHIP LIGHT IN THE HELICOPTER WARNING PANEL. KEPT THE POWER ON THE ENG & BEGIN A DESCENT TO A CLEARING ON A LOGGING ROAD. THE INSPECTION OF THE THREE NON-ELEC CHIP PLUGS REVEALED NUMEROUS CHIPS ASDR QMLA2015051715039Hose · separatedDURING FLIGHT WITH THE AIR CONDITIONER ON HIGH, SMOKE ENTERED THE CABIN FROM AN UNKNOWN SOURCE. THE PILOT CONCLUDED THE MOST LIKELY CAUSE WAS THE AIR CONDITIONER. TURNED OFF AIR CONDITIONER, OPENED VENTS & WINDOWS. MADE UNSCHEDULED LANDING WITH SMOKE DISSISDR PG9A2015F00064Engine · warning lightDURING CRUISE FLIGHT, ENROUTE, PILOT RECEIVED A WARNING INDICATION FROM ENGINE CHIP LIGHT ILLUMINATION CAUTION PANEL AND FOLLOWED THE FLIGHT MANUAL AND LANDED.SDR CA150508010Dampener · dislodged(CAN) DURING A DAILY INSPECTION, STARTER GENERATOR DAMPENING PLATE WAS DISCOVERED PROTRUDING OUT BETWEEN THE 2 METAL DISCS ALONG SHAFT.SDR B3OR2015FA0000178B-Nut · disconnectedENGINE RPM DECREASED CAUSING A LOSS OF POWER IN FLIGHT WHICH FORCED THE PILOT TO AUTO-ROTATE TO ROUGH TERRAIN. THE ACFT CAME TO REST ON ITS SIDE WITH SUBSTANTIAL DAMAGE AND INJURY TO THE PILOT. POST ACCIDENT INVESTIGATION BY OWNER/OPERATOR AND THE OEM TECH RESDR CA150429007Starflex · cracked(CAN) DURING VISUAL INSPECTION, IT WAS NOTICED THAT A PORTION OF THE STARFLEX EPOXY BUILD-UP, AT THE BUSHING SHOULDER, WAS CRACKED ALL THE WAY AROUND AND CHUNKS OF EPOXY WHERE MISSING FROM THE TOP AND BOTTOM RADIUS OF SAME SHOULDER. REMOVED.SDR USX2015F00000Display · overheatedPILOT REPORTED BURNING ELECTRICAL ODOR IN COCKPIT AND MADE PRECAUTIONARY LANDING TO PRIVATE HELIPORT. LOCAL FIRE DEPARTMENT RESPONDED AND CONFIRMED ODOR. USING AN INFRARED SCANNER. THE LOCAL F/D IDENTIFIED A HEAT SOURCE TO BE COMING FROM THE PILOTS FLIGHT SDR QMLA2015042415031Motor · failedWHILE CLIMBING TO ALTITUDE, ACFT EXPERIENCED A SIGNIFICANT VIBRATION IN THE AIRFRAME & PEDALS. WHEN THE ACFT WAS ON SHORT FINAL FOR THE EMER LANDING, ALL THREE CREW MEMBERS SMELLED SMOKE & FUMES IN THE COCKPIT. ALL ENG INDICATIONS & ELEC INDICATIONS WERE NORSDR 2015FA0000122Compressor · lockedA/C BELT FOUND MELTED AND BROKEN DUE TO A/C COMPRESSOR LOCK UP. HEAT GENERATED ON PULLEY CAUSED REJECTION OF THE PULLEY DUE TO OVERHEATING RESULTING IN CHANGES TO THE METALLURGY. REPLACED A/C COMPRESSOR, PULLEY AND RECEIVER/DRYER AS REQUIRED IAW APPLICABLE STSDR QMLA2015040215024Filter Element · bypassingON APPROACH FOR LANDING, DURING FLIGHT RECEIVED A MOMENTARY, FUEL FILTER BYPASS, WARNING LIGHT ILLUMINATION. REDUCED POWER & THE LIGHT EXTINGUISHED. AS POWER WAS INTRODUCED AGAIN DURING LANDING THE WARNING LIGHT MOMENTARILY ILLUMINATED AGAIN. LANDED & SHUTDSDR CA150320004Shaft · sheared(CAN) DURING CRUISE FLIGHT THE PILOT HAD THE FUEL INDICATION WARNING. ACFT IS EQUIPPED WITH TWO FUEL PUMPS AND THE PILOT FINISHED HIS FLIGHT IAW FLIGHT MANUAL. ONCE ON THE GROUND THE MAINTENANCE DEPARTMENT HAS ABLE TO CONFIRM THE FUEL PUMP NR 2 WAS ENERGIZED SDR 9EKA20150313012Spider · brokenLOST RT PEDAL IN FLIGHT. PERFORMED RUN ON LANDING.SDR QMLA2015030615013Unknown · smokeAT CRUISE FLIGHT, THE PILOT TURNED ON THE CABIN HEAT & APPROX 3 MINUTES LATER, THE MEDICAL CREW NOTICED SMOKE FILLING UP THE CABIN AS WELL AS NOXIOUS FUMES. THE CABIN HEAT WAS TURNED OFF & THE WINDOWS WERE OPENED TO VENT THE CABIN. THE FLIGHT WAS ABORTED & TSDR CA150212007Line · leaking(CAN) HYDRAULIC LINE LEAKING EXCESSIVELY. THIS LINE IS INSTALLED AT THE PUMP PRESSURE OUTPUT.SDR CA141209001Igniter · eroded(CAN) UPON VISUAL INSPECTION OF IGNITER, FOUND SMALL ROUND PART INSIDE TIP OF IGNITER LOOSE, ABOUT TO FALL OFF INTO COMBUSTION CHAMBER. HAD THE TIP COME OFF IT COULD POTENTIALLY HAVE CAUSED SIGNIFICANT FOD DAMAGE TO TURBINE BLADES.SDR CA141209002Starflex · damaged(CAN) VISUAL INSPECTION REVEALED THAT 1 OF THE STARFLEX ARM END BUSHINGS HAS STARTED TO SEPARATE FROM THE STARFLEX. STARLEX HAS BEEN REMOVED FROM SERVICE.SDR CA141120019Pump · inoperative(CAN) OVERHAULED BOOST PUMP INSTALLED. DURING TESTING, FOUND PUMP INOPERATIVE, BLOWS THE FUSE. REMOVED PUMP AND BENCH TESTED ONLY TO FIND ITS SUFFERS FROM THE SAME PROBLEM IT WENT IN FOR. A SHORT TO GROUND. RETURNED TO O/H SHOP.SDR 2014FA0000636Engine · contaminatedBETWEEN FLIGHTS WHILE ON GROUND AT FLIGHT IDLE, THE PILOT RECEIVED A ENGINE CHIP LIGHT. MAINTENANCE FOUND A 1.5 MM PIECE OF CARBON ON LOWER ELETRICAL ENGINE CHIP DETECTOR. MAINTENACE PERFORMED ENGINE OIL RINSE, REPLACEMENT, FILTER CHANGE AND GROUND RUNS. CHIPSDR QMLA2014102514126O-Ring · damagedAFTER LANDING, ON POST FLIGHT WALK AROUND, DISCOVERED OIL PRESENCE FROM ENG DECK DRAIN UNDER ACFT. UPON OPENING ENG COWLING IT WAS DISCOVERED THAT THE OIL PRESENCE WAS ON THE ENG DECK & LEAKAGE APPEARED TO BE COMING FROM THE BASE OF THE ENG OIL FILTER CUP HOUSDR QMLA2014102014124Adapter · crackedFREQUENCY ADAPTER IS CRACKED ON THE YELLOW BLADE.SDR QMLA2014102214122Compressor · failedDURING THE RETURN FLIGHT TEN MILES NORTH OF OUR BASE, THE MEDICAL CREW & I SMELLED FUMES IN THE COCKPIT. THE SMELL WAS COMING THROUGH THE AIR CONDITIONER VENTS, TURNED THE AIR CONDITIONER SYS OFF. THE SMELL IMMEDIATELY DISSIPATED & CONTINUED THE FLIGHT TO A SDR CA140814004Spherical Stop · cracked(CAN) ELASTOMERIC RUBBER OF THE SPHERICAL STOPS, FOUND TO BE CRACKED AND EXTRUDING BEYOND LIMITS.SDR CA140821007Engine · making metal(CAN) CHIP LIGHT EVENT OCCURRED4. THE ENGINE WAS INSPECTED IAW MM. A SMALL PIECE OF METAL WAS FOUND ON THE OIL RETURN ELECTRIC CHIP DETECTOR AND ALSO ON THE NON-ELECTRIC MO5 CHIP DETECTOR. THE MODULE 4/5 SCAVENGE OIL STRAINER WAS REMOVED AND A LARGE PIECE OSDR CA140731014Pulley · worn(CAN) BEARING, WAS SPINING ON PULLEY MADE A GROOVE IN THE CIRCLIP AND PULLEY.SDR QMLA2014072314089Starter Gen · failedUNUSUAL SMELL AS RETURNING TO BASE FOLLOWING A BASE TRANSFER. MADE DECISION TO LAND AT THE NEAREST AIRPORT. THE TURN EXECUTED TO NAVIGATE TO THE AIRPORT PUT THEM IN HEAVY RAIN WHICH DIMINISHED VISIBILITY. AT THIS TIME HE NOTICED A FUEL P LIGHT ILLUMINATE ONSDR I2WA201407180001Control Servo · leakingDURING CRUISE FLIGHT, THE HYDRAULIC LIGHT ILLUMINATED AND THE HORN CAME ON. THE PILOT SLOWED THE ACFT AIRSPEED AND TURNED THE HYDRAULICS OFF. HE THEN PROCEEDED TO MAKE A RUN ON LANDING AT A PRIVATE AIRPORT. MECHANIC DISCOVERED THERE WAS NO HYDRAULIC FLUID ISDR CA140724011Armature · shorted(CAN) WHILE BUCKETING WATER, PILOT SMELLED ELECTRICAL BURNING AND THE GENERATOR FAIL LIGHT ILLUMINATED, LANDED. NOTICED BURNED GROUND WIRE BETWEEN STARTER GEN AND FIREWALL GROUND LUG. NEW STARTER GEN INSTALLED, NO DEFECTS NOTED. SENT FAILED STARTER GEN TO ASDR CA140702006Igniter · worn(CAN) DURING SCHEDULED INSPECTION, ENGINE FAILED TO START ON LT IGNITION SYS IAW TEST CRITERIA. IGNITER REMOVED AND FOUND ERODED, AND A SMALL ROUND PART FROM INSIDE THE IGNITER HAD MIGRATED TO THE TIP OF THE IGNITER AND BECOME STUCK AT THE END OF THE BODY. APSDR QMLA2014062614079Pump · faultyTHE PILOT NOTICED A FUEL P LIGHT ILLUMINATE ON APPROACH WITH APPROXIMATELY FIVE MILES REMAINING UNTIL LANDING. THE INDICATION WAS TO ADVISE LOSS ON ONE FUEL PUMP WITH ANOTHER ONE STILL OPERATIONAL. THE PILOT DECIDED AFTER REVIEW THE RFM TO STAY ON COURSE FORSDR CA140702016Skin · cracked(CAN) DURING MAINTENANCE VISIT, EDDY CURRENT INSPECTION AT STA 9900 TAILBOOM FITTINGS OF EASA REGISTERED ACFT, IT WAS DISCOVERED THAT CRACKS PROPOGATED FROM 3 OF THE 4 FITTINGS ON THE TAILBOOM. UPPER RT AND LT TAILBOOM ATTACH FITTINGS AND RT LOWER ATTACH FITTI
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