Turbomeca ARRIUS-2B1

Service difficulty reports · 92

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 = 'ARRIUS2B1'
  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.

SDR 2026F00116Engine · flamed outDURING ENROUTE PHASE OF FLIGHT, ENGINE #1 FLAMED OUT. PILOT REPORTED FUEL PRESSURE CAUTION LIGHT ILLUMINATED. PILOT UTILIZED #2 ENGINE TO PERFORM A RUN ON LANDING SUCCESSFULLY WITH NO DAMAGE TO AIRCRAFT, NO INJURY TO PILOT OR PASSENGERS. AIRCRAFT HAS BEEN TRUCMay 26, 2026 · N911AX · Urocop EC135T1 · Engine (Turbine/Turboprop)SDR QMLA2024102120135Potentiometer · faultedTORQUE SPLIT ON TAKE OFF. REDUCED COLLECTIVE, AND TORQUE MATCHED. TORQUE SPLIT AGAIN IN CRUISE FLIGHT. #1 TORQUE WAS 12-15% HIGHER AND FLUCTUATING. TORQUES HELD THAT SPLIT, THEN # 1 WOULD FLUCTUATE. UNABLE TO MATCH TORQUES. DIVERTED BACK TO BASE WITH PATIENT OOct 20, 2024 · N136VA · Urocop EC135T2 · Engine ControlsSDR B1EA20231127109BCUnknown · unknownSHORTLY AFTER TAKEOFF PILOT/CREW HEARD A BANG. PILOT NOTICED #1 ENGINE TOT RISING RAPIDLY AND DETERMINED THERE WAS AN ENGINE FAILURE. PILOT TURNED THE AIRCRAFT AROUND TO RETURN TO THE AIRFIELD. UNKNOWN TO THE PILOT, BUT CAUGHT ON VIDEO, THERE WAS AN UNCONTAINEAug 28, 2023 · N109BC · Urocop EC135T1 · Fuselage Structure (General)SDR UX9R2021F00047Floor Support · corrodedDISCOVERED FILIFORM CORROSION ON THE LEFT HAND OUTER CABIN FLOOR EDGE BETWEEN FUSELAGE STATION 33.30 TO 61.02. CORROSION WAS NOTICED BY VISUAL INSPECTION USING NAKED EYE WITH NO SPECIAL EQUIPMENT.Jan 28, 2021 · N506LF · Urocop EC130B4 · Fuselage Miscellaneous StructureSDR QMLA02020083141Chip Detector · false activationWHILE IN ROUTE BACK TO OUR BASE, THE FLIGHT MEDIC AND MYSELF NOTICED AN ENGINE CHIP LIGHT ON THE NUMBER ONE ENGINE. THE MEDIC WENT TO THE EC 135 EMERGENCY BOOK AND STARTED READING THE PROCEDURE FOR ENGINE CHIP LIGHT. I TOOK THE EFFECTED ENGINE TO IDLE AND BURNAug 28, 2020 · N136VA · Urocop EC135T2 · Turbine Engine Oil SystemSDR CA190204014Engine · making metal(CAN) AFTER STARTING THE ENGINE, AND, WHILE THE PILOT WAS SELECTING THE `FLIGHT` MODE, HE NOTICED THAT THE `ENGINE CD 1 INOP: MESSAGE WAS DISPLAYED ON THE AVIONICS.SHUTDOWN THE ENGINE AND CANCELLED THE MISSION. THE INSPECTION OF THE FRONT ELECTRIC MAGNETIC PLJan 26, 2019 · Bell 505 · Engine (Turbine/Turboprop)SDR 2019F00052Unknown · odorCREW IN CABIN AREA REPORTED ELECTRICAL BURNING ODOR NEAR THE MED AVIONICS PANEL, COINCIDING WITH ATTEMPTING TO TRANSMIT ON THE AUX SELECTOR. REMOVED RADIOS FROM PANEL AND INSPECTED WIRE BUNDLES FOR SIGNS OF BURNING & ARCING WITH NONE FOUND. PERFORMED RADIO CHEAug 14, 2018 · N135MH · Urocop EC135T1 · Air Distribution SystemSDR CCHA20180608001Engine · failedPILOT HEARD A LOUD BANG COMING FROM THE NR 1 ENGINE AND FELT A SLIGHT YAW. THE NR 1 ENG CHIP, NR 1 ENG FAIL AND NR 1 ENG FIRE CAUTION LIGHTS ILLUMINATED. PILOT PERFORMED A SINGLE ENGINE EMERGENCY SHUTDOWN AND MADE A RUNNING LANDING.May 21, 2018 · N911CK · Urocop EC135T1 · Engine (Turbine/Turboprop)SDR CA180530013Bearing · loose(CAN) THE FOLLOWING WAS REPORTED TO BELL: ONE OF THE SPHERICAL BEARINGS WAS LOOSE AND HAD SPUN IN THE HORN OF THE INNER RING. THE SAME SWASHPLATE ASSEMBLY WAS ALSO FOUND WITH THE UPPER GREASE SEAL INSTALLED INCORRECTLY. (INVERTED). (TC# 20180530013)May 17, 2018 · Bell 505 · Main Rotor Mast/SwashplateSDR HDNA20170323016Engine · failedCREW HEARD A POP WITH SMALL YAW MOVEMENT. ENGINE CHIP INDICATION. UPON INSPECTION AFTER LANDING FOUND MULTIPLE METAL PARTICLES ON ENGINE CHIP DETECTORS. OIL LEAKING THROUGH TURBINE WHEEL AND OUT EXHAUST CAUSING SMOKE.Mar 23, 2017 · N911XA · Urocop EC135T1 · Engine (Turbine/Turboprop)SDR 7AJA20170209001Warning Light · illuminatedNR 2 ENGINE LOW OIL PRESSURE CAUTION ANNUNCIATOR ILLUMINATED SHORTLY AFTER TAKEOFF.Jan 19, 2017 · N911AX · Urocop EC135T1 · Engine Oil Indicating SystemSDR HDNA20150513004Pressure Sensor · defectiveNUMBER 2 ENG INDICTED OIL PRESS TO BE OVER LIMITS SPECIFIED. PILOT WAS FORCED TO MAKE A PRECAUTIONARY LANDING.May 20, 2015 · N911XG · Urocop EC135T1 · Engine Oil PressureSDR QMLA2014110714130Unknown · odorPILOT REPORTED SMELLING SOMETHING HOT IN THE COCKPIT, NO SMOKE PRESENT. INSPECTED THE ACFT, THEN THEY FLEW FOR APPROX ONE HOUR. COULD NOT DUPLICATE PROBLEM.Nov 7, 2014 · N433AE · Urocop AS365N3 · Air Distribution SystemSDR HDNA2013F00138Eec · shutdownPILOT INITIATED A HOVER CLIMB TAKE OFF TO APPROX 150 FT PRIOR TO DEPARTING FROM HOSPITAL HELIPAD. AT THAT TIME, THE TORQUES STARTED TO SPLIT AND THE NR 2 ENGINE DROPPED OFFLINE AND SHUTDOWN. A SINGLE ENGINE LANDING WAS PERFORMED WITHOUT INCIDENT.Jun 28, 2013 · N911XC · Urocop EC135T1 · Fuel Control/Turbine EnginesSDR QMLA2012042312069Belt · brokenWHILE RETURNING TO BASE, EXPERIENCED A BURNING ODOR AND SMOKE IN CABIN. SMOKE CLEARED, MADE A PRECAUTIONARY LANDING. AFTER LANDING AND SHUTTING DOWN IT WAS DETERMINDED THAT THE AIR CONDITIONING BELT HAD BROKEN. REPLACED THE BELT AND CLEARED THE ACFT FOR FLApr 23, 2012 · N418TY · Snias AS350B3 · Cabin Cooling SystemSDR QMLDMG2492Gear · wornWHILE PERFORMING AN INSP OF THE MAIN ROTOR MAST, FOUND LATERAL PLAY IN THE COLLECTOR GEAR. UPON REMOVAL OF THE MAST NUT THE LOWER MAST BEARING FELL OUT OF THE MAIN TRANSMISSION. UPON FURTHER INVESTIGATION FOUND DAMAGE ON THE LOWER BEARING FACE AND THE MAST NUAug 26, 2011 · N969ME · Urocop EC135T1 · Main Rotor Mast/SwashplateSDR QMLA2011040311044Shaft · shearedDURING GROUND RUN, THE PILOT OBSERVED THE NR 1 ENGINE OIL TEMP WAS ELEVATED. UPON ARRIVING BACK TO DEPARTURE, IT WAS FOUND THAT THE LT OIL COOLER BLOWER WAS NOT TURNING WHILE ROTATING THE MGB. MECHANIC CONFIRMED DISCREPENCY. NO METAL FOUND IN MGB OIL FILTERApr 3, 2011 · N969ME · Urocop EC135T1 · Turbine Engine Oil SystemSDR QMLA2011021111041Bearing · failedDURING A GROUND RUN, THE NR 1 ENGINE CHIP LIGHT ILLUMINATED. THE MECHANIC INSPECTED THE ACFT AND FOUND CHIPS IN THE GEARBOX CHIP PLUG. THE MECHANIC CONSULTED WITH MFG WHO ADVISED HIM TO SEND THE CHIPS TO A LAB FOR ANALYSIS. THE MECHANIC THEN PERFORMED AN OIFeb 11, 2011 · N969ME · Urocop EC135T1 · Engine (Turbine/Turboprop)SDR CA090702006Electrical Sys · malfunctionedINVESTIGATION REVEALED THAT THE CAROUSEL RELAY PROVIDES AN UNANTICIPATED 6 TO 9 VOLTS VDC TO PIN C OF THE UTILITY CONNECTION ON THE BELLY OF THE AIRFRAME WHEN IT SHOULD ONLY BE SUPPLING 28 VDC TO PIN E OF THE CONNECTION. THIS ERRANT VOLTAGE INS`T ENOUGH TO OPEJul 1, 2009 · Urocop EC130B4 · Electrical Power SystemSDR 2008FA0000483Belt · brokenGROUND CREW NOTICED THE SMELL OF FUEL AND VAPOR COMING FROM AIRCRAFT AFTER LIFTING FROM SCENE. PIC NOTIFIED OF THE CIRCUMSTANCES. PIC MADE A PRECAUTIONARY LANDING WITH PATIENT ON BOARD. PIC DETERMINED THAT THE VAPOR WAS COMING FROM THE AIR CONDITIONER, AND NJul 4, 2008 · N105LN · Snias AS350B3 · Cabin Cooling SystemSDR QMLA010108001Canister · fullAFTER DEPARTURE FROM BASE HOSPITAL AND ENROUTE TO SENDING HOSPITAL, PILOT NOTICED A PERSISTENT FUEL ODOR IN THE CABIN. THE PILOT THEN ABORTED THE MISSION AND RETURNED TO BASE MAINTENANCE HELIPAD. TROUBLESHOT THE PROBLEM. FOUND THE FUEL PURGE CANISTER FULL Jan 1, 2008 · N397LG · Snias AS350B3 · Fuel Dump SystemSDR E3MA071115001Bearing · roughDURING A DAILY CHECK OF THE AIRCRAFT A GRINDING NOISE WAS DETECTED FROM THE TAIL ROTOR DRIVESHAFT COVER, AFTER AN INVESTIGATION THE GRINDING NOISE WAS FOUND TO BE COMING FROM THE 2 AFT TAIL ROTOR DRIVESHAFT HANGAR BEARINGS. THE BEARING PN: BB1B649616B, SN: N18Oct 18, 2007 · N639ME · Urocop EC135T1 · Tail Rotor Drive ShaftSDR BAQA200700025Switch · wornDURING REGULAR FUNCTIONAL CHECK OF ENGINE START SWITCHES, DISCOVERED THE NR1 AND NR2 ENGINE STARTING SWITCHES TO HAVE WORN DETENT IN THE SWITCH. THE SWITCH WAS ABLE TO BE MOVED FROM THE FLY POSITION TO THE OFF POSITION WITH OUT PULLING OUT OF DETENT.May 18, 2007 · N969ME · Urocop EC135T1 · Engine SynchronizingSDR 0511070132Bearing Cage · failedTHE -CHIP LIGHT- WARNING WAS ILLUMINATED ON THE CAD. FOUND BROKEN BEARING CAGE MATERIAL LAYING IN THE BASE OF THE MAIN GEAR BOX. MATERIAL APPEARED TO COME FROM THE OIL COOLER BLOWER QUILL BEARING.May 11, 2007 · N533ME · Urocop EC135T1 · Main Rotor GearboxSDR B65A112894Gauge · fluctuatesROTOR SPEED FLUCTUATED AND THEN FAILED.Nov 21, 2006 · N135CR · Urocop EC135T1 · Rotor Drive Indicating SystemSDR BAQ2006F00002Line · contaminatedWATER GETTING INTO FIRE DISCHARGE LINES AND HAS NO WAY TO GET OUT. (K)Jul 3, 2006 · N533ME · Urocop EC135T1 · Extinguishing SystemSDR MHIA106721Frame · damagedSMALL HOLE FOUND ON BOTTEM OF TAIL BOOM AFT OF 2ND FRAME IN TAIL BOOM. 556MM AFT OF TAIL BOOM FLANGE. REPAIRED IAW MFG REPAIR SCHEME MG110220053 NO REVISION, DATED 11/2/05 AND FAA FORM 8110-03 FILE NR DERY-710242-SW/05/331 DATED 11/2/2005. FAA FORM 337 SUBMNov 4, 2005 · N454AE · Urocop EC130B4 · Rotorcraft Tail BoomSDR Z1RA106192Transducer · intermittentDURING FLIGHT AL-300 DISPLAYS 1E30 CODE INTERMITTENTLY.Sep 26, 2005 · N761AF · Skrsky S76C · Autopilot SystemSDR B65A105845Pump · unserviceablePART FAILED IN FLIGHT, REPLACED PART.Aug 14, 2005 · N135CR · Urocop EC135T1 · Engine Fuel PumpSDR ALG2005F00036Accumulator · malfunctionedAT HOVER FOR TAKEOFF, PICKED AIRCRAFT UP TO A HOVER 2 TIMES AND BOTH TIMES AT A STEADY HOVER, AIRCRAFT OSCILLATED FORE AND AFT WITH NO PILOT INPUT (NOSE UP AND DOWN). MAINTENANCE INSPECTED SERVO INPUTS FOR WEAR, NO DEFECTS FOUND, SERVICED SERVO CONTROL ACCUMUJun 30, 2005 · N524AL · Urocop EC120B · Rotorcraft Servo SystemSDR ALGA096029Bolt · corrodedBOLT PITTED. REPLACED BY FIELD MAINT.Jul 8, 2004 · N513AL · Urocop EC120B · FastenersSDR HE66096544Computer · unreliableCOMPUTER CAUSING THE TRANSPONDER TO REPORT INACCURATE INFORMATION TO FLIGHT SERVICES.Jul 8, 2004 · N135CR · Urocop EC135T1 · Altimeter, Barometric/EncoderSDR HE66096791Altimeter · out of toleranceBOUNCES ALL OVER THE PLACE, NOT GOOD FOR IFR FLIGHT.Jul 8, 2004 · N135CR · Urocop EC135T1 · Altimeter, Barometric/EncoderSDR HE66094420Computer · unserviceableTRANSPONDER WOULD NOT WORK ABOVE 4000 FT AND NR 2 DME WOULD NOT WORK. AFTER HAVING THE TRANSPONDER REPAIRED SEVERAL TIMES AND FINALLY REPLACED PROBLEM STILL NOT CORRECTED. REPLACED NR 2 FCDM AND ALL PROBLEMS CORRECTED.May 7, 2004 · N135CR · Urocop EC135T1 · ATC Transponder SystemSDR HE66094217Button · brokenWHEN ACTIVATING ALT HOLD, THE LIGHT WOULD NOT IGNITE CONFIRMING ALT HOLD WAS ENGAGED.Apr 16, 2004 · N135CR · Urocop EC135T1 · Altitude ControllerSDR BAQA094225Actuator · wornEXCHANGE. OUTPUT SHAFT HAS EXCESSIVE SIDE PLAY. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 04/22/2004Apr 13, 2004 · N554ME · Urocop EC135T1 · Main Rotor ControlSDR BAQA094194Panel · crackedPANEL HAD STRESS CRACK IAW SITE MECHANIC, UPON REMOVAL, PANEL SHATTERED AND MECHANIC SCRAPPED ON SITE. REPLACED WITH SERVICEABLE PANEL FROM AEC, 04/16/2004Apr 1, 2004 · N522ME · Urocop EC135T1 · Passenger/Crew DoorsSDR HE66094001Autopilot Sys · intermittentAUTO PILOT FAILED INFLIGHT. AFTER RESETTING AUTOPILOT, IT WOULD FAIL AGAIN.Mar 29, 2004 · N135CR · Urocop EC135T1 · Autopilot ComputerSDR BAQA093969Cable · disconnectedWARRANTY. CABLE UNWEDGED FROM AFT CABLE. REPLACED WITH SERVICABLE UNIT. 04/07/2004Mar 29, 2004 · N135MF · Urocop EC135T1 · Tail Rotor Control SystemSDR BAQA094226Igniter · unserviceableWARRANTY. ELECTRODE GONE IN UNIT. REPLACED WITH SERVICEABLE ASSET UNIT. 04/26/2004Mar 29, 2004 · N135MF · Urocop EC135T1 · Spark Plug/IgniterSDR BAQA094029Injector · cloggedINJECTOR REMOVED DUE TO SUSPECTED CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 26, 2004 · N135MF · Urocop EC135T1 · Fuel Injector NozzleSDR BAQ2004F00000Housing · brokenTHE TAIL ROTOR/ ANTI-TORQUE BALL BEARING CONTROL SYSTEM CONTROL CABLE HOUSING BROKE AND SEPARATED FROM THE ACTUATOR HOUSING NEAR THE AFT SUPPORT ON THE TAIL BOOM. THIS DISCREPANCY WAS FOUND DURING A SCHEDULED INSPECTION.Mar 26, 2004 · N135MF · Urocop EC135T1 · Tail Rotor Control SystemSDR BAQA093758Mount · leakingLEAKING AND RETRACTED TOO FAR. REPLACED WITH SERVICABLE UNIT. 03/26/2004Mar 24, 2004 · N522ME · Urocop EC135T1 · Main Rotor Transmission MountSDR BAQA093759Mount · leakingLEAKING FLUID, AND RETRACTED ALL THE WAY INTO UNIT. REPLACED WITH SERVICABLE UNIT. 03/26/2004Mar 24, 2004 · N522ME · Urocop EC135T1 · Main Rotor Transmission MountSDR BAQA094030Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1 · Engine Fuel DistributionSDR BAQA094031Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1 · Engine Fuel DistributionSDR BAQA094032Injector · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1 · Engine Fuel DistributionSDR BAQA094033Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1 · Engine Fuel DistributionSDR BAQA094034Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING, RETURNED TO TEC BY TONY N, WITHOUT NOTIFICATION. HARCARD WAS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1 · Engine Fuel DistributionSDR BAQA093774Warning System · noisyEXCESSIVE ICS BACKGROUND NOISE, AND EXCESSIVELY LOUD WARNING TONES. REPLACED WITH SERVICABLE UNIT. 03/22/2004Mar 22, 2004 · N533ME · Urocop EC135T1 · Central Warning
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