Turbomeca ARRIEL-2B
Service difficulty reports · 332
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 = 'ARRIEL2B' 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 = 'ARRIEL2B' 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 CA090622013Bracket · worn(CAN) UPON LANDING PILOT CARRIED OUT WALK AROUND, DISCOVERED VERTICAL FIN BEACON LIGHT ASSY HANGING ON SIDE OF FIN BY WIRE BUNDLE, MUST HAVE JUST HAPPENED AS MINIMAL DAMAGE TO PAINT AND NO DAMAGE TO FIN STRUCTURE. MOUNTING FLANGE OR BRACKET THAT AFIXES BEACONSDR QMLA2009041109016Engine · making metalENG 1 CHIP LIGHT ILLUMINATED IN CRUISE FLIGHT. 3 ATTEMPTS WERE MADE WITH THE CHIP BURNING SYS TO EXTINGUISH LIGHT. LIGHT REMAINED ILLUMINATED. PILOT SET UP ACFT FOR OEI OPERATIONS AND PLACED 1 ENG SWITCH TO IDLE. 1 ENG OIL PRESSURE AND TEMPS WERE MONITORED ANDSDR RMXA029H325622609Fitting · corrodedUPON REMOVAL OF THE AIRFRAME VERTICAL FIN ASSY, THE UPPER VERTICAL FIN FWD ATTACH STEEL FITTING SEPARATED FROM THE UPPER VERTICAL FIN. INSP REVEALED THAT ALL RIVETS ATTACHING THE FITTING TO THE FIN WERE CORRODED BEYOND RETENTION. ALSO FOUND THE SHIN OF THE FINSDR CA090217002Angle · loose(CAN) WHILE PERFORMING DAILY INSP ON ACFT NOTICED THE RIVETS THAT ATTACH THE T/E ANGLE TO UPPER VERTICAL STABILIZER (PN 350A14-0020-1902) WERE "SMOKING" AND ANGLE FELT LOOSE.SDR CA090223013Friction Ring · failedPRIOR TO INSTALLING STARTER GEN SB 80.00.07 PARA 2B2B AND 2B3 WERE APPLIED. THE STARTER WAS THEN INSTALLED AS PER MM AND A GROUND RUN WAS DONE. DURING THE GROUND RUN NO VIBRATION WAS NOTED ON THE STARTER, VOLTAGE AND AMPERAGE WAS NORMAL. I NOTICED A BURNINGSDR 2008FA0000729Unknown · odorSHORTLY AFTER TAKEOFF, PERSONNEL ONBOARD REPORTED A BURNING ODOR TO THE PILOT. ABORTED FLT AND RETURNED TO HELIPAD TO INVESTIGATE. MECH PERFORMED AN INSPECTION OF THE AIRFRAME, ENGINE, WIRING, HOSES AND THE BELTS OF ALL COMPONENTS. NO DEFECTS OR THE SOURCE OFSDR QML2008F00007Starter Gen · disintegratedGENERATOR LIGHT ILLUMINATED JUST AFTER TAKE OFF FOR AN NVG TRAINING FLIGHT, WITH AN ELECTRICAL BURNING/OZONE ODOR IN THE COCKPIT. THE PILOT RETURNED TO BASE AND LANDED WITHOUT FURTHER INCIDENT. ELECTRICAL ODOR DISPERSED BEFORE LANDING. UPON INSPECTION OF THSDR 2008FA0000481Connector · contaminatedDURING CRUISE FLIGHT, THE ENGINE FIRE LIGHT ILLUMINATED. DURING THE DESCENT FOR A PRECAUTIONARY LANDING, THERE WAS NO SMOKE TRAILING THE AC AND THE ENGINE FIRE LIGHT EXTINGUISHED AND ILLUMINATED SEVERAL TIMES. AFTER SECURING THE AC UPON LANDING, THE PILOT INSDR 399505152008Garlock Seal · leakingAC WAS REQUESTED TO RESPOND TO THE AIRPORT FOR A SCENE RENDEZVOUS WITH THE AMBULANCE. AFTER DEPARTURE FROM HOSPITAL, THE MEDICAL CREW NOTICED A FUEL ODOR. THE FLIGHT WAS ABORTED AND AC LANDED AT MEDICAL CENTER WITH ALL AIRCRAFT INDICATIONS NORMAL. ON FINAL APPSDR CA080407006Pump · malfunctioned(CAN) DURING NORMAL FLIGHT DURING A BIRD TOWING OPERATION THE PILOT RECEIVED A BING INDICATING A FAILURE. AIRSPEED 60KTS, 1000 FT AGL, 170 FT LINE WITH BIRD, 45 MINUTES INTO FIRST FLIGHT OF THE DAY: " BING " HEARD IN HEADSET, HYD WARNING LIGHT OBSERVED, NOTICSDR CA080226003Annunciator · malfunctioned(CAN) ON A ROUTINE CHECK FOLLOWING START, THE ANNUNCIATOR LIGHT FOR GOV FAILURE (RED) FAILED TO ILLUMINATE WHEN THE ENGINE GOV SWITCH WAS MOVED FROM AUTO TO MANUAL. OTHER FUNCTIONS ASSOCIATED WITH MOVING TO MANUAL (SOLENOID, VEMD FAILURE CODES) OPERATED NORMALSDR CA080218002Heat Shield · chafed(CAN) WHILE REPLACING THE MO5, SEVERAL HOLES WERE NOTICED. THESE HOLES WERE DUE TO RUBBING AND WERE ONLY THROUGH THE OUTER LAYER OF THE HEAT SHIELD. (TC NR 20080218002)SDR CA080218005Thermocouple · grooved(CAN) AFTER LESS THAN 500 HRS THERMOCOUPLES FOUND WITH A GROOVE WORN INTO TIPS. THIS IS THE SECOND TIME THIS DEFECT HAS BEEN FOUND. (TC NR 20080218005)SDR CA080218006Thermocouple · grooved(CAN) AFTER LESS THAN 500 HRS THERMOCOUPLES FOUND WITH A GROOVE WORN INTO TIPS. THIS IS THE SECOND TIME THIS DEFECT HAS BEEN FOUND. (TC NR 20080218006)SDR CA080314021Engine · making metalON THE FIRST GROUND RUN OF THE DAY DURING GROUND WARM UP, A NOISE WAS EMITTED FROM THE ENGINE AND IMMEDIATLEY AFTER NOISE WAS HEARD THE ENGINE CHIP LIGHT ILLUMINATED. PILOT SHUT ENGINE DOWN. METAL PARTICLES WERE FOUND ON MOS CHIP PLUG AND SOME ON THE ELECTRISDR CA080208003Reduction Gb · making metal(CAN) DURING DAILY INSPECTION SMALL FLAKES WERE FOUND ON THE NON-MAGNETIC CHIP PLUG ON (MODULE) MO 5. ENGINE OIL WAS CHANGED OIL FILTER WAS CHANGED ALL MAG PLUGS INSPECTED AND CLEANED. A/C FLEW FOR 11.1 HRS AND SMALL FLAKES WERE FOUND ON SAME PLUG. A/C WAS GRSDR M7K2008F00001Freq Adapter · crackedDURING ROUTINE 100 HOUR INSPECTION, A CRACK IN THE BLUE BLADE ELASTOMER WAS FOUND ON THE T/E LWR IB SURFACE RADIATING FROM THE INSPECTION BORE. THIS CRACK HAD REACHED THE MM LIMITATION OF 10MM IN TOTAL LENGTH. THIS IS A VERY COMMON FAILURE FOR A PART WITH A SDR CA080115012Combust Chamber · fod(CAN) DURING A 600 HR ENGINE INSPECTION, A BORESCOPE INSPECTION WAS CONDUCTED IN THE COMBUSTION CHAMBER AREA( INTERNAL) AN OBJECT WAS DISCOVERED HANGING OUT INTO THE FLAME PATH JUST UPSTREAM OF THE POWER TURBINE. THE OBJECT WAS PROTRUDING FROM AN INNER COOLINGSDR 363011292007Hydromech Unit · leakingDURING PATIENT TRANSFER FLIGHT FROM OUTLYING HOSPITAL TO MAIN HOSPITAL, FUEL FUMES NOTED BY ALL CABIN OCCUPANTS. VENTS AND HEATER DUCTS MANIPULATED WITH NO DISCERNABLE EFFECT. SMELL OF FUEL FUMES INCREASED IN INTENSITY TO UNPLEASANT LEVELS UPON REDUCTION OF COSDR CA071206008Module · damaged(CAN) IN A CRUISE FLIGHT OR CLIMB POWER, THE AC ENGINE WOULD SURGE. THE AC WAS REMOVED FROM SERVICE FOR INSP. A CLOSE INSPECTION OF THE COVER THAT IS LOCATED OVER THE COMPRESSOR IMPELLOR, REVEALED A HOLE APPX. 4-5MM IN DIAMETER. THE MODULE 3 WAS REMOVED AND RSDR CA071123002Engine · malfunctioned(CAN) PILOT IN CRUISE FLIGHT, APPROX 2000 FEET, EXPERIENCED ENGINE PROBLEMS WITH ANNUNCIATOR INDICATIONS . PROCEEDED WITH SUCCESSFUL AUTOROTATION LANDING IN FIELD. REST IS UNDER INVESTIGATION (TC NR 20071123002)SDR CA071022004Switch · malfunctioned(CAN) DURING GROUND RUN THE FORCED IDLE FUNCTION OF THE TWIST GRIP WAS BEING TESTED WHEN IT WAS OBSERVED TO NOT ACCELERATE BACK TO FLIGHT IDLE WHEN RETURNED TO THE (VOL) POSITION. THIS FUNCTION IS USED TO SIMULATE ENGINE FAILURE DURING PRACTICE AUTOROTATION. SSDR CA080123004Spherical Stop · cracked(CAN) PROTRUDING RUBBER FOUND COMING OUT, IN THE MIDDLE OF STOP. (TC NR 20080123004)SDR CA080123005Freq Adapter · blistered(CAN) ON INSP OF MAIN ROTOR HEAD AT THE END OF THE DAY ENGINEER FOUND BLISTERS ON THE SIDE OF ONE FREQUENCY ADAPTER. BLISTERS WHERE FOUND TO BE BEYOND LIMITS: REPLACED ALL (3) ADAPTERS. (TC NR 20080123005)SDR CA070917009Servo Control · leaking(CAN) M/R SERVO REMOVED FROM RT POSITION DUE TO LEAKAGE. (TC NR 20070917009)SDR HEEA117053Terminal · corrodedENGINE FIRE WARNING LIGHT ILLUMINATED DURING START UP. CLEANED CORROSION FROM LT REAR FIRE DETECTOR WIRE TERMINALS IAW MM 26-10-10, ASB072760 AND EMM TASK 26-11-00-050-001. PERFORMED OPERATIONAL CHECK WITH PILOT. CHECKS GOOD.SDR HEEA116984Connector · malfunctionedAMBER GOV LIGHT ILLUMINATED PRIOR TO LANDING, UPON SHUTDOWN, ENGINE WOULD NOT REDUCE RPM FROM FLIGHT POSITION WHEN START SELECT SWITCH SET TO IDLE. ENGINE WOULD NOT RESTART. CLEANED CONNECTIONS AND REPLACED GOVERNOR FUSE, REPLACED FUSE HOLDER AND REPLACED ESDR HEEA116829Engine · making metalDEPARTED, ENROUTE, THE AIRCRAFT ENGINE OIL PRESSURE LIGHT STARTED INTERMITTENTLY TO COME ON AND OFF THEN STAYED ON CONTINOUS WITH A GONG SOUND FOLLOWING. REFERRED TO AS350B3 EMERGENCY GUIDE, REDUCED POWER, AIRSPEED, AND AT 2148 ADVISED OPERATIONS OF THE SITUSDR 2007FA0000606Shaft · wornDURING DAILY INSPECTION DISCOVERED EXCESSIVE PLAY IN HYDRAULIC PUMP DRIVE PULLEY. HYDRAULIC PUMP DRIVE WAS THEN REMOVED FOR FURTHER INSPECTION. IT WAS DISCOVERED THAT THE DRIVE PULLEY SHAFT HAD WORN EXCESSIVELY WHERE THE DRIVE BEARING HAD BEEN SPINNING AROUND SDR 2007FA0000607Pulley · wornDURING DAILY INSPECTION DISCOVERED EXCESSIVE PLAY IN HYDRAULIC PUMP DRIVE PULLEY. HYDRAULIC PUMP DRIVE WAS THEN REMOVED FOR FURTHER INSPECTION. IT WAS DISCOVERED THAT THE DRIVE PULLEY SHAFT HAD WORN EXCESSIVELY WHERE THE DRIVE BEARING HAD BEEN SPINNING AROUND SDR HEEA115978Indicator · failedRETURNED TO BASE, WHEN LANE 2 OF VEMD FAILED TO ILLUMINATE. REPLACEMENT OF VEMD CURED PROBLEM.SDR 3732060207Hydromech Unit · uncontrollableON A LOCAL TRANSPORT FLT , THE AIRCRAFT LAUNCHED AT 0930 P.M. & FLT TO PICK UP THE PATIENT WAS UNEVENTFUL. THE HOSPITAL IS A 15 MIN. FLT. WITH THE PATIENT ON BOARD, (5 PAX TOTAL), AT 2000 FT. MSL IN CRUISE FLT AT 110 KTS & 3 OR 4 MINUTES INTO THE FLT, A LOUD JSDR HEEA115520Switch · inoperativeAMBER GOV CAUTION LIGHT IN FLIGHT, RED GOV CAUTION LIGHT AFTER SHUTDOWN. MAINTENANCE REPLACED START SWITCH.SDR 2007FA0000447Hose · burstHIGH PRESSURE AIR CONDITIONER HOSE BURST.SDR CA070425005Bearing · worn(CAN) DURING DI, HYDRAULIC PUMP PULLEY WAS NOTICED TO BE LOOSE LATERALLY WHEN MOVED SIDE TO SIDE. WHEN MAIN ROTOR WAS ROTATED HYDRAULIC PUMP PULLEY WAS FOUND NOT SPINNING SQUARE AND THE HYDRAULIC BELT WAS OFF SET FROM CENTER. HYDRAULIC PUMP PULLEY WAS REMOVED SDR 2007FA0000263Solenoid · unserviceable(REF NR: 186AE-2007-I-0032) WHILE PERFORMING A CHECK OF THE TWIST GRIP SOLENOID, ENGAGED THE SOLENOID BY PLACING THE AUTO/MAN SWITCH TO MAN MODE FOR A TOTAL OF 10 MINUTES. AFTER THE 10 MINUTE PERIOD HAD ELAPSED, RETURNED THE AUTO/MAN SWITCH TO AUTO. AFTER 1SDR CA070213009Servo · leaking(CAN) SERVO FOUND LEAKING BY ENGINEER ON POST FLIGHT INSP. SERVO REPLACED WITH SERVICABLE UNIT. SERVO WAS SENT OUT FOR REPAIR. THE SERVO WAS OVERHAULED AND IS BEING SHIPPED BACK TO US FOR INSTALLATION. (TC NR 20070213009)SDR BAQA200700002Turbine Wheel · damagedDURING MAINTENANCE GROUND RUNS, STARTED NR 1 ENGINE AND NR 2 ENGINES TO PERFORM REQUIRED MAINTENANCE CHECKS AFTER INSPECTION OF AIRCRAFT AND ENGINES. SHUTDOWN ENGINES TO MAKE TAILROTOR BLADE WEIGHT CHANGE. ATTEMPTED TO START NR 1 ENGINE AND IT WOULD NOT TURN. SDR HCM2007F00000Chip Detector · activatedSHORTLY AFTER TAKEOFF OF A TOUR FLIGHT FROM AIRPORT, THE (ENGINE CHIP) WARNING LIGHT ILLUMINATED. PILOT PERFORMED A PRECAUTIONARY LANDING. INSP REVEALED 1 SMALL METAL SLIVER FOUND ON THE ENGINE FULL FLOW ELECTRICAL CHIP DETECTOR, ALL OTHER ENG DETECTORS INSPSDR 2007FA0000002Doubler · crackedFOUND CRACKS 2 EA ON LT OUTSIDE DOUBLER ASSY. 2 RIVETS WERE POPED OUT. DAMAGE VISIBLE ONLY AFTER REMOVAL OF TAIL ROTOR GEARBOX COWLING. FOUND DURING 100 HR INSP. (K)SDR CA061218004Engine · making metal(CAN) AIRCRAFT HAD AN INFLIGHT ENGINE CHIP LIGHT. PILOT LANDED AS SOON AS POSSIBLE. AIRCRAFT WAS LANDED UNDER ITS OWN POWER (NORMAL LANDING). PILOT THEN SHUT THE AIRCRAFT DOWN TO CHECK ALL ENGINE CHIP DETECTORS. HE FOUND METAL ON THE ELECTRIC CHIP PLUG, ENSDR 1114063927Doubler · crackedDURING ROUTINE PREFLIGHT/AFTER FLIGHT INSPECTION A CRACK WAS OBSERVED IN THE PAINT ON THE DOUBLER WHICH SURROUNDS THE ACCESS FOR THE TAILBOOM MOUNTED BATTERY AND WHICH AN ACCESS DOOR IS ATTACHED. A CLOSER INSPECTION REVEALED THAT THE DOUBLER HAD A CRACK THAT SDR PG9A111542Drive Shaft · out of toleranceDURING INSPECTION, THE DRIVE SPLINES OF THE T/R DRIVE SHAFT CENTER SECTION, WERE FOUND TO BE WORN AND OUT OF LIMITS SPECIFIED IN THE MM CH 65-11-00, 6-2. SHAFT WAS REPLACED WITH A NEW SHAFT.SDR CA070115008Engine · failed(CAN) AIRCRAFT FAILED POWER CHECK: ON INSPECTION ON WHY WE DID A BORESCOPE INSPECTION ON THE ENGINE AND FOUND THAT WE HAD A POSSIBLE TURBINE RUB. AS THIS ENGINE IS A RENTAL FROM MFG, WE CHANGED OUT THE MODULE 2 AND 3 AND SENT IT BACK TO THEM. THE NEW M02 AND MSDR HEEA111185Valve · odorFUEL ODOR IN CABIN DURING CLIMBOUT. MAINTENANCE REPLACED THE ADJUSTED VALVE ASSY.SDR BHH11QC789Manifold · cokedCOKING ON INJECTION MANIFOLD LABRYNITH SEAL TO INJECTION WHEEL. CAUSED NG SECTION LOCKUP AFTER SHUTDOWN, PRIOR TO START UP. FUEL SAMPLES AND DELIVERY SYSTEM UNDER INSPECTION AND PARTS SENT FOR EVALUATION. THIS PROBLEM ISOLATED TO AC OPERATIONS. (K)SDR BHH11QL787Seal · cokedCOKING ON INJECTION MANIFOLD LABRYNITH SEAL TO INJECTION WHEEL. CAUSED NG SECTION LOCKUP AFTER SHUTDOWN, PRIOR TO START UP. FUEL SAMPLES AND DELIVERY SYSTEM UNDER INSPECTION AND PARTS SENT FOR EVALUATION. THIS PROBLEM ISOLATED TO AIRCRAFT OPERATIONS. (K)SDR BHH11QL788Manifold · cokedCOKING ON INJECTION MANIFOLD LABRYNITH SEAL TO INJECTION WHEEL. CAUSED NG SECTION LOCK UP AFTER SHUTDOWN, PRIOR TO START UP. FUEL SAMPLES AND DELIVERY SYSTEM UNDER INSPECTION AND PARTS SENT FOR EVALUATION. THIS PROBLEM ISOLATED TO AIRCRAFT OPERATIONS. (K)SDR PG9A110603Pressure Switch · no testPRESSURE SWITCH PRODUCED NO INDICATION DURING TESTING./ REPLACED WITH SERVICEABLE PART.SDR 0727063707Hmu · malfunctionedDURING CRUISE FLIGHT AC CWP RED AND YELLOW GOV GOVERNOR LIGHT SEGMENTS ILLUMINATED AND ROTOR RPM BEGAN TO DECAY WITH A LOW ROTOR WARNING AS PILOT ENTERED AUTOROTATION. A NORMAL AUTOROTATION WAS COMPLETED WITH NO DAMAGE SUSTAINED BY THE AIRCRAFT. THE VEMD IND
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