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 CA140402010Circuit Card · failed(CAN) A ARNIC FAULT CODE WAS NOTED ON SHUTDOWN BUT NO OCCURRENCE ON SUBSEQUENT FLIGHT OR FAULT COULD BE FOUND, THOUGHT TO BE A SOFTWARE GLITCH AS THESE PHANTOM CODES SOMETIMES HAPPEN. SUBSEQUENTLY A OUT RANGE NR CODE STARTED TO APPEAR ON EVERY SHUTDOWN. THISSDR CA140318012Pulley · failed(CAN) HERE IS A REPORT ON THE HYD PUMP PULLEY FAILURE. AT THE LAST 100 HOUR THE HYD PUMP WAS INSPECTED IAW THE AMM. NO DISCREPANCIES WERE NOTED AT THIS TIME. AROUND THE LAST 50 HOURS OR SO AN INTERMITTENT TICK TICK SOUND WAS NOTED ON SHUT DOWN. NORMALLY THSDR QMLA2014010614001Gearbox · making metalAFTER STARTUP & WARM UP ON GND, FUEL LEVER MOVED FROM GROUND IDLE TO FLY POSITION. MGB CHIP LIGHT ILLUMINATED, PILOT BEGAN ENG SHUTDOWN. GRINDING NOISE HEARD COMING FROM MGB DURING SHUTDOWN. SUBSEQUENT INSPECTION BY MECHANIC FOUND HEAVY CONTAMINATION OF LOWSDR CA140115005Bearing · worn(CAN) BEARING INNER RACE SUPPORT WAS FOUND EXCESSIVELY WORN FROM BEARING ROTATION DURING 100MR INSPECTION. H4D PULLEY ASSY WAS REPLACED COMPLETELY BEFORE FURTHER FLIGHT. H4D PULLEY INNER RACE SUPPORT HAD APPROXIMATELY .0625 METAL LOSS/DETERIORATION FROM BEARSDR QMLA2013120813173Windscreen · crackedDURING PREFLIGHT INSPECTION, CREW FOUND A CRACK IN THE RT WINDSCREEN PROTRUDING FROM THE UPPER RT CORNER EXTENDING TOWARDS THE CTR OF THE WINDSCREEN. THE CRACK WAS APPROXIMATELY 8.5 INCHES LONG. IT IS BELIEVED THAT THE CRACK DEVELOPED AFTER THE PREVIOUS NIGHSDR CA131210003Fcu · failed(CAN) FUEL ODOR IN CABIN AREA, TROUBLESHOOTING FOUND FUEL IN P3 AIR TUBE, CAUSING FUEL TO GO INTO P3 HEATING SYSTEM. REPLACED WITH SERVICEABLE UNIT, TEST FLIGHT, NO FURTHER PROBLEM.SDR CA131210005Valve · leaking(CAN) VALVE FOUND TO BE LEAKING BEYOND LIMITS.SDR CA131210006Valve · leaking(CAN) REPLACED THIS VALVE, IT WAS THE 3RD ONE WE HAD REPLACED DUE TO LEAKAGE BEYOND LIMITS. ON GROUND RUN WITH TEST TOOL, WE FOUND THIS TO BE LEAKING BEYOND LIMITS. THE TREND WAS WITH AN O/H UNIT, IT WAS LEAKING. ALLOWABLE LEAKAGE RATE IS 3 DROPS PER MIN , SDR CA131210004Valve · leaking(CAN) FUEL ODOR IN CABIN, FOUND LEAKING FUEL AT VALVE AT A RATE OF 10 DROPS IAW MIN, ALLOWED 3.SDR QMLA2013081813118Blower · failedAIR CONDITIONER AFT EVAPORATOR BLOWER INTERMITTENT AND NOISY OPERATION. CREW SMELLED HOT FUMES AND HEARD NOISE FROM THE REAR OF ACFT WITH NO ACCOMPANYING SMOKE OR OTHER COCKPIT INDICATIONS.SDR CA130619002Wire · failed(CAN) WHILE INVESTIGATING A RADIO MASTER SWITCH MALFUNCTION, AVIONICS MASTER WOULD NOT TURN ON RADIOS UNLESS THE CONSOLE WAS TAPPED ON THE SIDE, A BURNT/OVERHEATED WIRE WAS NOTICED UNDER THE RADIOS AT THE BOTTOM OF THE GENEVA CONSOLE. WHILE REPAIRING THE WIRESSDR CA130610007Hose · leaking(CAN) INSTALLED NEW, THIS IS THE SECOND ONE WE HAVE HAD LEAK IN LESS THEN 10 HOURS. SHOWS LEAKS AROUND JACKET OF HOSE.SDR 2013FA0000318Line · leakingDEFECTIVE HOSE, PILOT NOTICED LOSS OF HYD FLUID ON POST FLIGHT.SDR CA130610008Hose · leaking(CAN) LEAKS AFTER 2 HOURS TIME SINCE NEW.SDR CA130513024Hose · failed(CAN) LINE WAS INITIALLY REPLACED AT 967.5.8. TO DATE 5 MORE OF THESE HOSES HAVE BEEN REPLACED EACH 1 FAILING.SDR CA130510004Potentiometer · intermittent(CAN) ON A FLIGHT JUST BEFORE A FUEL STOP THE YELLOW GOVERNOR LIGHT ILLUMINATED ON THE MASTER CAUTION PANEL. THE PILOT LANDED WITH OUT INCIDENT. AFTER DISCUSSION WITH THE PILOT ABOUT THE FAULT CODE AND THE POWER BEING CYCLED ON THE ACFT THERE WAS NO SIGN OF SDR QMLA2013050213062Audio Panel · failedPILOT WAS GOING INTO A HOVER DETECTED SOMETHING BURNING, AT THE SAME TIME LOST ALL RADIO AND ICS COMMUNICATIONS. PILOT PUT THE ACFT BACK DOWN AND NOTICED HIS PILOT ICS CIRCUIT BREAKER POPPED. AFTER EXTENSIVE TROUBLESHOOTING, MX AOG ORDERED A 2 AMP CIRCUIT BRESDR CA130429012Line · leaking(CAN) HYDRAULIC HOSE REPLACED WITH NEW HOSE AT 972.8 HRS. HELICOPTER LANDED AFTER TRAINING FLIGHT. THE PILOT NOTICED HYDRAULIC FLUID ON THE RT SIDE OF THE ACFT. ENGINEER CHECKED AND THE DECK WAS COVERED WITH HYDRAULIC FLUID. ACFT WAS GROUNDED WAITING ON REPSDR CA130424006Hose · leaking(CAN) NOUS AVONS INSTALLER UNE DEUXIEME HOSE A 3458. 6HRES ET A 3472.2 HRES LA HOSE A COMMENCER A FUIRE. VOIR LES DERNIERS RAPPORT RDS (TC# 20130424006)SDR CA130426004Magnetic Plug · failed(CAN) WHILE PREFORMING 30 INSPECTION OF THE MAGNETIC PLUGS ON THE ENGINE AS I WAS WIPING THE PLUG WITH A RAG I FELT SOMETHING "GIVE" I WHEN I LOOKED AT THE PART I SAW THE TIP OF THE MAGNETIC PLUG HAD BROKEN OFF. TO THE BEST OF KNOWLEGE THIS PART HASN`T BEEN DSDR CA130412013Hose · leaking(CAN) HYDRAULIC HOSES WERE REPLACED WITH NEW HOSES AT TTAF 949.9 HRS. HELICOPTER LANDED FOR FUEL AND SHUTDOWN. THE PILOT NOTICED A SMALL AMOUNT OF HYDRAULIC FLUID ON THE RT SIDE OF THE ACFT AND NOTIFIED THE ENGINEER. THE RT MGB COWLING WAS OPENED THE DECK WASDR JAPA2013FA0000214Line · leakingPILOT AND MECHANIC NOTICED LOSS OF HYD FLUID WHEN ACFT LANDED. FOUND DEFECTIVE HOSE.SDR 2013FA0000202Line · leakingDEFECTIVE HYD HOSE = MECHANIC NOTICED EXCESSIVE AMOUNT OF HYD FLUID.SDR JAPA2013FA0000182Hose · leakingDEFECTIVE HYDRAULIC HOSE.SDR 2013FA0000138Line · leakingPILOT LANDED AND LET PASSENGERS OFF AND NOTICE ALOT OF FLUID, MAINTENANCE WAS CALLED TO SITE AND DISCOVERED FLUID COMING OUT OF HOSE FITTING. FOUND DEFECTIVE HYDRAULIC HOSE.SDR 2013FA0000046Line · leakingDEFECTIVE HYD HOSE - AFTER 5.2 HRS TIME INSERVICE - PILOT LANDED, WHILE LETTING PASSENGERS OFF, NOTICED ALOT OF FLUID - MX WENT TO SITE AND DISCOVERED FLUID COMING OUT OF FITTING OF HOSE.SDR 2012FA0000831Line · leakingDEFECTIVE HUD HOSE, INSTALLED NEW TYPE HOSE AND AFTER 44.0 HOURS - IT STARTED LEAKING WHERE HOSE GOES INTO FITTING.SDR 2012FA0000830Line · leakingDEFECTIVE HYDRAULIC HOSE, INSTALLED NEW TYPE HOSES AND AFTER 24.0 HRS IT STARTED LEAKING.SDR QMLA2012091312151Unknown · odorDURING FLIGHT, PPROXIMATELY 5 MINUTES FROM DESTINATION HEARD A POP ON THE LT SIDE OF THE ACFT. OPERATIONS SEEMED NORMAL. ON LANDING, THERE WAS A FAINT RUBBER BURNING ODOR NOTED IN THE AIRCRAFT. DID A NORMAL SHUTDOWN, INSPECTED THE ACFT AND FOUND NOTHING UNUSDR QMLA2012082212141Gearbox · making metalTAIL GEARBOX CHIP LIGHT ILLUMMINATED DURING FLIGHT. 3 MM CHIP WAS FOUND.SDR HEEA20120811480Belt · failedDURING CLIMB OUT FROM HOSPITAL, STRONG FUMES AND LIGHT SMOKE ENTERED CREW CABIN. TURNED AIR CONDITIONER OFF, OPENED WINDOWS AND VENTS, DIVERTED, APPROXIMATELY 1 TO 2 MILES AWAY AND PERFORMED PRECAUTIONARY LANDING. MX REPLACED THE AIR CONDITIONER COMPRESSOR DSDR QMLA2012061712099Motor · failedIN CRUISE FLIGHT, AN UNUSUAL NOISE WAS HEARD IN CABIN FOLLOWED BY A BURNING ODOR. IAW THE RFM SUSPECTED ELECTRICAL COMPONENTS WERE TURNED OFF. ODOR AND NOISE DISSIPATED AFTER AIR CONDITIONING UNIT TURNED OFF. CONTINUED FLIGHT FOLLOWING PROCEDURES PUBLISHED SDR QMLA2012033012039Air Filter · overservicedIN CRUISE FLIGHT, CREW SMELLED WHAT WAS AT FIRST BELIEVED TO BE AN ELECTRICAL ODOR. CREW ELECTED TO MAKE A PRECAUTIONARY LANDING. MX REVEALED VISUALLY INSPECTED AND FOUND THE FDC AIR INTAKE FILTER HAD BEEN RECENTLY CLEANED AND SERVICED AND THE BLUE OIL HAD BESDR CA120330006Support · cracked(CAN) RT UPPER REAR SLIDING DOOR SUPPORT FOUND CRACKED DURING AIRFRAME 12 YR CALENDAR INSPECTION. THE CRACK WAS NOT VISIBLE UNTIL FAIRING THAT ENCLOSES THE PART WAS REMOVED TO FACILITATE DOOR REMOVAL. PART IS CRACKED IN 2 LOCATIONS. ONE CRACK IS .550" LONG SDR QMLA2012011812007Battery Box · crackedDURING 200 HOUR ICA INSPECTION OF THE TAILBOOM MOUNTED BATTERY, FOUND A CRACK APPROX 1.5 INCHES IN LENGTH IN BATTERY TRAY SUPPORT.SDR RMXA201112288980Wire · shortedUPON LANDING, THE AFT OVERHEAD LIGHT PANEL STARTED TO FLICKER ON AND OFF THEN THE ODOR AND SMOKE WAS IN CABIN. DISASSEMBLED THE OVERHEAD LIGHT PANEL AND NOTED THAT THE SOCKET FOR THE BULB HAD CRACKED. THERE WAS EVIDENCE OF OVERHEATING IN THE SOCKET DUE TO THESDR CA110930019Starter Gen · failed(CAN) WHILE BIRD TOWING WITH STC SH04-57 INSTALLED, THE GEN WENT OFF LINE. THERE WERE REPORTS OF A BURNING ODOR IN THE CABIN, FOLLOWED SHORTLY BY THE GEN FAIL WARNING. THE PILOT MADE AN UNSCHEDULED, UNHURRIED LANDING. DISCOVERED THE STARTER GEN HAD TWO BURNSDR CA110816004Control Lever · loose(CAN) THE UPPER BUSHING ON THE TAIL ROTOR LEVER BECAME LOOSE. INSTALLED A NEW LEVER WITH NO FURTHER DEFECTS.SDR QMLA2011051711057Search Light · malfunctionedTHE LEFT SEARCHLIGHT WILL NOT SHUT OFF. THIS HAS BEEN A RECURRING EVENT FOR THIS PARTICULAR HELICOPTER OVER THE PAST 3 MONTHS. THERE HAS BEEN 3 SEARCHLIGHTS REPLACED. THE TEAR DOWN REPORTS STATE THAT A SOLID STATE RELAY HAS BEEN REPLACED TO RETURN THE LIGHTSDR RMXA308852Potentiometer · intermittentACFT INDICATED AN AMBER GOV LIGHT IN FLIGHT, WITH NO ENGINE, MAIN ROTOR, OR TAIL ROTOR FLUCTUATIONS IN FLIGHT. TECH RETRIEVED AN INTERMITTENT FAILURE CODE 122 FOR THE COLLECTIVE POTENTIOMETER. WHEN THE ACFT WAS POWERED BACK UP AFTER LANDING THE AMBER GOV LIGHSDR QMLA2011020311019Window · crackedTHE PILOT NOTICED ON A PREFLIGHT CHECK A CRACK IN THE RT REAR PASSENGER DOOR MIDWAY UP ON THE FWD EDGE. THE CAUSE OF THE CRACK IS NOT KNOWN AT THIS POINT, HOWEVER, THE TEMPERATURES IN THE AREA WERE BEEN ABNORMALLY COLD WHEN THIS HAPPENED. THE WINDOW WAS REPLSDR QMLA2011011511009Brushes · wornDURING STARTER GENERATOR 300HR INSP FOUND BRUSH RIVET MISSING AND TENSION SPRING BROKEN. SECOND OCCURANCE OF BROKEN BRUSH, RIVET AND SPRING IN 5 MONTHS 142+12HRS, SN 10938XL2 TIME SINCE O/H 676+16 TIME SINCE REPAIR 142+12 PREVIOUS OCCURANCE SN 10260 8-24-2010SDR QMLA2011010111002Shutoff Valve · leakingSHORTLY AFTER TAKEOFF THE MED CREW NOTICED A STRONG FUEL SMELL IN THE CABIN AND COULD SEE LIQUID ON THE BACK CLAMSHELL WINDOW. THE PILOT IMMEDIATELY RETURNED TO THE DEPARTURE AIRPORT AND AWAITED THE MECHANIC TO ARRIVE. THE MECHANIC TROUBLESHOT THE FUEL LEAK SDR CA101105005Nozzle · damaged(CAN) THE END OF JET TUBE NOZZLE CONTACTED THE M/R BLADE DURING GROUND RUN WITH THE ENGINE COWL OPEN IN THE FIRST/LOWEST POSITION. KIT NR 0617-71-03 INSTALLED IAW SB 0617-71-00 .03 0 TO REPLACE ECL SAND FILTER. WITH THE COWLING OPEN, IN THE FIRST POSITION, TSDR CA101018015Pump · wornIN FLIGHT, HYD SYS FAILURE DUE TO DAMAGED SPLINES ON HYD PUMP, PN-704A34310006 AND DRIVE COUPLING, PN-704A33635002. SPLINES FOUND TO BE SEVERLY WORN AND UNABLE TO ENGAGE FOR PUMP OPERATION. UNSURE OF REASONING FOR SPLINE FAILURE AT THIS POINT.SDR CA100816001Hmu · malfunctioned(CAN) ON FINAL APPROACH TO A CONFINED AREA, PILOT HEARD LOW ROTOR WARNING HORN FOLLOWED BY DROOP IN MAIN ROTOR SPEED. EMERGENCY AUTO ROTATION WAS EXECUTED INTO THE LANDING AREA. UPON TOUCHING THE GROUND ELT WAS SET OFF. INITIAL MAINTENANCE INVESTIGATION INDSDR CA100429007Bushing · loose(CAN) DURING A ROUTINE INSPECTION, THE LEVER ARM WAS REMOVED FOR AN UNRELATED PURPOSE. WHEN THE ARM WAS REMOVED THE BUSHINGS WERE NOTED AS BEING LOOSE. NORMALLY BONDED IN, BOTH BUSHINGS WERE ABLE TO FREELY MOVE. A NEW LEVER ARM WILL BE INSTALLED.SDR RMXA418TY21610Skin · crackedAN 38MM CRACK IN THE UPPER FIN WAS DISCOVERED DURING A DAILY INSP. THE CRACK IS LOCATED ON THE INNER LT UNDERSIDE LOWER L/E RIB STARTING FROM A RIVET AND PROGRESSING AFT ALONG THE RADIUS. ACFT WAS PLACED OUT OF SERVICE AND THE UPPER FIN REPLACED.SDR QMLA2009111209039Valve · leakingON FINAL FOR LANDING AT HOSPITAL PAD, MEDICAL CREW MENTIONED STRONG FUEL ODOR. AFTER SAFE LANDING AND SHUTDOWN, POSTFLIGHT DISCOVERED SHEEN BELOW NR 2 ENG COWLING, FURTHER INSP IN ENG COMPARTMENT DISCOVERED APPARENT FUEL LEAK WITH NOTICEABLE DRIPPING AFT OF THSDR CA090806013Wire Harness · unknownWHEN ACFT POWERED UP DURING SERVICING A FLASHING AMBER GOV LIGHT DISPLAYED ON ANNUNCIATOR PANEL. FAILURE CODE 123 CHECKED INDICATING "T4 FADEC L", GOING FURTHER INTO FADEC DATA -FAIL 1 CODE WAS 0020 (RAW T4.5 FAILURE) WAS DISPLAYED AND T4 INDICATION IN FADEC
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