Turbomeca ARRIEL-2B1
Service difficulty reports · 757
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 = 'ARRIEL2B1' 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 = 'ARRIEL2B1' 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 QMLA2013101113142Fire Detector · shortedDURING APPROACH, PILOT HAD AN ENGINE FIRE INDICATION ON CAUTION PANEL. PERFORMED A NORMAL LANDING AND ACFT TAKEN OUT OF SERVICE. HAD BEEN AN ISSUE ON A PRIOR FLIGHT, TROUBLESHOT AND PARTS REPLACED WHICH WERE THOUGHT TO CORRECT THE PROBLEM. REPLACED THREESDR QMLA2013100713144Circuit Card · malfunctionedDURING APPROACH, PILOT HAD AN ENGINE FIRE INDICATION ON THE CAUTION PANEL. PERFORMED A NORMAL LANDING AND TAKEN OUT OF SERVICE. REPLACED ASU1 CARD, CHECKED WIRING IAW WIRING MANUAL, AND PERFORMED CHECK FLIGHT. COULD NOT DUPLICATE ISSUE, RETURNED TO SERVICE.SDR CA131001011Housing · damaged(CAN) DURING INITIAL INSTALLATION THE UPPER AND LOWER HALVES ARE MATED TOGETHER WHILE BEING INDIVIDUALLY FITTED TO EACH ACFT. THE UPPER HOUSING HAS A SHORT EXTENDED LIP AT HE AFT OF THE HOUSING TO ALLOW FOR THE ADJUSTMENT FOR THE CUSTOM FIT. THE EXCESS APPROSDR QMLA2013092513143Fire Warning · false activationDURING APPROACH, PILOT HAD AN ENGINE FIRE INDICATION ON THE CAUTION PANEL. PERFORMED A NORMAL LANDING AND TAKEN OUT OF SERVICE. CLEANED CONNECTORS ON ENGINE DECK AND ASU CARD. COULD NOT DUPLICATE.SDR QMLA2013091913135Skin · crackedDURING A 100 HOUR INSPECTION, A CRACK WAS FOUND IN THE SKIN ADJACENT OF THE RT CANOPY WEB. THE SKIN CRACK HAS APPROXIMATELY 30MM VISIBLE LENGTH PARALLEL TO INBD EDGE OF THE RT CANOPY WEB. IT TURNS OTBD ALONG THE TOP RADIUS OF THE CANOPY WEB. IT IS POSSIBLE THSDR QMLA2013091613134Connector · contaminatedDURING CRUISE FLIGHT PILOT REPORTS HEARING GONG AND "ENG P" LIGHT ILLUMINATED. INSPECTIONS END WITH POSITIVE RESULTS AND RELEASED ACFT FOR SERVICE. ON SECOND LEG OF THE RETURN THE GONG SOUNDED WITH NO ASSOCIATED LIGHT WITH AN INCREASE IN INTERVAL ON APPROACHSDR CA131010008Fuel Tank · cracked(CAN) CUSTOMER REPORTED A CRACK IN THE SIDE PANEL OF THEIR AUXILIARY FUEL TANK AND WERE ADVISED TO RETURN FOR EVALUATION. UPON INSPECTION OF INTERIOR OF TANK ASSY IT WAS FOUND SEVERAL WELDS ATTACHING THE SIDE PANEL TO THE SUPPORTING FRAMES WERE BROKEN. ALSO,SDR QMLA2013091213131Mount · crackedDURING SCHEDULED INSPECTION OF HORIZONTAL STABILIZER MOUNTS, FOUND RT LOWER MOUNT CRACKED, ACROSS ROW OF BOLT HOLES. ACFT OUT OF SERVICE.SDR CA130826016Hose · leaking(CAN) DURING THE ALF INSPECTION IT WAS NOTICED THAT THE HYDRAULIC TANK HAD LOST 50 PERCENT OF IT FLUID. UPON FURTHER INVESTIGATION THE LOSS OF FLUID WAS FROM THE HYDRAULIC PRESSURE LINE, PN 70A34-412-251. NEW LINE WAS REPLACED AND ACFT RETURNED TO SERVICE.SDR QMLA2013082313124Gearbox · making metalPILOT REPORTED GEARBOX CHIP LIGHT ON APPROACH. AFTER LANDING, REMOVED AND INSPECTED CHIP DETECTOR AND FOUND CHIP DETECTOR COVERED WITH SMALL CHIPS. AFTER LOOKING IN THE MM FOR LIMITS, FOUND THE AMOUNT OF CHIPS EXCEEDED LIMITS. GEARBOX WAS REMOVED FROM SERVICE.SDR CA130821001Hose · leaking(CAN) FOUND HYDRAULIC FLUID ALL OVER THE TRANSMISSION DECK ON PREFLIGHT. GROUND RUN CONFIRMED LEAKING HYDRAULIC HOSE, ONLY 224,5 HRS TSN.SDR QMLA2013080613111Carrier Assy · crackedDURING A ROUTINE AIRWORTHINESS CHECK, MECHANIC PERFORMED A VISUAL INSPECTION OF THE ACFT. ON INSPECTING THE HORIZONTAL STABILIZER AREA, A CRACK WAS NOTICED ON THE RT LOWER CARRIER ATTACH FITTING. REPLACED CRACKED CARRIER.SDR QMLA2013080513109Battery · dischargedPILOT REPORTED THAT HE BEGAIN TO LOSE ELECTRICAL POWER TO INSTRUMENTS AND INSTRUMENT LIGHTS, PILOT PREFORMED A PRECAUTIONARY LANDING. BATTERY WAS FOUND TO ONLY HAVE 16 VOLTS.SDR QMLA2013080513112Bulkhead · crackedRIGHT FWD FLOOR BULKHEAD CRACKED AJACENT TO RT FWD CANOPY FRAME ATTACH WEB.SDR QMLA2013072913103Elt · malfunctionedELT ACTIVATED IN FLIGHT AND WOULD NOT RESET. IT ALSO ACTIVATED ON THE BENCH AFTER THE BATTERY WAS REPLACED AND RESET, DURING THE INSPECTION RECEIVED TWO DIFFERENT CODES, A G SWITCH LOOP OPEN FALURE AND NO NAVIGATION DATA PRESENT. THESE CODES WERE AT DIFFERESDR QMLA2013072513102Compressor · seizedAIR CONDITIONER COMPRESSOR PULLEY BEARING AND CLUTCH OVERHEAT WITH PULLEY BEARING SEIZING. DURING TROUBLESHOOTING DETERMINED AIR CONDITIONER CONDENSOR BLOWER INTERMITTENT OPERATION.SDR QMLA2013071713101Unknown · smokeDURING FLIGHT, WITH FAN SWITCH ON, SMOKE CAME OUT OF VENT ON TOP OF GLARESHIELD. WHEN FAN WAS TURNED OFF THE SMOKE STOPPED. REMOVED AND INSTALLED INSTRUMENT PANEL SHROUD IAW AMMS 050-0416. INSPECTED ALL INSTRUMENTS AND WIRE HARNESSES. NO INDICATIONS OF OVERSDR QMLA2013071413098Evaporator · overheatedABNORMAL ODOR IN CABIN, POSSIBLE ELECTRICAL RELATED, FOUND ODOR IN THE NOSE OF THE ACFT AROUND THE FWD EVAPORATOR, FOUND TRIPPED CIRCUIT BREAKER FOR THE FWD EVAPORATOR. APPEARS IT WAS OVERHEATED "OHMD" OUT SEEMS TO BE INTERNALLY SHORTED.SDR QMLA2013060613077Warning Light · illuminatedTWO MINUTES OUT, AMBER GOVERNOR CATUION LIGHT ILLUMINATED. EXECUTED AN UNEVENTFUL PRECAUTIONARY LANDING ON THE HOSPITAL AUXILLARY LANDING AREA ADJACENT TO THE MAIN HELIPADSDR QMLA2013060513075Unknown · odorTWELVE MINUTES INTO A FIFTEEN MINUTE FLIGHT, THE PILOT REPORTED THAT HE DETECTED A FAINT "HOT WIRING" ODOR COMING FROM THE FORWARD PORTION OF THE COCKPIT, NO AMP OR VOLTAGE FLUCTUATIONS WERE NOTED DURING THAT TIME. VISUALY INSPECTED THE WIRING FOR THE AVIONICSDR QMLA2013060313074Blower Motor · inoperativeRETURNING TO BASE AFTER A PREFLIGHT, ONCE ESTABLISHED ON LOCAL AIRPORT GPS PRACTICE APPROACH, AT A DISTANCE OF ABOUT 5 NM, ANNOUNCED THAT NO AIR COMING OUT OF AFT A/C CABIN BLOWERS. DETECTED AN ELECTRICAL ODOR IN CABIN. TROUBLESHOT BY TURNING A/C OFF & SWITSDR QMLA2013052713071Control Unit · failedNR 1 ENGINE DEGRADE & FADEC FAILURE CAUTION. ENGINE FAILURE, ATTEMPTING MANUAL THROTTLE BY PILOT DURING FLIGHT, TROUBLESHOT SYSTEM FOUND DECU/FADEC HARD FAILED.SDR QMLA2013051313066Warning Light · false activationAFTER LANDING, THE FIRE LIGHT ILLUMINATED BRIEFLY THEN EXTINGUISHED. CHECKED CONTINUITY OF FIRE DETECTORS REF AMM 26-11-00, 6-2, CHECKED WIRING REF WDM 26-11, CHECKED AND APPLIED STABILANT 22 TO PLUG 22 DELTA, CHECKED 38W HOLD STRIP, CHECKED 40W RELAY AND APPSDR CA130516012Bearing · loose(CAN) DURING INSPECTION IT WAS NOTED THE BEARING ON THE LOAD COMPENSATOR WAS LOOSE AND COULD BE PUSHED OUT OF THE COMPENSATOR BODY. THE BEARING IS STAKED INTO POSTION AT THE MFG AND THE MARKINGS FROM THE PROCEDURE WERE ON THE BODY, BUT THE STAKING WAS NOT SUFSDR QMLA2013050813065Unknown · odorDURING CRUISE, ODOR OF JET FUEL WAS NOTICED. DURING THE FIRST AND SECOND LEG OF THE FLIGHT NO FUMES WERE NOTED IN THE CABIN. THE FUMES WERE FAINT INITIALLY, BUT NOTICED THAT THE FUMES WERE TO BECOME MORE PUNGENT.SDR CA130509004Elt · failed(CAN) ELT FAILED POWER OUTPUT TEST FOR 121.5 MHZ AND 406 MHZ. UNIT FLASHED CODE INDICATING LO RF POWER. POWER CONFIRMED WITH BEACON TEST EQUIPMENT.SDR QMLA2013041313052Warning Light · false activationDURING THE LANDING PHASE OF FLIGHT THE PILOT RECEIVED AN AUDIBLE GONG INDICATION. APPROX 10 SECONDS LATER THE ENGINE FIRE WARNING INDICATOR ILLUMINATED ON THE CAUTION WARNING PANEL. AT THIS TIME THE PILOT OBSERVED THAT ALL OTHER ENGINE INDICATIONS WERE WITHINSDR QMLA2013041213051Hose · leakingPILOT DISCOVERED HYD FLUID LEAKEAGE IN TRANSMISSION AREA UPON POST-FLIGHT VISUAL CHECK. SQUEEZING THE HOSE BY HAND REVEALED FLUID REVEALED ADDITIONAL FLUID LOSS. THIS HYD LINE CONNECTS TO THE AFT OTBD PORT ON THE FILTER MODULE. THIS PORT IS MARKED WITH A "U".SDR CA130328007Pulley · worn(CAN) PULLEY OUTSIDE DIAMETER WORN BEYOND LIMITS. BEARING SHOULD BE A FRICTION/PRESS FIT, INSTALLED WITH TEMPERATURE DIFFERENTIAL, AND IS NOT.SDR M7KA2013032500001Switch · unserviceableDURING CRUISE, . PILOT DETECTED AN ELECTRICAL ODOR, SLIGHT & DEVELOPED TO A STRONG ODOR WITH SOME MODERATE SMOKE DEVELOPMENT. FOLLOWED FLIGHT MANUAL EMERGENCY PROCEDURES, PILOT USED EMERGENCY ELECTRICAL SYS BREAKAWAY WIRED CUTOUT SWITCH TO CUT OFF ALL ELECTRSDR QMLA2013030113030Spar · crackedTAILROTOR ASSY SPAR CRACKED INTERNALLY. FOUND DURING MX.SDR QMLA2013020813024Wire Harness · faultyWITHIN A COUPLE OF MINUTES OF DEPARTING BASE, RECEIVED AN INDICATION OF FLI FAIL ON THE VEMD. RETURNED TO BASE WITHOUT INCIDENT. MECHANIC FOUND A FAULTY T4 HARNESS.SDR CA130203001Igniter Box · failed2 CHANNEL IGNITION HAD APPARENTLY FAILED ONE CHANNEL SINCE BOTH WERE INSPECTED DURING THE SCHEDULED INSPECTION 600 HRS. WHEN 2ND CHANNEL FAILED THE ENGINE WOULD NOT START.SDR QMLA2013012913017Engine · contaminatedNORMAL DEPARTURE, AT APPROX 400' AGL; ABOUT 5 MINUTES AFTER TAKEOFF, OPENED VALVE FOR THE WINDSHIELD DEMIST. AT 500 FT AGL AND BEGAN A TURN FOR A DOWNWIND DEPARTURE, AN ODOR WAS BECOMING OBVIOUS. IN LESS THAN ONE MINUTE, FUMES BECAME OBNOXIOUS. COULD SEE SSDR QMLA2013012913018Warning Message · illuminatedTEN MINUTES INTO A FLIGHT, ENGINE OIL PRESSURE ENTERED YELLOW AREA. SLIGHTLY LOWERED THE COLLECTIVE TO RELIEVE PRESSURE. NEEDLE CONTINUED TO CLIMB AND PROCEEDED INTO RED. SHORTLY AFTER REACHING MAXIMUM INDICATION AVAILABLE ON THE GAUGE, GAUGE DISSAPPEAREDSDR QMLA2013012213009Warning Light · false activationAMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT. MADE PRECAUTIONARY LANDING. MECHANIC WAS UNABLE TO REPRODUCE FAULT AFTER INSPECTION OF ACFT. THE ACFT WAS RETURNED TO SERVICE WITH NO FAULTS FOUND.SDR M7KA201301301125Bearing · failedON SHORT FINAL TO LANDING, ACFT CAUTION WARNING PANEL ENGINE CHIP LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN NORMALLY, INSPECTION OF THE CHIP DETECTORS, METAL WAS FOUND THAT APPEARED TO BE MORE THAN TYPICAL. CLEANED THE CHIP PLUGS, A 10 MINUTE PENALTY GROUND SDR VY1R2013FA0000048Servo · leakingDURING INSPECTION, MX FOUND THE TAIL ROTOR SERVO HAD DEVELOPED A STATIC LEAK. REPLACED IAW AMM 67-33-00.SDR CA130129002Bearing · cracked(CAN) LAMINATED BEARINGS INSPECTED IAW EASA AD 2012-0217E, SEPARATION NOTICED ON THE INBD AND OTBD AREA`S OF EACH HALF BEARINGS.SDR QMLA2013011413006Windshield · crackedBIRD STRIKE IN FLIGHT, CAUSED 8" CRACK TO COMPOSITE NOSE AREA OF ACFT ON PILOT SIDE BETWEEN PILOT WINDSHIELD AND CENTER WINDSHIELD.SDR QMLA2013122513001Windshield · crackedRIGHT WINDSCREEN CRACKED. THE CRACK IS ABOUT HALF WAY UP THE WINDSHIELD ON THE RT SIDE AT THE FRAME. IT EXTENDS ABOUT .7500 THE WAY ACROSS.SDR 2013FA0000000Door · openRIGHT TRANSMISSION DOOR OPENED IN FLIGHT. STRIKE ON THREE MAIN ROTOR BLADES.SDR CA130503004Gearbox · fod(CAN) WHILE CHANGING CHIP PLUG RECEPTACLE, ENGINEER USED SYRINGE TO SUCK REMAINING OIL OUT OF GEARBOX WHEN HE VIEWED IN THROUGH RECEPTACLE HOLE WITH FLASHLIGHT HE DISCOVERED A WASHER UPON RETREIVING WASHER, HE DISCOVERED THAT IT WAS BENT AND APPARENTLY HAD GONSDR QMLA2012122812199Acm · seizedSEIZED AC COMPRESSOR DAMAGED THE BELT CAUSING BURNED RUBBER SMOKE TO CIRCULATE INTO THE CABIN. EXECUTED AN EMERGENCY LANDING. NO INJURIES ON DAMAGED FOUND OTHER THAN THE FREON AC COMPRESSOR AND DRIVE BELT.SDR QMLA2012121712192Valve · dirtyCREW SMELLED BURNED POPCORN ODOR IN CABIN ON TAKEOFF, INSPECTED FOUND THAT SODA HAD BEEN SPILLED ON PILOTS FLOOR, RAN DOWN ON HEATER KNOB AND ON HEATER (HOT) VALVE IN CABIN FLOOR VALVES. CLEANED AND REINSTALLED PANELS.SDR CA130103008Engine · making metal(CAN) INFLIGHT ENGINE CHIP LIGHT. LANDED WITHOUT FURTHER EVENT.SDR QMLA2012112412188Stop · crackedLEFT SLIDING DOOR OPENED IN FLIGHT. LANDED TO SHUT THE DOOR. AFTER LANDING THE DOOR STOP WAS FOUND TO BE CRACKED. NO OTHER DAMAGE WAS FOUND. A NEW DOOR STOP INSTALLED. ACFT RETURNED TO SERVICE.SDR CA121219003Pressure Switch · failed(CAN) DURING SCHEDULED INSPECTION, ENGINE FUEL FILTER PRE BLOCKAGE SWITCH BENCH TESTED AND FOUND TO BE STUCK IN THE OPEN POSITION. NO WARNING TO FLIGHT CREW OF FUEL FILTER BLOCKAGE. DURING THE BENCH CHECK OF THE SWITCH WITH PSI APPLIED TECHNICIAN TAPPED SWITSDR QMLA2012111112178Warning Light · intermittentWHILE IN CRUISE FLIGHT, STEADY AMBER GOVERNOR LIGHT ILLUMINATED. PERFORMED A PRECAUTIONARY LANDING AT HOME BASE. TROUBLESHOT SOLID AMBER GOVERNOR LIGHT IAW MM. DETERMINED FAULT WAS "INTERMITTENT" IAW 71-00-06-817-808. COULD NOT GET DUPLICATE FAILURE ON TSDR QMLA2012110712174Chip Detector · false activationENIGINE CHIP LIGHT ILLUMINATED IN FLIGHT. INSPECTED ELECTRIC CHIP PLUG, STRAINERS, MAGNETIC CHIP PLUGS, OIL FILTER, ENG OIL FILTER FACET, N2 SENSORS FOR METAL NONE DETECTED, COMPLIED WITH CHECK LIST 71-02-07, 280-802-A01. NO DEFECTS NOTED, IAW MM.
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