Turbomeca ARRIEL-1B
Service difficulty reports · 807
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 = 'ARRIEL1B' 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 = 'ARRIEL1B' 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 2009FA0000334Line · looseDURING ROUTINE INSP FOUND P2 LINE LOOSE AT FUEL CONTROL. THE B-NUT WAS STILL TIGHT. APPLIED LIGHT UPWARD FORCE AND LINE PULLED OUT OF B-NUT. REMOVED B-NUT AND FOUND REMAINDER OF BROKEN FLARE. SLEEVE WAS ALSO SEIZED IN B-NUT. RECOMMEND PERIODIC REMOVAL ANDSDR CA090318001Engine · fod(CAN) PILOT WAS TAKING OFF FROM BASE, REPORTED HEARING ODD WHINING FROM ENGINE DURING TAKEOFF AND POWER CHANGES, ABORTED TAKEOFF AND RETURNED TO STAGING. OPENED ENGINE COWL, NOTED ALUMINUM SHAVINGS ON ENGINE DECK. VISUAL INSP IDENTIFIED THE COMPRESSOR WASH UNISDR CA090315001Structure · corroded(CAN) UPON ROUTINE INSP, IT WAS FOUND THAT THE RT CABIN RESONATOR STRUCTURE WAS CORRODED AT THE INNER ATTACHMENT FLANGE TO THE POINT THAT BUCKLING OF THE OUTER ATTACHMENT PLATE HAD OCCURED. THE ASSY WAS REMOVED FROM THE ACFT. IT WAS FOUND THAT THE OUTER ATTACHSDR CA090227011Cone · separated(CAN) A/C WAS IN CRUISE AT 5000 FT WHEN A LOUD POP WAS HEARD ACCOMPANIED BY A SINGLE TORQUE OSCILLATION. PILOT REDUCED HIS POWER TO LAND. A BURNING OIL ODOR WAS DETECTED ON THE DESCENT. THE PILOT LANDED NORMALLY WITH FULL POWER AVAILABLE ON LANDING. INVESTIGATSDR CA090204006Servo · faulty(CAN) SERVO WAS REMOVED FROM ACFT DURING A 12 YEARS INSP FOR OVERHAUL. SERVO WAS SENT TO FOR O/H. SERVO INSTALLED ON THE ACFT, FOLLOWING FLIGHT CONTROL GROUND CHECK WITHOUT HYD, SERVO DID NOT HOLD IN LOCK POSITION. SERVO WAS SENT BACK AND NO FAULT WAS FOUND. SDR CA081119003Bearing · blocked(CAN) OIL WAS COMING OUT OF TURBINE EXHAUST AND M03 BEARING VENT TUBE ON START UP. DISASSEMBLED THE ENGINE AND FOUND M03 REAR BEARING CAKED WITH BURNED OIL. M03 REAR BEARING OIL RETURN TUBE PARTIALLY BLOCKED WITH BURNED OIL.SDR CA080730005Fuel Control · failed(CAN) FLUCTUATION OF NG (+/- 2 PERCENT) IN CRUISE FLIGHT. ACFT LANDED AT THE BASE NORMALLY. ENGINE INSPECTED. RUN-UP CARRIED OUT, NG FLUCTUATION CONFIRMED ON THE GROUND (82.5 TO 84.5 PERCENT), NR FLUCTUATION ON THE GROUND (374 - 380). FCU REPLACED (PART REMOVESDR ML62008F00000Filter · cloggedA REDUCED FUEL FLOW CONDITION DEVELOPED AS THE ELECTRIC FUEL BOOST PUMP BEGAN TO DISINTEGRATE AS IT NEARED IT TBO (APPROX 70 HRS TO REPLACEMENT). INTRODUCING METAL AND CONTAMINATING THE AIRFRAME FUEL FILTER, THIS IS A BYPASS CONDITION AND PROVIDED UNFILTERED SDR CA080523005Transceiver · inoperative(CAN) RADIO WOULD NOT TRANSMIT, REMOVED AND INSTALLED SERVICABLE RADIO.SDR CA080619008Pump · inoperative(CAN) BOOST PUMP FAILED IN FLIGHT, MOTOR STILL TURNING BUT NOT CREATING PRESSURE. SUSPECT SHEARED SHAFT OR DRIVE.SDR KNK2008F00001Manifold · cokedFUEL COKING MATERIAL IN THE FUEL MANIFOLD LABYRINTH SEAL AREA CAUSED SEIZURE BETWEEN MANIFOLD AND FUEL INJECTION WHEEL. ENGINE WILL NOT ROTATE. (K)SDR CA080415006Blade · damaged1ST STAGE TURBINE WHEEL BLADE LEADING EDGE DAMAGE IN ZONE 2 ON A TOTAL OF 8 BLADES. THE DAMAGE WAS CAUSED BY THE SEMI-CONDUCTOR OF THE IGNITER, P/N 9550175400, THAT DISLODGED ITSELF FROM THE HOUSING. THIS WAS FOUND DURING A SCHEDULED 100/150 HR ENGINE INSPECTSDR CA080406001Line · brokenTUBE WAS DISCOVERED CRACKED AND SEPARATED FROM FLARE AT P2 TAP END DURING ROUTINE INSPECTION. ORIGINALLY, BLACK DEPOSITS WERE NOTICED AT B-NUT AND WHEN DISASSEMBLED, FOUND COMPLETE FAILURE OF TUBE FROM FLARE END. CLOSE TOLERANCE FIT OF TUBE PROBABLY PROHIBITSDR CA080320011Lock · cracked(CAN) CRACKED MAIN ROTOR MAST LOCK.SDR CA080417010Seal · departed(CAN) CHIN BUBBLE WINDOW AND SEAL DEPARTED THE AIRCRAFT IN CRUISE FLIGHT. AIRCRAFT WAS LANDED AND CHECKED FOR DAMAGE, NOT FOUND. REVIEW INDCATED THAT THE WINDOW WAS REMOVED FOR MAINT BEFORE THE OCCURANCE. WILL FOLLOW UP FOR SPECIFIC PN (TC NR 20080417010)SDR 183801212008Solenoid · leakingAT APPROX 01:30 MDT, MEDFLIGHT 2 WAS ATTEMPTING TO DEPART SCENE WITH PATIENT. PILOT DETECTED ODOR OF SMOKE IN THE COCKPIT AND ABORTED TAKEOFF. PILOT SECURED ENGINE AND ADVISED GROUND PERSONS THAT HE WAS UNABLE TO TRANSPORT PATIENT VIA HELICOPTER. PATIENT WASSDR CA080104003Trim Tab · unserviceable(CAN) WHILE PERFORMING A BRIDGING INSPECTION ON AN A/C PREVIOUSLY LEASED TO A DIFFERENT COMPANY, AD 2007-0138-E WAS BEING C/O. SECTION OF MISSING PAINT NOTED ON AREA REQUIRING INSPECTION IAW ASB 05-00.40( IB ATTACHMENT POINT OF T/E TAB). A CRACK WAS NOTED THROSDR CA071212014Strainer · contaminated(CAN) STRAINER WAS INSPECTED AND FOUND CONTAMINATED WITH PARTICLES FOREIGN MATTER AND SLIVERS OF MATERIAL FROM THE O-RING, P/N MS28775-016, WHICH WAS HARD AND BRITTLE. THE MFG MM REQUIRES INSPECTION AND CLEANING OF THE STRAINER ONLY WHEN THE MANIFOLD IS REPLASDR CA071208001Fcu · surges(CAN) FCU WAS SURGING DURING A GROUND RUN LEAK CHECK, BLEED VALVE TACH BOX HAD BEEN CHANGED FOR TROUBLESHOOTING, SURGING CONTINUED. FCU CHANGED OUT AND SURGING PROBLEM WAS RESOLVED. AC RETURN TO SERVICE. (TC NR 20071208001)SDR CA071205002Windshield · cracked(CAN) DURING PREFILGHT INSP, CRACKS WERE DISCOVERED ON LT WINDSHIELD TECH TOOLS PLASTICS P/N 350126231 AND RT WINDSHIELD TECH TOOLS PLASTICS P/N 3501-2623-1. BOTH LT AND RT WINDSHIELDS WERE CRACKED 4.5 TO 5 INCHES LONG ON BOTTOM EDGE. THE AIRCRAFT HAND FLOWN TSDR CA070906001Spar · cracked(CAN) CRACKS DISCOVERED ON BOTH SIDES OF STABILIZER THROUGH LOWER DOUBLER AT SPAR. FOUR RIVETS FOUND MISSING FROM FORWARD SPAR ATTACHMENT OF LOWER STABILIZER FRAME. (VISISBLE UPON REMOVAL ONLY) SUSPECT INCORRECT SHIMMING AT THIS TIME. (TC NR 20070906001)SDR CA070222004Module · malfunctioned(CAN) POSSIBLE T1 OR T2 MO3 TURBINE RUB. REMOVED MO3 AND SEND TO MFG FOR INVESTIGATION. THE TURBINE RUB WAS NOTICED AFTER SHUTDOWN OF THE ENGINE. (TC NR 20070222004)SDR CA070205001Spring · broken(CAN) WE ARE DOING A 12 YEAR INSPECTION ON AIRCRAFT, AS WELL AS SEND IT OUT FOR PAINT. THE MAIN ROTOR ANTI-VIBRATOR WAS REMOVED FOR CHECK AND MODIFICATION. WHEN SPRINGS WERE REMOVED, ONE WAS FOUND TO BE BROKEN 40 MM FROM OB END. THIS AREA IS HIDDEN BEHIND SIDESDR CA070118011Servo · unserviceable(CAN) DURING HYDRAULIC PRE-FLIGHT CHECK CAUSED CYCLIC TO MOVE 4-5 INCHES TOWARDS 8 O’CLOCK POSITION. SERVO REMOVED SERVICEABLE UNIT INSTALLED. SERVO SENT OUT FOR REPAIR AWAITING TEARDOWN REPORT. (TC NR 20070118011)SDR ML62007F00000Case · crackedAT APPROXIMATELY 0200, 22 DEC, 2006, WHILE RETURNING FROM A MEDICAL TRANSFER, AIRCRAFT EXPERIENCED AN ENGINE FAILURE WHILE IN CRUISE FLIGHT. PILOT INITIATED AN AUTOROTATION AND SUCCESSFULLY LANDED THE AIRCRAFT APPROXIMATELY 5SM WEST OF 4SD WITHOUT DAMAGE OR ISDR CA061108001Mount · damaged(CAN) DURING A 100 HOUR INSPECTION IT WAS DISCOVERED THAT TWO OF THE FOUR RIVETS USED TO ATTACH THE BEARING SUPPORT TO THE PUMP MOUNT WERE BROKEN. THE BEARING SUPPORT AND ATTACHING RIVETS ARE NOT LISTED IN THE AS350 ILLUSTRATED PARTS CATALOG, AS THEY ARE PARTSDR KNK2006F00010Manifold · cokedCOMPRESSOR HARD TO ROTATE DUE TO INJECTION MANIFOLD COKING. (K)SDR KNK2006F00008Manifold · cokedENGINE HARD TO ROTATE FOR START DUE TO FUEL COKING IT. THE INJECTION MANIFOLD LABYRINTH SEAL. (K)SDR KNK2006F00006Manifold · cokedENGINE COMPRESSOR HARD TO ROTATE DUE TO FUEL COKING IN INJECTION MANIFOLD LABYRINTH SEAL AREA. (K)SDR CA060921001Gearbox · damaged(CAN) OIL PRESSURE LINE FITTING AT ACCESSORY GEARBOX (FELL OUT) OF GEARCASE AND SUBSEQUENT COMPLETE LOSS OF OIL IN FLIGHT. THREADS IN GEARCASE STRIPPED 90 PERCENT; NO PREVIOUS INDICATION OF DISCREPANCY, IE: OIL LEAK OR LOOSENESS. (TC NR 20060921001)SDR DCG2006F00002Manifold · malfunctionedBEFORE THE FIRST FLIGHT OF THE DAY THE PILOT COULD NOT START THE ENGINE.. INSPECTED ENGINE ASSY AND FOUND THE GAS GENERATOR LOCKED UP DUE TO COKING FROM THE FUEL INJECTION MANIFOLD. REMOVED THE ENGINE ASSY AND ASSIST MFG TEC IN REPLACING THE FUEL INJECTION MSDR DCG2006F00004Manifold · cokedBEFORE THE FIRST FLIGHT OF THE DAY, THE PILOT COULD NOT START THE ENGINE. INSPECTED ENGINE ASSY AND FOUND THE GAS GENERATOR LOCKED UP DUE TO COKING FROM THE FUEL INJECTION MANIFOLD. REMOVE THE ENGINE ASSY AND ASSIST TECH IN REPLACING THE FUEL INJECTION MANIFSDR 2006FA0000887Connector · contaminatedDEPARTED BASE, HEADED FOR THE GLACIER, EN ROUTE THE PILOT NOTICED HIS TORQUE READING WAS FLUCTUATING. THE PILOT RETURNED TO BASE AND THE MECHANIC FOUND THAT THE ENGINE DECK PLUG HAD WATER IN IT FROM THE HEAVY RAINS WE HAVE BEEN ENDURING. THE MECHANIC CLEANEDSDR KNK2006F00004Manifold · cokedENGINE HARD TO ROTATE DUE TO FUEL COKING IN INJECTION MANIFOLD LABYRINTH SEAL AREA. (K)SDR CA060804007Coupling · leaking(CAN) PILOT FELT STIFFNESS IN FLIGHT CONTROLS AND LANDED. INVESTIGATION REVEALED THAT THE SLEEVE COUPLING INTERNAL SPLINES HAD WORN EXCESSIVELY SO THAT THE FLIGHT CONTROL HYDRAULIC PUMP WAS NO LONGER DRIVEN BY THE DRIVE BELT FROM THE MAIN GREAR BOX. THE FAILESDR CA060726001Igniter · loose(CAN) INSULATION WITHIN IGNITOR FOUND LOSE. IN LIGHT OF PAST INCIDENCE OF ENGINE FOD, IGNITORS WERE CHANGED. IGNITOR P/N 955075400/CH34745 (TC NR 20060726001)SDR KBM2006F00223Motor · inoperative5 INCH MOTOR, FAN INOPERATIVE, REMOVED AND REPLACED. (K)SDR CA060630006Gearbox · failed(CAN) TAIL ROTOR GEARBOX CHIP LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT LANDED AND CHIP DETECTOR EXAMINED, MALL AMOUNT OF FERROUS MATERIAL ON DETECTOR. DETECTOR CLEANED AND SERVICEABILITY CHECK CARRIED OUT. ON RETURN TO LANDING SITE, SMALL AMOUNT OF FINE HAIR LISDR CA060629006Retaining Nut · broken(CAN) RETAINING NUT FOR THE INPUT FLANGE ON THE TRANSMISSION (MAIN GEARBOX) BROKE IN 2 PIECES CAUSING THE SPLINED ADAPTER TO BACK OFF, WHICH CAUSED THE HYDRAULIC BELT TO RUN ON THE EDGE OF THE PULLEY. (TC NR 20060629006)SDR KBM2006F00213Indicator · inoperativeTURN AND SLIP, NEEDLE INOPERATIVE, REMOVED AND REPLACED. (K)SDR KBM2006F00212Pitch Link · wornT/R PITCH LINK, UNIT WORN, REMOVED AND REPLACED. (K)SDR KBM2006F00211Gyro · intermittentPUSH BUTTON INOPERATIVE, VERTIAL. PUSH KNOB IS INTERMITTENT, LOOSES GEARING AT CERTAIN COMPASS SETTING. REMOVED AND REPLACED. (K)SDR KBM2006F00219Guide · groovedSTOVE PIPE, UNIT GROOVED, REMOVED AND REPLACED. (K)SDR KBM2006F00220Bushing · debondedSCISSOR LINK, UNIT BUSHINGS ARE DEBONDED, REMOVED AND REPLACED. (K)SDR KBM2006F00221Bearing · wornHALF SHELLS, UNIT WORN BEYOND LIMITS, REMOVED AND REPLACED. (K)SDR KBM2006F00222Brake Disc · wornMAIN ROTOR BRAKE DISK, WORN BEYOND LIMITS, REMOVED AND REPLACED. (K)SDR KBM2006F00198Altimeter · stickingALTIMETER, UNIT STICKS AND IS NOT OFF MORE THAN 300 FT. REMOVED AND REPLACED. (K)SDR KBM2006F00205Blower Motor · inoperativeAC BLOWER MOTOR, AC IS NOT WORKING, REMOVED AND REPLACED. (K)SDR KBM2006F00204Battery · inoperativeBATTERY, UNIT HAS SLOW START, REMOVED AND REPLACED. (K)SDR KBM2006F00201Pitch Link · loosePITCH LINK, UNIT LOOSE, REMOVED AND REPLACED. (K)
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