Turbomeca ARRIEL-1D1
Service difficulty reports · 933
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 = 'ARRIEL1D1' 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 = 'ARRIEL1D1' 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 HXSD094146Bulkhead · crackedON 3/25/04 DURING ANNUAL INSPECTION OF N913LP TAIL BOOM BULKHEAD P/N 350A21-1247-0051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLACED WITH A NEW COMPONENT, SAME P/N ON WORK ORDER 24-36502.SDR HXS2004F00001Bulkhead · crackedDURING ANNUAL INSPECTION, TAILBOOM BULKHEAD PN 350A2112470051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLACED WITH A NEW COMPONENT, SAME PN ON WO NR 24-36502.SDR CA040325004Drive Assy · broken(CAN) DURING A HOVER FLIGHT HYDRAULIC WARNING LIGHT CAME ON. THE PILOT STABILIZED THE A/C AND RETURNED TO CAMP IN MANUAL CONTROL MODE. UPON INSPECTION, AME DISCOVERED BROKEN HYDRAULIC PUMP PULLEY DRIVE BELT. BELT REPLACED, A/C RETURNED TO SERVICE.SDR KBM2004F00025Guide Vane · crackedREMOVAL OF ENGINE FOR DISC REPLACEMENT. FOUND CRACK ON 1ST STG NOZZLE GUIDE VANES. DURING 2ND STAGE TURBINE WHEEL AND BLADE REPLACEMENT 263 SB. REMOVED AND REPLACED ENGINE WITH RENTAL.SDR CA040805008Bearing · worn(CAN) WHILE PERFORMING A 100 HOUR INSPECTION THE TAIL ROTOR SPIDER WAS DISCONNECTED FROM THE INPUT BELLCRANK TO CHECK THE SPIDER SWASHPLATE BEARING. NOTICED THAT THE BALL END BEARING ON THE SWASHPLATE INPUT WAS WORN OUT. ( IPC 65.20.30 FIG 1A ITEM 95 ) MEASURSDR CA040315012Servo Valve · unserviceable(CAN) PILOT REPORTED THAT WHEN HE TRIED TO PULL THE COLLECTIVE UP, IT FELT VERY HEAVY. IT WAS NOTED DURING TROUBLESHOOTING THAT THE SPOOL VALVE WAS VERY DIFFICULT TO MOVE AND THEN IT WOULD ONLY MOVE A SMALL AMOUNT. A SERVICEABLE SERVO WAS INSTALLED AND CONSDR HCM2004F00000Sensor · failedON MARCH 9, 2004 WHILE ON A SIGHT SEEING TRIP, THE PILOT NOTICED A HIGH ENGINE OIL TEMPERATURE INDICATION. HE MADE A PRECAUTIONARY LANDING. A MECHANIC WAS FLOWN TO THE SCENE AND REPLACED THE ENGINE OIL TEMPERATURE SENSOR. THE AIRCRAFT WAS FLOWN BACK TO BASESDR CA040308002Belt · stretched(CAN) WHILE INSPECTING THE HYDRAULIC DRIVE BELT IAW 63.00.00.601 PARA 4 FOR PROPER TENSION IT WAS FOUND TO BE LOOSE. ATTEMPTS WERE MADE TO TENSION THE BELT IAW 63.00.00.401 PARA 4.2.3. WE WERE UNABLE TO GET THE REQUIRED TENSION DUE TO NO MORE MOTION OF THE SDR B3O2004F00000Blade · damagedMAIN ROTOR BLADE RECEIVED FROM AEC WITH DAMAGE TO THE TRAILING EDGE OF THE NR 3 TRIM TAB. TRIM TABS RESET AT AEC PRIOR TO RECEIPT AEC WO NR W0078958. BLADE NOT ABLE TO FLY CORRECTLY ON TWO DIFFERENT AC. REQUEST EVALUATION OF BLADE.SDR KBM2005F00025Bearing · crackedT/R HINGE LAMS CRACKED .6666 THE WAY AROUND ON SIDE OF FORK. REMOVED AND REPLACED. (K)SDR KBM2004F00176Blower · inoperativeCONDENSER BLOWER INOPERATIVE. REMOVED AND REPLACED.SDR KBM2005F00024Pitch Link · crackedTAIL ROTOR PITCH LINK ROD HAS SILENT BLOCK HAS V-CRACK. REMOVED AND REPLACED. (K)SDR B30R20040226Door Frame · crackedDURING 100 HOUR INSPECTION DISCOVERED CO-PILOT DOOR POST CRACKED 14 INCHES LONG STARTING 8 INCHES ABOVE CABIN FLOOR, EXCEEDING THE LIMITS IN REPAIR MANUAL. REPAIRED CRACK IAW MM. REQUESTED FROM MFG.SDR CA040301005Support · cracked(CAN) A CRACK WAS DISCOVERED IN MAY ON THE NR 5 HANGER BEARING SUPPORT. THIS PART WAS REPLACED IN THE FIELD USING ALL THE APPROPIATE TOOLING. SOMETIME LATER THE PILOT COMPLAINED OF A HIGH FREQ VIBRATION. THE SHAFT WAS REBALANCED TO .2 IPS. AGAIN ABOUT 20 HOURSSDR KBM2005F00019Seal · leakingMAG SEAL, LEAKING, REMOVED AND REPLACED. (K)SDR 2004FA0000272Pipe · crackedDURING ENGINE START AFTER CHANGING THE START DRAIN VALVE, LT FUEL INJECTOR PIPE WAS SPRAYING FUEL AT INJECTOR FITTING. INSPECTION OF PIPE REVEALED A CACK AT THE TOP OF THE FLARE ON THE PIPE. CAUSE OF CRACK APPEARS TO BE FROM THE FLARE NOT BEING CENTERED ON TSDR KBM2005F00018Control Cable · bindingT/R CONTROL CABLE, CABLE IS BINDING, REMOVED AND REPLACED. (K)SDR KBM2004F00017Bearing · wornTAIL ROTOR HUB LAMINATED RUBBER HINGE BEARING ARE WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW.SDR KBM2004F00018Blower · inoperativeOIL COOLER MOTOR INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE.SDR CA040129006Beam · cracked(CAN) AIRCRAFT ON HELISKIING WHEN THIS OCCURRED. INSPECTED IAW AD96-156-071(B) R1 PART 1.1, EVERY 30 HOURS OR 150 CYCLES. THIS WAS BEING INSPECTED DUE TO THE CYCLES EVERY 2 OR 3 DAYS. THE CROSSBEAM WAS FOUND SMOKING IN THE REGION OF SUSPECTED CRACK. THE AREASDR KBM2005F00033Bearing · wornLAMINATED BEARING, WORN, REMOVED AND REPLACED. (K)SDR KBM2005F00031Bearing · failedLAMINATE BEARINGS, VIBRATION FELT IN TAILROTOR AT NG 65->70 PERCENT. REMOVED AND REPLACED. (K)SDR CA040211011Starflex · cracked(CAN) ON A ROUTINE AIRFRAME INSPECTION, A CRACK WAS NOTED ON THE TRAILING EDGE OF THE STAR ARM. AFTER COMPLETING THE REPAIR TO THE AREA IAW THE SRM, IT WAS FOUND TO STILL BE A MUCH DEEPER FLAW. THE STAR WAS SENT TO MFG FOR FURTHER INVESTIGATION. A NEW STARSDR 2004FA0000328Starter Gen · inoperativePILOT REPORTED DEFECT AND MAINTENANCE CORRECTIVE ACTION: ON 3RD HOP, 2 MINUTES INTO FLIGHT VOLTMETER READ 23 VOLTS. NO GENERATOR LIGHT. SHUT DOWN FOR 10 MINUTES. CONTINUED FLIGHT FOR 3 HOURS. AT 29 VOLTS ON 4TH HOP, JUST PRIOR TO LIFT-OFF, GENERATOR LIGHT CAMSDR HEEA092084Fuel Control · malfunctionedWHEN COLLECTIVE WAS LOWERED TO LAND, THE ENGINE WOULD OVERSPEED. MAINTENANCE REPLACED THE FUEL CONTROL UNIT.SDR KBM2005F00029Gyro · malfunctionedDG, FLAG REMAINS OFF, REMOVED AND REPLACED. (K)SDR CA031216007Line · broken(CAN) PILOT ATTEMPTED A START AND THE ENGINE FAILED TO ACCELERATE. INITIAL T4 INDICATION WAS VERY LOW AND THE T4 DID NOT INCREASE AS THE THROTTLE WAS MOVED FORWARD DURING THE STARTING SEQUENCE. THE PILOT ABORTED THE START. UPON INSPECTION THE PILOT NOTICED FSDR CA040108004Tab · cracked(CAN) ON AN OCCURRENCE TEARDOWN OF ENGINE, BETWEEN MODULE 2 AND MODULE 3, THE TECHNICIANS DISCOVERED A TAB BRIDGE CRACKED AND WAS INGESTED INTO THE ENGINE SUBSEQUENTLY CAUSING DAMAGE TO THE CENTRIFUGAL COMPRESSOR, WHICH WAS REPLACED.SDR KBT2004F00001Control Rod · crackedDURING COMPLIANCE WITH AD, INSPECTED BOTH CONTROL RODS. FOUND BOTH BUSHINGS IN ELASTOMERIC BEARING CRACKED THROUGH TO BOTH ENDS. BOTH CONTROL RODS REJECTED FROM FURTHER SERVICE. INSTALLED NEW CONTROL RODS. NO RECORD OF REPLACEMENT IN AC LOGBOOK. THIS PUTSSDR B30R20031120Skin · delaminatedDURING 100 HOUR INSPECTION, IT WAS DISCOVERED THAT THE INNER FIBERGLASS SKIN OF THE UPPER AFT SECTION OF THE ENGINE COWLING HAD DISBONDED FROM THE HONEYCOMB STRUCTURE OF THE COWLING. PRYROPEL INSULATION WAS TO BE INSTALLED WHILE THE AIRCRAFT WAS IN INSPECTION SDR 2004FA0000327Starter Gen · inoperativePILOT REPORTED DEFECT AND MAINTENANCE CORRECTIVE ACTION: GENERATOR LIGHT CAME ON IN FLIGHT, WILL NOT RESET. REPLACED STARTER/GENERATOR AND 16 AMP FUSE.SDR 2004FA0000326Starter Gen · inoperativePILOT REPORTED DEFECT AND MAINTENANCE. STARTER/GENERATOR LIGHT CAME ON IN FLIGHT. REPLACED STARTER/GENERATOR AND 16 AMP FUSE.SDR KBM2003F00110Fuel Control · leakingENGINE FUEL CONTROL UNIT P2 AIR CAVITY IS LEAKING FUEL. INSTALLED SERVICEABLE FUEL CONTROL UNIT.SDR KBM2004F00012Bearing · wornTAIL DRIVE SHAFT NR 5 BEARING, WORN. REMOVED AND REPLACED WITH NEW BEARING. (K)SDR KBM2004F00013Bearing · wornTAIL DRIVE SHAFT NR 5 BEARING, WORN. REMOVED AND REPLACED WITH NEW. (K)SDR CA031120007Spherical Stop · worn(CAN) A WORN SPHERICAL STOP WAS CHANGED DUE TO DEBOND. WITH THE ONE STOP CHANGED AND THE ROTORS TURNING AT FULL RPM ON THE GROUND AND HYDRAULIC SYSTEM TURNED 'OFF' THE CYCLIC STICK MOVED VIA ROTOR HEAD FEED BACK. TO DETERMINE THE CAUSE OF THE FEED BACK , THE SDR KBM2005F00034Coupling · fatiguedBELT SLIPPAGE OVERTEMP. POSSIBLE METAL FATIGUE. (K)SDR CA031119009Elt · misinstalled(CAN) ARTEX ELT MODEL ELT 110-4 P/N 453-0150 WAS WIRED INCORRECTLY- THE ELT WOULD ONLY ACTIVATE BY PANEL SWITCH OR THE SWITCH ON THE ELT. FOR THE ELT TO BE OPERATED IN AUTOMATIC MODE A JUMPER WIRE BETWEEN PINS 5 AND 8 OF MOLEX TRAY CONNECTOR NEEDS TO BE INSTASDR CA031113006Line · broken(CAN) THE PILOT EXPERIENCED A SLOW SLUGGISH START. ON INVESTIGATION HE FOUND FUEL ON THE DECK AND DOWN THE LT SIDE OF THE ENGINE. HE FOUND THE LT START INJECTOR FUEL SUPPLY LINE CRACKED NEAR THE FLARE AT THE POINT WHERE IT IS ATTACHED TO THE INJECTOR. THE LISDR RX8R2003002Thermoswitch · inoperativeWHILE PERFORMING THE 6 YR. 2000 HR. INSPECTION TO TEST THE MAIN GEARBOX OIL TEMPERATURE PROBE, IT WAS DETERMINED THAT THE PROBE WAS INOPERATIVE AND HAD TO BE REPLACED. WE PERFORMED THE SAME TEST ON ANOTHER AS350B2 AIRCRAFT (N4043L, SN 3015) ON OCT. 23, 2003 ANSDR KBM2004F00007Connector · inoperativeHEATER INOPERATIVE, BLOW A/C AIR. REMOVED AND REPLACED WITH NEW. (K)SDR KBM2003F00085Inertia Reel · failedINERTIA REEL ON PILOTS SEAT WILL NOT RETRACT. INSTALLED O/H UNIT.SDR KBM2003F00086Indicator · noisyTURN COORDINATOR MAKES LOUD SQUEEKING NOISE. MEL NR 10.SDR 2003FA0001163Module · seizedON 17, OCT. 2003, FIRST START OF THE DAY, PILOT REPORTED ENGINE WOULD NOT START. SUBSEQUENT INSPECTION REVEALED THAT AXIAL COMPRESSOR WAS SEIZED. ONLY WITH GREAT EFFORT COULD THE AXIAL COMPRESSOR BE TURNED BY HAND. ENGINE WAS REMOVED FOR RETURNED TO FACILITSDR 2003FA0001133Gas Generator · noisyRUBBING NOISE AFTER SHUT DOWN. ONLY WHEN ENGINE IS HOT.SDR 2004FA0000335Starter Gen · inoperativePILOT REPORTED DEFECT AND MAINTENANCE CORRECTIVE ACTION: GENERATOR WENT OFF-LINE. REPLACED GENERATOR AND BATTERYSDR KBM2003F00075Pad · wornRT SLIDING DOOR FRICTION PAD SLIDER WORN EXCESSIVELY. REMOVED AND REPLACED WITH NEW. (K)SDR KBM2003F00076Rod End · wornROD END IS WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW ONES. (K)SDR KBM2003F00064Drain Valve · failedAIRCRAFT STARTS SLOW, MUST INCREASE TO 750 DEGREE TO 760 DEGREE TO START. REMOVED AND REPLACED WITH OVERHAULED START DRAIN VALVE.SDR 2003FA0001096Module · seizedPILOT REPORTED; ENGINE WOULD NOT START. WHEN START BUTTON PUSHED, IGNITERS WOULD FIRE BUT NO NG ROTATION. STARTER MADE AN (THUNK). VOLTS WERE GOOD, SUBSEQUENT INSPECTION BY MAINTENANCE PERSONNEL DETERMINED THAT THE AXIAL COMPRESSOR HAD SEIZED.(K)
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