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 KBM2005F00080Transmitter · failedENGINE OIL INDICATION AT -0-. REMOVED AND REPLACED. (K)SDR KBM2005F00174Belt · crackedHYDRAULIC BELT, CRACKED AND SPLIT (LONGITUDE) OVER HALF CIRCUMFERENCE, REMOVED AND REPLACED. (K)SDR CA050417006Igniter · damaged(CAN) CENTER CERAMIC MISSING, BOROSCOPE OF ENGINE FOUND NO DAMAGE, IGNITER REPLACED.SDR CA050417005Igniter · damaged(CAN) CENTER CERAMIC LOOSE, PLUG REPLACED.SDR KBM2005F00185Drain Valve · leakingSTART/ DRAIN VALVE, LEAKING EXTERNALLY. REMOVED AND REPLACED. (K)SDR KBM2005F00060Control Box · inoperativeECE BOX, INOPERATIVE, GENERATOR LIGHT WOULD NOT GO OUT DURING RUN-UP. REMOVED AND REPLACED. (K)SDR KBM2005F00075Gyro · inoperativeD.G. INOPERATIVE, SPINS IN FLIGHT. REMOVED AND REPLACED. (K)SDR CA050331001Hose · collapsed(CAN) HOSE COLLAPSED IN FLIGHT FILLING CABIN WITH INSULATION PARTICLES AND DUST.SDR CA050428003Igniter · failedENGINE WOULD NOT START. IGNITORS FOUND UNSERVICEABLE. ORIGINALLY INSTALLED APRIL 4, 2003.SDR KBM2005F00041Motor · incorrect5 INCH BLOWER MOTOR, ARMATURE NO POSITIONED CORRECTLY. REMOVED AND REPLACED. (K)SDR CA050301011Pin · cracked(CAN) REMOVED SLIDING DOOR PINS FROM A AS 350 TO CONDUCT AN DYE PENETRANT INSPECTION IAW ALERT TELEX 05.00.47. THE INSPECTION WAS CONDUCTED. DURING THE DYE CHECK A SMALL INDICATION WAS REVEALED BUT WAS NOT VERY APPARENT AND EASILY DISTINQUISHED. THE NDT INSPESDR KBM2005F00009Transponder · inoperativeUNIT RAMP CHECK INOPERATIVE, TRANSPONDER, REMOVED AND REPLACED. (K)SDR KBM2005F00011Bleed Valve · stickingBLEED VALVE STICKS, REMOVED AND REPLACED. (K)SDR KBM2005F00038Bearing · wornLAMINATED BEARING, WORN. REMOVED AND REPLACED. (K)SDR CA050202002Screen · cracked(CAN) WIRE BROKEN ON SCREEN THAT IS ATTACHED TO BLEED VALVE.SDR CA050315005Line · cracked(CAN) THE AIRCRAFT SHOWED SIGNS OF IRREGULAR STARTS. WHILE WATCHING A START, THE ENGINEER NOTICED WHISPS OF SMOKE COMING FROM THE RT SIDE OF THE ENGINE. TUBE WAS REMOVED AND INSPECTED AND FOUND CRACK ON FLARED END UNDER FERRULE.SDR CA050215009Switch · defective(CAN) PILOT COULD NOT TURN HYD OFF DURING FLIGHT BY PRESSING BUTTON ON COLLECTIVE STICK. TROUBLESHOOTING DETERMINE THE SWITCH WAS DEFECTIVE AND NOT SUPPLYING VOLTAGE TO SOLENOIDS. NEW SWITCH INSTALLED.SDR CA050120013Swashplate · worn(CAN) DURING A DAILY INSPECTION, WITH THE COLLECTIVE CONTROL RAISED, AME NOTICED THAT PROTECTIVE TEFLON TAPE WAS MISSING ON THE SWASHPLATE GUIDE (SEVERAL SQUARE INCHES IN AREA, FROM 7:30 O'CLOCK TO 2:00 O'CLOCK). CORRESPONDING WEAR STEP OF APPROXIMATELY .040SDR KBM2005F00003Transducer · failedOIL PRESSURE GAUGE SHOWING NO INDICATION OF PRESSURE. REMOVED AND REPLACED.SDR KBM2005F00012Gyro · inoperativeLOOSE PARTS INSIDE, HORIZON GYRO, REMOVED AND REPLACED. (K)SDR CA041209005Servo · malfunctioned(CAN) PILOT REPORTED THAT CYCLIC WAS STIFF WHEN MOVED TO LEFT AND IT WANTED TO MOVE RIGHT WHEN COLLECTIVE LOWERED (NO PROBLEMS WHEN COLLECTIVE WAS RAISED). LEFT MAIN SERVO WAS CHANGED AND DEFECT WAS CURED.SDR KBM2005F00000Bearing · crackedHALF SHELLS CRACKED. REMOVED AND REPLACED. (K)SDR CA041110009Igniter · unserviceable(CAN) WHILE TROUBLESHOOTING A SLOW STARTING ENGINE, THE LT IGNITER PLUG WAS REMOVED FOR INSPECTION. AN OPERATIONAL (SPARK) CHECK WAS CARRIED OUT WITH NO DEFECTS FOUND. UPON A SECOND LOOK AT THE IGNITER, IT WAS NOTICED THE SEMI CONDUCTOR SURROUNDING THE CENTRSDR CA041105006Fuel Control · failed(CAN) ON P2 CHAMBER INSPECTION AND CLEANING OF FCU. WHEN BELLOWS WERE REMOVED WE FOUNDTHAT THE PIN THAT HOLDS THE METERING VALVE IN PLACE WAS BROKEN OFF AND HALF OFTHE PIN WAS FOUND IN THE CHAMBER.SDR CA041110016Servo · malfunctionedWHEN HYDRAULIC POWER IS RE-ESTABLISHED AFTER DOING HYDRAULIC ACCUMULATOR PREFLIGHT CHECK, THE CYCLIC STICK WOULD GO HARD LEFT, BUT WAS ABLE TO BE OVERCOME AND WOULD ONLY LAST BRIEFLY. LEFT HAND SERVO WAS REPLACED FOR TROUBLESHOOTING AND PROBLEM WAS RECTIFIED.SDR KBM2004F00238Indicator · inoperativeTURN AND BANK INOPERATIVE, REMOVED AND REPLACED.SDR KBM2004F00239Bearing · splitLAMINATED BEARINGS ARE SPLIT. REMOVED AND REPLACED.SDR KBM2004F00218Bleed Valve · stuckBLEED VALVE STUCK OPEN IN FLIGHT. REMOVED AND REPLACED.SDR CA041022005Servo · failed(CAN) PILOT WAS DOING HIS PREFLT HYD TESTS AND THEY FAILED. AFTER TROUBLESHOOTING HYDRAULIC SYSTEM FOUND THAT ONE LATERAL SERVO WAS THE CAUSE OF THIS MOVEMENT EVEN THOUGH DURING OUR TROUBLESHOOTING THE LATERAL SERVOS WERE SWAPPED OVER BUT THE PROBLEM STAYED GSDR CA041110008Plate · missingDURING AN INSPECTION OF THE CABLE ASSEMBLY, THE BACKING PLATE FOR THE CABLE SUPPORT BEARING AT THE TAIL BOOM/AIRFRAME JUNCTION WAS FOUND TO BE MISSING. AIRCRAFT GROUNDED AND A PLATE INSTALLED. THE MISSING PLATE RESULTED IN EXCESS PLAY IN THE TAILROTOR PEDAL SDR PG92004F00014Blade · crackedT/R SPAR FOUND CRACKED DURING COMPLIANCE OF SB 05.11R5. THIS CONDITION PERSISTS ON THIS MODEL HELICOPTER AND PN COMPONENT. REPLACED T/R BLADE WITH NEW UNIT. RETURNED HELICOPTER TO SERVICE.SDR KBM2004F00227Bearing · wornT/R BLADE WORN. REMOVED AND REPLACED HALF SHELLS.SDR KBM2004F00228Gauge · stuckTORQUE GAUGE STUCK, REPLACED WITH SERVICEABLE UNIT. ROBBED FROM 350SH.SDR KBM2004F00221Gauge · stuckTORQUE GAUGE STUCK AT 70 PERCENT. REPLACED WITH SERVICEABLE GAUGE.SDR KBM2004F00230Gauge · stuckTORQUE GAUGE STUCK AT 75 PERCENT. REPLACED WITH SERVICEABLE GAUGE.SDR CA041110002Compressor Wheel · damaged(CAN) MO 2/3 FIRST STAGE WHEEL RUBBING ON THE PLASMA SPRAY IN LINER.. (PLASMA LIFTINGOFF IN TO THE BLADE PATH.)SDR CA040916007Switch · malfunctionedSHORTLY AFTER T/O, WARNING HORN & NOTICED 'HYD CAUTION LIGHT' ON. A FEW SECONDS LATER, ERRATIC CYC MOVEMENT FELT. RETURNED & LANDED W/O INCIDENT. MX INSPECT DID NOT ISOLATE CAUSE FOR MALFUNCTION. HYD SYS CK APPEARED TO BE NORM. HYD PUMP SPLINES INSPECTED & SDR KBM2004F00229Belt · brokenAIR CONDITIONER BELT BROKE DURING FLIGHT. REPLACED BELT.SDR CA040910006Filter · debonded(CAN) DURING A SCHEDULED INSPECTION AME ATTEMPTED TO REMOVE HYDRAULIC FILTER ELEMENT. THE SREW IN PLUG PORTION SEPARATED FROM THE FILTER ELEMENT THAT REMAINED IN THE FILTER BOWL. THE SYSTEM WAS FLUSHED, FILTER REPLACED AND A/C RETURNED TO SERVICE.SDR KBM2004F00208Belt · burnedBELT BURNED AND SNAPPED (AIR CONDITIONING). REPLACED BELT, EXPANSION VALVES, HIGH PRESSURE SWITCH AND RESERVICED SYSTEM TO 2.75 LBS OF R-138.SDR KBM2004F00194Display · inoperativeVHF DISPLAY BAD. REMOVED AND REPLACED.SDR KBM2004F00207Bellcrank · looseBUSHINGS LOOSE IN EXPANDABLE BOLT BOXES. REPLACED BELLCRANK WITH NEW.SDR KBM2004F00206Compressor · failedBELT BROKE, UPON INSPECTION FOR COMPRESSOR PULLEY AND CLUTCH BURNED UP. REPLACED BELT AND COMPRESSOR AND PULLEY ASSY.SDR KBM2004F00210Brushes · failed7 IN BRUSHES, CONDENSER MOTOR, UNIT INOPERATIVE. REMOVED AND REPLACED.SDR CA040809007Pinion Gear · vibration(CAN) AIRCRAFT HAD 3 PER VIBRATION APPEAR DURING FORWARD FLIGHT. PILOT LANDED AT DESTINATION AND PHONED IN FOR A PRECAUTIONARY MEASURE. COMPANY DISPATCHED ANOTHER AIRCRAFT AND ENGINEER TO ACCESS THE PROBLEM. TRANSMISSION WAS CHANGED AND AIRCRAFT WAS RETURNED SDR KBM2004F00205Servo · restrictedRESISTANCE FELT WHEN APPLYING LT INPUT ON CYCLE. REMOVED DEFECTIVE SERVO AND INSTALLED UNIT, RESISTANCE IS NO LONGER FELT.SDR CA040806010Support · cracked(CAN) HYDRAULIC PUMP SUPPORT HOUSING HAD A CRACK ON FLANGE, CAUSING PUMP AND BEARING ASSEMBLY TO VIBRATE. HYDRAULIC BEARING (704A33-651-206) FOR THE POLY (V) BELT WAS REPLACED AT THIS TIME TO ENSURE THAT NO DAMAGE MAY HAVE BEEN CAUSED TO THIS BEARING DUE TO VSDR CA040805011Casting · cracked(CAN) CRACK FOUND ON WEB CASTING DURING A 100 HOUR INSPECTION. (BUTTERFLY) PLATE VERY LOOSE (WORN OUT END BUSHINGS).SDR CA041022003Turbine Wheel · unserviceable(CAN) DURING A SCHEDULED CHECK OF THE SECOND STAGE TURBINE BLADES (T2 ) IAW TURBOMECA ASB 292-72-0807 AND AD2004-047 IT WAS DETERMINE THE BLADE SHIFT HAD FAILED THE CHECK. THE GAS GENERATOR WAS REPLACEDSDR CA040817002Switch · inoperative(CAN) BLEED VALVE LIGHT MICROSWITCH CAME APART. THE BROKEN PIECES OF THE ROLLER JAMMED BETWEEN THE PLUNGER AND HOUSING PREVENTING SMOOTH BLEED VALVE BUTTERFLY OPENING AND CLOSING. BUTTERFLY WAS FOUND PARTIALLY CLOSED CAUSING COMPRESSOR STALL WHEN ATTEMPTING TH
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