Turbomeca ARRIEL-1
Service difficulty reports · 670
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 = 'ARRIEL1' 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 = 'ARRIEL1' 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 KBM2004F00190Support Bracket · crackedUNDERNEATH FLOOR T/R PEDAL BELLCRANK BRACKET SUPPORT IS CRACK. REMOVED AND REPLACED.SDR KBM2004F00191Bearing · wornT/R SPIDER END BALL BEARINGS WORN BEYOND LIMITS. REMOVED AND REPLACED.SDR 2004F00356Bleed Valve · failedWHILE HOVERING FOR TAKEOFF A LOUD BANG CAME FOR THE ENGINE COMPARTMENT FOLLOWED BY A TORQUE FLUCTUATION AND A RIGHT YAW. CHECKED ALL THE SYSTEMS ALL IN GREEN AND THEN HOVERED TO PARKING. MAINTENANCE INSPECTED COMPRESSOR FOR FOD AND LEAKS, NO DEFECTED NOTED. SDR KBM2004F00192Motor · inoperativeAC INOPERATIVE RESET 1 AMP CIRCUIT BREAKER POPPED. REMOVED AND REPLACED.SDR I7LA0002725Trunnion · overheatedUPON 25 HOUR INSPECTION, TRUNION SHOWS SIGNS OF EXCESSIVE HEAT, DISCOLORED (BROWN) COATING. ENAMEL PAINT.SDR KBM2004F00199Gyro · inoperativeFLAG STAYS INOPERATIVE. REMOVED AND REPLACED DG.SDR KBM2004F00139Motor · inoperativeA/C BLOWER WARM. RT CONDENSOR BLOWER INOPERATIVE. REMOVED AND REPLACED. RT CONDENSOR BLOWER.SDR KBM2004F00116Indicator · inoperativeTURN AND BANK, WILL NOT POWER ON. MEL AC (DMI NR 19 DUE 7-20-04).SDR HXS2004F2004ACompressor · fodENGINE WAS FOUND TO HAVE INGESTED A ROCK THROUGH THE INTAKE AND DAMAGED TO INLET COMPRESSOR. FOD DAMAGE. THIS ENGINE IS TO BE SENT FOR EVALUATION AND REPAIR.SDR KBM2004F00120Indicator · inoperativeTURN COORDINATOR, INOPERATIVE. REMOVED AND REPLACED.SDR S9HA095372Transmitter · inoperativeENGINE OIL PRESSURE TRANSMITTER FAILED AFTER 0.0 HRS TSN. REPLACED WITH 3RD NEW TRANSMITTER .SDR S9HA095371Transmitter · inoperativeENGINE OIL PRESSURE TRANSMITTER FAILED AFTER 1.5 HRS TSN. REPLACED WITH 2ND NEW TRANSMITTER WHICH FAILED AT 0.0 HRS TSNSDR KBM2004F00119Motor · inoperativeMOTOR WILL NOT ROTATE WHEN POWER IS APPLIED. REPLACED MOTOR WITH REPAIR UNIT OPS, GOOD.SDR KBM2004F00118Control Tube · wornCHAFED CONTROL TUBE, WEAR SLEEVE WORN THRU, FURTHER INSPECTION OF TUBE FOUND WEAR TO BE WITHIN LIMITS. REPLACED ROD WITH SERVICEABLE UNIT. NEW HEATSHRINK OR WEAR SLEEVES INSTALLED.SDR KBM2004F00138Magnetic Seal · leakingNR 5 MAG SEAL, LEAKING SEAL. REPLACED WITH RECONDITIONED UNIT.SDR KBM2004F00137Fuel Control · failedFUEL CONTROL UNIT, UNABLE TO OBTAIN DESIRED NR. REPLACED WITH 0.0 TSO UNIT. OPS CHECK GOOD.SDR BAQA094478Indicator · burned outLED DISPLAY LIGHTING BURNED OUT. REPLACED WITH SERVICABLE UNIT.SDR KBM2004FAAPulley · undertorquedENGINE TO MGB POWER SHAFT FORWARD PULLEY ATTACH HOLES ELONGATED DUE TO ATTACHMENT BOLT TORQUE LESS THAN MINIMUM TORQUE AT ORIGINAL INSTALLATION. REMOVED AND REPLACED. ASSELBL AT FACTORY DURING 5900 HR/ 12 YEAR INSPECTION.SDR KBM2004F00186Bolt · undertorquedENGINE TO MGB POWER SHAFT FORWARD COUPLING BOLT TO PULLEY FAIL TORQUE LOAD CHECK, COUPLING REJECTION MANDATORY. REMOVED AND REPLACED.SDR KBM2004F00187Spider · wornT/R SPIDER BALL END WORN. REMOVED AND REPLACED.SDR KBM2004F00188Drive Assy · damagedT/R DRIVE (SHORT SHAFT) FORWARD COUPLING ATT BOLTS TO ENGINE TAKE OFF FLANGE FAIL TORQUE LOAD CHECK REQUIRES UNIT TO BE SENT TO MANUFACTURER FOR INSPECTION. ASSEMBLED AT FACTORY DURING 12 YEAR 5000 HOUR INSPECTION. REMOVED AND REPLACED.SDR FF62004F00000Magnetic Seal · galledSEAL LEAKING AFTER 200 HOURS. SEAL WAS GALLED.SDR BAQA094704Bearing · wornBEARINGS WORN AND SLOPPY. REPLACED WITH SERVICABLE UNIT. 05/24/2004SDR BAQA093902Receiver · unserviceableRENTAL - RETURN OF RENTAL UNIT S/N 10327 IN SERVICEABLE CONDITION REPLACED WITH UNIT BACK FROM REPAIR, 04/21/2004SDR TXER096035Spherical Stop · wornMAIN ROTOR SPHERICAL STOPS WORN.SDR BAQA094099Start Valve · inoperativeWARRANTY - CORE RETURN FOR WARRANTY PO 202317606, ENG S/N 18167, VALVE WAS REMOVED IN THE TROUBLESHOOTING PROCESS OF HAR STARTING NR 1 ENGINE. REPLACED WITH SERVICEABLE UNIT FROM MFG, 04/21/2004SDR BAQA094174Blower · noisyBLOWER IS EXCESSIVELY NOISY OPERATION AND INTERMITTENT STARTING AND STOPPING. S/N 105 WAS TAKEN FROM ASSET STOCK AND INSTALLED ON A/C. YET TO RECEIVE THE REPLACEMENT FROM AEC AS OF 04/15/2004. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 105). 04/15/2004SDR HXS2004F00000Blade · crackedON 3/25/04, MAIN ROTOR BLADE, SN 7530 REMOVED FROM AC DURING ANNUAL INSPECTION. 130MM SPANWISE CRACK FOUND AT 68.375.SDR BAQA093894Wire Harness · damagedENGINE, PROBES DAMAGED AT SOLDER JOINT. REPLACED WITH SERVICABLE UNIT.SDR BAQA094041Wire Harness · damagedWIRE HARNESS HAS DAMAGED SOLDER JOINTS ON UNIT. REPLACED WITH SERVICABLE UNIT. 04/02/2004SDR KBM2004F00090Rod End · damagedBLUE AND RED MAIN ROTOR PITCH CHARGE LINK UPPER END ROD BEARING STAKE HAS DAMAGE MARK. REMOVED AND REPLACED.SDR KBM2004F00114Suspension Bar · wornSUSPENSION BAR, LT SIDE REAR MAIN GEARBOX SUPPORT BAR HAS EXCESSIVE BEARING PLAY. REMOVED AND REPLACED.SDR KBM2004F00115Strap · wornEXHAUST HEAT SHRINK STRAP WORN. REMOVED AND REPLACED.SDR KBM2004F00136Strap · wornEXHAUST HEAT SHIELD STRAP. HEAT SHRINK WORN REGS REPLACEMENT. REMOVED AND REPLACED.SDR BAQA093939Compass · brokenWARRANTY. ADUSTMENT SCREW ON UNIT IS BROKEN. REPLACED WITH SERVICABLE UNIT. 03/25/2004SDR BAQA093879Manifold · cloggedWARRANTY. ENG S/N 32047. UNIT REMOVED DUE TO CLOGGING OF NOZZLES. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 03/19/2004SDR BAQA093880Manifold · cloggedWARRANTY. ENG S/N 32047. UNIT REMOVED DUE TO CLOGGING OF NOZZLES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/19/2004SDR BAQA093881Injector · cloggedWARRANTY. ENG S/N 32047. UNIT REMOVED DUE TO CLOGGING OF NOZZLES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/19/2004SDR BAQA093735Actuator · unserviceableACTUATOR FAILED, NO REFERENCE VOLTAGE FOR ACT. POSITION. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/17/2004SDR BAQA093737Pump · leakingHYDRAULIC PUMP IS LEAKING AT SHAFT. REPLACED WITH SERVICABLE UNIT. 03/17/2004SDR BAQA093829Control Unit · failedYAW CSAS MADE UNCOMMANDED YAW OSCILLATIONS IN NORMAL AND STANDBY MODE AT APPROX. TWO SECOND INTERVALS. UNIT WAS INSTALLED 02/16/2004 AT A/C TT 5145.8 AND WAS REMOVED 03/12/2004 AT A/C TT 5172.2 FOR A TOTAL OF 26.4 HOURS. LAST REPAIR REF RO 9-090006-18 MMIR CLSDR BAQA093947Window · crackedWINDOW CRACKED NEAR HANDLE. REPLACED WITH SERVICEABLE UNIT. 03/25/2004SDR BAQA093950Lamp · shortedSTROBE LAMP ASSY HAS AN INTERNAL SHORT, WILL NOT FLASH. REPALCED WITH SERVICABLE UNIT 03/26/2004SDR ULX2004F00001Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION-USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00003Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00004Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATIONS- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR 2004F00101Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION-USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00006Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR ULX2004F00008Housing · crackedCRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS.SDR BAQA093684Transponder · failedEXCHANGE. UNIT GIVING WRONG ALTITUDE, BAD WIRES IN UNIT. REPLACED WITH SERVICABLE UNIT. 03/15/2004
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