GE CT58-140-2

Service difficulty reports · 112

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 = 'CT581402'
  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.

SDR CA070726004Seal · cracked(CAN) MULTIPLE CRACKS THROUGH KNIFE EDGE SEALS. THIS REPORT WILL ALSO BE SUBMITTED TO MFG IAW SEI-183 SECTION 72-32-7 PAGE 302. (TC NR 20070726004)Jul 26, 2007 · Turbine Engine Compressor SectionSDR CA070221006Motor · inoperative(CAN) ON PRELANDING CHECK, MAIN LANGDNG GEAR FAILED TO EXTEND. EMERGENCY BLOW DOWN PROCEDURE WAS FOLLOWED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INVESTIGATION DETERMINED THAT THE ELECTRIC MOTOR THAT DRIVES THE MLG HYDRAULIC PUMP HAD FAILED AND TRIPPED Feb 13, 2007 · Skrsky S61N · Landing Gear Retraction/Extension SystemSDR U0GA113313Radar · malfunctionedDURING CLIMBOUT SWITCHED WEATHER RADAR FROM STANDBY MODE TO SEARCH 3 MODE. RADAR SCREEN WAS FUZZY AND RT FAILURE LIGHT WAS ILLUMINATED. AT FIRST SUSPECTED MOISTURE AND WAS WAITING FOR MOISTURE TO EVAPORATE. AFTER APPROXIMATELY 15 SECONDS NOTICED ACRID ODOR FRDec 20, 2006 · N564EH · Skrsky S61N · Weather Radar SystemSDR CA061214004Blade · missing(CAN) RECEIVED THIS ENGINE WITH A DEFECT OF LOW POWER. IT WAS RUN ON THE TEST STAND TO CONFIRM THE POWER OUTPUT WHICH WAS 1440 SHP. WHEN THE ENGINE WAS DISASSEMBLED THEY FOUND THAT A BLADE WAS MISSING FROM THE COMPRESSOR 4TH STAGE. THERE WAS NO DAMAGE TO THEDec 14, 2006 · Turbine Engine Compressor SectionSDR CA060517003Damper · leakingPILOT FELT A YAW ON APPROACH, AND AFTER CONFIRMING A YAW HARDOVER, SWITCHED OFF AUX HYDRAULICS, AND CONTINUED TO LAND. ON INSPECTION IT WAS FOUND THAT THE PEDAL DAMPER WAS LEAKING EXCESSIVELY DUE TO A BROKEN BOLT AND CAP.May 5, 2006 · Skrsky S61N · Rudder Control SystemSDR ERAA097087Throttle · contaminatedWATER CONTAMINATED, EMERGENCY THROTTLE LOCKED UP. DUE L/O IN 96 HOURS. ECU SHAFT AND THROTTLE VALVE STIFF 6O ROTATE, FUEL PUMP DRIVE SHAFT VERY STIFF. INTERNAL CORROSION TO FUEL SYSTEM DUE 6O WATER CONTAMINATION. INHIBIT AND PRESERVE ENGINE FUEL SYSTEM IAWAug 20, 2004 · N562EH · Skrsky S61N · Power LeverSDR CA040213006Spar · cracked(CAN) MAIN ROTOR BLADE LEAK CHECKED AT BASE AND SPAR FOUND TO BE CRACKED.Feb 2, 2004 · Skrsky S61N · Main Rotor BladesSDR CA040117001Warning Light · illuminated(CAN) AT 5500 FT VFR ENROUTE TO THE PLATFORM, JUST NEARING THE COASTLINE, THE MASTER CAUTION AND INTERMEDIATE GEARBOX CHIP LIGHT ILLUMINATED.Jan 15, 2004 · Skrsky S61N · Main Rotor GearboxSDR CA030610002Blade · cracked(CAN) DURING A DAILY INSPECTION A CRACK WAS FOUND IN THE INBOARD SIDE OF THE TRAILING EDGE POCKET. THE CRACK STARTED AT THE TRAILING EDGE AND PROPAGATED FORWARD APPROXIMATELY 70MM. (2.75 INCHES)Jun 5, 2003 · Skrsky S61N · Tail Rotor BladesSDR CA030212009Blade · cracked(CAN) INBOUND FROM RIG, 'BIM' LIGHT ILLUMINATED. EMERGENCY CHECKLIST C/W. AIRCRAFT DIVERTED TO SABLE ISLAND FOR PRECAUTIONARY LANDING. COMM CENTRE ADVISED.POST S/D CHECK CONFIRMED PRESSURE BELOW LIMITS.Feb 7, 2003 · Skrsky S61N · Main Rotor BladesSDR 20001019SH024Freewheel Unit · slippedWHILE IN CRUISE FLIGHT, AIRCRAFT YAWED AND THE NOSE DROPPED. FOUND NR 1 TORQUE AT TOPPING AND NR 2 TORQUE AT ZERO. CONTROLLED RPM (ROTOR) WITH COLLECTIVE. FOLLOWED EMERGENCY CHECKLIST, RETURNED, AND LANDED. SUBSEQUENT PRELIMINARY INVESTIGATION REVEALED FRSep 15, 2000 · N562EH · Skrsky S61N · Engine/Transmission CouplingSDR 20001024SH001Valve · brokenDEPARTED MC822 EN ROUTE TO VENICE. DURING LETDOWN TO VENICE, A SLIGHT FUEL ODOR DETECTED. AS POWER INCREASED TO LEVEL AT 500 FEET, NR 2 ENGINE CAME OFF-LINE. N1 NOTED AT APPROX 60 PERCENT, TORQUE AT 20-30 PERCENT, NF HAD SPLIT FROM NR 1 NF. A STRONG FUEL OAug 29, 2000 · N563EH · Skrsky S61N · Fuel Controlling System
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