GE CF6-80C2B2

Service difficulty reports · 156

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 = 'CF680C2B2'
  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 CA980707023Blade · worn(CAN) DURING HIGH PRESSURE COMPRESSOR (HPC) BORESCOPE INSPECTION, DISCOVERED THE FIRST STAGE HPC HAD WORN IN THE PARENT METAL OF A BLADE MID-SPAN SHROUD AND THE CARBOLOY PAD WAS MISSING. PER THE AIRLINES WORK CARD 72004, ITEM 1, THE DAMAGE IS NOT PERMITTED. Jun 10, 1998 · Turbine Engine Compressor SectionSDR CA980602024Duct · broken(CAN) LEFT EGT ABNORMALLY HIGH ON TAKEOFF (APPROACHING AMBER ZONE). DURING CLIMB, THE LT ENGINE EGT REMAINED 60 DEGREES HIGHER THAN THE RT ENGINE. LT PNEUMATIC PRESSURE 25 PSI. IN CRUISE, THE LT ENGINE DROPPED TO A MORE ACCEPTABLE LEVEL. ON ARRIVAL AND INSApr 27, 1998 · Turbine Engine Compressor SectionSDR DL76G980255Thermal Shield · crackedSHOP FINDINGS - NO FLIGHT INCIDENT. DURING OVERHAUL OF ENGINE 695373, THE HPT THERMAL SHIELD WAS FOUND TO HAVE A FLANGE TO FLANGE CRACK. THIS PART PROVIDES THE ROTATING SEAL BETWEEN THE T1 AND T2 DISK. THE THERMAL SHIELD IS NOT LIFE LIMITED. DUE TO THE CRAJan 29, 1998 · N154DL · Boeing 7673P6 · Engine (Turbine/Turboprop)SDR CA970922001Compressor · failed(CAN) NR 1 ENG FAILED DURING TAKEOFF ROLL AT APPROACH AT APPROX 20 KNOTS. COMPRESSOR FAILED AND CAUSED DAMAGE TO THE REVERSER HALVES, FAN COWL, INBD AILERON AND FUSELAGE. AILERON HAS TWO SMALL HOLES AND FUSELAGE HAS ONE HOLE 1.5 INCHES IN DIAMETER. REPAIREDSep 5, 1997 · Turbine Engine Compressor SectionSDR CA970130006Plug · not engaged(CAN) ON TAKE-OFF, EICAS LT HP SOV GAVE AN INDICATION. AFTER REDUCING TO FLIGHT IDLE, THERE WAS STILL NO CHANGE. INSPECTION FOUND THAT PLUG D4210P WAS NOT FULLY ENGAGED. PLUG REMOVED, CHECKED AND REINSTALLED. ENGINE RUN PERFORMED AND CHECKED. THE LEFT HANDec 12, 1996 · Engine (Turbine/Turboprop)SDR UPS604852Fuel Pump · failedCREW REPORTED, RT ENGINE FLAMED-OUT AT TOP OF DESCENT. INFLIGHT START ATTEMPT UNSUCCESSFUL DUE TO NO FUEL FLOW. MAINTENANCE REMOVED AND REPLACED FUEL PUMP IAW MM 73-11-01.Oct 23, 1995 · N302UP · Boeing 76734AF · Engine Fuel Pump
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