[FlusiRainer]

In der aircraft.cfg

[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 113.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 84000 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?


den Wert für "fuel_flow_gain =" verringern.