SYSTEM AND METHOD FOR ADJUSTING A DYNAMIC SCALE INDICATOR ON A FLIGHT DISPLAY OF AN AIRCRAFT

Methods and systems are provided for adjusting a dynamic scale indicator on a flight display of an aircraft. The method comprises receiving an operational status parameter for the aircraft and generating the dynamic scale indicator located on the flight display of the aircraft. The dynamic scale indicator includes a positive value range that represents operational status parameter values greater than a selected setting value and a negative value range that represents operational status parameter values less than the selected setting value. The operational status parameter is translated into a value that is represented on the dynamic scale indicator. The value ranges shown on the dynamic scale indicator are adjusted by fading the negative value range when the operational status parameter value is positive, fading the positive value range when the operational status parameter value is negative, and fading the value range to the extent that the value range exceeds the operational status parameter value.