Systems and methods of warning a pilot of a helicopter about a servo transparency condition include devices and steps for retrieving, from a design performance database, a plurality of design performance parameters of the helicopter, and receiving avionics data from an avionics data source, the avionics data representative of a plurality of actual performance parameters of the helicopter. The design performance parameters and the avionics data are processed to determine whether one or more of the actual performance parameters exceed the design performance parameters, thereby indicating a servo transparency condition exists. One or more alerts are generated when the servo transparency condition exists.