Aircraft weight and center of gravity cockpit readout system

Claim 1

An in-flight aircraft weight and center of gravity cockpit readout device comprising: a plurality of lifting hooks for attaching to and lifting a load external to said aircraft; a plurality of load measuring means, adapted to sense the weight of said external load suspended from said lifting hooks, for continuously producing a first electrical signal proportional to said weight during the in-flight time of said aircraft; fuel measuring means for continuously producing a second electrical signal proportional to the amount of fuel remaining in said aircraft's fuel tanks during the in-flight time of said aircraft; keyboard input means for providing a third electrical signal proportional to said aircraft's weight and center of gravity prior to the takeoff of said aircraft lifting of said external load; means for receiving and processing said first, second and third electrical signals from said plurality of load measuring means, said fuel measuring means and said keyboard input means respectively to produce a combined weight and center of gravity output signal; indicator means for receiving and displaying said combined weight and center of gravity output signal from said microprocessor means and weight on wheels interlock switch, connected between said microprocessor means and a weight on wheels interlock switch, connected between said microprocessor means and said keyboard input means, for disabling said keyboard input means while said aircraft is in flight thus preventing data alterations from being entered therefrom.