Flight control indicator for an aircraft, in particular a transport airplane,
intended to supply the thrust generated by at least one engine of the aircraft.
The flight control indicator (1) comprises display means (4) which
present, on a viewing screen (5), a dial (6) which is graduated in
percentage, whose maximum represents the maximum thrust available for the current
phase of flight, in the current configuration of the aircraft and for the current
anemometric conditions, and which is furnished with characteristic signs (7,
8), whose positions on the dial (6) respectively represent prescribed
and actual thrusts which are expressed as a percentage of the maximum thrust.
