FIELD: transport.
SUBSTANCE: aircraft pilotage device (1) comprises data sources (2) determining airscrew and turbine parametres and aircraft parametres, processing device (3) that computes, proceeding from aforesaid magnitudes, power parametre that allows for current power vs maximum power produced without aid intake at altitude at sea level in standard atmosphere, display (5) that displays on screen (7) at least one characteristic symbol (11) describing aforesaid power parametre.
EFFECT: optimum feedback with respect to engine output in whatever power range of aircraft turboprop engine.
5 cl, 5 dwg
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