A method of providing power information in a rotorcraft, the rotorcraft having a powerplant. The method comprising calculating a real-time power required and calculating a real-time power available, and orienting power required and power available indicators on a power safety instrument, the position of the power required indicator being dependent upon the calculated power required, and the position of the power available indicator being dependent upon the calculated power available.
POWER SAFETY INSTRUMENT
LEISTUNGSSICHERHEITSINSTRUMENT
INSTRUMENT DE SÉCURITÉ DE PUISSANCE
09.11.2016
Patent
Elektronische Ressource
Englisch