Method for piloting an aircraft in approach phase

Details Method for piloting an aircraft in approach phase Method for piloting an aircraft in approach phase

G - Physics

05

D

G05D 1/06 (2006.01) B64C 13/18 (2006.01)

Patent

CA 2653638

According to the invention, high lift leading-edge slats (13) and high lift flaps (14) are simultaneously deployed, when the speed of the aircraft is equal to and less than an AES threshold.

Selon l'invention, on déploie simultanément et automatiquement les becs hypersustentateurs (13) et les volets hypersustentateurs (14), lorsque la vitesse de l'aéronef est égale et inférieure à un seuil AES.

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