Patent ID: 11952109
Assignee: AIRBUS OPERATIONS S.L.
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 1:
2. The piloting-assisting system according to claim 1, wherein each of the first and second pieces of information is determined based on at least one or based on a plurality of pieces of information representative of conditions from the following list:
a predefined position of a lever for controlling retraction of the landing gear,
a predefined position of the landing gear,
a climb rate higher than a predefined climb-rate threshold value,
a climb rate higher than a predefined climb-rate threshold value for a predetermined climb time,
an air speed higher than a predefined air-speed threshold value,
a flight phase for a minimum predefined flight time,
an altitude or a flight level higher than a predefined altitude or flight-level value,
a variation in a reference speed of an engine greater than a predefined threshold value in a course of a predetermined period,
a presence of a condition indicating that a lowered position of the landing gear is preferable,
a position of leading-edge slats,
a position of flaps,
a determination of one flight phase among a plurality of predefined flight phases,
an exceedance of a maximum flight speed in flight configuration with a landing gear deployed.