Maneuvering limit load factors with Flaps Down are within which range?

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Multiple Choice

Maneuvering limit load factors with Flaps Down are within which range?

Explanation:
Maneuvering load limits show the G-forces the airframe is certified to tolerate during maneuvers in a given configuration. When the flaps are down, the airplane is in a high‑lift, slower‑flight setup, which changes the loads on the wing and flap system. To prevent overstressing the structure in this configuration, the allowable maneuvering G-range is reduced to a safer window: from 0.0 g up to 2.0 g. The lower bound of zero means sustained negative G in this configuration isn’t permitted, and the upper bound of 2.0 g covers typical slow-flight maneuvers without risking structural damage.

Maneuvering load limits show the G-forces the airframe is certified to tolerate during maneuvers in a given configuration. When the flaps are down, the airplane is in a high‑lift, slower‑flight setup, which changes the loads on the wing and flap system. To prevent overstressing the structure in this configuration, the allowable maneuvering G-range is reduced to a safer window: from 0.0 g up to 2.0 g. The lower bound of zero means sustained negative G in this configuration isn’t permitted, and the upper bound of 2.0 g covers typical slow-flight maneuvers without risking structural damage.

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