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

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Multiple Choice

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

Explanation:
Maneuvering limit load factors define the maximum g-forces the airframe is designed to endure during flight maneuvers. When the flaps are up, the aircraft is in a clean configuration, which allows a higher positive limit while keeping a modest negative limit to protect the structure. The standard values for this setup are +2.5 g in the positive direction and -1.0 g in the negative direction. So the allowable maneuvering range is -1.0 g to +2.5 g. Other ranges would either exceed the positive limit, go beyond the negative limit, or omit the negative side, which isn’t consistent with the configured structural limits.

Maneuvering limit load factors define the maximum g-forces the airframe is designed to endure during flight maneuvers. When the flaps are up, the aircraft is in a clean configuration, which allows a higher positive limit while keeping a modest negative limit to protect the structure. The standard values for this setup are +2.5 g in the positive direction and -1.0 g in the negative direction. So the allowable maneuvering range is -1.0 g to +2.5 g. Other ranges would either exceed the positive limit, go beyond the negative limit, or omit the negative side, which isn’t consistent with the configured structural limits.

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