题目内容
When an aircraft is designed, it is made as ______ as the required structural strength will allow.
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The wings are designed to support the ______ allowable weight.
When the weight of an aircraft is increased, the wings must produce ______ lift.
When the weight of an aircraft is increased, the structure must support not only the additional static load, but also the ______ load imposed by flight maneuvers.
The pilot in ______ of the aircraft has the responsibility on every flight to know the maximum allowable weight and its CG limits.
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