The ideal location of the center of ______ was very carefully determined by the designers.
A. gravity
B. weight
C. balance
D. lift
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When an aircraft is designed, it is made as ______ as the required structural strength will allow.
A. slow
B. heavy
C. slight
D. light
The wings are designed to support the ______ allowable weight.
A. minimum
B. maximum
C. proper
D. appropriate
When the weight of an aircraft is increased, the wings must produce ______ lift.
A. additional
B. different
C. less
D. active
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.
A. active
B. inactive
C. dynamic
D. positive