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During steady-state climb, which mechanism assists maintaining lift on aircraft wings?

A)Angle-of-attack adjustment via elevator
B)Reduced engine power during ascent
C)Activating spoilers for increased drag
D)Deploying flaps to streamline airflow

💡 Explanation

Maintaining climb attitude necessitates actively managing angle-of-attack through **elevator control** because this directly regulates the airflow over the wing, thereby generating lift. Therefore, continuous adjustment maintains the necessary aerodynamic force, rather than reducing power or increasing drag.

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