Step 1: Recall the purpose of a trim tab.
A trim tab is a small adjustable control surface attached to the trailing edge of a primary control surface.
Its purpose is to reduce the pilot's control force by balancing the aerodynamic moments.
Step 2: Identify its primary function.
During trimmed flight,
\[
\boxed{
\sum M_{CG}=0,
}
\]
where
\[
\sum M_{CG}
\]
is the total moment about the aircraft's center of gravity.
Thus, the trim tab helps maintain equilibrium without continuous pilot input.
Therefore,
\[
\boxed{\text{Ensure that the total moment about the center of gravity equals zero}}
\]
is the correct answer.
Thus,
\[
\boxed{(A)}
\]
is the correct answer.