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CG expressed as 25% MAC means the CG is located:
A
25% of MAC aft of the leading edge of MAC
B
25% of fuselage length from the nose
C
25% of total weight forward
D
25% of MAC forward of the trailing edge
A
25% of MAC aft of the leading edge of MAC✓ Correct Answer
Explanation
CG at 25% MAC means it is located at a point 25% of the MAC length aft of the leading edge of the MAC.
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