Not sure about the question but consider that many aircraft have two or more forward CG limits.
1. Most forward CG at gross weight and a sloping forward limit, moving more forward as weight reduces:
2. Most forward CG regardless of weight.
The CG range is the range between forward CG limit and aft CG limit at the specified weight.. If the aircraft has a sloping forward limit, the most forward CG limit moves aft as weight is increased. Answer A.
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