Discussion
Arrange the steps of a longitudinal stability check in order:
1. Report the static margin
2. Add the tail contribution to find the neutral point
3. Locate the wing aerodynamic centre
4. Compare the neutral point with the aft centre of gravity limit
Select the correct sequence.
Answer: B
The wing sets the starting point, the tail moves it aft, the aft loading limit is then measured against it, and the margin is what that comparison yields. Reversing any pair leaves you reporting a number you have not yet computed.
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