Which has what to do with the MAC on the weight and balance sheet? You can be they did their own weight and balance analysis too!!!
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The only thing that changed was the revised CoG limits for the aircraft with Rotol propeller and bob weighs if the CoG went beyond the normal limits, as often happened in the case of the Spitfire V.
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Negative.
Spitfire K-9788 shows an aft CG that is 33.2%.
The most aft MAC with the Feb 1944 revision is 31.7%.
They closed up the CG limits to address the longitudinal instability.
You have presented the solution to the problem in an effort to claim the problem never existed.