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Otherwise you seem to have chosen same tactics as in the FTH discussion so my part end here now.
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What "tactic" is that?
You mean showing you the question on an A&P exam?
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If a turbo engine is rated at 310 HP up to 18,000', the altitude specified is pressure altitude?
False, the altitude specified is density altitude
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http://quizlet.com/2496371/print/
Start another thread on the weight and balance or send me a PM. I would be happy to walk you through the steps in determining percentage MAC.
It is not that hard to do. You will understand it and see how ridiculus the theory the NACA could not do one really is!!
In presenting a February 1944 weight and balance document and for the purposes of this discussion on 1940 Spitfires:
You have presented the solution to the problem in an effort to claim the problem never existed.