I posted the charts for the P-39 N and Q and both sets of flight operation instruction chart contain this statement, varying with configuration:
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So that chart tells me that there is a 20 gallon allowance for warm up and climb to 5000'.
BUT on the climb data chart we have this:
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it also says this on the bottom of the same chart;
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If you look at the climb chart and flight operation instruction chart. they are in conflict with each other as the climb to 5000' is more than 20 gallons (depending on weight)
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So let me put this out there to my fellow pilots, especially Wes, Bill and Biff (if you wish to partake in this groundhoggery) who are all ATPs and have way more time in the air than this Commercially Rated CFII who only flies SEL aircraft - how would you interpret this?
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