Stability and Control characteristics of the Early Mark Spitfires

[Glider]

Originally Posted by Crumpp

????

I never said it was complete. I counted 13 incidents only halfway thru the serial listings for the just the Mark I in Morgan and Shacklady.

There some 9 pages of this irritating tiny print. You can go through them.

Again,

The measured and defined stability and control of the early mark Spitfires is neutral to unstable at normal and aft CG.

That statement holds true for any measured results.

Unfortunately, there are only a few measured results from the United Kingdom because there was no standard in place. In otherwords, there was no ruler outside of pilot opinion.

I know it isn't complete and I appreciate the effort but all the ones you mention are not relevent to the case, so as I said, is this the best you can do.

Have you found any at all so far re spins, you will recall that you were once very keen saying that spits broke up in a spin and so far nothing to support it. In a similar manner we have nothing to support the piles of bent wings, or an unusual number of accidents, nothing at all. No mention of this as an issue in any of the hundreds of books that have been written about this aircraft and the BOB.

All we have is your spin of a known factor which pilots were warned of.

All we have is you making a worst case scenario out of something everyone was aware of and wasn't a major problem.

Edit - I should add that also have yet to prove that the level of instability admitted by one and all, is an unsafe level or even that it is unsuitable for a fighter.