Mike Halbrook wrote:
Interesting document about the Spitfire. The Spit TR9 I flew in had a placard in the rear cockpit. "Maximum diving speed 370Kts IAS".
The document mentioned they had to add weight to the tail to get the correct CG, I think if they had put a book shelf in the unused radio rack and put in all the documents generated in this rebuild, they wouldn't have needed any lead at all.
It all depends on where it is registered and what the bureaucrats deem is required. Each country and even different aircraft of the same species may end up different.
A while back new spar booms were extruded using an Alum Alloy that ended up testing less than the original. Those ended up with more restrictive speed and G loads IIRC.
I would guess every Spitfire has weight in the back since they all differ from the early models. Each improvement in power brought a larger, heavier engine and prop. The nose extended forward but the tail stayed pretty much in the same spot. To balance the titter-totter you add weight to the aft end.
The Bald Eagle thread has some pics of the Mk XVIII weight installation some where back a few pages.