New structural G-limit feature

[Tempest123]

Originally Posted by Bellator

Well if they use the real life limit load factors then it would be pretty bad for Spitfire pilots as the limit load factor for the Spitfire was some 5.33 G's compared to the std. German 8 G's and US 7.33 G's.

But then again, most pilots back then blacked out at around 4 G, so anything above 5 G is gonna entail flying in the blind anyway

5.33 g's for a spitfire max g-limit? Where does this information come from? For example the F8F Bearcat was restricted to 7.5 g's after failures of its wingtip ejection system, I highly doubt that a lighter and smaller fighter which saw exponentially more combat than the Bearcat, and with no history of chronic failures would have a limit of 5.33 g's. The g-limit would vary between aircraft, not between countries.