New structural G-limit feature

[WTE_Galway]

Originally Posted by Bellator

The Spitfire II might be able to take ~12 G's before suffering a catastrophic failure, if those tests are accurate mind you, but damage would occur way before.

Point is though that the Spitfire got a lot heavier through each version, and by the time of the Spitfire Mk.IX you'd have crept up around the 5.3 G load limit area with a 1.5 safety factor. (8 G breaking point)

By comparison the Fw190 A-8 had a load limit factor of 6 G at take off weight with a safety factor of 1.8. (10.8 G breaking point)

So it really aint true what you're saying, i.e. that the Spitfire's wings could take as much as the Fw190's, which would also seem abit odd as the Fw190's wings look a lot more robustly constructed.

Among other differences the fw190 undercarriage is outboard and the wheels fold inwards.