The design limit is not really lower for negative G. Remember that you are
starting at +1G so, if the limits are +3.8G and -1.8G, the limits are both
2.0g away from steady state flight.

Mike
MU-2

"Peter" wrote in message
...

I think I understand the reasoning behind Va, the max maneuvering
speed, being that the wing will stall (and thus dispose of the
loading) before it breaks. This is why Va falls as the weight falls,
because at any given IAS a higher weight takes the aircraft closer to
stall already.

So, how is it possible to have aircraft destruction due to weather,
e.g. flying into a strong updraught in a CB, if flying below Va?

A DOWNdraught would do it more easily because most aircraft designs
have a lower design limit for negative G.


Peter.
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