12 G!!!!!
I understand the Rumorous nature of PPrune...but I would have thought that it would take less than that to break the airframe in pieces, yet obviously that did not happen here or this thread would have been two pages long already. Perhaps I under-estimated the strength. Does anyone know what the design parameters are for landing loads?
Last edited by FlyVMO; 17th Dec 2006 at 17:25.
Reason: spelling