CaptainSandl.
While on the general discussion on VMC and I will the first to admit it is probably a stupid and far fetched question (age shall not weary us and all that sort of jazz) - but, if by chance one inadvertently enters an incipient or full spin in a 737 such as may be caused by slow reaction to a flame-out on one engine at high altitude, will full rudder be available for recovery action? - keeping in mind relatively low IAS at the time and the fact that the rudder pressure reducer would have been activated automatically at 700ft (?) after take off?
