the (3 in most cases) main structural supports in the tail (i.e. spars), of the (again in most cases) left and right horizontal stabilizers, and the vertical stabilizer.
I been finding some oddities in AH lately and I don't think using a preconceived notion that may or may not be based on fact (because dang if I can remember which) is very wise so I'm doing a little back ground study first

This particular one is the treatment of both the left and right tail spars as one in the damage model, yet if this was so the vertical stabilizer should come off as well do to the interconnection of the three, correct? (i.e. if it has enough force to rip off both spars then the joint would come off too, where the vertical stabilizer spar is connected, in most cases)
I am taking into account that the damage model in AH does represent varying degrees of damage, although they are not shown (if it's damaged enough to impair flight, it comes off) But even if the tip of one side is hit of the horizontal stabilizer, all direction stability is lost.
Because of the amount of force excerted on the tail in flight, I have the preconceived notion that, while it would be greatly hamperd, SOME control should still exiest, due to the strength of tail spars.
Sooo...just curious if that assumption on the strength of spars is correct.

[This message has been edited by Jigster (edited 12-08-2000).]