[EMAIL PROTECTED] (Harry) wrote:
> I do wonder, tho, with a E split tail if one could  get enough prop wash
over
> the elevators to equal the short field take off of a straight elevator
> type...just from total area.......might be offset by the increase in
travel
> as it is in landing and climbing....If both had excess static tail
height.....

I think that the specific design of the split elevator is that the
slipstream does NOT have significant effect upon the elevator's
down-push.

The nine hours I flew in an E model I found this to be the case.

I'd guess that, an overly high C, CD or D tail would handle short
take-offs better than would a later model with the split tail. The max
power slipstream would help the elevator push down the tail. Landings
wouldn't change much.

I think the critical info is now clear about the aileron free play --
7/16 inch if you have balance weights and 5/16 inch if you do not -- and
why it's so important.

Thanks for typing in the AD text in your message, Harry.

-- 
Ed Burkhead
Peoria, Ill.
Ercoupe N3802H, 415-D
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