OK, OK, I religiously practice the no drink an fly rule, unlike those
morons from Southwest...

but I'm sitting here in my workshop after a hard day of making ribs and
spars for my tail, with a beer in EACH hand, staring at the rear end of
my plane, and looking forward...

I see that the exit point molded into the fuselage for the right rudder
cable is .53" lower than the exit point for the left cable.

Since I've heard no discussion on this list concerning this topic, I
have come to the conclusion after only two beers, that the .53"
difference was designed into the fuselage intentionally, for the
singleminded purpose of making the plane go faster!

Am I right? Did I pass the test?

Angier Ames