Gordon,

All I'm saying is that there's more opportunity to do low labor per
square foot of fuse with fiberglass than with aluminum, ans since we are
talking about commercially built structures, that's all that matters
when you are trying to get a basic airplane out the door for less than
80, or even 60K.

As for using pull type rivets... do you really think any commercial
entity is going to roll out insured airplanes with the equivalent of pop
rivets?