Oh yeah, every forum where you've bullshat your way into a corner.
> So, let me get this straight.
> "the FAA itself" has actually verified your position?
It most certainly did, to anyone who actually has some understanding of the subject matter. You can "beg to differ" all you want. Someone who thinks "load" in structural engineering only means "weight" -- and that that's all the FAA cares about! -- is manifestly unqualified to understand either FAR 25 or the direct answer I got from the FAA about limit and ultimate loads.
But let's put that assertion to the test. In his response, Mr. Johnson said, "The loads then that are considered would include such loads flight maneuver, gust, torsion, delta P."
"Flight maneuver" would indeed be those g-loads you've been talking about, which are covered the Flight Loads section. Please explain the rest of that sentence in your own words, and then explain to me why you think they are excluded from the 1.5 factor of safety.
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