I think the question has been posed of Van's from time to time and I think the answer has come back that there is no structural loss of integrity here.
I put screws on the floor AND the baggage compartment. I'm glad I did (though I recommend if you do this, get yourself a nutplate jig to make the process easier).
And, sure, it's true you can always drill out pop rivets if you want to get under there for inspection etc., but I hate drilling out pop rivets. What can I say?
Originally I put the screws in the baggage area so that I could add the steps on my 7A to the annual inspection and it just seemed easier to me to be able to do it that way.
If you follow the RV Builder's Hotline, you know that I messed up the edge distance on my rear spar doubler when mating the wings. I've replaced that now (see article in last week's issue), but now I want to replace the fuselage "clevis" too (the edge distance is fine on it, but it has a hole drilled it in nonetheless and I figure if I'm going to start fresh, I might as well start fresh).
Not having to drill out all the pop rivets to get access to it will be one less thing to do, although I wish I didn't have to take off the flap control rods to get access to it.
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