Nihon_Ni
Well Known Member
I may have been in the sun too much this weekend, but I'm having trouble understanding when to join the center bottom skins (under the seat rib assembly) and I hope someone can point me in the right direction.
In the "Seat Substructure Assembly" section of the plans, p. 8-13 says to dimple all #40 holes in the F-826/27 which are common in the Seat Rib Assembly. There's a note against dimpling the forward and aft two rows of holes that are not common with holes in any of the seat ribs, but no mention of the holes that join the two skins in the center of the aircraft. A few steps later the plans say to rivet the F-826 & 827 to the rear spar attach bulkhead assembly and the inboard seat ribs, so it seems like these holes should be dimpled prior to this step, but I haven't been able to find mention of them. Dwg 74 calls out AN426AD3-3.5 rivets for these holes, so they certainly need dimpled, but when do I do it?
Thanks,
Rob
In the "Seat Substructure Assembly" section of the plans, p. 8-13 says to dimple all #40 holes in the F-826/27 which are common in the Seat Rib Assembly. There's a note against dimpling the forward and aft two rows of holes that are not common with holes in any of the seat ribs, but no mention of the holes that join the two skins in the center of the aircraft. A few steps later the plans say to rivet the F-826 & 827 to the rear spar attach bulkhead assembly and the inboard seat ribs, so it seems like these holes should be dimpled prior to this step, but I haven't been able to find mention of them. Dwg 74 calls out AN426AD3-3.5 rivets for these holes, so they certainly need dimpled, but when do I do it?
Thanks,
Rob