Friday, October 12, 2018

Fuselage, Part 5 Edge Distance

As others have said, the forward fuselage becomes an exercise in edge distance. This means the closeness of a hole to the edge of the aluminum. It is suppose to be 2 times the hole diameter from the center of the hole to the the edge. So a little fancy math gives 1 1/2 hole diameters from the edge of the hole to the edge of the metal.

This first became a problem for the F-623A clips that couple the mid and aft fuselages. In the picture you will see the plans-built version all primed and ready to go. The non-primed are the ones I remade to solve the edge distance problem as evident by the "x" on the part, where the hole would have ended up.

 Everything was going great until I arrived at the F-719 installation. These parts are "joggled" to overlap the F-904 bulkhead. My parts didn't fit very well; and the rivet would have been right at the jog.  I ended up adapting, as builders often do, and used a second angle piece as shown in the picture. I will round the edges so that these pieces play nice with the passengers. 

Following others advice, I was very careful to measure all edge distances before drilling. Some are VERY close. I followed the plans and drilled the holes in the F-713 longeron on the center line, this puts the hole in the F-9101 close to the edge. But there is also a 3/16" bolt that goes thru this longeron for the front tank mount; everything must be dead nuts on. The F-9101 needs to have the edges radius per the plans, otherwise the holes in F-713 are pushed pretty far off as shown in the picture.



So far the kit pieces do fit together very well. I think most of my trouble has been operator error. No more beer for you- Seinfeld