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SECTION 29: FUSE SIDE SKINS: Difference between revisions
SECTION 29: FUSE SIDE SKINS (view source)
Revision as of 22:33, 28 September 2024
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* 10/05/21 [https://www.vansaircraft.com/wp-content/uploads/2021/04/29_10.pdf 29_10.pdf] | * 10/05/21 [https://www.vansaircraft.com/wp-content/uploads/2021/04/29_10.pdf 29_10.pdf] | ||
Check for more recent updates [https://www.vansaircraft.com/service-information-and-revisions/?aircraft=rv-10&doctype=revisions-changes&sort=date here] | Check for more recent updates [https://www.vansaircraft.com/service-information-and-revisions/?aircraft=rv-10&doctype=revisions-changes&sort=date here] | ||
== 29-2 == | |||
Note that when bending the longerons, the template has parts that are almost completely straight. It is easiest to identify that and avoid curving that part (don't be like me and just start curving everything to start). | |||
Note that the "Aft Twist Mark" is not applicable for F-1013-L because it is the shorter longeron. | |||
== 29-3 == | |||
The instructions don't specify, but you do the FWD TWIST on both longerons since the parts are symmetrical (other than the fact that one is shorter to accommodate the cargo door). | |||
== 29-6 == | |||
I found Step 2 and especially Step 4 to be fiddly. Note that the thickness of the AA6-063 is 1/16" thick so I used as scrap piece of this to make sure the 1/16" offset was implemented correctly. | |||
== 29-7 == | |||
* Step 3: The number of holes in the top flanges of the F-1015C Mid Cabin Decks is one greater than the number of holes drilled into the F-1013 longerons using the template. I haven't finished the chapter yet so I'm not sure what will happen, but for now I'm not match-drilling that extra hole. I'll try to remember to update this when I'm done with this chapter. | |||
== 29-11 == | == 29-11 == | ||