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* 10/05/21 [https://www.vansaircraft.com/wp-content/uploads/2021/10/08_10.pdf 08_10.pdf] | * 10/05/21 [https://www.vansaircraft.com/wp-content/uploads/2021/10/08_10.pdf 08_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] | ||
==== Page 8-3 ==== | |||
* Step3: The 1 21/32 lower flange width dimension is to be applied at the 1 inch line, not at 2 inches, the raw angle size. | |||
==== Page 8-7 ==== | ==== Page 8-7 ==== | ||
* Step 3: only cut back the two corners on the front edge of the nose rib, not the entire edge because then you will violate the edge distance for the foremost rivet. See also this [https://www.facebook.com/groups/vansrv10/posts/5918655041588879 FB thread]. | * Step 3: only cut back the two corners on the front edge of the nose rib, not the entire edge because then you will violate the edge distance for the foremost rivet. See also this [https://www.facebook.com/groups/vansrv10/posts/5918655041588879 FB thread]. | ||
* Step 4: Very likely that the nose rib that came with a recent kit already has the holes in the web that step 4 calls out for making | * Step 4: Very likely that the nose rib that came with a recent kit already has the holes in the web that step 4 calls out for making |
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