3,777
edits
SECTION 29: FUSE SIDE SKINS: Difference between revisions
m
→29-14
m (→29-14) |
|||
| Line 3: | Line 3: | ||
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] | ||
== 29-11 == | |||
* See this [https://www.facebook.com/groups/vansrv10/posts/4218804234907310 FB Post] on how to keep the skin and clamping block in place while bending. | |||
== 29-14 == | == 29-14 == | ||
* Step 5<br>When match drilling from the F-1001B angle into the WD-1002-L / WD-1002-R firewall steel brackets, be aware that it's easy to violate the edge distance in the steel bracket (2 x D, measured from the center of hole). Remedy is to temporarily install a bolt into the engine mount hole to pull the bracket into place and to use a clamp to move the steel bracket to increase edge distance.<br>See also [https://www.facebook.com/groups/vansrv10/posts/4932489646872095/ FB post 4/17/2022] | * Step 5<br>When match drilling from the F-1001B angle into the WD-1002-L / WD-1002-R firewall steel brackets, be aware that it's easy to violate the edge distance in the steel bracket (2 x D, measured from the center of hole). Remedy is to temporarily install a bolt into the engine mount hole to pull the bracket into place and to use a clamp to move the steel bracket to increase edge distance.<br>See also [https://www.facebook.com/groups/vansrv10/posts/4932489646872095/ FB post 4/17/2022] | ||