I finally got back to drilling of the firewall. I had taken a break from the main airframe and worked on a few smaller parts (brake pedals and seat components).
I spent the beginning of the day getting the firewall properly aligned with the forward edge of the fuselage. I had to grind away a little material on the left longeron to get everything to align properly. There’s a discrepancy in the manual in regards to the position of the firewall. Van’s provides 2 different positions that differ by 1/32 inch. Based on some internet research, it looks like this discrepancy doesn’t matter because any mismatch in spacing will be handled when the cowling gets trimmed.
I used a bunch of clamps to properly locate the firewall to the fuselage. This required a ton of minor adjustments and position checking.
![]()
I used several C-clamps to constraint the longeron against the steel angle.
![]()
Here are the rivets temporarily installed to align the skin to the longeron.
![]()
Van’s doesn’t tell you when to actually drill the bottom skin to the firewall, so I drilled half of the bottom skin holes to lock in the position. I’ll do the other bottom skin holes next time I go in. I drilled all the holes from the side skins to the firewall. ![]()