Brief Description: Horizontal Stab dimple and prime. Begin assembly
0830-1130 finish dimpling parts. primed all interior parts 1300-1730 Assembly of rear spar and front spar. Ran out of AD4704-7 rivets. after looking another time at the plans, they say to use 426 rivets so used these on upper and lower tips of the strength bars. Stopped construction until I get more -7 rivets...ordered from Vans. 6/10/14 update: downloaded the service bulletin for adding the doublers to existing aircraft. The riviet callout on this bulletin clearly shows all rivets are 470 vs the plan callout of 426. I did realize that I used -7 rivets vs -5 rivets in the center area of the doubler.
