Van's Aircraft RV-12

Van's Aircraft RV-12

Sunday, October 17, 2010

10172010 Empennage (Build Session 10)

Build Session 10, 10172010, 1.5 hours, 24 total

Empennage, Rudder Page 07-02 and 07-03

Completed through Step 07-03 and stopped to Prime contact parts.

Rivet Count 63 Solid 347 Pulled

Trial fitting rudder spar caps and hinge brackets


Trial fitting the rudder control horn



Fitting the rudder spar to the vertical stabilizer to check hardware and clearance, send ing question to Vans re the gap seen below, the plans allow for only one washer between the brackets. I don't think their should be a gap otherwise it will pinch when tightened, may be by design but it does not look right to me. (Note the spar holes and the brackets were pre-drilled and are self aligning)

Priming for assembly



No comments:

Post a Comment