Stabilator skins

This morning I spent about 1.5 hrs clecoing the stabilator skins to the skeleton.  This afternoon with the help of S and B we were able to rivet both of the skins to skeleton in about 45 minutes.  We worked very efficiently together.  It is nice to have good help at these stages of the project.

Time: 2.25 hrs.

Right skin attached to skeleton

Right skin attached to skeleton

Skins clecoed in place

B helping to rivet the skins

Stabilator main skins complete

Stabilator skeleton

After over a week from not working on the plane it was good to get back to the project. All the stabilator parts we deburred, prepared for priming, and primed.  Both of the stabilator skins were prepared by priming the matting surfaces and deburring edges. The stabilator skeleton was then assembled and the hinges were placed.

Time: 5 hrs.

Priming of Stabilator Skeleton Parts

Priming of the matting surfaces of skin

Matting surfaces of skin primed

Skin ready for attachment to Skeleton

Assembly of Stabilator skeleton

Hinges on stabilator

Wings kit ordered

Since it will be about an 8 weeks time frame to get the wings kit I decided to go ahead and get it ordered today.  The empennage seems to be going together fairly quickly.  I didn't want to get it finished and then not have the wing kit here.  That gives me 8 weeks to finish the empennage which shouldn't be a problem.

Stabilator Spar / nutplates

Spent a little longer than planned placing the nutplates on the stabilator spar. It seemed like some I had to try several times with a few to get them flush. After trial and error I was able to get a system down and finally got them finished.

I attached the counter balance brackets to the front and aft spar and then started riveting the spar together. 

Time: 3 hrs. 

Nutplates in Spar

Counter Balance Brackets

Beginning of spar riveting

Stabilator begins

We got a great start on the stabilator today.  The RV 12 has what is called a "stabilator" which is a combination of the horizontal stabilizer and elevator.  We deburred and primed all the internal parts. We then worked on drilling of the upper and lower horns and the counter balance arm and bracket.  I did not take a picture of the drilling of the counter balance arm.  It took quite a bit of time to get the holes drilled in the arm. The tougher metal was harder on the bit and I think dulled the bit quite a bit, but we got the holes drilled.  The hard part came in taking the arm and brackets off of the spar.  I think the holes drilled leaved enough burr around the hole that the parts stuck together.  With a mallet and other tools we were finally able to get them apart.  We immediately deburred those holes so we won't have that problem again.

Time: 3.5 hrs.

Priming of Stabilator Spars

Placing clecos in stabilator spar in preparation for drilling of Upper and lower horns and Counter Balance brackets

Drilling of horns

Anti-servo Tabs

I was able to complete section 8 today of the Anti Servo Tabs.  Things went fairly smoothly.  All internal parts were primed with NAPA 7220.

Time 3.5 hrs

Skin Clecoed for match drilling

Match Drilling Hinge with guide

Priming with NAPA 7220

Riveting

Completed Anti-servo tabs

Rudder completed

Boy did I have some great help from N, T, and B this evening. We were able to get the rudder skeleton riveted and then the skin riveted on. We each took a part in the riveting process. One of us took clecoes out, another reamed the holes, another place the rivet in the hole and the fourth used the pop rivet gun to pull the rivet.

At the end of the day we had the VS and the rudder complete. A great accomplishment for beginners of aircraft construction. 

Time: 2.75 hrs. 

Test fitting rudder spar to VS hinges

B Riveting Rudder

Placing clecoes in rudder

Riveting rudder

Riveting rudder

Completed Vertical stabilizer and rudder