Yearly Archives: 2015


Fuselage 26 – Mounting the Horizontal Stab

Today is an exciting, and somewhat nerve racking day. Its time to begin attaching the horizontal stabilizer to the fuselage. A few of these bolts require an accurate drill, and leave little room for error. The first step was to sit the horizontal stab in place. The forward spar sits on top of the 1/8 aluminum spacers shown here. 

The rear spar requires a 3/16″ lift. The best spacer to use is a 3/16″ drill bit. Lightly clamp the fuselage in place and center it using the intersection of the rear spar halves.

Here is the centered position marked with the ruler and blue ink. You can see perfect alignment with the intersection of the two spar halves.   

Now its time to clamp the front lightly. The clamps at the rear should be firmly in place to ensure the center position does not move. However, you want some wiggle room in the front as you ensure that horizontal stab is perpendicular to the fuselage.

This is also the time to ensure the horizontal stab is level. Mine appears just ever so slightly higher on the left. However, its true to the fuselage level. I sat a portion of aluminum angle on top of two wooden block spacers.   

Here’s a good picture of the level, angle, and spacers in position.   

After this, you want to verify that the angle of incidence is zero degrees. This is measured between the chord line of the horizontal stabilizer and the top longerons. The tooling holes in the ribs are centered on the chord line. I used a cleco in each tooling hole and then measured. The alignment was correct.
  

To ensure the stab is perpendicular to the fuselage at a 90 degree angle, I measured from the intersection of the cockpit rails to the aft outer corner of each side of the stab.

I offset the starting point at 2 feet to counterbalance the tape measure.   

Now here comes the tricky part. After the fuselage has been leveled and trued in each direction, its time to drill the most difficult holes. These holes will go through the forward spar splice angle, the aft deck, angle and upper longerons. There isn’t much, if any wiggle room. Further compounding the difficulty, is the ambiguity of the diagrams and instructions. The instructions call for the outside bolt to be 1/2″ in from the outside of the upper longeron. I used my small ruler placed between the skin and the longeron to draw the precise location of the outer edge of the longeron. 

I then measured 1/2″ in.   

Here is a good shot of the underneath. You can see the intersection gives little room for proper edge distances. Be sure to start with a small pilot hole so that you can walk the larger drill bits in the direction you need as appropriate.
  

My right outer bolt is too close to the longeron edge for my comfort. Its only just on the good side of edge distances for the angle. This illustrates the futility of trying to have all 3 edge distances in alignment. Some people argue that the longeron is the most important.

The other hole is much more comfortably in edge distance tolerances.   

Here’s why I don’t necessarily buy the longeron being the most important edge distance. The diagram, which is to scale, clearly shows that the hole as positioned by Van’s engineering team does not meet the edge distance requirements. I have marked the appropriate edge distance in blue on the ruler below.    

All this being said, I was rather perturbed by the edge distance of the hole on the right longeron, and I decided to call it a night. I’d need to read up on this issue and give it some thought.


Fuselage 25 – Prep for empennage attachment

My hangar mate’s plane is out for its annual inspection, so I have a few weeks where I have extra room. I decided this was the perfect opportunity to get started on the empennage attachment.

I knew I’d need a second set of hands to remove the fuselage from the rotisserie and get everything situated. Luckily my buddy Mike was willing to help. The first step was to rearrange the hangar as best I could and prepare space for removing the fuselage from the rotisserie.

After we removed the fuselage from the rotisserie, Mike was kind enough to keep my mobile platform in the back of his hangar. While he put that away, I built a quick and dirty fuselage stand from some basic saw horses.

Here you can see the fuselage in its new location. I’ve offset the tail to allow for the empennage to be attached.   

Fancy? Nope. Effective? Yes.

We put the tail feathers in place just to see it. Its a good feeling. This actually looks like a plane! I can’t wait until the wings go on!  

In the next session I will begin work on the actual attachment of the empennage.   


Fastback 12 – Vert Stab Modification

The Showplanes Fastback is slightly higher than stock at the intersection of the turtle deck and the vertical stabilizer. As a result, the front of the vertical stabilizer must be trimmed to allow sufficient clearance. 175 degrees to be exact. I bought a protractor on my way to the shop today, and presto here’s the result. Before this photo was even taken, I removed all the appropriate rivets. 

As you can see, this doesn’t allow the existing rivet holes to be placed nicely in the new layout. The new line is close to the second hole, and essentially bisects the next two. I gave careful consideration to how I should approach this problem. Online I found a few pictures, but nothing with enough detail. I found one builder who build a new rib. I briefly considered doing this as well. Getting the existing rib to fit, turns out to be a challenge.
  

Next, nothing to do but start the cut!

I really didn’t want to have any chance to harm the front spar so I protected it with some scrap aluminum I had laying around.   

Here’s the part that has only one photo, but took a ton of time!! Fitting that rib into position. I wound up fluting the nose and redoing some of the flange bends to narrow the nose of the rib down. I also redid the rear flange bend to pull the entire rib aft. This is a better solution (in my mind) than creating a new rib from scratch (which for me, is something I’ve never done).   

Here’s a good picture of where the previous rivet holes are after the cut. Not optimal. If I keep the same holes in the rib, there will likely be some of these that are very close together, especially those closes to the spar. I measured, and the aft most rivet (not in the spar) would almost touch one another. That won’t do!

The best solution I came up with was to create three new rivet locations aft. You can see them marked here. I was able to keep approximately the same spacing, and ensure that there was ample edge distance for every new hole.   

As for the old holes, I flattened them, and made sure they were as smooth as possible. They each have a firm new rivet on either side of them, which according to the acceptable methods of aircraft repair is the appropriate method.

I filled in the holes with a little JB Weld. Not for strength, but to build the primer / pain on to later.

Here’s a good picture of the end result. I’ve tried to diagram where the original holes are in the rib, and where the new ones are. The original holes in the skin are fairly obvious.   

Apparently I missed the note to leave these spots empty for the fairing. I did the same thing on the elevator. Man, what a newb I was then!

Next, I pulled the horizontal stab down, and removed the elevators. (They were just placed there temporarily for storage). I’m considering taking care of Service Bulletin 14-01-31 before installing the empennage. This is a bear of a project, so I’m not convinced yet. It isn’t required unless cracks form in the spar. Until such time the only requirement is yearly inspection. However, this project will not become easier after installation.   

I do not have the required relief notches. Upon review you can see them in the drawings, but there are no reference to them in the instructions.

Again with the fairings!  

Session time: 7 hours