Van's released SB 18-09-17 to address some cases of the aft fuse bottom skin cracking (examples of the cracks in flying aircraft can be found here and here).
Following inspection of my airframe, I found no evidence of cracks.
However, I chose to install the stiffeners as described in the
service bulletin. The process took less than an hour with two
people: One in the empennage and other underneath.
Here are the parts associated with the service bulletin.
Because the F-14148A Skin Doubler (the
diamond) is affixed to the exterior of the dimpled F-01478 Bottom
Skin, the dimples would remain unfilled and preserve voids under the
six rivets which attach the Skin Doubler. So I chose to create
fillers for the dimples by using drilled out rivet heads for the
purpose. Thus, I drilled out about 25 rivets on scrap to make
sure I could obtain 6 rivets with well-centered holes. I then
sanded them smooth. These six fillers were cleco'd into place on the
Skin Doubler prior to cleco'ing on the skin (after all, we're working
upside down here!), as shown below.
Removing the F-01406F Baggage Bulkhead
Corrugration, placing boards and towels in the baggage area and a
blanket in the tail, it was trivial to access the area required to
install the stiffeners.
A 12 inch #30 drill bit was used to match
drill the bottom holes in each of the F-14147 Stiffener Clips. There
was adequate space available to squeeze the AN470AD4-4 universal
rivets with my longeron yoke. Tungsten bucking bars were used
to buck the AN426AD3-x rivets. It's worth noting that I
increased the length of each AD3 size rivets by 0.5 as compared to
what the SB calls out.
Forward side of the Side Frames showing
forward interior stiffeners in place.
Aft side of Side Frames showing single
aft interior stiffener in place.
Exterior views of diamond Skin Doubler.
I need to clean up the area with acetone as I chose to prime the
associated surfaces.
No comments:
Post a Comment