One of the first items in Van’s instructions for
assembling the tail cone fuselage frames is to rivet the F-1208A nylon wear
plate onto the F-1208-R fuselage frame with two LP4-3 rivets. The wear plate
prevents the control cables from wearing into the fuselage frame. There is also an
accompanying note stating the wear plate can be turned 180 degrees before
requiring total replacement. Just thinking about drilling out rivets in the
tail cone makes me cringe … even if the F-1208 frame is near the baggage
compartment. To my way of thinking, it won’t be any fun at all drilling out
those two rivets to flip or replace the wear plate … plus ugly things can
happen when drilling out a perfectly good rivet.
I decided to just use two 6/32 Allen socket head
cap screws (aircraft grade of course) to mount the wear plate to the F-1208-R fuselage
frame. I was thinking about drilling for nutplates but since both parts already
had rivet holes, I decided to use those holes to mount the wear plate. Now the servicing of the wear plate should be
much simpler.
Wear plate screwed onto the F-1208 fuselage
frame using 6/32 hardware for easy (well, easier) servicing.
The two 6/32 Allen socket head cap screws used to secure the wear plate to the fuselage frame.
Van’s plans call for the F-1208 and F-1209 frame
halves to get riveted together using LP4-3 pop rivets … I elected to use
AN470AD4-4 rivets, stronger and less weight (have to make up for that wear
plate 6/32 hardware).
Riveting the fuselage frames using solid rivets
as opposed to pop rivets.
The F-1210 left and right frames are a little
more complex because there is a mounting plate for the vertical stabilizer that
is attached to the F-1210 frame along with a bracket to support the top
fuselage skin aft of the stabilizer’s attach plate. Van’s plans call for two
sizes of solid rivets here … but the AN470AD4-4 rivets called for in the plans
are just a little short (I know I’m being overly picky). Having some half sized
rivets, determined that AN470AD4-4.5 rivets fit perfectly … so they were used
in place of the 4-4 rivets. The longer AN470AD4-5 rivets called for where the
bracket is located were a good fit.
Completed F-1210 fuselage frame/vertical stabilizer mounting plate – manufactured rivet
head side.
Completed F-1210 fuselage frame/vertical stabilizer mounting plate - rivet shop
head side.
Completed tail cone fuselage frames.