Fuselage


July 1, 2006
A critical part of the fuselage construction is making sure
that there is no twist in the fuselage as it is riveted together. Twist is
eliminated when installing the aft deck. Both the forward and aft end of the
fuselage are leveled then the aft deck is clamped in place and match
drilled. This stiffens up the fuselage and keeps it from twisting during the
remaining construction steps.
Here's
a shot of the aft deck riveted in place.

July
2, 2006
Fit and match drilled the F-757 plates. These plates
strengthen the seatback bulkhead and provide some reinforcement to the
slider canopy that I will be installing.

July
3, 2006
Fit and match drilled the F-685 forward gussets to the
forward ends of the longerons and the firewall angle. This adds support to
the firewall.


July 4, 2006
Riveted the reinforcement angle to the elevator bellcrank
channel. Fit and match drilled the seat belt anchors to the longeron. The
seat belt cables attach to these brackets. They will be bolted in place
later in construction.
July 5-6, 2006
Match drilled and riveted the lower elevator bellcrank
channel to the F-706 bulkhead. Fabricated some miscellaneous elevator
bellcrank parts. (No pics)

July
8, 2006
After looking over the plans more closely, I found that the
F-711D angle should have been riveted on prior to riveting the aft
deck. The photo shows the angle riveted on. This was particularly difficult
to reach due to the aft deck already being in place. Fabricated the F-710C
spacer, F-711E spacer/down elevator stop and the F-712D up elevator stop.
Also fabricated the F-798 shims. Deburred all these parts.


July 9-12, 2006
Pulled out the two aft top skins and the top j-stiffeners.
Deburred the edges then clecoed to the fuselage. This required some further
fluting and flange adjustments to the bulkheads for a better fit. Deburred
and clecoed the F-665 gussets to the F-706 and F-707 to longeron
intersections. Match drilled the skins to the ribs and stiffeners. Tried to
cut and fit the F-6111 stiffener ribs to the forward ends of the F-7112
skin. The manual says that these need to be trimmed and twisted to fit to
the shape of the skin. Well, I trimmed them too short to where they were not
going to work, so I trashed them and ordered new ones. After the fact, I
read on Mike Schipper's website
the trick to installing them. I'll see what happens when I get the
replacements.


July 13-14, 2006
Fit and drilled steps to the right and left fuselage. I
started out the drilling process by using a #40 to drill the pilot holes
then finished with a #30. I wasn't real happy with the gap at the bottom of
the fuselage opening (I made the opening too large) but I can fix this later
with some fiberglass. I was able to get them to fit flush to the skin by
bending them a little to match the curve of the fuselage.
Tested
the fit with the delrin block that supports the interior side of the step.
July 24-28, 2006 OFF TO OSHKOSH!
Check out my
pics from Airventure
2006
