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A little trimming was required to get the firewall to fit in the back of the airplane, but that's normal. Overall it fit without giving me any fits. Once it was clamped into position, I filled the gaps and radiused the inside corners with potting compound and glassed it in place with 2 plies of S2 glass. Glassing the joint between the firewall and the lower surface of the spar wasn't too fun. It was awkward and kind of hard to get to, much like doing a layup on the underside of your desk. Do you lay on your back and work over your head, or kneel and reach around? I think I did a combination of both. To keep things purely chronological, you would skip ahead to the NACA scoop installation chapter now, and then come back here. I installed that before continuing on with the aft side fiberglass work. But it really doesn't matter... there are plenty of chronology violations on my website, and I haven't received a ticket yet. Access to do the aft side
firewall layups was much better, but there was an added complication: I had to
incorporate After the fiberglass had cured, I removed the plastic strips and trimmed up the flange. You can see the result in the photo on the right. At some point in the future, I'll install some nutplates or ¼-turn fasteners on this flange, and the engine cowling will attach here. To complete the fiberglass portion of this chapter, I added a bunch of plies to locally strengthen the engine mount attach points. While structurally sound
at this point, there was one important feature that my firewall installation was
lacking: Fire resistance. Making that happen involves bonding a
fire-resistant ceramic felt (Fiberfrax®) directly to the firewall
followed by a metal face sheet. Most people use steel for this, as the
melting point of aluminum is too low. But steel is heavy. Indeed,
the SQ2000 construction manual also called for steel. This was a pretty big
part to be building out of steel, I thought, so why not use titanium instead?
That's what Boeing and Northrop would do. Titanium is light weight, has a
very high melting point, and doesn't corrode. The main drawbacks to using
titanium are that it's expensive, and it's fairly hard to work with. It
also doesn't get along well with cad plated hardware, which is typical of AN and
NAS parts. But I
was determined. My first stop was Boeing Surplus down in Kent, WA to look
for titanium sheet. No luck. All they had was thin strips, and a
bunch of Ti I surfed the internet a
while, and eventually landed on Titanium
Joe's website. Ti Joe is a scrap metal
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