I looked into it a while back.  I wanted to see what the price difference
and the weight difference would be.  After doing some reasearch on the web I
found that you could find all kinds of low priced aircraft grade titanium
bolts on EBAY.  If most of them were used, rejects, surplus, counterfeit AN
bolts made in China, who knows.  All the places I found that sold real
certified bolts didn't have online pricing.

The thing that made me stop looking was information about lubing the threads
correctly before putting the nuts on and critical torques to keep them from
snapping.  I got the impression that you really needed to know what you were
doing if you were going to replace high stressed bolts in structural areas
and most of the weight in bolts on a KR are high stress in structural areas.
Even if they have the same or higher tensile strength as what you are
replacing there are other considerations such as ductility and other things
that I don't know enough about to know if you can use them where I wanted.

I did come up with tons of links for titanium bolt replacement kits for
racing bicycles and they were all pretty expensive.

Brian Kraut
Engineering Alternatives, Inc.
www.engalt.com

-----Original Message-----
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net]On
Behalf Of Scott William
Sent: Saturday, September 24, 2005 2:47 PM
To: KRnet
Subject: KR> Hardware



Ok.....I've done my homework and I understand the
difference between ASE graded hardware and AN standard
hardware. Has anyone here used titanium bolts in thier
airframe?  Other than FAA examiner scrutiny (such as
with the WAF) is there any reason not to use them
besides price?


Scott

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