1. At each annual the looseness condition can be checked while the
aircraft is on jacks by wiggling the nose gear fwd and aft. It
shouldn't wiggle.
2. The bolt length specified by Lancair is too short and bolt threads can
quickly wear down against the tab hole. Using extra washers,
make sure the body of the bolt is bearing on both tabs. Replace this bolt
if it becomes worn (excessive practice landings ;-)).
3. Of course, one should be using a drilled bolt and castle nut
since the bolt may turn. It should be only tightened enough that there is
no added friction between the tab and link.
4. Keep this joint lubricated -- I am fortunate (?) that my engine
produces a minor nuisance oil leak - just enough to keep the nose gear system
oily.
Grayhawk