A went through the Q1 and Q2 plans this past weekend. Nowhere in the plans
did I see mention of what weight glass they are using for the unidirectional
and bidirectional glass.

"James R. Freeman" wrote in message
...
Dave for Your info. The Quickie and Q2 use a fiberglass build up spar as
You
will see from the plans. The Q-200 uses a carbon fiber spar.
Yes the Quickie canard (front wing) can be removed.


Jim

"James R. Freeman" wrote in message
...
Dave:
I found the URL. It is:

http://www.finleyweb.net/default.asp?id=141

Jim

"Dave Schneider" wrote in message
...
after a bit of surfing i found this. Is something like this what you
are
talking about?

http://www.hinkleymall.com/airplane_cd.html

There is also this on ebay:




http://cgi.ebay.com/ebaymotors/ws/eB...ory=26441&item
=4510814564&rd=1


Basic question for the Quickie, do the wings disassemble? I'm also
looking
for techniques for attaching wings.

Thanks!
Dave

"James R. Freeman" wrote in message
...
Dave:
Take a look at the ruttan wings on a q-1 or q2 it will fit the
bill
for
what you want. There is one site on the web for free downloads of
the
q2
info but I do not have the URL at hand. Q1 plan can be had on C.D.
for
less
than $10 via EBay.

"Dave Schneider" wrote in message
...
Can anyone suggest some home built construction sites where they
show
the
process of building a spar for a foam composite wing. I'm
confused
on
how
a
spar is built for a foam wing. It doesn't seem like the foam
itself
would
provide enough structure to provide a web. It would seem like
you'd
have
to cut the wing foil, cut out the location of the spar, build the
spar,
and
then reinstert that section back into the foam wing.

Thanks,
Dave