Eric Evezard wrote:
> What would be a typical thickness to accept for fibreglass wheel spats ?
Maybe the reason I haven't seen an answer is that it's not an easy one. If
done efficiently, the thickness will vary, being maybe .020" at the rear
where it tapers to a cone and is inherently stronge
I had rather go to the dentist than post this. I now am in the position of
having to sell my 1946 T-Craft. It has the wings and tail feathers removed.
The fuselage was stripped, cleaned and epoxy sprayed in then covered with
cenconite(sp?). The wings were stripped and new spars then covered
Randy,
Best of luck with that. I sincerely hope it works for you. If not, let
me know.
Ron Piekaar
On Mar 4, 2010, at 10:46 AM, wrote:
> Hi Ron, I'm interested yes, but I just had a fantastic deal drop into
> my
> lap from a whole lot closer.
>
> p.s. I'm originally from Bonners Ferry, ID. al
Now let's not get silly-- What in the world do you think was going to hold the
deck cloth to the structure anyway (which was infact the original question). I
used the epoxy instead of another type of wood sealer that was going to have to
be put on any way. The epoxy was harder for sanding purpos
Here, here! epoxy is heavy! Heavier than the wood.
Fred Johnson
Reno, NV
Joe wrote:
Hey Mike
Sounds like you are really getting there. I did not put the cloth on my
fuselage. I did when ever I had extra epoxy mixed up use it to coat the
sides and other wood and only after I was certain that I
Hey Mike
Sounds like you are really getting there. I did not put the cloth on my
fuselage. I did when ever I had extra epoxy mixed up use it to coat the sides
and other wood and only after I was certain that I did not have to glue
anything else to the wood. I don't have any cracks in mine after
Hi Netters,
What would be a typical thickness to accept for fibreglass wheel spats ?
Best Regards,
Eric,
S.Africa
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