I happen to have a stock per plans seat laying in the shop if needed. let
me know if you want it.Don
On Thu, Aug 30, 2018 at 7:46 PM Mike Sylvester via KRnet <
krnet@list.krnet.org> wrote:
> Since I am in a hurry to have a seat for the Gathering, (after destroying
> my original glass/foam seat) I
Since I am in a hurry to have a seat for the Gathering, (after destroying my
original glass/foam seat) I have just completed my plywood seat. Compared to by
composite seat, it's a few pounds heavier. Now I just need to go to the airport
Saturday morning for a test fit and fly. Thanks for all the
Why not try a sling seat like the Taylor mono plane and keep things simple.
I can see that Alum seat cracking and your a$$ landing on the elevator
cables and then what a mess
On Thu, Aug 30, 2018 at 7:14 AM Teate, Stephen via KRnet <
krnet@list.krnet.org> wrote:
> I think the decision of what kin
Larry Flesner wrote:
> 200 pounds for 700 hours = 140,000 pound test
You missed your calling Larry. You could have made a fortune in
marketing!
Mark Langford, Huntsville, AL
ML "at" N56ML.com
www.N56ML.com
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I think the decision of what kind of seat is every bit as important a decision
as to what resin or wood we use in our airplanes. I would say that there is
little argument as to the simplicity of the stock sling seat but if you are
going beyond that then it should require some real thought espec
On 8/30/2018 6:50 AM, Mark Langford via KRnet wrote:
I used one sheet of aluminum, fairly thin gage as I recall (T6061 0.016 gage
3’x3’ sheet worked for me).
+++
Fiberglass seats are not that d
Rob Schmitt wrote:
>> I used one sheet of aluminum, fairly thin gage as I recall (T6061 0.016 gage
>> 3’x3’ sheet worked for me). It spans the back and front spar. It does bend
>> down over the front of the front spar and I used a “bar” of aluminum
>> probably 1/8” thick by 1” to secure it (Scr
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