John, I didn't pluck a number from the sky. I don't just haphazardly put airplanes together and hope for the best. I'm basing my decisions on reliable information provided to me by other Tri-Q200

Hi Raoul, Ya, wife had some other function to go to so I took Phil. Let me know when your at the taxi test stage and I'll come up and get you in the Q200. Problem is that a Q200 doesn't perform like

Mark, have you learn nothing from the previous discussions? It is simply unsafe to do as you propose. It is irresponsible with respect to those who may finish up owing that airframe because you

Nice pictures Mike, I see you did not take your wife this time, I wonder why? See you sometime soon at Dunnellon it's were my Q is now. Getting there but still far, the engine is almost ready, I fixed

More video... Pamela (my wife) took this yesterday on our way home from breakfast from a neighbors C195. I thought the second half came out very nicely so had to share. Current the last item on my

Hey Guys, Flew from PIE to OCF today. Had a nice flight. Turns out there was a B17 and B25 on tour there. Had lunch and watched Wayne Newton deplane from his Lear jets and take off in a stretch

Thanks everyone for their response, I've been working on and flying airplanes for 28 years. My basic rule is safety first, how fast can I go and how much will it cost me. The Tri-Q200 fits me like

Sorry Sebastian, no layup schedule exists for the fuselage. For repair, refer to the education section of the plans. Basically, you would clear out the damaged area, repair the foam, then glass with

Can someone point me to any existing 3-D CAD drawings, that may exist? I happened to meet a fellow from Japan who is selling a fluid dynamics modeling software package, and he needs a drawing to

In a message dated 2/9/2008 9:39:11 A.M. Central Standard Time, sam.hoskins@... writes: Sorry Sebastian, no layup schedule exists for the fuselage. Sam's advice is valid. If you

Hi group, I am repairing a small cut out in the fuselage and am looking for the lay up schedule for the inner and outer skin. Any help with the data is greatly appreciated. Thanks Sebastian Q200,

I agree with Paul. One possibly interesting note, aren't we G limited by the canard. I heard that the most G's we can pull is around 4. I've never tried to pull more than about 3 in the air (not

I would have thought that, on a Q2/Q200, the main wing would be the weakest part of the primary structure and would have to be properly load tested before exceeding 1100 lbs gross, especially going as

Hi Barry, email me off list at: HawkiDoug@... so I have your email. Let me know if you are ever in Omaha. Doug "Hawkeye" Humble A Sign Above www.asignabove.net Omaha NE N25974

IMHO Mark, you start with the 1100 gross number and thru your own flight test you determine what you airplanes gross weight is and document it. Of course you need to this systematically and

Greetings all. Some of you will recognize my name and some won't as I was a builder for a while and then had to sell my kit to afford changes in my life (getting married, buying a house, and having a

So it seems that there's a disagreement of sorts but no real answer on data on the Tri-Q200's gross weight. So I guess I'll have to list it as 1100 as the LS wing suggest. Mark

http://oklahomacity.craigslist.org/for/547912789.html I talked with John for about a half hour yesterday; project seems pretty nice. It's tough for him , because this is the death of a

Does anybody know the g limits of a q2? Thanks, Justin --------------------------------- Looking for last minute shopping deals? Find them fast with Yahoo! Search.

wrote: because I are Doc, one of the good things abou this book: Composite Aircraft Design , by Martin Hollmann is the appendix. In which he gives the written programs for running the the formulas on