Does anyone have autocad 14 files for the Q2, especially the canard? Larry Severson Fountain Valley, CA 92708 (714) 968-9852 larry2@...

Jon & Mike, I bought a set of the Mach 1's offered by Lightspeed. The "osh special" was to have the audiologist fit the custom molds for nearly free. I very much liked the set. However, I could

Sure, check the presentation I posted this morning in the files section. John http://club.live.com/star_shuffle.aspx?icid=starshuffle_wlmailtextlink_oct homepage.

Please check the archives on this subject. It has been discuss at length. I believe there is a description on how to do it and an opinion why you shouldn't do it. Doug "Hawkeye" Humble A Sign Above

A Swiss gentleman by the name of Rudi Brandenburger did a load test on a Q2 for the Swiss FAA. He used to be a ground engineer for Swissair but I have lost contact with him now. His Q2 was registered

John, Could you post some pictures of your Q? Dave D. johntenhave <johntenhave@...> wrote: Paul, no offence taken, and there is nothing like a healthy, reasoned

Hi I'm completing a Q-200 project over here in Switzerland! I'd like to perform a wing loading test! Anyone has infos about a load test on a quickie? Thanks Tom

No, but it is heavier. The more micro put in the epoxy, the thicker the medium becomes and the harder it is to spread. More micro is easier to sand than less. The ability of the alcohol to evaporate

Hi Mike I find John Tenhave very irritating with his arrogant and patronising manner! I know I shouldn't let it get to me (and I am not the first) and usually I don't, but this time it

Sorry, I had not gotten to that stage of my mind build - I was thinking you were talking about what I had posted the question about with the inital alignment - then next step (wet micro or

NO! The alcohol/micro/epoxy mix is very weak by design. It provides a good sanding surface to provide a super smooth base for your paint job. Do not apply to the foam! It is used ONLY for the final

We did 2 or 3 layers at a time on the Cozy b/c it was a lot easier to control the resin on a flat surface (workbench) then transfer it to the wing on plastic and do final "attachment" with a stippling

Paul, All this makes sense. I still think the bond between hardshell or micro-wet layup the weak point is between the micro (whether hard or wet) and not the rough sanded hard and glass. Yes the

Paul, I was actually going to build a "finish template" to determine how close the final profile is to the true airfoil. I see Johns point about how adding .0013 and .0009 layers can add up to a

Paul, no offence taken, and there is nothing like a healthy, reasoned debate. Rather than clutter the bandwidth, let your comments stand. Let me comment briefly on incorrect assumptions and may I

Hello, This email message is a notification to let you know that a file has been uploaded to the Files area of the Q-LIST group. File : /Composite Finishing/SAAA composite finishing.ppt

Looking for a template to rig the elevators. Does anyone have a drawing they could part with? Gordon Q2 revmaster Atlanta Getting close

Was this for the hardshelling method? How thick (thinking pretty thin) do you apply to the foam? Does the alcohol eat the foam? I have heard the by adding alcohol (to the mix - not to the builder )

Paul, Do you have a couple pilots wings left and I'll send you the $. John Packer

Hi Alan, Do you sell drawings for a graphlite spar version of the LS1 canard? If so I would like to purchase them or otherwise obtain a copy. Thanks, Tim