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Hey Tailwind Fam, Has anyone been in contact with Jim Stanton? I sent him a check but he never cashed it or responded. Do you know if he will publish his manual again? Any information will be

Jim Rust, Your estimate was perfect. I reduced pitch 3 degrees and now at ~7500 MSL WOT exceeds 2700rpm so the flightaware plot is at less than WOT at ~23” MAP and about 2680rpm. Average ground

Joe, Thanks, I have a DAR that I trust out of Kankakee, IL. Jim Leon. He is of aways away, but is willing to help me....which is more than the FAA will do. Pat Reilly Rockford, IL

Andy, I did like exactly like your proposed setup.? When I did my first engine run I had two people on the wings helping to keep the plane from rolling.? Now, the brakes hadn't been broken in

Clement method, works great lasts a long time no issues with inadvertent brake application. I don't do hammerheads in the Tailwind so no need for much rudder except taxiing in a strong wind.?

The pictures I sent were of Earl's final setup... You can see that the "horn" was lowered twice, and the link plates allow much more leverage and therefore hydraulic force applied to the calipers.

My Buttercup plans show one way for this wrote:

Do it like this. It solves the lack of pressure due to lever arm. The geometry has been discussed ad infinitum... [image: thumbnail.jpg] [image: thumbnail.jpg] -DjD [email protected]>

I’ve been trying to figure out my redesign as the way it was built won’t work. Thank you all for replies and links been reading alot on this.. I drew up my current setup and proposed setup. Not

Brady, one of the key things to making the geometry on the pedals work is to keep the base of the master cylinder as close to the pivot point of the rudder padal I did this and when I press on the

thanks for sharing Jim, intriguing to know this.?

Here is how I solved the excess MC push rod length. What you see is a 3/8 x 3/4 x 1.5" long piece of key stock, drilled and tapped to thread onto the MC with a jam nut, drilled hole for the pedal

While the brake part stays vertical, no brake should be applied.Hans Yahoo Mail - Correo electrónico simplificado El jue, 27 de feb. de 2025 a la(s) 16:48, David Powell via

Toes only on the rudder pedals. <brady.w.cope@...> wrote:

Should be close to a parallelo gram. <brady.w.cope@...> wrote:

I’m sorry if this is a dumb question, but I can’t figure out how the rudder pedals are supposed to move more than a few degrees without applying the brakes inadvertently. As opposed to the

Gene passed away at age 95. Most probably don't know that Gene built airplanes with his son at Santa Paula Airport in CA. Glasair, I think a 3, and a Pitts or maybe a Christen Eagle.? I think Gene

Thanks for the interesting data points, Jim. Great performance even with a 2700 rpm limit. Bob W. summed it up nicely in a previous post, Steve's TW design was/is a quantum leap in performance

The following photos have been uploaded to the N83CJ ( /g/TailwindForum/album?id=300930 ) photo album of the [email protected] group. * Tailwind N83CJ big.jpg (

Jim, Is your whirlwind prop a 72”? What angle do you have your blades set too? [email protected]> wrote: