Bearhawk Experimental Airplane Build : Horizontal Stabilizer

Experimental airplane scratch build Bearhawk 4 place. Horizontal stabilizer fabrication.
Build Log: bearhawk2020.blogspot.com/
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[@tomstrum6259]

Master metal fabrication skills for sure...You make an Overwhelmingly complex fabrication project look almost manageable by a regular dude....Thx for taking time to show All this at the Perfect presentation speed....

[@BSpotBuilds]

Thanks

[@Kevin_747]

Great work. Many of these tasks I did 11 years ago on my Patrol but I still like to watch your videos. I don't need to tell you if you scratch build any model of Bearhawk you better love to fabricate.

[@Nicky.Stiles]

Thanks for another good one. Shop looks good too! I’ve noticed production really increases on my scratch build when the shop is tidy.

[@BSpotBuilds]

🙂

[@sirnewton6874]

Your patience to make videos is astounding. we could be friends imo

[@BSpotBuilds]

Thanks

[@scratchbuilder5952]

Thanks for posting this There is a lot of content about building Bearhawk wings, but very little on the fuselage. Your fuselage videos will be gold, please video as much as you can

[@BSpotBuilds]

🙂

[@tat2joeelliott]

i thought you were only supposed to gas weld chromemoly?

[@BSpotBuilds]

Both are acceptable. kzbin.info/www/bejne/h6mUqIWObL2AeNk

[@sirnewton6874]

ever since watching your video, my gears are grinding on this subject. I have a question about the horizontal stab strut connection point. How are you installing this bushing? Do you plan on clocking the axis of the bushing to the same axis of the load from the strut? as well what material are you planning to use for the strut its self?

[@BSpotBuilds]

I put the bushing for the strut in the leading edge. It's in the video at 37:55. As for the connection to the lower longeron it is show on my plans page 20 and connects to J-H. As for material, connections and adapting to the angles involved I haven't really thought about it yet. It's something I will evaluate when I get the parts of the tail assembled.