A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Home Built
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Airframe finishing and tooling



 
 
Thread Tools Display Modes
  #1  
Old May 22nd 06, 07:21 PM posted to rec.aviation.homebuilt
external usenet poster
 
Posts: n/a
Default Airframe finishing and tooling

Thanks for the info - I just realized I was wrong thinking the 6061-T6
came already anodized. I've been reading so many specifications I got
them mixed up.
I won't be anodizing....

  #2  
Old May 23rd 06, 04:58 AM posted to rec.aviation.homebuilt
external usenet poster
 
Posts: n/a
Default Airframe finishing and tooling

In article . com,
"nondem" wrote:

Thanks for the info - I just realized I was wrong thinking the 6061-T6
came already anodized. I've been reading so many specifications I got
them mixed up.
I won't be anodizing....


Do NOT use steel wool on aluminum! It will leave tiny bits of steel
embedded in the surface and will induce electrolytic corrosion!

Why 6061? Most aircraft sheet metal is 2024 T-3 Alclad; structural is
2024 T-3 plate.
  #3  
Old May 23rd 06, 04:09 PM posted to rec.aviation.homebuilt
external usenet poster
 
Posts: n/a
Default Airframe finishing and tooling

The plane design I'm building uses 2x2x.125" 6061-T6 for the fuselage
frame. I did notice that older versions of the same plans specified
6063-T351.


I checked the specs on both and as I remember the 6061 is a stronger
alloy. There is almost no aluminum sheet used in this design
either...Just angles/square and round tubing for the most part.

  #4  
Old May 23rd 06, 09:31 PM posted to rec.aviation.homebuilt
external usenet poster
 
Posts: n/a
Default Airframe finishing and tooling

nondem wrote:
The plane design I'm building uses 2x2x.125" 6061-T6 for the fuselage
frame. I did notice that older versions of the same plans specified
6063-T351.


I checked the specs on both and as I remember the 6061 is a stronger
alloy. There is almost no aluminum sheet used in this design
either...Just angles/square and round tubing for the most part.


That sounds a lot like one of the late Graham Lee's UL designs.

Close?

Richard
  #5  
Old May 24th 06, 01:03 PM posted to rec.aviation.homebuilt
external usenet poster
 
Posts: n/a
Default Airframe finishing and tooling

It's an Affordaplane...

  #6  
Old May 25th 06, 03:01 AM posted to rec.aviation.homebuilt
external usenet poster
 
Posts: n/a
Default Airframe finishing and tooling


"nondem" wrote in message
ups.com...
It's an Affordaplane...


Short for VaporWare.

See any fly at national flyins yet?
--
Jim in NC


  #7  
Old May 25th 06, 05:14 AM posted to rec.aviation.homebuilt
external usenet poster
 
Posts: n/a
Default Airframe finishing and tooling

"Morgans" wrote:

"nondem" wrote in message
ups.com...
It's an Affordaplane...


Short for VaporWare.


When nondem first mentioned it, I did a Google search for it. There is a
web site for it, even has pictures showing the ultralight in the air:

http://affordaplane.com/
 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump


All times are GMT +1. The time now is 03:14 PM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.