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  #1  
Old 07-16-2019, 12:34 AM
Steve Crewdog Steve Crewdog is offline
 
Join Date: Mar 2019
Location: KBVS
Posts: 53
Default 2024T3 vs 606T3 for home made instrument panel?

Any thoughts pro vs con? My metal guru wants me to use 2024 but some other gents tell me I should be using 6061 for corrosion resistance.



TIA
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  #2  
Old 07-16-2019, 02:03 AM
bobnoffs bobnoffs is offline
 
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Location: n. wi
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pretty much whatever you have on hand. 2024 is maybe 10% stronger. i have used both. i don't think corrosion is an issue , considering it is going to be painted for sure and no big deal to rattle can the back if you're worried about it.
can't say i noticed any difference ''machining'' one metal over the other.
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  #3  
Old 07-16-2019, 06:11 AM
gmcjetpilot's Avatar
gmcjetpilot gmcjetpilot is offline
 
Join Date: Jan 2005
Posts: 4,283
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Quote:
Originally Posted by Steve Crewdog View Post
Any thoughts pro vs con? My metal guru wants me to use 2024 but some other gents tell me I should be using 6061 for corrosion resistance.

TIA
Actually 2024-T3 is X2 stronger than 6061-T4. Common temper for 6061 is T4 or T6

Alloy Temper E G Yield Ult
2024 T3 10.6 4.00 42 64
2024 T4 10.6 4.00 40 62
6061 T4 10.0 3.80 16 30
6061 T6 10.0 3.80 35 42

The last column ULT is ultimate tensile strength. E and G are elastic and shear modulus (think stiffness). You can see 6061 T4 is easier to bend with yield of 16 KSI.

Question, is instrument panel structural part of airplane. Well in an RV it does attach to the fuselage and will pick up some loads but don't think it's critical. You do have to support the instruments and avionics. I am sure 6061I-T4 in proper thickness would get the job done, but get 6062-T6, closer to 2024-T3.

Instrument panel corrosion is not an issue. You are going to paint it yes? Most of the airplane is made of 2024T3 clad. Un-clad aluminum of any alloy or temper will corrode.

Why are you not using Van's supplied panel? What material is the Van's panel made of? Bottom line it probably does not matter.
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Last edited by gmcjetpilot : 07-16-2019 at 06:18 AM.
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  #4  
Old 07-16-2019, 06:27 AM
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maniago maniago is offline
 
Join Date: Aug 2014
Location: Bowie MD
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Rarely if ever is the instrument panel relied on as a load bearing piece, because you punch so many holes in it - its just an item to mount things in.

We dont know what youre building or what your mission is - so you need to do some evaluation - but chances are that what you use is immaterial - you could use fiberboard if it supports you gear if you wanted to.....or have no panel at all - just use a helmet mounted hud.

2024 is more expensive than 6061, so your metal guru may either want more of your pocket money or hes defaulting to the best you can get vs what you need.

Just as food for thought, my panel isnt a panel at all, but a substructure upon which I bolt individual panels or racks and such to......I wouldnt have any metal to speak of if I'd just done it as a flat panel plate.....

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Last edited by maniago : 07-16-2019 at 06:46 AM.
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  #5  
Old 07-16-2019, 06:55 AM
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Dan Langhout Dan Langhout is offline
 
Join Date: Mar 2008
Location: Huntsville, AL USA
Posts: 545
Default .071" 2024-T3

. . . . . . . . but I really didn't think about it very much given the application.
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  #6  
Old 07-16-2019, 08:35 AM
Steve Crewdog Steve Crewdog is offline
 
Join Date: Mar 2019
Location: KBVS
Posts: 53
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My apologies, I thought I had unmasked already. I'm actually building a Progressive Aerodyne SeaRey, but with fewer than 500 of them flying the expertise here far overwhelms the limited tech support on our site. My metalworking seadday is a great guy, but some fo the SeaRey guys were asking why 2024 when they normally used 6061, and it's because I was doing what I was told. Now I'm trying to avoid spending $100 for a new sheet of 6061 and redoing the panel.

I fully admit I am flying wing/leeching on the Vans knowledge base, donated my $25, and hope it's Ok if i ask an occasional non-VAF question in the General forum. If the Mods and members don't want me to post, Fair skies and tailwinds, see you at Sun n Fun, and I'll go back to lurking.





Steve
http://seareybuild.blogspot.com/

Last edited by Steve Crewdog : 07-16-2019 at 08:39 AM.
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  #7  
Old 07-17-2019, 06:32 AM
rongawer rongawer is offline
 
Join Date: Dec 2007
Location: Brentwood, CA
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Strength of the metal by itself is only part of the picture, but also how is it braced? If it’s braced in the middle, say from the the FW to the center, or with a lateral angled bracket of some sort, then 6061 should work fine. But if it’s unbraced or has any structure aspect to it, then I recommend 2024-T3, which is really the most common alloy for this job.

I prefer 2024-T3 in 0.080”.
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- RV10, Build in progress.
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  #8  
Old 07-17-2019, 06:41 AM
F1R F1R is offline
 
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Location: ____
Posts: 829
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Consider making a trial 1 or 2 panels out of 3/32 lexan or 1/8 lexan. When you are sure you have it the way you really want, you can make he final one in AL.

Check with the kit MFG and other truly experienced builders. Running on waves at take off and landing speeds really beats he He11 out of everything. Lots of shock loads and hundreds of cycles per take off run.
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  #9  
Old 07-17-2019, 07:43 AM
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DanH DanH is offline
 
Join Date: Oct 2005
Location: 08A
Posts: 9,476
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I'll take the 2024 simply because it cuts and edges more cleanly. 6061 is kinda sticky to file and sand.

That said, I've made panels from 3003. Depends on support.
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  #10  
Old 07-17-2019, 08:21 AM
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Mike S Mike S is offline
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
Default Welcome to VAF

Steve, welcome to VAF.

Lots of members are building non Vans aircraft, myself included.

When you get that SeaRey, try on an RV for size------you might like it.
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Flying as of 12/4/2010

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