The person in question imports  metals for race cars, aircraft grade 
steel and aluminium tube, but sells a lot of material to the local home 
aircraft builder market, the local sport aircraft chapter seem to think hes 
great, so I was very surprised when he told me he was getting a plasma 
cutter especially for cutting 4130 steel plate, so thought I had better 
check with someone more learned than me in these things, heat and aircraft 
grade metals are not a good combination in my opininon.



                                    Chris Johnston

                                    North Richmond NSW

                                    Australia.
----- Original Message ----- 
From: "Brian Kraut" <brian.kr...@engalt.com>
To: "KRnet" <kr...@mylist.net>
Sent: Saturday, August 26, 2006 1:23 PM
Subject: RE: KR> WAF Plasma cutting


>I am not a structural or materials engineer.  I design electronics.  I 
>would
> think that engineers working for an aircraft manufacturing company would
> know more about it than I do, BUT it sounds a little fishy to me.  They 
> may
> be doing the equivalent of shot peening, but as far as I know that is only 
> a
> stress relieving treatment and will not change the hardness and therefore
> the brittleness of the metal.  Of course a lot of what is acceptable and
> what is not depends on the safey factor that is designed into the part to
> begin with.  There are also different methods of plasma cutting using 
> oxygen
> or nitrogen and they do not each leave the same edge on the part.
>
> It all boils down to my stock answer.  If you don't know for sure that it 
> is
> O.K. then use a method that you know is O.K.
>
> Brian Kraut
> Engineering Alternatives, Inc.
> www.engalt.com
>
> -----Original Message-----
> From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net]On
> Behalf Of Larry H.
> Sent: Wednesday, August 23, 2006 12:15 AM
> To: KRnet
> Subject: KR> WAF Plasma cutting
>
>
> Brian, I know someone who is making all of the 4130 fittings which 
> includes
> wing attach for an aircraft mfg  company. All of the parts are being 
> plasma
> cut by computer and then the parts are being tumbled to deburr. The 
> tumbling
> process is the normalizing effect. Their engineers think the parts are 
> fine.
>  What do you think about this practice?
>  Larry H.
>
> Brian Kraut <brian.kr...@engalt.com> wrote:
>  Absolutely not. Plasma cutting leaves a very hard edge. I have had 
> several
> 4130 parts plasma cut including my lower gear attach fittings for the KR 
> and
> the seatbelt attach fittings and canopy latch parts for the Stang. I did
> some finish machining on some of the parts and the edges were hard as 
> rocks
> and needed carbide tools to cut them. Hard edges mean brittle edges.
> Brittle edges mean the high liklihood of cracks starting. The parts I have
> plasma cut are sent to a heat treater to be normalized when done, but if 
> you
> are not getting that done don't do it for structural parts. Same applies
> for laser cutting. Water jet is O.K.
>
> Another problem with plasma and water jet depending on the thickness is 
> that
> they both cut with a taper and sometimes also a slightly rough edge. If 
> you
> do water jet and have the bolt holes cut you want to have them done
> undersized and ream them to finish the holes.
>
> Brian Kraut
> Engineering Alternatives, Inc.
> www.engalt.com
>
> -----Original Message-----
> From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net]On
> Behalf Of Chris Johnston
> Sent: Tuesday, August 22, 2006 6:56 AM
> To: KRnet
> Subject: KR> WAF Plasma cutting
>
>
> Can you plasma cut the wafs without affecting the metal??????
> Are the tailplane hinge ply backup plates glued in place or just held on
> by the nuts and aluminium backup plates?
> The plans state the inner hinges have two bolts, does this mean the
> outer hinges have only one bolt per hinge half?
> Can you use two bolts on the outer tailplane and elevator hinge without
> weakening the spars too much?
>
>
>
>
> Chris Johnston
>
> North Richmond NSW
>
> Australia
> _______________________________________
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>
>
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>
>
> _______________________________________
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