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I DON'T WANT to discourage you from asking your engineer.  But.  The Coupe
spars were an extrusion with extruded caps if my casual knowledge is
correct.  There's been some muttering about trying to get new wing spars
made but it has fallen through due to the extreme cost of tooling.

Perhaps you could persuade the FAA to sign off on a spar made in a
considerably different way.  Good luck on getting a chicken FAA wienie to
sign off on a replacement spar of a different design.

So far as I know, we've been able to find enough parts to rebuild the
planes
with bad spars up to this point.  With the AD this year, that situation
may
change radically.

Ed Burkhead
http://edburkhead.com/
[EMAIL PROTECTED]

-----Original Message-----
From: David Johnson [mailto:[EMAIL PROTECTED]
Sent: Wednesanuary 22, 2003 6:41 PM
To: Ercoupe Tech List
Subject: [COUPERS-TECH] RE: [COUPERS-FLYIN] C-section & corrosion

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advice in this forum.]----


With all the talk about corrosion, especially in the carry-through spar
section, does anyone think that there might be enough interest in
developing
an STC to replace the spar? If we are to continue to keep these old birds
airworthy, we need to take a pro-active approach. I'm sure that there
would
be some development cost, structural load analysis and such. At work, we
have an outside DER review all of our structural modifications. Is it
worth
starting a dialog with him? Feed back, anybody?





Coupers.
I sent this last night to the coupers-tech list.
I think it is interesting for every one. So here my  posting again.

Hartmut

-------- Original Message --------
From: Hartmut <[EMAIL PROTECTED]>
Subject: C-section & corrosion.
To: Coupers Tech <[EMAIL PROTECTED]>

Coupers.
I finally opened up the center section to remove the corrosion we found
today.
To avoid the data congestion, I prepared a little page with six images
to look at .
Check it out and learn from the tragedies of others. grin

http://home.pacbell.net/hbeil/ercoupe/corrosion.htm

Hartmut
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