On Thu, 02 Feb 2006 09:26:20 GMT, "Capt.Doug"
wrote:

I tried to post some bitmap images with this but it didn't come up on my
server. Anyways..

Concerning the Chalks seaplane crash in Miami, fatigue features were
observed in the lower spar cap of the rear spar of the inboard end of the
right wing, bisecting 2 offset drilled holes.

D.


Send them to me.

I've got the web space to share them.

I'm not a lawyer, I'm just an engineer that is interested in metal
fatigue and aging aircraft.

In particular, I'm going to buy an old 7AC or L-16.

Mike Weller