Hello,

Our 235 has a forward cg. The allowable max forward CG which was used
for registering at the german FAA (LBA) was 15%MAC. I searched the LML and got the information that the factory revised the
allowable forward CG to 11%MAC.

What I need is a confirmation of the revised CG range from Lancair, but
they show no reaction on my mail :-( !?. Anybody having such a
confirmation, letter, fax etc., which he could share with me?

Thank you

Rudolf Winter

235 99%, LNC4-P 17,5%