See message below, and link to Christian's spreadsheet at http://www.krnet.org/misc/stability_kr-2s.xls . Any questions should be probably be directed at Christian, and through KRnet would be fine, since others might have the same questions.
----- Original Message ----- From: "Kogelmann Christian - OS TDA" <[email protected]> Subject: RE: KR> AS 504X CofG I have an MS Excel File to determine the C/G (RAF48) and the stability of my airplane. I could not put it on my web page yet so I thought you might want to publish it. I had to do this for our authorities and of course they moved the allowable aft C/G forward..... In the File: HLW = Horizontal Stabilizer (including Elevator) And other German Expressions should be self explanatory (if not I will prepare a full english version) I have an input page for fuel and crew and based on the input the C/G moves in the chart. We did increase our HLW but did not manage to move the stability line out of the c/g range, there the authority will limit us at 29,5% C/G. If you think it is useful, you are welcome to publish it. Brgds Christian OE-VPD
