Cirrus DESIGN SR20 Information Manual page 153

Table of Contents

Advertisement

Cirrus Design
Section 6
SR20
Weight & Balance
The above procedure determines the airplane Basic Empty Weight,
moment, and center of gravity in inches aft of datum. C.G. can also be
expressed in terms of its location as a percentage of the airplane
Mean Aerodynamic Cord (MAC) using the following formula:
C.G. % MAC = 100 x (C.G. Inches – LEMAC) / MAC
Where:
LEMAC = 132.9
MAC = 48.4
P/N 13999-002 Info Manual
6-9
September 2011

Advertisement

Table of Contents
loading

Table of Contents