CIRRUS DESIGN SR20 - Center of Gravity Limits

6-14 P/N 11934-003
Section 6 Cirrus Design
Weight & Balance SR20
Figure 6-6
Center of Gravity Limits
The charts below depict the airplane center-of-gravity envelope in
terms of inches aft of the reference datum and as a percentage of the
Mean Aerodynamic Cord (MAC). The relationship between the two is
detailed in the weighing instructions.
SR20_FM06_1941
138 140 142 144 146 148 150
2000
2200
2400
2600
2800
3000
C.G. - Inches Aft of Datum
Weight - Pounds
10 15 20 25 30 35
2000
2200
2400
2600
2800
3000
C.G. - % MAC
Weight - Pounds
Center of Gravity Limits
Reissue A