Specifications

44 of 56 11934-S37
Section 9 Cirrus Design
Supplements SR20
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.
FS 148.1
2100 lb
FS 148.1
3050 lb
FS 139.1
2700 lb
FS 140.7
3050 lb
FS 137.8
2100 lb
2000
2050
2100
2150
2200
2250
2300
2350
2400
2450
2500
2550
2600
2650
2700
2750
2800
2850
2900
2950
3000
3050
3100
136 137 138 139 140 141 142 143 144 145 146 147 148 149 150
C.G. - Inches Aft of Datum
Weight - Pounds
Revision 01: 08-26-09