Specifications

10 of 56 11934-S37
Section 9 Cirrus Design
Supplements SR20
Flight Load Factor Limits
Flaps UP (0%), 3050 lb.......................................................+3.8g, -1.9g
Flaps 50%, 3050 lb................................................................+1.9g, -0g
Flaps 100% (Down), 3050 lb. ................................................+1.9g, -0g
Fuel Limits
The maximum allowable fuel imbalance is 7.5 U.S. gallons (¼ tank).
Approved Fuel ............... Aviation Grade 100 LL (Blue) or 100 (Green)
Total Fuel Capacity..................................... 58.5 U.S. gallons (229.0 L)
Total Fuel Each Tank .................................. 29.3 U.S. gallons (114.5 L)
Total Usable Fuel (all flight conditions)....... 56.0 U.S. gallons (212.0 L)
Cirrus Airframe Parachute System (CAPS)
V
PD
Maximum Demonstrated Deployment Speed..................133 KIAS
• Note •
Refer to Section 10 – Safety Information, for additional CAPS
guidance.
Revision 01: 08-26-09