Cirrus Design
Section 1
SR20
General
Fuel
Total Capacity.............................................60.5 U.S. Gallons (229.0 L)
Total Usable...................................................56 U.S. Gallons (212.0 L)
Approved Fuel Grades:
100 LL Grade Aviation Fuel (Blue)
100 (Formerly 100/130) Grade Aviation Fuel (Green)
Oil
Oil Capacity (Sump) ............................................. 8 U.S. Quarts (7.6 L)
Oil Grades:
All Temperatures ............................................SAE 15W-50 or 20W-50
Below 40 ° F (4° C) ................................................. SAE 30 or 10W-30
Above 40 ° F (4° C) ................................................................... SAE 50
Maximum Certificated Weights
Maximum Gross for Takeoff...................................... 3000 lb (1361 Kg)
Maximum Landing Weight ........................................ 2900 lb (1315 Kg)
Maximum Baggage Compartment Loading.................... 130 lb (59 Kg)
Standard Empty Weight ............................................. 2050 lb (930 Kg)
Maximum Useful Load.................................................. 950 lb (431 Kg)
Full Fuel Payload.......................................................... 622 lb (282 Kg)
Cabin and Entry Dimensions
Dimensions of the cabin interior and entry door openings are
illustrated in detail in Section 6.
Baggage Spaces and Entry Dimensions
Dimensions of the baggage area and baggage door opening are
illustrated in detail in Section 6.
Specific Loadings
Wing Loading .................................................... 22.2 lb per square foot
Power Loading................................................................. 15.0 lb per hp
P/N 13999-002 Info Manual
1-7
September 2011