Specifications

8 of 56 11934-S37
Section 9 Cirrus Design
Supplements SR20
Airspeed Indicator Markings
The airspeed indicator markings are based upon Section 5 Airspeed
Calibrations using the normal static source. When using the alternate
static source, allow for the airspeed calibration variations between the
normal and alternate static sources.
Weight Limits
Maximum Takeoff Weight ......................................... 3050 lb (1383 Kg)
Maximum Landing Weight ........................................ 3050 lb (1383 Kg)
Marking
Value
(KIAS)
Remarks
White
Arc
61 - 104 Full Flap Operating Range. Lower limit is the most
adverse stall speed in the landing configuration.
Upper limit is the maximum speed permissible with
flaps extended.
Green
Arc
69 - 163 Normal Operating Range. Lower limit is the
maximum weight stall at most forward C.G. with
flaps retracted. Upper limit is the maximum structural
cruising speed.
Ye l l o w
Arc
163 - 200 Caution Range. Operations must be conducted with
caution and only in smooth air.
Red Line 200 Never exceed speed. Maximum speed for all
operations.
Revision 01: 08-26-09