Cirrus SR22 Pilot Operating Handbook page 432

Section 9
Supplements
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.
Value
Marking
(KIAS)
White 62 - 104
Arc
Green 73 - 177
Arc
Yellow 177 - 200
Arc
Red Line 200
Power Plant Limitations
Weight Limits
Maximum Takeoff Weight ........................................ 3400 lb (1542 Kg)*
*
no change
Fuel Limits
Total Fuel Capacity ...................................... 94.5 U.S. Gallon (358.0 L)
Total Fuel Each Tank ................................. 47.25 U.S. Gallon (179.0 L)
Total Usable Fuel (all flight conditions) ........ 92.0 U.S. Gallon (348.0 L)
8 of 48
Remarks
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.
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.
Caution Range. Operations must be conducted with
caution and only in smooth air.
Never exceed speed. Maximum speed for all
operations.
Cirrus Design
SR22
13772-130
Revision 03: 05-09-11