Cirrus DESIGN SR22T User Manual

P/N 13772-134 17 of 48
Cirrus Design Section 9
SR22 / SR22T Supplements
Left/Right Fluid Quantity Caution
PFD Alerts Window: “Right/Left tank fluid quantity is unreliable (TKS)”
L / R fluid quantities on Anti Ice - TKS block of ENGINE page is
“greyed out” and/or fluid quantity is marked with a “Red X”. The deicing
fluid sensing system has detected conflicting system information
regarding the fluid quantity in the tanks.
1. Revert to manual control of the fluid source to control the fluid level
quantity.
If ANTI ICE FLO or ANTI ICE PSI annunciates:
a. Fluid Quantity ......................... SWITCH TO OPPOSITE TANK
b. WIND SHLD Push-Button ............................................PRESS
(1) Repeat operation of windshield pump to verify metering
pumps are primed properly as evidenced by deicing fluid
exiting windshield nozzles.
Dynamic Stall Speed Band Unavailable Advisory
PFD Alerts Window: “Dynamic stall speed band is unavailable.”
Angle of Attack signal has failed. This signal is used to calculate and
display a dynamic stall speed awareness band (red band) on airspeed
tape. With a failed AOA signal, the low speed red band extends to a
fixed value of 61 knots.
ANTI ICE LVL
AOA FAIL
Revision 04: 12-17-10

Cirrus DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches