Cirrus SR22T User Manual

12 of 52 P/N 13772-151
Section 9 Cirrus Design
Supplements SR22T
Static System Malfunction
If erroneous readings on the pilot’s flight instruments are suspected
the static button(s) on side of fuselage may be obstructed. Refer to
Section 3A - Abnormal Procedures, Static Source Blocked in the basic
handbook.
Anti-Ice System CAS Annunciations
• Note •
During Anti-Ice System activation, system mode changes,
operation at temperatures above freezing or with warm
deicing fluid, occasional ANTI ICE annunciations are normal.
Low Fluid Quantity Caution and Warning
PFD Alerts Window: “Fluid quantity is low (TKS)”
ANTI ICE QTY Warning: Fluid quantity is less than 0.5 gallon. (1.9 L)
ANTI ICE QTY Caution: Fluid quantity is less than 1.0 gallon. (3.8 L)
• Note •
Depending on the selected flow rate, ANTI ICE QTY
annunciation may occur at lower fluid quantities
1. Icing Conditions ........................................................ AVOID / EXIT
Low Flow Rate Warning
PFD Alerts Window: “Flow rate is low (TKS)”
1. ICE PROTECT A and B Circuit Breakers.................................SET
2. Fluid Quantity...................................SWITCH TO FULLEST TANK
3. WIND SHLD Push-Button ...................................................PRESS
a. Repeat operation of windshield pump to verify metering
pumps are primed properly as evidenced by deicing fluid
exiting windshield nozzles.
ANTI ICE QTY
ANTI ICE FLO
Original Issue: 02-01-13

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots