Cirrus SR22T User Manual

4 of 6 P/N 13772-143
Section 9 Cirrus Design
Supplements SR22 / SR22T
8. Reduce loads as required for flight conditions:
a. Air Conditioning and Fan ..................................................OFF
b. Convenience Outlet ................................Disconnect appliance
c. Audio Panel .......................................................................OFF
COM 1 will be supplied to pilot’s headset. Communication with
passengers through audio panel will not be available.
d. GPS/COM 2.......................................................................OFF
e. Fuel Pump .........................................................................OFF
except for landing and switching tanks.
f. Panel and Overhead Lights ...............................................OFF
g. Landing Light.....................................................................OFF
• WARNING •
Do not shed loads from Avionics Essential, Essential, or
Essential 2 Bus row.
h. Skywatch/TAWS Circuit Breaker......................................PULL
i. Weather/Stmscpe Circuit Breaker ...................................PULL
j. MFD Circuit Breaker ........................................................PULL
9. Assess flight conditions:
If in Visual Meteorological Conditions (VMC):
a. Pitot Heat...........................................................................OFF
b. Ice Protection.....................................................................OFF
If in Instrument Meteorological Conditions (IMC) or visible
moisture:
a. Pitot Heat............................................................................ ON
b. Ice Protection.......................................................ON, As Reqd
c. Strobe Lights .....................................................................OFF
10. Replan flight for a landing as soon as practical (within one hour) at
a landing field with visual minimums. Increase landing speed 10
KIAS for flaps up. Do not use landing lights.
Revision 02: 01-06-10

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