Cirrus SR22T User Manual

P/N 13772-136 1 of 6
Cirrus Design Section 9
SR22 / SR22T Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual Supplement
for the
Garmin Terrain Awareness/Warning System
(Aircraft Serials w/ Perspective Avionics Only)
When the Garmin Terrain Awareness/Warning System is installed on
the aircraft, this POH Supplement is applicable and must be inserted
in the Supplements Section of the Pilot’s Operating Handbook. This
document must be carried in the airplane at all times. Information in
this supplement adds to, supersedes, or deletes information in the
basic Pilot’s Operating Handbook.
• Note •
This POH Supplement Change, dated Revision 01: 01-06-10,
supersedes and replaces the Original release of this POH
Supplement dated 05-13-08.
Revision 01: 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