Cirrus DESIGN SR22T User Manual

P/N 13772-115 1 of 20
Cirrus Design Section 9
SR22 / SR22T Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for the
Basic Ice Protection System
When the Basic Ice Protection 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 •
Noted effectivity “Serials with G3 Wing” indicates Serials 22-
2334, 22-2420, 22-2438 and subsequent, 22T-0001 and
subsequent.
Noted effectivity “Serials before G3 Wing” indicates Serials
22-0334 thru 22-2333, 22-2335 thru 22-2419, 22-2421 thru
22-2437 unless otherwise noted.
This POH Supplement Change, dated Revision 09: 12-17-10,
supersedes and replaces revision 08 of this POH Supplement
dated 01-06-10.
Revision 09: 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