Cirrus DESIGN SR22T User Manual

P/N 13772-134 1 of 48
Cirrus Design Section 9
SR22 / SR22T Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for the
TKS Anti-Ice System
• Approved for Flight Into Known Icing (FIKI)
• 8.0 gallon usable capacity.
• 4.0 gallon tank in each wing.
When the TKS Anti-Ice 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 04: 12-17-10,
supersedes and replaces the Revision 03 Issue of this POH
Supplement dated 01-06-10.
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