Cirrus SR22T User Manual

P/N 13772-109 1 of 6
Cirrus Design Section 9
SR22 / SR22T Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Approved Oxygen Systems
When supplemental oxygen is required by the applicable operating
rules (FAR Part 91 or FAR Part 135), this 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 Revision dated Revision 02: 01-06-10,
supersedes and replaces the Revision 01 release of this POH
Supplement dated 10-10-03.
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