Cirrus SR22T User Manual

Cirrus Design Section 9
SR22 / SR22T Supplements
P/N 13772-135 1 of 30
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for the
GFC 700 Automatic Flight Control System
(Aircraft Serials w/ Perspective Avionics Only)
Including optionally installed Electronic Stability and Protection
(ESP), Underspeed Protection (USP), and Hypoxia Detection and
Automatic Descent functions.
When the GFC 700 Automatic Flight Control System is installed on the
aircraft, this POH Supplement is applicable and must be inserted in
the Supplements Section of the basic 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 03: 12-14-10,
supersedes and replaces the Revision 02 release of this POH
Supplement dated 01-06-10.
Revision 03: 12-14-10

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