Cirrus SR22T User Manual

Cirrus Design Section 9
SR22 / SR22T Supplements
P/N 13772-135 15 of 30
Figure -1
GFC 700 Automatic Flight Control System Schematic
GFC 705
MODE CONTROLLER
PITCH TRIM
CARTRIDGE
INTEGRATED
AVIONICS UNIT 2
INTEGRATED
AVIONICS UNIT 1
MFD PFD
PITCH TRIM
ADAPTER
YAW SERVO
(optional)
ROLL SERVO PITCH SERVO
SR22_FM09_2919
4-WAY
TRIM
GO-AROUND
SWITCH
A/P DISC
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