Cirrus SR22T User Manual

7-14 P/N 13772-005
Section 7 Cirrus Design
Systems Description SR22T
Instrument Panel
The instrument panel is of all metal construction and is installed in
sections so equipment can be easily removed for maintenance. The
surrounding glareshield is made of composite material and projects
over the instrument panel to reduce reflections on the windshield from
lighted equipment and to shield the panel equipment from glare.
Pilot Panel Arrangement
Two co lor l andscape -or iented elec tronic f light d ispl ays ar e i nstalle d to
the instrument panel; the Primary Flight Display (PFD) and the
Multifunction Display (MFD). The PFD, installed directly in front of the
pilot, is a intended to be the primary display of flight parameter
information (attitude, airspeed, heading, and altitude). The MFD,
installed to the right of the PFD, provides supplemental situational and
navigation information to the pilot. The ignition switch is located on the
left side of the instrument panel. The cabin environmental control
switches are located on the right side of the instrument panel.
Instrument panel air vents are located on the outboard sections of the
panel.
Center Console Arrangement
A center console contains the Flight Management System Keyboard,
autopilot and audio controls, flap system control and indication, fuel
selector valve, and the power and mixture levers. System circuit
breakers, the alternate static source valve, and the ELT panel switch
are located on the left side of the console. A friction knob for adjusting
throttle and mixture control feel and position stability is located on the
right side of the console. The accessory outlet, map compartment,
audio jacks, hour meters, and emergency egress hammer are installed
inside the console armrest.
Bolster Panel Arrangement
A switch panel located in the “dash board” bolster below the
instrument panel contains the master, avionics power, ice protection
(optional), Pitot heat, and exterior and interior lighting switches and
controls. The standby airspeed, attitude, and altimeter instruments are
located below bolster switch panel.
Original Issue

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