Cirrus SR22T User Manual

7-86 P/N 13772-005
Section 7 Cirrus Design
Systems Description SR22T
Headset and Microphone Installation
The airplane is equipped with provisions for five Active Noise
Reduction (ANR) and three conventional (MIC/HEADPHONES)
headsets. Headset jacks for the pilot, front, and rear seat passenger
are located in the map case.
The forward headset mics use the remote Push-To-Talk (PTT)
switches located on the top of the associated control yoke grip. The
rear headsets do not have COM transmit capabilities and do not
require PTT switches. Audio to headsets is controlled by the individual
audio selector switches on the audio control panel
Audio Input Jack
The aircraft contains multiple audio input jacks which can be used to
connect personal entertainment devices into the cabin sound system.
Two 3.5 mm audio input jacks (AUDIO INPUT) are provided on the
center console. One jack is located near the convenience outlet for
use by the pilot and forward passenger, and the other is located on the
aft portion of the center console for the rear passengers.
Distribution of a device connected to the forward jack is through the
MUS 1 selection on the audio panel. Distribution of the rear jack is by
the MUS 2 selection on the audio panel. A third jack on the audio
panel will also accept an entertainment input. A device connected to
this jack is distributed by selecting the Entertainment button (shown as
a phone and music-note symbol) on the audio panel. Audio volume
can be controlled by the device itself and can be further refined by the
audio panel distribution volume control.
Cell Phone Input Jack
One 2.5 mm cell phone jack is located on the front of the audio panel
and is distributed by selecting the Entertainment button (shown as a
phone and music-note symbol) on the audio panel. Volume is
controlled by the volume selector on the audio panel
Avionics Cooling Fans
Electric fans provide forced ambient-air cooling for the Integrated
Avionics System. A fan located forward of the instrument panel
provides ambient air cooling directly to the Integrated Avionics Units.
Two a dditio nal fa ns bl ow air dir ectly on to the heat s inks l oca ted on the
forward sides of the PFD and MFD.
28 VDC for MFD Fan operation is supplied through the 5-amp
AVIONICS FAN 1 circuit breaker on NON-ESSENTIAL BUS. 28 VDC
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