Cirrus SR22T User Manual

7-74 P/N 13772-005
Section 7 Cirrus Design
Systems Description SR22T
3 and the 5-amp MFD 2 circuit breaker on MAIN BUS 1. Either circuit
is capable of powering the MFD. System start-up is automatic once
power is applied. Power-on default brightness is determined by
ambient lighting and is user adjustable.
GCU 478 Flight Management System Keyboard
The Flight Management System Keyboard is found on the upper
section of the center console and is the primary interface for avionics
system data entry, PFD/MFD operation, NAV/COM tuning, and
heading, course and altitude selection.
28 VDC for Flight Management System Keyboard operation is
supplied through the 5-amp KEYPADS / AP CTRL circuit breaker on
MAIN BUS 1.
GRS 77 Attitude and Heading Reference System (AHRS)
The Attitude and Heading Reference System (AHRS) unit(s), mounted
behind the PFD, provide airplane attitude and heading information to
both the PFD and the primary Air Data Computer. The AHRS units(s)
contain advanced sensors (including accelerometers and rate
sensors) and interfaces with the: primary Magnetometer to obtain
magnetic field information, the Air Data Computer to obtain air data,
and both Integrated Avionics Units to obtain GPS information.
28 VDC for AHRS 1 operation is supplied through the 5-amp AHRS 1
circuit breaker on the ESS BUS 1. If option installed, 28 VDC for
AHRS 2 operation is supplied through the 5-amp AHRS 2 circuit
breaker on the MAIN BUS 2.
GDC 74A Air Data Computer (ADC)
The Air Data Computer(s), mounted behind the instrument panel to
the right of the MFD, process data from the Pitot/Static system and
outside air temperature (OAT) sensor(s). This unit(s) provide pressure
altitude, airspeed, vertical speed and OAT information to the
Integrated Avionics System, and communicate with the primary PFD,
Integrated Avionics Unit, and AHRS units. The Air Data Computer(s) is
also connected directly to the Outside Air Temperature probe(s) and
Pitot-Static System.
28 VDC for ADC 1 operation is supplied through the 5-amp ADC 1
circuit breaker on the ESS BUS 1. If option installed, 28VDC for ADC 2
operation is supplied through a 5-amp AHRS 2 / ADC 2 circuit breaker
on the MAIN BUS 2.
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