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Rudder (yaw) trim operates on 28 VDC supplied through the 2-amp
PITCH / YAW TRIM circuit breaker on Main Bus 1. The switch and
indicator are not internally illuminated.
Revision A5
7-16 P/N 13772-001
Section 7 Cirrus Design
Airplane Description SR22
Flight Deck Arrangement
The following paragraphs are a general description of the flight deck,
instrumentation, and controls. The instrument panel is designed for
glare-free use in all flight conditions. The instrument panel is arranged
primarily for use by the pilot in the left seat; however, it can be viewed
from either seat. For details relating to the instrumentation, switches,
circuit breakers, and controls on the instrument panel, bolster, and
center console, refer to the related topics in this section.
Instrument Panel
Serials 0002 through 1601, 1603 through 1643 and 1645 through
1662 without PFD: Flight instruments and annunciators are located on
the left side of the panel and engine instruments are located on the
right side of the instrument panel. A large color multifunction display is
located between the flight instruments and the engine instruments.
Temperature controls are located on the right side below the engine
instruments.
The SR22 uses standard flight instruments arranged in the 'basic-six'
pattern. They include:
Serials 0002 through 0434, an electronic clock and VOR/LOC/ILS
(CDI) are located immediately to the left of the flight instruments on the
instrument panel.
A switch panel located in the “dash board” bolster below the flight
instruments contains the master and ignition switches, avionics power
switch, pitot heat switch, and lighting switches.
Airspeed Indicator Attitude Gyro Altimeter
Turn Coordinator HSI
Vertical Speed
Indicator
Revision A5
P/N 13772-001 7-17
Cirrus Design Section 7
SR22 Airplane Description
Serials 0435 and subsequent with PFD: The airplane is equipped with
an Avidyne FlightMax Entegra-Series Primary Flight Display (PFD).
The PFD is a 10.4” landscape-oriented display intended to be the
primary display of primary flight parameter information (attitude,
airspeed, heading, and altitude) to the pilot. The PFD accepts data
from a variety of sources, including the GPS sensors, the System 55X
Autopilot, and is the primary heading source for the Multifunction
Display.
Standby altimeter, airspeed, and attitude indicators are mounted on
the bolster panel in case of total or partial PFD failure. To provide roll
data to the autopilot system, a Turn Coordinator is mounted behind the
RH bolster panel.
Annunciators and the ignition switch are located on the left side of the
panel and a large color multifunction display is located adjacent to the
primary flight display. Temperature controls are located on the right
side below the glove compartment.
A switch panel located in the “dash board” bolster below the flight
instruments contains the master switch, avionics power switch, pitot
heat switch, and lighting switches.
Center Console
A center console contains the avionics, flap control and position lights,
power lever and mixture controls, fuel system indicator and controls,
and audio controls. System circuit breakers, the alternate static source
valve, alternate induction air control, and ELT panel switch are located
on the left side of the console for easy access by the pilot. A friction
knob for adjusting throttle and mixture control feel and position stability
is located on the right side of the console. An accessory outlet, map
compartment, audio jacks, hour meter, emergency egress hammer,
and headset jacks are installed inside the console armrest.
Revision A5
7-18 P/N 13772-001
Section 7 Cirrus Design
Airplane Description SR22
Figure 7-4
18
12
11
10
9
17
22
21
20
19
16 15 14 13
1 2 3 4 5 6 7 8
PUSH/HOL D A P DISC
NO PITCH INFORMATION
L R
LO HI
TURN COORDINATOR
2 MIN
UP
TRIM
RDY DN
ALT
ST HD TRK
L R
18. Rudder Trim Switch/Indicator
19. Avionics Panel
20. Bolster Switch Panel
21. Control Yoke
22. Start/Ignition Key Switch
Legend
1. Flight Instrument Panel
2. Annunciator Panel
3. Overhead Light & Switch
4. Magnetic Compass
5. Cirrus Airframe Parachute System
(CAPS) Activation T-Handle Cover
6. Multifunction Display
7. Engine Instruments
8. Temperature/Ventilation Controls
9. Control Yoke
10. Fresh Air “Eyeball” Outlet
11. Conditioned Air Outlet
　
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