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7-16 Information Manual
Section 7 Cirrus Design
Airplane Description SR20
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 1268 through 1336: 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 SR20 uses standard flight instruments arranged in the 'basic-six'
pattern. They include:
Serials 1268 through 1337, an electronic clock is 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
March 2010
Information Manual 7-17
Cirrus Design Section 7
SR20 Airplane Description
Serials 1337 and subsequent: 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.
March 2010
7-18 Information Manual
Section 7 Cirrus Design
Airplane Description SR20
Figure 7-4
1 2 3 4 5 6 7 8
16 15 14 13
18
19
20
21
17
9
10
11
12
KNOTS
120 130
140 150 160
120
140
160
100
80
60
11. Conditioned Air Outlet
12. Rudder Pedals
13. Flap Control & Position Indicators
14. Passenger Audio Jacks
15. Armrest
16. Engine & Fuel System Controls
17. Left Side Console
· Circuit Breaker Panel
· Alternate Engine Air
· Parking Brake
· Alternate Static Source
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
16
0
60
30
30
20
24
28
32 + 60
P
M A
T
L
O V
9
8
7
　
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