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yaw trim is ground adjustable only.
A ground adjustable trim tab is installed on the rudder to provide small
adjustments in neutral trim. This tab is factory set and does not
normally require adjustment.
Control Locks
The aircraft’s control system is not equipped with gust locks. The trim
spring cartridges have sufficient power to act as a gust damper without
rigidly locking the position.
March 2010
Cirrus Design Section 7
SR22 Airplane and Systems Description
Information Manual 7-13
Figure 7-3
Rudder System
SR22_FM07_1463
March 2010
7-14 Information Manual
Section 7 Cirrus Design
Airplane and Systems Description SR22
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 color landscape-oriented electronic flight displays are installed 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
system indicator and controls, and the power and mixture levers.
System circuit breakers, the alternate static source valve, alternate
induction air control, 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.
March 2010
Cirrus Design Section 7
SR22 Airplane and Systems Description
Information Manual 7-15
Figure 7-4
Instrument Panel and Console
15
18
20
2
1
3
4
5
9
11
12 10
14
17
16
13
6
47
8
6
19
13. Left Side Console
· Circuit Breaker Panel
· Alternate Engine Air
· ELT Remote Switch
· Alternate Static Source
14. Avionics Panel
15. Parking Brake
16. Flight Instrument Panel
17. Bolster Switch Panel
18. Start/Ignition Key Switch
19. Primary Flight Display
20. Overhead Light & Switch
Legend
1. Cirrus Airframe Parachute System
(CAPS) Activation T-Handle Cover
2. Magnetic Compass
3. Multifunction Display
4. Fresh Air “Eyeball” Outlet
5. Temperature/Ventilation Controls
6. Control Yoke
7. Conditioned Air Outlet
8. Rudder Pedals
9. Flap Control & Position Indicators
10. Armrest
11. Passenger Audio Jacks
12. Engine & Fuel System Controls SR22_FM07_2688A
March 2010
7-16 Information Manual
Section 7 Cirrus Design
Airplane and Systems Description SR22
Flight Instruments
Flight instruments and annunciations are displayed on the Primary
Flight Display (PFD) located directed in front of the pilot. The PFD
presents the primary flight instruments arranged in the conventional
basic “T” configuration. Standby instruments for airspeed, attitude and
altitude are mounted on the LH bolster panel and are on separate
power sources than the PFD.
Knobs, knob sets, and membrane-type push button switches are
located along the inboard edge of the PFD and MFD and provide
control for communication (COM), navigation (NAV), heading (HDG),
　
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