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uses standard flight instruments arranged in the ‘basic-six’ pattern.
They include:
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. A parking brake knob is
mounted below the flight instruments inboard of the pilot at knee level.
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.
Airspeed Indicator Attitude Gyro Altimeter
Turn/Bank
Coordinator
Directional Gyro
Vertical Speed
Indicator
March 2010
Information Manual 7-17
Cirrus Design Section 7
SR20 Airplane Description
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
5
4
1
0
ALTIMETER 3
6
2
SPEED
VERTICAL
0
5
5
15
15
10
20
10
S
E
W
N
SR20_FM07_1059E
G I
T F
E
R
LL L
FUEL
W
H R
I N H G G A L
O L
F
L
E
U F
0
6
9
12
18
N A
M
S S E
R P
20
10
30
S U C T I O N
4 6
5
X
100
RPM
0
5
10
35
30
25
15 20
P
E T
M
OIL
E
S S
R P
75 0
50
25
75
100
150
200
240 100
PUSH/HOLD A P DISC
NO PITCH INFORMA TION
L R
LO HI
TURN COORDINATOR
2 MIN
UP
TRIM
RDY DN
ALT
ST HD TRK
L R
PULL ON
ALT AIR
SOURCE
ALT STATIC
NORMAL
PULL ON
PARK BRAKE
20 20
10
O
R
Y
G
CIRRUS
10
10 10
18. Avionics Panel
19. Bolster Switch Panel
20. Control Yoke
21. Start/Ignition Key Switch
6420
30- +30
.P
T
AL
TEMP C
AIRSPEED
200
180
40
O F
O F
T
E
T
C
G H
300
400
200
500
300
1400
1500
600
Figure 7-4
Instrument Panel and Console
March 2010
7-18 Information Manual
Section 7 Cirrus Design
Airplane Description SR20
Flight Instruments
• Note •
For additional information on instrument limit markings, refer
to Section 2, Limitations.
Attitude Indicator
The attitude gyro gives a visual indication of flight attitude. Bank
attitude is indicated by a pointer at the top of the indicator relative to
the bank scale with index marks at 10°, 20°, 30°, 60°, and 90° either
side of the center mark. A fixed miniature airplane superimposed over
a movable mask containing a white symbolic horizon bar, which
divides the mask into two sections, indicates pitch and roll attitudes.
The upper “blue sky” section and the lower “earth” section have pitch
　
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本文鏈接地址：西銳20飛機信息手冊 SR22 AIRPLANE INFORMATION MANUAL 1148-126(54)