曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

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
SR22_FM07_1455B
Instrument Panel and Console (Sheet 1 of 3)
Revision A5
P/N 13772-001 7-19
Cirrus Design Section 7
SR22 Airplane Description
1 2 4 5 6 7 8 9
17 16 15 14
19
20
22
18
10
11
12
13
21
ALTITUDE GPH
16000 17
12000 18
8000 21
4000 24
SL 27
MAX POWER FUEL FLOWS
FIRE EXTINGUISHER UNDER PILOT SEAT FRONT FASTEN SEATBELTS NO SMOKING
BATT
AMMETER
SELECT
ALT 1 ALT 2
3
9. Temperature/Ventilation Controls
10. Control Yoke
11. Fresh Air “Eyeball” Outlet
12. Conditioned Air Outlet
13. Rudder Pedals
14. Flap Control & Position Indicators
15. Passenger Audio Jacks
16. Armrest
17. Engine & Fuel System Controls
Legend
1. Start/Ignition Key Switch
2. Annunciator Panel
3. Primary Flight Display
4. Overhead Light & Switch
5. Magnetic Compass
6. Cirrus Airframe Parachute System
(CAPS) Activation T-Handle Cover
7. Multifunction Display
8. Engine Instruments
SR22_FM07_1730
18. Left Side Console
· Circuit Breaker Panel
· Alternate Engine Air
· Parking Brake
· Alternate Static Source
19. Avionics Panel
20. Bolster Switch Panel
21. Control Yoke
22. Flight Instrument Panel
PULL ON
ALT AIR
SOURCE
ALT STATIC
NORMAL
PULL ON
PARK BRAKE
G I
T F
E
R
LL L
FUEL
Figure 7-4
Instrument Panel and Console (Sheet 2 of 3)
Revision A5
7-20 P/N 13772-001
Section 7 Cirrus Design
Airplane Description SR22
Figure 7-4
1 2 4 5 6 7 8 9
17 16 15 14
19
20
22
18
10
11
12
13
21
SR22_FM07_2216
3
9. Temperature/Ventilation Controls
10. Control Yoke
11. Fresh Air “Eyeball” Outlet
12. Conditioned Air Outlet
13. Rudder Pedals
14. Flap Control & Position Indicators
15. Passenger Audio Jacks
16. Armrest
17. Engine & Fuel System Controls
Legend
1. Start/Ignition Key Switch
2. Annunciator Panel
3. Primary Flight Display
4. Overhead Light & Switch
5. Magnetic Compass
6. Cirrus Airframe Parachute System
(CAPS) Activation T-Handle Cover
7. Multifunction Display
8. Glove Box
18. Left Side Console
· Circuit Breaker Panel
· Alternate Engine Air
· Parking Brake
· Alternate Static Source
19. Avionics Panel
20. Bolster Switch Panel
21. Control Yoke
22. Flight Instrument Panel
PULL ON
SOURCE
PULL ON
G I
T F
E
R
LL L
FUEL
ALT AIR
ALT STATIC
NORMAL
PARK BRAKE
Instrument Panel and Console (Sheet 3 of 3)
Revision A5
P/N 13772-001 7-21
Cirrus Design Section 7
SR22 Airplane Description
Flight Instruments
• Note •
For additional information on instrument limit markings, refer
to Section 2, Limitations.
Primary Flight Display - Serials 0435 and Subsequent
The Primary Flight Display (PFD) provides the functions of the attitude
indicator, heading indicator, airspeed indicator, altimeter, vertical
speed indicator, directional gyro, course deviation indicator, and
altitude pre-select controller onto a single electronic display. In
addition, the PFD communicates with GPS1, GPS2, NAV1, NAV2, the
Multifunction Display, and Autopilot System.
An integral air data/attitude and heading reference system (ADAHRS)
uses a 3-axis solid state gyro and accelerometer system combined
with a magnetometer to replace the vertical and directional gyros.
ADAHRS also provides roll, pitch, heading data and continually
updates the winds aloft and true airspeed (TAS) indications on the
PFD. The magnetometer assembly mounted in the wing also provides
outside air temperature (OAT) data.
The airplane’s Pitot-Static system is connected to the PFD to provide
airspeed, altitude, and vertical speed.
Standby instruments for airspeed, attitude and altitude are mounted on
the LH bolster panel and are on separate power sources than the PFD.
Redundant power sources provide 28 VDC for system operation.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：CIRRUS DESIGN SR22西銳22飛行員操作手冊和飛機飛行手冊(61)