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Power Distribution......................................................................7-68
BAT & ALT Master Switches......................................................7-70
Avionics Power Switch...............................................................7-71
Volts and Ampere Meter/Indication............................................7-71
Ammeter Select Switch..............................................................7-73
Low-Volts Warning Light ............................................................7-73
ALT Fail Caution Lights..............................................................7-73
Circuit Breakers and Fuses........................................................7-74
Ground Service Receptacle .......................................................7-75
Convenience Outlet ...................................................................7-75
Exterior Lighting ............................................................................7-76
Navigation Lights .......................................................................7-76
Strobe Light................................................................................7-76
Landing Light .............................................................................7-76
March 2010
Interior Lighting .............................................................................7-76
Instrument Lights .......................................................................7-77
Panel Flood Lights .....................................................................7-77
Reading Lights...........................................................................7-77
Overhead Dome Light................................................................7-77
Environmental System..................................................................7-78
Description and Operation .........................................................7-82
Pitot-Static System........................................................................7-84
Pitot Heat Switch .......................................................................7-84
Pitot Heat Light ..........................................................................7-84
Alternate Static Source ..............................................................7-86
Stall Warning System....................................................................7-86
Standard Avionics .........................................................................7-87
Multi-Function Display ...............................................................7-89
Autopilot.....................................................................................7-90
GPS Navigation .........................................................................7-93
Communication (COM) Transceivers ........................................7-95
Navigation (Nav) Receiver.........................................................7-96
Transponder ..............................................................................7-98
Audio System.............................................................................7-98
Emergency Locator Transmitter ................................................7-99
Hour Meter(s)...........................................................................7-100
Digital Clock.............................................................................7-101
Cirrus Airplane Parachute System..............................................7-103
System Description..................................................................7-103
Activation Handle .....................................................................7-104
Deployment Characteristics .....................................................7-105
Section 7 Cirrus Design
Airplane Description SR20
March 2010
Information Manual 4
7-4 Information Manual
Section 7 Cirrus Design
Airplane Description SR20
March 2010
Intentionally Left Blank
Information Manual 7-5
Cirrus Design Section 7
SR20 Airplane Description
Introduction
This section provides a basic description and operation of the
standard airplane and its systems. Optional equipment described
within this section is identified as optional.
• Note •
Some optional equipment, primarily avionics, may not be
described in this section. For description and operation of
optional equipment not described in this section, refer to
Section 9, Supplements
March 2010
7-6 Information Manual
Section 7 Cirrus Design
Airplane Description SR20
Airframe
Fuselage
The SR20 monocoque fuselage is constructed primarily of composite
materials and is designed to be aerodynamically efficient. The cabin
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西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(52)
