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Panel Flood Lights .....................................................................7-56
March 2010
Reading Lights...........................................................................7-56
Overhead Dome Light................................................................7-56
Environmental System..................................................................7-57
Cabin Heat Control ....................................................................7-59
Cabin Cooling Control................................................................7-59
Cabin Air Selector......................................................................7-59
Pitot-Static System........................................................................7-61
Pitot Heat Switch .......................................................................7-61
Pitot Heat Light ..........................................................................7-61
Alternate Static Source ..............................................................7-61
Vacuum System............................................................................7-62
Suction Gauge ...........................................................................7-64
Vacuum Warning Light ..............................................................7-64
Aux Vac Caution Light ...............................................................7-64
Stall Warning System....................................................................7-65
Standard Avionics .........................................................................7-66
Multi-Function Display ...............................................................7-68
Autopilot.....................................................................................7-70
GPS Navigation .........................................................................7-72
Communication (COM) Transceivers ........................................7-73
Navigation (Nav) Receiver.........................................................7-74
Transponder ..............................................................................7-74
Audio System.............................................................................7-75
Emergency Locator Transmitter ................................................7-76
Hour Meter .................................................................................7-77
Digital Clock...............................................................................7-78
Cirrus Airplane Parachute System................................................7-80
System Description....................................................................7-80
Activation Handle .......................................................................7-81
Deployment Characteristics .......................................................7-82
Section 7 Cirrus Design
Airplane Description SR20
March 2010
Information Manual 7-3
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
area is bounded on the forward side by the firewall at fuselage station
100, and on the rear by the aft baggage compartment bulkhead at
fuselage station 222. Comfortable seating is provided for four adults. A
composite roll cage within the fuselage structure provides roll
protection for the cabin occupants. The cabin and baggage
compartment floors are constructed of a foam core composite with
access to under-floor components.
All flight and static loads are transferred to the fuselage structure from
the wings and control surfaces through four wing attach points in two
locations under the front seats and two locations on the sidewall just
aft of the rear seats.
• Note •
Refer to Airplane Cabin description in this section for a
complete description of doors, windows, baggage
compartment, seats, and safety equipment.
　
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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(51)