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Strobe Light................................................................................7-74
Landing Light .............................................................................7-74
Interior Lighting .............................................................................7-74
Revision A7
Instrument Lights .......................................................................7-75
Panel Flood Lights .....................................................................7-75
Reading Lights...........................................................................7-75
Overhead Dome Light................................................................7-75
Environmental System..................................................................7-76
Description and Operation .........................................................7-76
Description and Operation .........................................................7-79
Pitot-Static System........................................................................7-82
Pitot Heat Switch .......................................................................7-82
Pitot Heat Light ..........................................................................7-82
Alternate Static Source ..............................................................7-84
Stall Warning System....................................................................7-84
Standard Avionics .........................................................................7-85
Multi-Function Display ...............................................................7-86
Autopilot.....................................................................................7-88
GPS Navigation .........................................................................7-91
Communication (COM) Transceivers ........................................7-93
Navigation (Nav) Receiver.........................................................7-94
Transponder ..............................................................................7-95
Audio System.............................................................................7-95
Emergency Locator Transmitter ................................................7-96
Hour Meter(s).............................................................................7-98
Digital Clock...............................................................................7-99
Cirrus Airplane Parachute System..............................................7-101
System Description..................................................................7-101
Activation Handle .....................................................................7-102
Deployment Characteristics .....................................................7-103
Section 7 Cirrus Design
Airplane Description SR22
Revision A7
P/N 13772-001 7-3
7-4 P/N 13772-001
Section 7 Cirrus Design
Airplane Description SR22
Revision A7
Intentionally Left Blank
P/N 13772-001 7-5
Cirrus Design Section 7
SR22 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
Revision A5
7-6 P/N 13772-001
Section 7 Cirrus Design
Airplane Description SR22
Airframe
Fuselage
The SR22 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.
Serials 0795, 0820 and subsequent: The lower firewall employes a 20°
bevel to improve crashworthiness. In addition, an avionics bay is
located aft of bulkhead 222 and accessible through an access panel
installed on the RH side of the aft fuselage.
• Note •
　
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