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transponder by sending and receiving pulse pairs - two pulses of fixed
duration and separation. The ground stations are typically collocated
with VORs. The system consists of an antenna installed on the
airplane exterior and the KN 63 receiver which communicates with the
Integrated Avionics System via the secondary Integrated Avionics
Unit.
28 VDC for ADF System operation is supplied through the 3-amp
DME/ADF circuit breaker on AVIONICS BUS. Refer to the Perspective
Integrated Avionics System Pilot’s Guide for a general description of
the system and its operating modes. Refer to the Bendix/King DME
System Pilot’s Guide for a detailed discussion of the system.
March 2010
7-76 Information Manual
Section 7 Cirrus Design
Airplane and Systems Description SR22
Synthetic Vision System
The Synthetic Vision System (SVS) is intended to provide the pilot with
enhanced situational awareness by placing a three dimensional
depiction of terrain, obstacles, traffic and the desired flight path on the
PFD so that proximity and location is more easily understood during
instrument scanning. The SVS database is created from a digital
elevation model with a 9 arc-sec (approx. 885 ft (270m)) horizontal
resolution.
The synthetic vision system is not intended to be used independently
of traditional attitude instrumentation. Consequently, SVS is disabled
when traditional attitude instrumentation is not available. Otherwise,
the traditional attitude instrumentation will always be visible in the
foreground with SVS features in the background. The PFD with SVS
installed includes:
• Perspective depiction of surrounding terrain,
• Zero pitch line,
• Perspective depiction of runways,
• Perspective depiction of large bodies of water,
• Perspective depiction of obstacles,
• Flight path marker,
• Terrain warning system,
• Field of view depiction on the MFD Navigation Page.
Refer to the Perspective Integrated Avionics System Pilot’s Guide for a
complete description of the system, its operating modes, and
additional detailed operating procedures
March 2010
Cirrus Design Section 7
SR22 Airplane and Systems Description
Information Manual 7-77
Annunciation and Alert System
Aircraft annunciations and alerts are displayed in the Crew Alerting
System (CAS) window located to the right of the altimeter and VSI.
Aircraft annunciations are grouped by criticality and sorted by order of
appearance with the most recent message on top. The color of the
message text is based on its urgency and required action:
• Warning (red) – Immediate crew awareness and action required.
• Caution (yellow) – Immediate crew awareness and future
corrective action required.
• Advisory (white) – Crew awareness required and subsequent
action may be required.
In combination with the CAS Window, the system issues an audio alert
when specific system conditions are met and an expanded description
of the condition is displayed in the Alerts Window located in the lower
RH corner of the PFD.
• Note •
For specific pilot actions in response to System
Annunciations, refer to Section 3 - Emergency Procedures
and Section 3A - Abnormal Procedures.
For additional information on Engine Instrument Markings and
Annunciations, refer to Section 2 - Limitations.
March 2010
7-78 Information Manual
Section 7 Cirrus Design
Airplane and Systems Description SR22
Figure 7-17
Equipment Locations
LEGEND
1. AHRS 1
2. Integrated
Avionics Unit 1
3. AHRS 2
4. Avionics Cooling Fan
5. Integrated
Avionics Unit 2
6. Engine Airframe Unit
7. Air Data Computer
8. GFC 705 Mode
Controller (opt)
9. ADF (Opt)
10. CAPS Activation Handle
(Cabin Ceiling)
11. Hour Meters
12. Egress Hammer
13. Telephone and
Audio Jacks
14. Cabin Speaker
15. Roll Servo (opt)
16. Pitch Trim Adapter (opt)
17. Pitch Servo (opt)
18. XM Radio
Transceiver (Opt)
19. Transponder
20. Satellite Data Link
Receiver (Opt)
21. ELT
22. Yaw Servo (opt)
23. Battery 2
24. Tiedown Loops
25. CAPS Parachute
26. WX Information
Receiver (Opt)
27. Microphone
28. TAS Receiver (Opt)
29. DME (Opt)
30. Fire Extinguisher
22
15
17
16
6 5 4
29
SR22_FM07_2786B
8
4
13
7
10
11
12
14
18
19
20
30
26
25
　
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