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The GTX 33 Mode S solid-state transponder communicates with the
primary Integrated Avionics Unit and provides Modes A, C, and S
interrogation/reply capabilities. The transponder is controlled via the
PFD or Flight Management System Keyboard and is located in the
empennage avionics compartment.
28 VDC for Mode S Transponder operation is supplied through the 2-
amp XPONDER circuit breaker on AVIONICS BUS. 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.
GDL 69/69A XM Satellite Weather and Radio
The Data Link Satellite Receiver, mounted in the empennage avionics
compartment, receives and transmits real-time weather information to
the MFD and PFD. If GDL 69A option is installed, this unit also
provides digital XM audio entertainment to the cabin audio system via
the GRT 10 XM Radio Remote Transceiver, mounted in the
empennage avionics compartment and controlled by the GRC 10
Remote Control.
28 VDC for Satellite Data Link Receiver operation is supplied through
the 3-amp WEATHER circuit breaker on AVIONICS BUS. 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
7-74 Information Manual
Section 7 Cirrus Design
Airplane and Systems Description SR22
L-3 Skywatch Traffic Advisory System
The L-3 Skywatch Traffic Advisory System (TAS) advises the pilot of
transponder-equipped aircraft that may pose a collision threat. TAS
information is displayed on the MFD and indicates the relative range,
bearing, and altitude of intruder aircraft. The Traffic Advisory System
consists of a Transmitter Receiver Computer installed in the avionics
bay, and a directional antenna installed on the airplane exterior. The
system utilizes inputs from the secondary Integrated Avionics Units via
the primary Air Data Computer and is controlled via the MFD or Flight
Management System Keyboard.
28 VDC for Traffic Advisory System operation is supplied through the
5-amp TRAFFIC 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 L-3
Skywatch Pilot’s Guide for a detailed discussion of the Traffic Advisory
System.
L-3 Stormscope WX-500 Weather Mapping Sensor
The L-3 Stormscope WX-500 Weather Mapping Sensor detects
electrical discharges associated with thunderstorms and displays the
activity on the MFD. The system consists of an antenna located on top
of the fuselage and a processor unit mounted under the aft baggage
floor. The antenna detects the electrical and magnetic fields generated
by intra-cloud, inter-cloud, or cloud to ground electrical discharges
occurring within 200 nm of the airplane and sends the “discharge” data
to the processor. The processor digitizes, analyzes, and converts the
“discharge” signals into range and bearing data and communicates
the data to the MFD every two seconds via the secondary Integrated
Avionics Unit.
28 VDC for Stormscope System operation is supplied through the 3-
amp WEATHER 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 L-3
Stormscope WX-500 Weather Mapping Sensor Pilot’s Guide for a
detailed discussion of the system.
March 2010
Cirrus Design Section 7
SR22 Airplane and Systems Description
Information Manual 7-75
Bendix/King KR 87 Automatic Direction Finder (ADF)
The KR 87 ADF System is used as a means of identifying positions,
receiving low and medium frequency voice communications, homing,
tracking, and for navigation on instrument approach procedures. The
system consists of an antenna installed on the airplane exterior and
the KR 87 receiver which communicates with the Integrated Avionics
System via the secondary Integrated Avionics Unit. The HSI Bearing
Needle may be configured to indicate ADF tracking and homing
information.
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 ADF
System Pilot’s Guide for a detailed discussion of the system.
Bendix/King KN 63 Distance Measuring Equipment (DME)
The KN 63 DME determines aircraft distance to a land-based
　
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