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Satcom Antenna Control Unit .................................................................................... 06-01-12
Data Link (Optional) ............................................................................................................ 06-01-12
Description................................................................................................................. 06-01-12
Static Wicks ......................................................................................................................... 06-01-13
Cockpit Voice Recorder (CVR)............................................................................................06-01-14
Description................................................................................................................. 06-01-14
Components and Operation....................................................................................... 06-01-14
CVR Control Panel..................................................................................................... 06-01-14
Area Microphone........................................................................................................ 06-01-15
Recorder Unit............................................................................................................. 06-01-15
Emergency Locator Transmitter .......................................................................................... 06-01-16
Description................................................................................................................. 06-01-16
Cabin Communication System (Optional) ........................................................................... 06-01-16
Description................................................................................................................. REV 1 06-01-16
COMMUNICATIONS
Table of Contents (Cont)
Volume 2 Flight Crew Operating Manual Sep 13/2004
06-00-02 CSP 100-6 REV 1
Flight Compartment Printer (Optional) ................................................................................ 06-01-16
Description................................................................................................................. 06-01-16
Components and Operation....................................................................................... 06-01-16
Flight Data Recorder (FDR) (Optional)................................................................................ 06-01-17
Description................................................................................................................. 06-01-17
Components and Operation....................................................................................... 06-01-17
Recorder Unit............................................................................................................. 06-01-17
Underwater Locator Device (ULD)............................................................................. 06-01-17
Tri-Axial Accelerometer.............................................................................................. 06-01-17
EICAS Messages ................................................................................................................ 06-01-18
COMMUNICATIONS
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 06-01-01
INTRODUCTION
The radio communication system (RCS) contains the radios and controls used for communication purposes. It
shares controls with other systems (intercom, audio, passenger address, navigation and FMS).
Two separate systems are provided for the VHF radio communication and they are designed and installed so that the failure
of one system does not preclude the operation of the other system. Both systems are connected to the onside and cross-side
cockpit controls, displays and audio features.
DESCRIPTION
The MFD is the primary radio tuning source for the radio communication system. Frequency, as well as the state of other
control functions, is maintained in memory such that the radio does not change state or frequency due to an interrupt in
power.
The CDU may also be used for tuning and control of VHF radios, either as a convenience in normal operation, or as a primary
control in reversionary operation if the RSP tune switch is selected to CDU ONLY. The CDU provides integrated
control of the combinations of aircraft communications radio subsystems. The CDU provides single point control of both
on-side and cross-side radios from the pilot or copilot position, in both normal and CDU ONLY configurations.
COMPONENTS
The radio communication system in the Challenger 300 consists of the following:
- Two VHF communication transceivers
- Two VHF communication antennas
- HF antenna (optional)
- Two radio integration units
　
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