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Components and Operation 06−10−5
Controls and Indicators 06−10−7
HF Communication System 06−10−7
Description 06−10−7
Components and Operation 06−10−7
Controls and Indicators 06−10−8
Radio Tuning System 06−10−10
Description 06−10−10
Components and Operation 06−10−10
Controls and Indicators 06−10−10
Operation 06−10−12
Cockpit Voice Recorder System 06−10−18
Description 06−10−18
Controls and Indicators 06−10−20
Operation 06−10−20
Flight Data Recorder System 06−10−21
Description 06−10−21
Components and Operation 06−10−21
Controls and Indicators 06−10−23
Static Dischargers 06−10−23
Description 06−10−23
EICAS Messages 06−10−24
SUMMARY
Power Supply and Circuit Breaker Summary 06−20−1
COMMUNICATIONS
Table of Contents
Vol. 2 06−00−1
REV 66, Feb 01/07
CHAPTER 6 - COMMUNICATIONS
06−00−1
CL−604 Operating Manual
PSP 604−6
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 06−10−1 Audio Integrating System Components 06−10−3
Figure 06−10−2 Audio Control Panel 06−10−4
Figure 06−10−3 VHF Communication System − Block Diagram 06−10−6
Figure 06−10−4 HF Communication System − Block Diagram 06−10−9
Figure 06−10−5 Radio Tuning Unit 06−10−11
Figure 06−10−6 Reversionary/Inhibit Panel 06−10−12
Figure 06−10−7 COM/NAV Selections 06−10−13
Figure 06−10−8 COM 3 Selections 06−10−14
Figure 06−10−9 ADF, ATC and TCAS Selections 06−10−15
Figure 06−10−10 HF Selections 06−10−16
Figure 06−10−11 RTU and COM/NAV Failure Indications 06−10−17
Figure 06−10−12 RTU TEMP Annunciation 06−10−18
Figure 06−10−13 CVR System 06−10−19
Figure 06−10−14 Cockpit Voice Recorder Panel 06−10−20
Figure 06−10−15 Flight Data Recorder System 06−10−22
Figure 06−10−16 Static Dischargers Location 06−10−23
COMMUNICATIONS
Table of Contents
Vol. 2 06−00−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
Page
GENERAL
Communication is a function of the Challenger 604 fully integrated avionics system and includes the
following:
• Audio integrating system
• VHF communication system
• HF communication system
• Radio tuning system
• Cockpit voice recorder (CVR) system
• Flight data recorder (FDR) system
• Static dischargers
AUDIO INTEGRATING SYSTEM
Description
The audio integrating system provides an interface between crew microphones, speakers,
headphones, and the aircraft’s radio, warning and recording systems. The audio integrating
system also provides an interface between any or all flight crew and ground crew stations.
Components and Operation
The audio integrating system consists of the following components:
• Two flight crew jack panels
• Three ground crew interphone units (jacks)
• Two speakers
• Two audio control panels
Flight Crew Jack Panels
Two flight crew jack panels (pilot and copilot) are located in the flight compartment.
Ground Crew Interphone-Jack Units
The three ground crew interphone-jack units are installed in the following locations:
• Nosewheel well
• Main avionics bay
• Aft equipment compartment
Each assembly is a metal-case sealed unit which has one microphone jack and one headphone
jack. The microphone jacks in the nosewheel well and aft compartment are deactivated in flight
by the WOW switch.
Speakers
Two independent speakers are mounted in the roof of the flight compartment for the pilot’s and
copilot’s audio systems. The speakers allow audio monitoring without the use of headphones.
COMMUNICATIONS
Description
Vol. 2 06−10−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
AUDIO INTEGRATING SYSTEM (CONT'D)
Controls and Indicators
The audio control panels provide controls for selecting and controlling receiver audio from the
　
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