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DESCRIPTION General 06−10−1 Audio Integrating System 06−10−1 Description 06−10−1 Components and Operation 06−10−1 Communication Radios 06−10−5 Description 06−10−5 Radio Tuning 06−10−6 Description 06−10−6 CDU Tuning 06−10−6 MFD Tuning 06−10−14 Tune Inhibiting 06−10−17 Cockpit Voice Recorder System 06−10−18 Description 06−10−18 Static Dischargers 06−10−20 Description 06−10−20 EICAS Messages 06−10−21 SUMMARY Power Supply and Circuit Breaker Summary 06−20−1 LIST OF ILLUSTRATIONS DESCRIPTION Figure 06−10−1 Communication System 06−10−1 Figure 06−10−2 Audio Integrating System Components 06−10−3 Figure 06−10−3 Audio Control Panel 06−10−5 Figure 06−10−4 Flight Management System Control Display Units 06−10−7 Figure 06−10−5 CDU TUNE Page 06−10−9 Figure 06−10−6 VHF Radio CONTROL Page 06−10−11 Figure 06−10−7 HF Radio CONTROL Page 06−10−13 Figure 06−10−8 Cursor Control Panel 06−10−14 Figure 06−10−9 MFD Radio Tuning Block 06−10−15 Figure 06−10−10 VHF Comm Submenu Control 06−10−16 COMMUNICATIONS Table of Contents Vol. 2 06−00−1 Oct 05/06 CHAPTER 6 - COMMUNICATIONS 06−00−1 CL−605 Flight Crew Operating Manual PSP 605−6 TABLE OF CONTENTS Page TABLE OF CONTENTS LIST OF ILLUSTRATIONS DESCRIPTION Figure 06−10−11 HF Comm Submenu Control 06−10−17 Figure 06−10−12 TUNE INHIBIT Switch/lights 06−10−18 Figure 06−10−13 Cockpit Voice Recorder 06−10−20 Figure 06−10−14 Static Dischargers Location 06−10−21 COMMUNICATIONS Table of Contents Vol. 2 06−00−2 Oct 05/06 CL−605 Flight Crew Operating Manual PSP 605−6 Page GENERAL The aircraft communication system includes those components and subsystems providing air-to-ground, interphone and cabin communications. The system is also responsible for recording communications and cabin audio. It includes the following: • Audio integrating system; • Communication radios; • Radio tuning system; • Cockpit voice recorder; and • Static dischargers. Communication System Figure 06−10−1 AUDIO INTEGRATING SYSTEM Description The audio integrating system integrates and manages audio from several audio sources, including crew and service interphone, communication radios and navigation receivers. In addition, the system integrates audio signals, tones and messages from the engine indication and crew alerting system (EICAS), and provides a summation of crew communications to the cockpit voice recorder (CVR). Components and Operation The audio integrating system includes the following components: • Audio electronics control unit; • Audio control panels; • Flight compartment speakers; • Microphone and headphone jacks; • Hand-held microphones; • Microphone push-to-talk (PTT) keying switches; and • External ground interphone jacks. COMMUNICATIONS Description Vol. 2 06−10−1 Oct 05/06 CL−605 Flight Crew Operating Manual PSP 605−6 AUDIO INTEGRATING SYSTEM (CONT'D) Audio Electronics Control Unit The audio electronics control unit is responsible for receiving and processing audio and microphone keying input. The unit interfaces with the following: • Boom, hand-held and oxygen mask microphones; • Microphone keying switches; • Ground interphone communication stations; • Communication and navigation radios; • Engine indication and crew alerting system (EICAS); and • Recording systems (voice, flight data). The unit integrates audio from the crew intercom, communication and navigation radios, and receives command input from the audio control panels. In addition, the unit receives microphone keying and audio, and routes it to the associated radio system. The audio is also provided to the voice recorder system for recording. EICAS audio is provided in the form of aural tones, chimes and voice messages. This audio is triggered by the DCUs, processed by the audio electronics control unit, and played through the www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：庞巴迪挑战者605机组操作手册 CL605-COMMUNICATIONS
