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DESCRIPTION General 06−10−1 Interphone Communication 06−10−1 Flight Compartment Speakers 06−10−1 Flight Crew Intercom 06−10−1 Service Intercom Panels 06−10−2 Forward External Services Panel Interphone Station 06−10−2 Aft External Services Panel Interphone Station 06−10−3 Aft Equipment Bay Interphone Station 06−10−3 Avionics Bay Interphone Station 06−10−3 Radio Transmit Switch 06−10−4 Audio Control Panel 06−10−4 Audio Control Panel Input Schematic 06−10−4 Audio Control Panel Switch Operation 06−10−5 Transmit/Emer 06−10−5 Microphone Selection 06−10−5 Speaker/Headphone 06−10−5 Radio Communication System 06−10−6 VHF 1 and 2 Communications Systems 06−10−6 VHF 3 Communications System 06−10−6 Integrated Radio System 06−10−7 Integrated Radio System Schematic 06−10−7 Radio Management Unit (RMU) Display 06−10−8 Radio Management System 06−10−9 General Colour Philosophy 06−10−10 Transfer Keys 06−10−11 Line Select Keys 06−10−11 Function Keys and Tuning Knobs 06−10−11 Function Keys 06−10−12 Direct COM Tuning 06−10−18 COM Memory 06−10−19 High Frequency (HF) Communication System 06−10−21 RMU HF Display 06−10−21 HF Preset and Direct Tuning Modes 06−10−22 HF Fault Annunciation 06−10−22 Menu Page 06−10−23 HF Memory and Control Pages 06−10−24 COMMUNICATIONS TABLE OF CONTENTS CHAPTER 6 06−00−1 Rev 3, Apr 25, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 06−00−1 Page TABLE OF CONTENTS DESCRIPTION SELCAL 06−10−25 Operation 06−10−25 Radio Altimeter 06−10−26 Static Discharger 06−10−27 Cockpit Voice Recorder 06−10−28 CVR Location 06−10−28 Microphone Monitor Control Panel 06−10−28 Remote Area Microphone 06−10−29 Impact Switch 06−10−29 Audio Control Panel Input 06−10−29 CVR System Schematic 06−10−30 Microphone Monitor Control Panel Test 06−10−31 Flight Data Recorder 06−10−32 Quick Access Recorder (If Installed) 06−10−32 Underwater Locator Beacon 06−10−33 Emergency Locator Transmitter 06−10−33 Light Sensor − ELT Panel 06−10−33 ELT Schematic 06−10−34 Airborne Data Link System 06−10−35 Communication Links 06−10−35 Data Link Features 06−10−35 SATCOM 06−10−36 Satellite Data Unit (SDU) 06−10−36 Radio Frequency Unit (RFU) 06−10−36 High Power Amplifier (HPA) 06−10−36 High Gain Antenna/Antenna Control Unit 06−10−37 Communication Link Schematic 06−10−37 Cabin Communication System 06−10−38 Flight Compartment Printer 06−10−39 EICAS Messages 06−10−41 EMS CIRCUIT PROTECTION CB − Comm System 06−20−1 COMMUNICATIONS TABLE OF CONTENTS Flight Crew Operating Manual Rev 12, Aug 14, 2006 CSP 700−5000−6 Volume 2 06−00−2 Page GENERAL The intercom system, VHF and HF communications transceivers, selective calling (SELCAL), comprise the basic communications system. All communication and navigation radios are tuned through the Radio Management Unit (RMU) installed in the centre pedestal. The RMU controls the TCAS modes and provides direct tuning of the NAV, COM, ADF, TCAS, ATC and HF radios. RMU color LCD can display several pages of radio system data including channels, frequencies, codes, backup engine data, strap options, maintenance data log and software versions. A cockpit voice recorder (CVR) is installed in the flight compartment, on the copilot’s side console. All incoming, outgoing and internal communications are recorded on the cockpit voice recorder. Radio frequency interference is reduced through a series of electrostatic dischargers and through an equipment bonding/grounding system. Audio control panels (centre pedestal) and the optional (completion centre installation) function as the interface to the remote NAV and COM units. www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier_Global_000-Communications
