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Multi-Function/Primary Flight Display Visual Annunciations ............................................... 11-01-37
EICAS Messages ................................................................................................................ 11-01-38
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
11-00-03
INTRODUCTION
The Challenger 300 is equipped with an electronic flight instrumentation system (EFIS). The EFIS consists of four adaptive flight displays (AFD), grouped as a left primary flight display (PFD) and multifunction display (MFD) and a right MFD and right PFD. The control portion of the system is made up of two display control panels (DCP), one MFD control panel, and one reversion switch panel (RSP). A DCP on the pilot and copilot side provides configuration and selection controls for the appropriate PFD, as well as radio controls for the MFD. The reversion panel provides the means for selecting a com-pressed PFD format on either AFD, as well as selecting reversion to cross-side attitude/heading data, air data, and radio tune control.
The adaptive flight displays provide airspeed, altitude, attitude, heading, navigation, and system information. Each pilot is presented with this information on a primary flight display (PFD) and a multifunction display (MFD).
A major interface with the EFIS is the integrated avionics processor system (IAPS), data concentrator units (DCU) and the remote data concentrators (RDC). The IAPS is the focal point of information flow for the entire aircraft. In addition to per-forming the integration function required to connect the various aircraft systems, the IAPS contains flight guidance com-puter, flight management computer (FMC), and maintenance diagnostic computer (MDC) modules. Other systems provide information to the EFIS for display as conventional flight instruments. This includes the air data system and the attitude and heading reference system.
Control for the EFIS display modes are provided by switches and push buttons located on the glareshield, the center console and the side instrument panels.
CO-PILOT
PILOT FGP DCP
DCP
PILOT
CO-PILOT
LEFT PFD LEFT MFD RIGHT MFD RIGHT PFD
CDU 2 CDU 1
(OPTION)
RSP
MFD CONTROL
CFO1101002_006
May 06/2005 Flight Crew Operating Manual Volume 2 REV 2 CSP 100-6
11-01-01
FLIGHT INSTRUMENTS
INTRODUCTION (Cont)
UNIT
SYSTEM
UNIT
UNIT
PANEL
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
11-01-02 PRIMARY FLIGHT DISPLAYS DESCRIPTION
The primary flight displays (PFD) are integrated displays of attitude, air data, and navigation information. The PFD is divided into the following main areas:
-Attitude display -Airspeed/Mach display -Altitude display -Vertical speed display -AFCS mode display -Navigation display
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本文链接地址：庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-飞行仪表(6)
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