FLIGHT INSTRUMENTS
May 06/2005 Flight Crew Operating Manual Volume 2
REV 2 CSP 100-6 11-01-01
REV 2
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 compressed
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 performing
the integration function required to connect the various aircraft systems, the IAPS contains flight guidance computer,
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.
CFO1101002_006
FGP
CDU 1
MFD CONTROL
RSP
CDU 2
(OPTION)
LEFT MFD RIGHT MFD RIGHT PFD
LEFT PFD
CO-PILOT
PILOT DCP
DCP
PILOT CO-PILOT
FLIGHT INSTRUMENTS
Volume 2 Flight Crew Operating Manual Sep 13/2004
11-01-02 CSP 100-6 REV 1
INTRODUCTION (Cont)
LIGHTNING DETECTION
SYSTEM (OPTION)
TERRAIN AWARENESS
AND WARNING SYSTEM
FLIGHT DECK
CONTROLS
FLUX DETECTOR
UNIT
ATTITUDE/HEADING
SYSTEM
RADIO INTEGRATION
UNIT
AUDIO CONTROL
PANEL
CONTROL PANEL
ELECTRONICS
VHF
ISI STANDBY
NAV
DME
VHF3/DATALINK
(OPTION)
TDR
GPS
HF COUPLER
(OPTION)
HF COM
(OPTION)
HF DATALINK
(OPTION)
PRINTER (OPTION)
CONTROL
DISPLAY
UNIT
AIR
DATA
SYSTEM
FLIGHT DECK
CONTROLS
CONTROL DISPLAY
UNIT (OPTION)
AIR DATA
SYSTEM
ATTITUDE/HEADING
SYSTEM
RADIO INTEGRATION
UNIT
CONTROL PANEL
ELECTRONICS
AUDIO CONTROL
PANEL
NAV
(OPTION ADF)
VHF
TDR
DME
(OPTION)
GPS
(OPTION)
HF COM
(OPTION)
HF COUPLER
(OPTION)
REVERSION
SWITCH PANEL
DISPLAY
CONTROL
PANEL
CURSOR
CONTROL
PANEL
WEATHER
RADAR
FLIGHT
GUIDANCE
PANEL
PORTABLE
MAINTENANCE
ACCESS TERMINAL
DBU
(OPTION)
YAW
SERVO
PITCH
SERVO
ROLL
SERVO
STALL PROTECTION SYSTEM
HORIZONTAL STABILIZER
TRIM SYSTEM
CVR CVR
CONTOL UNIT
FDR
(OPTION)
LAMP
DRIVER
UNIT
DATA
CONCENTRATOR
UNIT
REMOTE DATA
CONCENTRATOR
AIRCRAFT INTERFACE
FIRE DETECTION
APU
ELECTRICAL
ELT (OPTIONAL)
CLOCK
FUEL
AIR CONDITIONING
A-ICE
BLEED-LEAK
CABIN PRESS
SPOILER
BRAKES
NOSE WHEEL STEER
HYDRAULICS
PROXIMITY SENSING
FLIGHT CONTROLS
DISPLAY
CONTROL
PANEL
ADAPTIVE FLIGHT
DISPLAYS
RH
PWR
IOC
FCS
(FMS)
MAINT
LH
PWR
IOC
FCS
FMS
( ) OPTION
STICK SHAKER
STICK PUSHER
RADIO
ALTIMETER
TRAFFIC ALERT
COLLISION
AVOIDANCE
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