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- Zone 4 - Circuit breaker panels A brief explanation of the panels, locations, and the zones they control follows:
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
16-01-01
LIGHTING
FLIGHT COMPARTMENT LIGHTING (Cont)
ZONE 3
ZONE 1 GLARESHIELD +
GLARESHIELD + RIGHT SIDE
LEFT SIDE
ZONE 2
PEDESTAL
DIMMER DIMMER
ZONE 1 ZONE 3
COCKPIT LIGHTS GSHLD/L SIDE PEDESTAL DIMMER WING INSP NAV STROBE LIGHTING SMKG/ BELTS B COCKPIT LIGHTS GSHLD/R SIDE DOME
ZONE 2 B C N E L T
S
DIM BRT DIM BRT OFF EMER LTS OFF OFF LANDING OFF DIM BRT DIM BRT
BRT DIM ANNUN PFD MFD ON A R M L N LDG/TAXI T A X I R MFD PFD CB PANELS
OFF OFF OFF OFF
DIM BRT DIM BRT DIM BRT
DIMMER
ZONE 4
ZONE 4
CB PANELS
CFO1601002_012
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
16-01-02 FLIGHT COMPARTMENT LIGHTING (Cont) LEFT COCKPIT LIGHTS PANEL
The left COCKPIT LIGHTS panel is powered by 28 vdc.
A description of each of the potentiometer controls located on the left COCKPIT LIGHTS panel is as follows:
CFO1601002_005
GSHLD/L SIDE
Dimming the fluorescent light beneath the left side of the glareshield is controlled via this potentiometer.
PEDESTAL
This potentiometer controls the lighting intensity of equipment installed in the pedestal. The FMS display intensity is reg-ulated by the dim button on the FMS control panel.
ANNUN
This push button switch controls the brightness of the other switches from DIM to BRT as well as off.
PFD/MFD
Display units have internal lighting, and the intensity is controlled through the PFD/MFD potentiometer.
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
16-01-03 FLIGHT COMPARTMENT LIGHTING (Cont) RIGHT COCKPIT LIGHTS PANEL
The right COCKPIT LIGHTS panel is powered by 28 vdc.
Following is a description of each of the potentiometer controls located on the right COCKPIT LIGHTS panel.
CFO1601002_010
DOME
The center overhead dome light is controlled by the DOME potentiometer. The pilot dome light can also be turned on with the COCKPIT light switch on the main entryway control panel when the cabin door is open and the DOME control is off. When the cabin door is closed, cockpit overhead light control from the main entryway control panel is disabled. The dome light is powered by the right main bus and is protected by the DOME circuit breaker within the CABIN group on the copilot circuit breaker panel. When the pilot dome light is controlled via the main entryway switch, it receives power from the airplane hot bus system.
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