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PANEL of the centre pedestal. Turning on the floor lights will automatically illuminate the phone
lights.
COCKPIT LIGHTS INTEGRAL/MISC PANEL
GF1610_015
ON
OFF
FLOOR
LIGHTING
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
16−10−12
COCKPIT LIGHTS INTEGRAL/MISC PANEL (CONT'D)
Radio Management Unit (RMU) Display Dimming
The RMU brightness display will appear when the “DIM” function key is selected. Pressing the
“DIM” function key connects the RMU brightness control to the “TUNE” control knob allowing the
display to be adjusted to match overall flight compartment brightness.
TUNE CONTROL KNOB
LIGHT SENSOR
"DIM" FUNCTION KEY
GF1610_016
COM1 NAV1
118.00 112.00
130.27
TEMP−1 TEMP−1
113.10
ATC
1605 620.0
ADF1
STANDBY ANT
TCAS DSPY1 HF1
TUNE TO DIM DISPLAY
ANY KEY TO RETURN
NB
The “TUNE” control knob returns to normal operation when any function or line select key is
selected. Setting display brightness provides the bezel mounted light sensor with the pilot’s
desired reference about which they adjust the brightness for varying lighting conditions.
Flight Management Unit (FMS) Display Lighting
Both the manual and automatic (photo sensor) brightness controls are used to increase or
decrease the display brightness. The brightness knob manually adjusts the brightness. After the
adjustment is made, the photo sensors monitor the ambient light and maintain the brightness level
over various lighting conditions.
BRIGHTNESS
KNOB (MANUAL)
PHOTO SENSOR LIGHT SENSOR
(AUTOMATIC)
GF1610_017
KICT − KORL FPL 1/3
KICT 998/02 + 47 @ 359
ORIGIN DIST/ETE GS
MEM 01 + 06 − − − − −
1045 392NM
VUZ 00 + 29 − − − − −
1155 174NM
PATTERN FPL SEL
LIGHTING
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
16−10−13
COCKPIT LIGHTS INTEGRAL/MISC PANEL (CONT'D)
LASERTRACK Navigation Display Unit (if installed)
The LASERTRACK Navigation Display Unit (NDU) is located on the pilot’s side panel. The display
unit’s lighting control is from the left bright dim control on the COCKPIT LIGHTS INTEGRAL panel.
The bright/dim key is used to control the lighting of the Navigation Display Unit (NDU)
display. When first pressed and held, the display intensity increases until the brightest level is
reached. When pressed and held a second time, the display intensity decreases until the dimmest
level is reached.
The test key is used to initiate a test of all NDU annunciations, cue lights and display.
NOTE
During test the NDU annunciators and cue lights come on
sequentially.
BRIGHTNESS
CONTROL KEY
COCKPIT LIGHTS INTEGRAL PANEL
GF1610_018
INTEGRAL
COCKPIT LIGHTS
DIM BRT
L
DIM BRT
CTR
DIM BRT
R
LIGHTING
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
16−10−14
COCKPIT LIGHTS INTEGRAL/MISC PANEL (CONT'D)
HeadsUp
Guidance Display Lighting
The headsup
guidance system has a brightness control knob located on the glareshield (pilot’s
side), and ambient sensors (overhead HGS) which adjust the brightness for varying lighting
conditions.
AMBIENT LIGHT
GF1610_019
HUD BRIGHTNESS
SENSORS
CONTROL KNOB
MASTER
ROLL SPLRS
PLT CONT
WARNING/CAUTION
OFF
HUD
DIM BRT
ROLL
SEL
PLT
ROLL
WARNING
CAUTION
The brightness rotary knob allows the display to be adjusted manually to match overall flight
compartment brightness. After the adjustment is made, the ambient sensors monitor the ambient
light and maintain the brightness level over various lighting conditions.
LIGHTING
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
16−10−15
LAMP TEST
GF1610_020
LAMP TEST:
(duration approximately 20 seconds
for each test)
Press the LAMP TEST 1 (2) activation
button and note the following:
All Overhead push button
annunciators illuminate.
Glareshield lights illuminate.
Fire handles illuminate.
CTR pedestal panel lights
illuminate.
Oil replenishment system panel
lights illuminate.
TEST CONTROL 1/1
FIRE TEST
STALL TEST
AURAL WARNING TEST 1
AURAL WARNING TEST 2
　
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