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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.
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
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.
PHOTO SENSOR
PHOTO SENSOR (AUTOMATIC)
(AUTOMATIC)
BRIGHTNESS KNOB (MANUAL)
GF1610_017a
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
LASERTRACK IV Navigation Display Unit
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.
GF1610_018
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
Heads-Up Guidance Display Lighting
The heads-up 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.
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.
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
Enhanced Vision System (EVS) IF INSTALLED)
The EVS has a brightness control knob located on the glareshield (pilot’s side). For more information, refer to chapter 11 Flight Instruments.
HUD BRT Knob
GF1610_053
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
LIGHTING
LAMP TEST
TEST CONTROL 1/1
FIRE TEST OFF
STALL TEST OFF
AURAL WARNING TEST 1 OFF
AURAL WARNING TEST 2 LAMP TEST 2 LAMP TEST 1 OFF OFF TEST
M
After 20 seconds
TEST CONTROL 1/1
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