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Sept 04
P I LOT T R A I N I N G GU I D E
LIGHTING
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.
COMPARE FUEL QUANTITY
0DEPARTURE T.O.INIT0
000ACTIVE FLT PLAN 1/4
0BOW PASS/@ LB0
0/170
0055°00154NM
15820 (00+21
K00P0H0X0001152Z
SJN
0059°00121NM
15820 (00+15 .75M/10000A
CLS
ABQ
0ORIGIN
.75M/10000A
CLS
GX_15_018
Photo Sensor
(automatic)
Photo Sensor
(automatic)
Brightness
button (manual)
For Training Purposes Only
Sept 04
15-17
P I LOT T R A I N I N G GU I D E
LIGHTING
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 - BRT 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 - TST 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.
SYSTEM SELECT FAULT
ON
FROM TO WPT
WPT
LEG
CHG
XTK
DTK
WD
WS
DIS
TIM
HDG
STS
POS
TK
GS
1
M
2 T
BRT
3 DIM
TST
ENT
BCK
0 CLR
7 S
8
9
W
4
5
E
6
1
N
2
3
88888
8 8
8 8888888
GX_15_019
COCKPIT LIGHTS
L
DIM BRT DIM BRT
IM BR DIM BRT
INTEGRAL
CTR R
Brightness
Control Key
COCKPIT LIGHTS INTEGRAL PANEL
15-18 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
LIGHTING
HEADS-UP GUIDANCE DISPLAY LIGHTING
The heads-up guidance system has a brightness control knob 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.
Ambient Light
Sensors
ROLL SPLRS
PLT CONT
ROLL
SEL
PLT
ROLL
DIM
OFF
BRT
HUD
HGS Brightness Control Knob
GX_15_020
For Training Purposes Only
Sept 04
15-19
P I LOT T R A I N I N G GU I D E
LIGHTING
LAMP TEST
GX_15_021
LAMP TEST:
(duration approximately 20 seconds)
Press the LAMP TEST 1 (2) activation
button and note the following:
• All overhead pushbutton annunciators
illuminate.
• Glareshield lights illuminate.
• Pedestal panel lights illuminate.
M
TEST CONTROL 1/2
FIRE TEST
STALL TEST
AURAL WARNING TEST 1
AURAL WARNING TEST 2
LAMP TEST 2
LAMP TEST 1
OFF
OFF
OFF
OFF
OFF
TEST
M
TEST CONTROL 1/2
FIRE TEST
STALL TEST
AURAL WARNING TEST 1
AURAL WARNING TEST 2
LAMP TEST 1
LAMP TEST 2
OFF
OFF
OFF
OFF
OFF
OFF
M
TEST CONTROL 1/2
FIRE TEST
STALL TEST
AURAL WARNING TEST 1
AURAL WARNING TEST 2
LAMP TEST 1
LAMP TEST 2
OFF
OFF
OFF
OFF
OFF
TEST
M
TEST CONTROL 1/2
FIRE TEST
STALL TEST
AURAL WARNING TEST 1
AURAL WARNING TEST 2
LAMP TEST 1
LAMP TEST 2
OFF
OFF
OFF
OFF
OFF
OFF
15-20 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
LIGHTING
PASSENGER SIGNS/EMERGENCY LIGHTS PANEL
The PASS SIGNS switches for the no smoking and seat belts are located on the PASS
SIGNS/EMER LTS panel.
PASSENGER SIGNS
The NO SMKG and SEAT BLTS control switches are located on the overhead panel in
　
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