Bombardier Global Express - Lighting
INTRODUCTION
The airplane is equipped with a suite of lighting systems covering the direct and
indirect illumination of the flight compartment and airplane exterior.
The general airplane lighting includes:
•
•
•
•
•
Flight Compartment Lighting - Internal lighting is used in the flight compartment
for flight instrumentation and general lighting
Passenger Compartment Lighting - Lighting systems for the passenger cabin are
not provided, except for the main entrance
External Lighting - External lighting in the form of landing, taxi and airplane
identification are used
Service and Maintenance Lighting - Lighting is available to service areas to assist
maintenance personnel, in their airplane checks and inspections
Emergency Lighting - Lighting is provided to permit airplane occupants to safely
move away from the airplane in an emergency situation
DESCRIPTION
FLIGHT COMPARTMENT LIGHTING
Controls for the flight compartment are located on two panels on the center pedestal.
One panel controls the flight compartment flood and display lighting, while the other
controls the integral and miscellaneous lighting.
There are two types of integral lighting in the flight compartment; electroluminescent
(EL) lighting and incandescent lighting. All instrument panels are provided with
integral legend/edge lighting. The instrument panels are grouped in an area, with each
one having its dedicated dimming control.
The electrical power to the integral lighting system is through an ON/OFF or AUTO
mode selection of a MASTER switch. When in AUTO mode, to increase the life of the
lighting elements (example: daylight or high cockpit light conditions) the system will
be turned on or off automatically. This is accomplished through a light sensor circuit,
which is dependent upon the ambient lighting conditions in the flight compartment.
CRT display, fluorescent flood, integral instrument and instrument panel lights provide
instrument lighting. The EMS CDU provides two LAMP TEST positions in order to
test the indicator lights, through the electrical management system.
Page 1
Bombardier Global Express - Lighting
The flight compartment lighting includes the following:
•
•
•
•
•
•
•
Flight compartment flood lights
Flight compartment floor lights
Flight compartment area lights
Map lights
Flight compartment panels integral lighting
Flight compartment flashlights
Orientation light
Page 2
Bombardier Global Express - Lighting
FLIGHT COMPARTMENT INTEGRAL LIGHTING AREAS
AREA 1
AREA 5
AREA 5
AREA 4
GX_15_001
AREA 3
AREA 2
AREA 1
OVERHEAD PANEL - Electroluminescent lighting or EL
AREA 2
CENTER INSTRUMENT PANEL AND PEDESTAL - Mixed lighting; half EL lighting and half
incandescent
AREA 3
LEFT SIDE CONSOLE (Pilot) - Incandescent lighting
AREA 4
RIGHT SIDE CONSOLE (Copilot) - Incandescent lighting
AREA 5
CIRCUIT BREAKER/MISCELLANEOUS PANELS - Electroluminescent Lighting (EL)
Page 3
Bombardier Global Express - Lighting
FLIGHT COMPARTMENT LIGHTING PANELS
EXTERNAL LIGHTS
NAV
BEACON
L WING
STROBE
WHT
OFF
O
ON
OFF
ON
O
LANDING
PULSE
OFF
S
STEADY
NLG
WING INSP
OFF
O
ON
PULSE
OFF
S
STEADY
R WING
LOGO
OFF
O
ON
OFF
O
ON
TAXI/RECOG
WINGTIP
PULSE
OFF
S
STEADY
WINGTIP
OFF
O
ON
EXTERNAL LIGHTING
PASS SIGNS
NO SMKG
ON
OFF
A
AUTO
ELT
ON
FOR AVIATION
EMER USE ONLY
UNAUTHORIZED OPERATION PROHIBITED
EMER LIGHTS
SEAT BLTS
ON
OFF
ARM
A
ON
OFF
A
AUTO
PASSENGER SIGNS/EMERGENCY LIGHTS
A
ARM/
RESET
R
LIGHT SENSOR - ELT (Optional)
COCKPIT LIGHTS
INTEGRAL
DIM
M
COCKPIT LIGHTS
FLOOD
L
CB
BRT
BR
L
BRT
OFF
CTR
BRT
OFF
R
PBA
BRT
L
BRT
DIM
CTR
BRT
DIM
R
MASTER
DIM
M
R
OVHD
BRT
DIM
OFF
O
ON
OFF
O
EYE REF
DIM
M
AREA
BRT
BR
BRT
BR
ON
OFF
O
FLOOR
COCKPIT LIGHTS INTEGRAL/MISC.
DISPLAY
DIM
BRT
BR
CTR
ON
AUTO
OFF
O
BRT
BR
DIM
BRT
B
OFF
DIM
M
BRT
COCKPIT LIGHTS/FLOOD DISPLAY
Page 4
GX_15_002
DIM
M
Bombardier Global Express - Lighting
INTEGRAL LIGHTING
There are two types of integral lighting in the flight compartment: electroluminescent
lighting consisting of an assembly layered within the panel and powered by AC, and
incandescent lighting which is a bulb type lighting and can be AC- or DC-powered.
The integral lighting is divided into five control areas as described in the previous
illustration. A sensor is provided on the LIGHT SENSOR/ELT Panel in the flight
compartment, to turn the integral lighting system on/off for day/night time lighting
requirements.
Light Sensor
ELT
FOR AVIATION
EMER USE ONLY
GX_15_003
ON
A
ARM/
RESET
R
UNAUTHORIZED OPERATION PROHIBITED
LIGHT SENSOR - ELT (Optional) Panel
COCKPIT LIGHTS FLOOD/DISPLAY PANEL
All flood/display lighting is controlled by switches located on the COCKPIT LIGHTS
FLOOD/DISPLAY control panel in the center pedestal. The panel includes rotary
knobs for the following areas:
•
•
•
Pilot instrument flood light and display lights
Copilot instrument flood light and display lights, and
Center instrument flood lights and display panels
CTR FLOOD Control
OFF/BRT – Controls the OFF
selection and intensity (BRT) of the
center instrument panel flood light.
L FLOOD Control
OFF/BRT – Controls the OFF
selection and intensity (BRT)
of the left hand instrument
panel flood light on the pilot
side panel.
R FLOOD Control
OFF/BRT – Controls the OFF
selection and intensity (BRT) of the
right hand instrument panel flood
light on the copilot side panel.
COCKPIT LIGHTS
FLOOD
OFF
L
BRT
OFF
CTR
BRT
OFF
BRT
DIM
R
BRT
DIM
L DISPLAY Control
DIM/BRT – Controls the intensity
of the pilot instrument (primary
flight and multifunctional) displays.
L
BRT
DIM
CTR
CTR DISPLAY Control
DIM/BRT – Controls the intensity
of the center instrument (EICAS
and system) displays.
Page 5
R
BRT
GX_15_004
DISPLAY
R DISPLAY Control
DIM/BRT – Controls the intensity
of the copilot instrument (primary
flight and multifunctional) displays.
Bombardier Global Express - Lighting
FLIGHT COMPARTMENT FLOOD LIGHTS
Flood lights are installed at both crew stations for general illumination of the
instruments.
The flight compartment flood lights comprise: three LH and three RH side console
instrument panel lights, and four center instrument panel lights.
Dimming and off control of the lights is provided to the left, right and center areas of
the flight compartment, using a single OFF/BRT rotary control knob for each area.
The rotary control knobs are located on the COCKPIT LIGHTS FLOOD/DISPLAY
control panel in the center pedestal. Variable controls enable the lights to change
intensity gradually from off to full bright.
DISPLAY LIGHTING
Display lighting is provided for illumination of the pilot, copilot and center instrument
panels. The L and R DISPLAY knobs control the Electrical Management System/
Control Display Units (EMS/CDU), Primary Flight Displays (PFDs) and the
Multifunctional Displays (MFDs) for the pilot and copilot respectively.
Right Side
Console Control
COCKPIT LIGHTS
OFF
L
BRT
OFF
CTR
BRT
OFF
R
BRT
GX_15_005
FLOOD
COCKPIT LIGHTS FLOOD
The CTR DISPLAY controls the EICAS primary display and the system display. This
illumination is provided with a single switch DIM/BRT control. The left, right and
center areas of the flight compartment have dimming control. These three rotary
control knobs are located on the COCKPIT LIGHTS FLOOD/DISPLAY control panel
in the center pedestal.
Page 6
Bombardier Global Express - Lighting
COCKPIT LIGHTS FLOOD/DISPLAY SCHEMATIC
FLOOD LIGHTS
COCKPIT LIGHTS
FLOOD
OFF
BRT
CTR
OFF
BRT
R
MASTER
WARNING/CAUTION
MASTER
WARNING/CAUTION
WARNING
WARNING
CAUTION
CAUTION
ROLL SPLRS
ROLL
SEL
PLT
ROLL
ROLL
SEL
CPLT
ROLL
PLT CONT
CPLT CONT
33
10
LE
- 04
FMS1
LOC1
N
3
2
ET
00 : 10
0 . 05L
TOC
WX
4000
KKLM
FL180
LX
-56
TAT
-40
TAS
234
GSPD
345
TERR
INHIB
2
DN
DN
OIL
11.5
DN
10 0
IN
I
G
N
61.4
690
75
51
8
0
START
N2
FF (PPH)
OIL TEMP
OIL PRESS
61.4
690 NU
80
49
25750
TOTAL FUEL (LBS)
0
0
9
I
G
N
ITT
START
12950
3
443
12800
mb/hPa
10 1 3
– TRIMS –
AIL
0
FEE
T
1
4
1 3 000
IN HG
4
100
03
06
ET
00 : 10
KDEF
KGHJ
4000
4000
KKLM
FL180
RWD
IAS
SAT
-56
TAT
-40
TAS
234
GSPD
345
TERR
INHIB
KNOTS
10500
VSE (SLATS OUT, 0°FLAPS) . . . . . . . . . . . . 225
VFE (SLATS OUT, 6°FLAPS) . . . . . . . . . . . . 210
VFE (SLATS OUT, 16°FLAPS) . . . . . . . . . . . 210
VFE (SLATS OUT, 30°FLAPS) . . . . . . . . . . . 185
VA (MANEUVERING)
(AT SEA LEVEL @ 96,000 LB) . . . . . . . . . . . 254
(AT 20,000 FT @ 78,600 LB) . . . . . . . . . . . . . 250
STATIC GROUND OPERATION
PROHIBITED BETWEEN 66-80% N1
DISPLAY
DIM
L
BRT
DIM
CTR
BRT
DIM
DISPLAY LIGHTS
Page 7
R
BRT
ALT
20
10 RAD 10
2
20
300
M
20
LOC
150
EICAS
HDGT HDG2
DTK
360
VOR 1
ADF 2
10000
80
FMS1
LOC1
9500
29.92
HDG
N
33
3
3
2
1
0
1
2
3
AIRSPEED LIMITS - (INDICATING SPEEDS)
VMO (BELOW 8,000 FT) . . . . . . . . . . . . . . 300
VMO (8,000FT TO 30,267 FT) . . . . . . . . . . 340
MMO 30,267FT TO 35,000 FT) . . . . . . . . . .0.89
MMO (AT 41,000 FT) . . . . . . . . . . . . . . . . . 0.88
MMO (AT 47,000 FT) . . . . . . . . . . . . . . . . 0.858
MMO (AT 51,000 FT) . . . . . . . . . . . . . . . . 0.842
VLO (EXT) (L/G EXTENSION) . . . . . . . . . 200
VLO (RET) (L/G RETREACTION) . . . . . . 200
VLE (L/G EXTENDED) . . . . . . . . . . . . . . . 250
10400
G
S
0.450M
HDG
330
NL RUDDER NR
AIRSPEED LIMITS - (INDICATING SPEEDS)
VSE (SLATS OUT, 0°FLAPS) . . . . . . . . . . . . 225
VFE (SLATS OUT, 6°FLAPS) . . . . . . . . . . . . 210
VFE (SLATS OUT, 16°FLAPS) . . . . . . . . . . . 210
VFE (SLATS OUT, 30°FLAPS) . . . . . . . . . . . 185
VA (MANEUVERING)
(AT SEA LEVEL @ 96,000 LB) . . . . . . . . . . . 254
(AT 20,000 FT @ 78,600 LB) . . . . . . . . . . . . . 250
0 . 05L
TOC
WX
03
250
9500
VTA
10
LE
160
FL
BELOW
TCAS TEST
12 . 5NM
KDVT
ETE 1+36
ATT 2
ADC 3
20
10
F3
+ 12
5
AP1 ASEL
VNAV
20
ATT
170
- 02
5
650
03
1906
185
1804
+ 09
NO BEARING
RA 9 . 8NM +13
TA 4 . 5NM -04
HDG
VAPP
AT1
F1
200
- 02
LUF
KGHJ
- 04
QTY (QTS)
ENG 11.5
APU
5.2
RES
6.0
EGT
210
IAS
3
BRAKE TEMP
29 9 2
5
TOC
LX
6.0
LWD
ND
STAB
RPM
3
ALT
6
180 200 220
KABC
KKLM
KDEF
2
APU DOOR 11.2°
2
2
7
1
220
33
0
THRUST
FMS1
360
N
2
0
13 %
Honeywell
MAG2
HDG
315
12
12
1
SAT
443
1300
0.00
0
0
E
KGHJ
4000
1
13 %
GEAR
FL
BELOW
TCAS TEST
12 . 5NM
KDVT
ETE 1+36
CAB ALT
P
CAB RATE
LDG ELEV
6
E
KDEF
0
20
OUTFLOW VALVES
1
2
OPEN
OPEN
30
N1
5
NO BEARING
RA 9 . 8NM +13
TA 4 . 5NM -04
1
24
98.5
25.4
+ 09
6
15
S
21
VOR 1
ADF 2
9500
29.92
3
30
33
98.5
25.4
+ 12
5
LOC
22
20
90 %
10
20
- 02
M
20
HDG
W
DTK
360
300
KGHJ
OXYGEN
VMO (BELOW 8,000 FT) . . . . . . . . . . . . . . 300
VMO (8,000FT TO 30,267 FT) . . . . . . . . . . 340
MMO 30,267FT TO 35,000 FT) . . . . . . . . . .0.89
MMO (AT 41,000 FT) . . . . . . . . . . . . . . . . . 0.88
MMO (AT 47,000 FT) . . . . . . . . . . . . . . . . 0.858
MMO (AT 51,000 FT) . . . . . . . . . . . . . . . . 0.842
VLO (EXT) (L/G EXTENSION) . . . . . . . . . 200
VLO (RET) (L/G RETREACTION) . . . . . . 200
VLE (L/G EXTENDED) . . . . . . . . . . . . . . . 250
GX_15_006
20
EICAS
HDGT HDG2
- 02
LUF
AFT
CABIN (°C)
22
19
10
3
FWD
CABIN (°C)
20
20
6
2
150
TOC
Honeywell
CKPT (°C)
30
1.02
T/O
EPR
KDEF
10 RAD 10
0.450M
KKLM
6
160
KABC
20
10000
80
G
S
F3
Honeywell
NO TAKEOFF
1 . 64 PARK/EMER BRAKE ON
END
1 . 64
1.02
N
30
10
FMS1
360
W
Honeywell
MAG2
HDG
315
ALT
ATT
170
HDG
330
10400
24
9500
VTA
RO
ATT 2
ADC 3
20
10500
200
1906
185
1804
AP1 ASEL
VNAV
20
BA
HDG
VAPP
AT1
F1
30
210
IAS
30
Honeywell
THRUST
220
21
Honeywell
S
BRT
15
OFF
OFF
ROLL SPLRS
HUD
DIM
BRT
L
Bombardier Global Express - Lighting
COCKPIT LIGHTS INTEGRAL/MISC PANEL
The integral instrument and miscellaneous panel lighting is controlled by rotary
control knobs and switches located on the COCKPIT LIGHTS INTEGRAL/MISC
control panel in the center pedestal. The panel includes control for the following areas:
•
•
•
•
Pilot side panel and console
Copilot side panel and console
Circuit breaker panel, overhead panel, pushbutton annunciators, eye reference
lights, flight compartment area and floor lighting
Automatic adjustment of integral lighting (MASTER switch)
CTR Control
DIM/BRT – Controls the intensity
of the lights on the glareshield,
standby instrument panel and
center pedestal.
L Control
DIM/BRT – Controls
the intensity of the
lights on the pilot
side panel and side
console.
R Control
DIM/BRT – Controls
the intensity of the
lights on the copilot
side panel and side
console.
COCKPIT LIGHTS
INTEGRAL
DIM
M
DIM
M
L
CB
BRT
BR
PBA Switch
DIM/BRT – Controls the
intensity of all cockpit
pushbuttons.
EYE REF Switch
ON – Illuminates the eye
reference indicator.
OFF – Turns off the eye
reference indicator.
BRT
BR
CTR
DIM
M
ON
AUTO
OFF
O
BRT
BR
DIM
BRT
B
PBA
DIM
M
DIM
M
MASTER
AREA
MASTER Switch
ON position – Activates the
integral lighting.
OFF position – Extinguishes
all integral lighting.
AUTO position – will automatically extinguish all integral
lighting when there is
sufficient lighting. It will also
turn the system on if the light
sensor detects insufficient
lighting.
Page 8
OVHD
BRT
DIM
OFF
O
ON
OFF
O
EYE REF
R
BRT
BR
OVHD Control
DIM/BRT – Controls
the intensity of the
lights on the over
head panel.
BRT
BR
ON
OFF
O
GX_15_007
CB Switch
DIM/BRT – Controls
the intensity of the
lights on the circuit
breaker panel.
FLOOR
FLOOR Switch
ON/OFF – Illuminates
the area between the
rudder pedals and the
seat of each pilot (and
phone lights, if installed).
AREA Switch
BRT/DIM – Controls the
intensity of general
illumination of the flight
compartment.
OFF – Turns off the
area lighting of the flight
compartment.
Bombardier Global Express - Lighting
GLARESHIELD AND STANDBY INSTRUMENT LIGHTS
The standby instrument lights are powered from the battery bus whenever normal DC
power is lost. The standby instrument and glareshield lights are controlled by the
integral CTR switch on the COCKPIT LIGHTS INTEGRAL/MISC panel.
DIM
OFF
BRG
BRT
RAD
WARNING
ROLL
SEL
PLT
ROLL
Honeywell
DN
MASTER
WARNING/CAUTION
ROLL SPLRS
HUD
MINIMUMS
V/L
FMS
NAV SRC
BARO
BRG
IN
BARO SET
FD
CRS 1
Hpa
FLC
FMS
SPD
NAV
HDG
BANK
P
I
T
C
H
HDG
MAN
BC
HSI
CAUTION
UP
APR
PLT CONT
PUSH DCT
PUSH STD
Honeywell
PUSH CHG
VNAV
ALT
AP
ALT
BRG
FD
CRS 2
MINIMUMS
RAD
YD
V/L
BARO
FMS
NAV SRC
PUSH DCT
20
10
10
20
30
10 0
0 FEET
4
8 1 3 000
2
2
3
7
ALT
6
IN HG
4
IAS
29 9 2
5
180 200 220
B
A
R
O
1
250
KNOTS
COCKPIT LIGHTS
FLOOD
OFF
L
BRT
OFF
CTR
BRT
OFF
R
COCKPIT LIGHTS INTEGRAL/MISC PANEL
Page 9
BRT
GX_15_008
mb/hPa
10 1 3
Hpa
ROLL SPLRS
WARNING
CAUTION
PUSH STD
Honeywell
30
9
BARO SET
CPL
PUSH SYNC
MASTER
WARNING/CAUTION
BRG
IN
HSI
VS
ROLL
SEL
CPLT
ROLL
CPLT CONT
Bombardier Global Express - Lighting
PILOT/COPILOT SIDE PANEL LIGHTING
The pilot and copilot side panels are controlled by individual brightness controls
located on each EMS/CDU.
SEL
SEL
ET
STALL
11:13INT50
CHR 01:43
PUSHER
ER
ON
O
OFF
ET
RST
11:13INT50
CHR 01:43
PUSHER
ER
ON
O
OFF
MODE
MODE
CHR
CHR
CIRCUIT BREAKER - SYSTEM
AFCS
STALL
RST
AFCS
DC 1 DOORS
AIR COND/PRESS
DC ESS
APU
AC ESS ENGINE
ELEC
BATT
1
CIRCUIT BREAKER - SYSTEM
1/2
1/2
DC 1 DOORS
AIR COND/PRESS
DC ESS
APU
AC ESS ENGINE
ELEC
BATT
FIRE
BLEED
CAIMS
FLT CONTROLS
CAIMS
FLT CONTROLS
COMM
FUEL
COMM
FUEL
BLEED
M
FIRE
M
BRT
CIRCUIT BREAKER
STAT
SYS
SYSTEM
BUS
PILOT’S SIDE
PANEL
PREV
PAGE
NEXT
PAGE
CNTL
TEST
BRT
CIRCUIT BREAKER
BUS
EMER
CONT
STAT
SYS
SYSTEM
BUS
PREV
PAGE
NEXT
PAGE
CNTL
BUS
EMER
CONT
TEST
COPILOT’S SIDE
PANEL
EMS CDU
BRIGHTNESS
Control
OPEN
PUSH
EMS CDU
BRIGHTNESS
Control
COCKPIT LIGHTS
OFF
PUSH TO CLOSE
FAULT
INTEGRAL
ALRT
RST
TEST
LOW
PPR
888888 8888888
88
WPT
LEG
CHG
TK
GS
POS
XTK
DTK
WD
WS
SYSTEM SELECT
1
2
PPR
ADV
WPT
DIS
TIM
HDG
STS
1
N
2
3
W
4
5
E
6
7
S
8
9
ENT
BCK
0
CLR
FAULT
M
T
3
BRT
DIM
OPEN
PUSH
FROM TO
ON
TST
DIM
M
L
BRT
BR
DIM
M
CTR
BRT
BR
DIM
M
R
BRT
BR
OXYGEN
MASK
100%
PUSH
OXYGEN
MASK
100%
PUSH
PRESS
TO
TEST
AND
RESET
PRESS
TO
TEST
AND
RESET
EMERGENCY
EROS
COCKPIT LIGHTS INTEGRAL/MISC.
EROS
OXYGEN SUPPLY LOWER
DISCONNECT
PASSENGER OXYGEN
ON
THERAPEUTIC
OXYGEN
TEST PORT
NORMAL
CLOSED
ON
OVERRIDE
ON
OFF
PASS. ON
OFF
COCKPIT VOICE RECORDER MICROPHONE MONITOR
SELECT
LEFT
AUX
POWER
RIGHT
ERASE
STATUS
Page 10
TEST
HEADPHONE
GX_15_009
EMERGENCY
OXYGEN SUPPLY LOWER
DISCONNECT
Bombardier Global Express - Lighting
INTEGRAL LIGHTING MASTER CONTROL
The electrical power to the integral lighting is controlled by the MASTER switch on
the COCKPIT LIGHTS INTEGRAL/MISC panel in the center pedestal. The integral
lighting system can be turned ON/OFF or switched to AUTO mode through the
MASTER switch. When in AUTO, to increase the life of the lighting elements, the
system shall be turned on/off through a light sensor circuit depending on the ambient
lighting conditions in the flight compartment.
MASTER
OFF position – extinguishes all integral lighting.
GX_15_010
MASTER Switch
ON
ON position – Activates the integral lighting.
AUTO AUTO position – adjusts all integral lighting
automatically through a sensor unit.
OFF
O
COCKPIT AREA LIGHTS
Two area lights are provided for general illumination of the flight compartment and
controlled by a single switch OFF/DIM/BRT control located on the COCKPIT
LIGHTS INTEGRAL/MISC control panel, in the center pedestal.
The area lights receive 28 VDC from the Avionics Battery Direct Bus when the AREA
OFF/DIM BRT switch on the COCKPIT LIGHTS INTEGRAL/MISC control panel is
activated. Therefore, with no power on the airplane (BATT MASTER SWITCH OFF),
the area light may drain the AVIONICS BATTERY if left on after flight termination.
FLIGHT COMPARTMENT
AREA LIGHT
AREA - DIM/BRT Switch
BRT
BRT
DIM
DIM
D
OFF
O
OFF
O
AREA
COCKPIT LIGHTS INTEGRAL/MISC PANEL
Page 11
GX_15_011
Area Light
Bombardier Global Express - Lighting
EYE REFERENCE LIGHT
An eye reference light provides the pilot(s) orientation for optimal seat position. This
illumination is provided by a single switch ON/OFF switch, located on the COCKPIT
LIGHTS INTEGRAL/MISC control panel.
GX_15_012
EYE REF - ON/OFF Switch
ON
OFF
O
EYE REF
VIEW LOOKING FORWARD
COCKPIT LIGHTS
INTEGRAL/MISC
PANEL
Page 12
Bombardier Global Express - Lighting
FLIGHT COMPARTMENT FLOOR LIGHTS
GX_15_013
The floor lights illuminate the area between the rudder pedals and the seat of each
pilot. To illuminate these areas, a single on/off control switch is located on the
COCKPIT LIGHTS INTEGRAL/MISC control panel of the center pedestal.
ON
OFF
O
FLOOR
COCKPIT LIGHTS
INTEGRAL/MISC PANEL
PUSHBUTTON ANNUNCIATOR LIGHTS
DIM
BRT
B
PBA
PBA-DIM/BRT
Switch
COCKPIT LIGHTS INTEGRAL/MISC PANEL
Page 13
GX_15_014
The pushbutton annunciator lights illuminate all cockpit pushbuttons. This
illumination is provided with a single switch DIM/BRT control, located on the
COCKPIT LIGHTS INTEGRAL/MISC control panel in the center pedestal.
Bombardier Global Express - Lighting
MAP READING LIGHTS
Control
Selector
GX_15_015
Each crew member (pilot and copilot) position is provided with a map reading light.
These lights swivel and include on/off and dimming capabilities.
COCKPIT PHONE LIGHTS
ON
OFF
O
FLOOR
COCKPIT LIGHTS INTEGRAL/MISC PANEL
Page 14
GX_15_016
Two phone lights are controlled by the FLOOR switch on the COCKPIT LIGHTS
INTEGRAL/MISC PANEL of the center pedestal. Turning on the floor lights will
automatically illuminate the phone lights.
Bombardier Global Express - Lighting
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.
COM1
NAV1
11 8 . 0 0 11 2 . 0 0
1 3 0 . 2 7 11 3 . 1 0
TEMP-1
Light Sensor
TEMP-1
ADF1
ATC/TCAS
1605
620.0
1 ATC ALT
ADF
TCAS DSPY 1
HF1
TUNE TO DIM DISPLAY
RANGE:
12
15423
LV
ANY KEY TO 1
RETURN
NORMAL
5600
“DIM” function key
TUNE Control Knob
SQ
DIM
1/2
STO
ID
PGE
TST
DME
GX_15_017
TUNE
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.
Page 15
Bombardier Global Express - 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.
Photo Sensor
(automatic)
Photo Sensor
(automatic)
000ACTIVE FLT PLAN
0ORIGIN
0BOW
00000001152Z
KPHX
1/4
PASS/@ LB0
0/170
0055°00154NM
CLS
15820 (00+21 .75M/10000A
SJN
CLS
0059°00121NM
ABQ
15820 (00+15 .75M/10000A
0DEPARTURE
T.O.INIT0
COMPARE FUEL QUANTITY
GX_15_018
Brightness
button (manual)
Page 16
Bombardier Global Express - 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.
888888 8888888
FROM TO
WPT
8 8
ON
WPT
LEG
CHG
XTK
DTK
DIS
TIM
TK
GS
POS
WD
WS
HDG
STS
SYSTEM SELECT
1
2
1
N
2
3
W
4
5
E
6
7
S
8
9
ENT
BCK
0
CLR
FAULT
M
T
3
BRT
DIM
TST
Brightness
Control Key
COCKPIT LIGHTS
DIM
M
L
BRT
BR
DIM
M
CTR
BRT
BR
DIM
M
R
COCKPIT LIGHTS INTEGRAL PANEL
Page 17
BRT
BR
GX_15_019
INTEGRAL
Bombardier Global Express - 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.
ROLL SPLRS
HUD
ROLL
SEL
PLT
ROLL
DIM
OFF
BRT
PLT CONT
GX_15_020
HGS Brightness Control Knob
Ambient Light
Sensors
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.
Page 18
Bombardier Global Express - Lighting
LAMP TEST
TEST CONTROL
1/2
FIRE TEST
OFF
STALL TEST
OFF
AURAL WARNING TEST 1
OFF
AURAL WARNING TEST 2
OFF
LAMP TEST 1
TEST
LAMP TEST 2
OFF
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
OFF
STALL TEST
OFF
AURAL WARNING TEST 1
OFF
AURAL WARNING TEST 2
OFF
LAMP TEST 1
OFF
LAMP TEST 2
OFF
M
TEST CONTROL
1/2
FIRE TEST
OFF
STALL TEST
OFF
AURAL WARNING TEST 1
OFF
AURAL WARNING TEST 2
OFF
LAMP TEST 1
OFF
LAMP TEST 2
TEST
M
1/2
OFF
STALL TEST
OFF
AURAL WARNING TEST 1
OFF
AURAL WARNING TEST 2
OFF
LAMP TEST 1
OFF
LAMP TEST 2
OFF
GX_15_021
TEST CONTROL
FIRE TEST
M
Page 19
Bombardier Global Express - 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.
ON
OFF
AUTO
A
SEAT BLTS
ON
OFF
AUTO
A
NO SMKG Switch
ON - Turns on all no smoking signs.
OFF - Turns off all no smoking signs.
AUTO - NO SMKG switch will activate
the no smoking lights automatically,
when L/G down or when cabin alt
exceeds 8,000 ft.
EMER LIGHTS
ON
OFF
A
ARM
GX_15_022
PASS SIGNS
NO SMKG
SEAT BLTS Switch
ON - Turns on all seat belt signs.
OFF - Turns off all seat belt signs.
AUTO - SEAT BLTS switch will activate
the seat belt lights automatically, when
slats/flaps not in zero degree position or
when cabin alt exceeds 8,000 ft.
PASSENGER SIGNS
The NO SMKG and SEAT BLTS control switches are located on the overhead panel in
the flight compartment. The control panel has three positions, ON/OFF/AUTO. When
either switch is turned ON, light for the no smoking or seat belt symbol illuminates.
When the NO SMKG switch is set to AUTO, the no smoking lights in the cabin
illuminate automatically when the landing gear is selected down, or when cabin
depressurization occurs (cabin pressure greater than 8,000 feet).
When the SEAT BLTS switch is set to AUTO, the seat belt symbol in the cabin
illuminates automatically when the landing gear is selected down, or the slats/flaps are
not in the zero degree position, or when cabin depressurization occurs (cabin pressure
greater than 8,000 feet).
Passenger Signs Electronic Chime
The chime will sound when the system operates automatically, or if either the NO
SMKG or SEAT BLTS switch is selected to the ON position.
GX_15_023
PAX SIGNS
ELECTRONIC
CHIME
Page 20
Bombardier Global Express - Lighting
PASSENGER LIGHTING SYSTEM
Lighting is provided to illuminate the stairs which are part of the main passenger door,
when entering or exiting the airplane. The door stair lighting includes:
•
•
•
Door stair lights (each step)
Two stair ground lights (lower step)
Passenger door rear light (if installed)
Passenger/Crew Entrance Stair Lights
GX_15_024
Entrance area lighting is provided to illuminate the stairs and the area in front of the
passenger door. Lighting for the entrance area is provided by door stair lights. Each
door stair light is installed in the vertical part of the step. The lower folding step
contains two door stair lights to supply light to the area in front of the passenger door.
Internal Switch
(View looking from inside
the aircraft. Green aircraft
switches shown.)
NOTE:
Both switches are guarded
but not shown.
Page 21
Bombardier Global Express - Lighting
GX_15_025
The stair lighting is controlled on and off by the STAIRS lights switch installed
internally adjacent to the main passenger door.
The stair lights receive power when the passenger door STAIRS light switch is
selected ON and the passenger door is open. The door open signal is received from a
switch located on the door assembly. The DOOR switch is installed next to the
STAIRS light switch and closing the door automatically shuts off the stair lighting.
SERVICE AND MAINTENANCE LIGHTING
The service and maintenance lights supply lighting to the work areas of the airplane
for servicing, maintenance and inspection purposes. The areas illuminated are:
•
•
•
•
Nosewheel well
Avionics compartments
Aft equipment bay, and
APU bay
These lights are controlled to the on/off position by several switches located in
proximity to the normal access areas. All service and maintenance lights are connected
directly to an airplane battery. The nosewheel well light and the avionics compartment
lights interface with one another. The aft equipment bay lights and the APU bay light
interface with each other.
Page 22
Bombardier Global Express - Lighting
NOSEWHEEL BAY LIGHTING
A maintenance light is installed in the nosewheel bay. The light is controlled by the
switch on the forward external service control panel, or when any of the switches in
the avionics bay are selected.
ON
HDPH
MIC
NLG/AVIONICS
BAY MAINT
LIGHT
GEAR
DOORS
CLOSE
ENSURE ALL GEAR
DOORS ARE CLEAR
BEFORE CLOSING
GX_15_026
ON
FORWARD EXTERNAL SERVICE
CONTROL PANEL
All lights in the avionics bay and nose landing gear bay can be automatically turned
off by an autoshutoff device which prevents discharging of the avionics battery. After
15 minutes of normal operation, the lights will flash for approximately 10 seconds.
The lights will then resume normal operation. When 20 minutes of normal operation
(total time) have elapsed, the lights are automatically turned off. All lights can be
turned off and the timing sequence canceled by selecting any of the switches twice
within a three-second period.
Page 23
Bombardier Global Express - Lighting
AVIONICS BAY LIGHTING
Six maintenance lights are installed in the avionics bay. The lights are controlled by
the switch on the forward external service control panel, or when any of three switches
installed at different locations in the avionics bay are selected.
GX_15_027
Maintenance
Lighting
ON
ON
HDPH
MIC
NLG/AVIONICS
BAY MAINT
LIGHT
GEAR
DOORS
CLOSE
ENSURE ALL GEAR
DOORS ARE CLEAR
BEFORE CLOSING
FORWARD EXTERNAL SERVICE
CONTROL PANEL
Automatic shutoff (described in the nose landing gear bay lighting section) prevents
discharging of the avionics battery for prolonged periods of operation.
Page 24
Bombardier Global Express - Lighting
AFT EQUIPMENT BAY LIGHTS
There are three lights located in the aft equipment bay area. These lights can be
switched on by either of three switches:
•
•
Two in the aft equipment bay
One in the APU bay area
HDHP
GX_15_028
The aft equipment bay is equipped with one switch located on the aft equipment bay
door frame, and one located on one of the three light assemblies.
MIC
Aft Equipment Bay
Light Switch
Aft Equipment Bay
Light Switch Location
GX_15_029
All lights in the aft equipment and APU bays can be automatically turned off by an
autoshutoff device which prevents discharging of the APU battery. The design of this
autoshutoff device is similar to the one used for the avionics and nose gear bay
maintenance lights.
AFT EQUIPMENT BAY LIGHTS LOCATION
Light Switch
Page 25
Bombardier Global Express - Lighting
APU BAY LIGHTS
GX_15_030
There is one light located in the APU bay area. This light can be switched on by either
of three switches; two in the aft equipment bay or one located on the light assembly in
the APU bay area. This light can be automatically shut off by the autoshutoff device
described previously in the aft equipment bay light section.
APU Bay Access
EXTERNAL LIGHTING
External lighting provides high intensity lights for landing, and ground flood lighting
and taxiing. The external lighting includes the following:
•
•
•
Landing/taxi lights
Navigation (position) lights
Anticollision (strobe) lights
•
•
Wing inspection lights
Logo lights (if installed)
EXTERNAL LIGHTING SCHEMATIC
Anticollision
Strobe (white)
Primary Tail
Navlight (white)
Anticollision (beacon)
Lights (white/red)
Landing/Taxi Lights
Secondary Tail
Strobe/Navlight (white)
Nose Gear Lights
Wing Inspection Light
Navigation/Strobe
(red)
Not Shown: Navigation Right Hand Side (green)
Page 26
GX_15_031
Logo
Lights
(if Installed)
Bombardier Global Express - Lighting
EXTERNAL LIGHTS CONTROL PANEL
The external lights control panel includes switches for the following lights:
•
•
•
Navigation
Strobe beacon
Wing inspection
•
•
•
Landing/taxi
Taxi recognition
Logo (if installed)
All external lighting is controlled by switches located on the EXTERNAL LIGHTS
control panel.
BEACON Switch
WHT position – When selected, the
WING INSP Switch
beacon lights will illuminate white.
OFF – Turns off the
OFF position – When selected, the
wing inspection lights.
beacon lights will turn off.
ON – Illuminates the
ON position – When selected, the
wing inspection lights.
beacon lights will illuminate red.
STROBE Switch
NAV Switch
LOGO Lights (If installed)
OFF – Turns off the wing
OFF – Turns off the wing
OFF – Turns off the logo lights.
and tail anticollision lights.
and tail navigation lights.
ON – Illuminates the logo lights.
ON – Illuminates the wing
ON – Illuminates the wing
and tail anticollision lights.
and tail navigation lights.
EXTERNAL LIGHTS
BEACON
OFF
ON
O
L WING
STROBE
WHT
OFF
O
ON
OFF
O
ON
LANDING
PULSE
OFF
S
STEADY
L WING Switch
PULSE – Cycles the landing and
taxi lights on the left wing on/off
at 45 pulses per minute
(L wing/R wing pulse alternately).
OFF – Turns off the landing
and taxi lights on the left wing.
STEADY – Illuminates the landing
and taxi lights on the left wing.
NLG
WING INSP
PULSE
OFF
S
STEADY
R WING
PULSE
OFF
S
STEADY
OFF
O
ON
OFF
O
ON
TAXI/RECOG
WINGTIP
R WING Switch
PULSE – Cycles the landing and
taxi lights on the right wing on/off
at 45 pulses per minute
(L wing/R wing pulse alternately).
OFF – Turns off the landing
and taxi lights on the right wing.
STEADY – Illuminates the landing
and taxi lights on the right wing.
NLG Switch
PULSE – When selected, each NLG light pulses
with the corresponding wing landing and taxi lights.
OFF – Turns off the nose landing gear lights.
STEADY – Illuminates the nose landing gear lights.
Page 27
LOGO
WINGTIP
OFF
O
ON
GX_15_032
NAV
TAXI/RECOG Switch
WINGTIP – Illuminates
the wingtip taxi lights.
OFF – Turns off
the wing taxi lights.
ON – Illuminates
the wing taxi lights.
Bombardier Global Express - Lighting
LANDING LIGHTS
A landing light is installed in the wing leading edge on each side, and two landing
lights are installed on the nose gear. Each wing light is controlled by a dedicated on/off
switch, while both nose landing lights are controlled by a single on/off switch.
WING LANDING/TAXI LIGHTS
LANDING/TAXI LIGHTS
L WING
LANDING
PULSE
OFF
S
STEADY
NLG
PULSE
OFF
S
STEADY
R WING
EXTERNAL LIGHTS PANEL
Page 28
PULSE
OFF
S
STEADY
GX_15_033
Combined landing/taxi lights are installed in each wing fairing (leading edge), and
controlled by individual switches on the EXTERNAL LIGHTS panel in the overhead
panel. Selecting the individual L or R WING switch will illuminate the landing and
taxi lights on the applicable side.
Bombardier Global Express - Lighting
NOSE GEAR LANDING LIGHTS
Two seal beam lamp landing lights are installed on the nose landing gear assembly.
Both are controlled by an individual NLG switch on the EXTERNAL LIGHTS panel
in the overhead panel.
NLG
LANDING LIGHTS
PULSE
OFF
S
STEADY
GX_15_034
LANDING
EXTERNAL LIGHTS PANEL
The nose gear landing lights illuminate when the switch is selected and the nose
landing gear is down and locked.
TAXI LIGHTS
A taxi light is installed in each wing leading edge and controlled by a single TAXI/
RECOG switch on the EXTERNAL LIGHTS panel for ground operation. These lights
are also used as in-flight recognition lights.
WINGTIP
OFF
O
ON
Landing/Taxi Lights
EXTERNAL LIGHTS
PANEL
Page 29
GX_15_035
TAXI/RECOG
WINGTIP
Bombardier Global Express - Lighting
WING NAVIGATION LIGHTS
Dual forward navigation lights are installed in each wing tip. The wing-mounted
navigation lights are covered by wing tip lenses on both wings. Two green primary and
secondary navigation lights (position lights) are located in the right wing tip. Two red
primary and secondary navigation lights (position lights) are located in the left wing
tip. These lights are controlled by the NAV switch located on the EXTERNAL
LIGHTS panel.
Wing Tip
Lens Cover
GX_15_036
Primary Wing
Navigation Light
NAV
OFF
ON
O
Secondary Wing
Navigation Light
EXTERNAL LIGHTS PANEL
When the NAV switch is selected, the primary lights on each wing illuminate.
Switchover from the primary to the secondary light system due to a navigation light
failure is achieved automatically, by means of a navigation light control/indication unit
(control box).
The primary wing navigation lights have a higher wattage than the secondary lights
and are protected from overheat due to insufficient cooling. Due to high temperature
conditions (limit temperature of the wing tip lens material) experienced on the ground,
the system will automatically switch to the secondary wing navigation lights. A
thermal switch is integrated in the equipment below each lens to detect temperature
changes for automatic switching to the backup (secondary) system.
Page 30
Bombardier Global Express - Lighting
TAIL NAVIGATION LIGHTS
GX_15_037
Two white navigation lights (primary and secondary) are located at the aft extremity of
the airplane (fin and tail cone).
PRIMARY TAIL
NAVIGATION LIGHT
SECONDARY TAIL
STROBE/NAVIGATION LIGHT
NAV
OFF
ON
O
EXTERNAL LIGHTS PANEL
•
•
•
Primary Light - One primary navigation light is located on the trailing edge at the
tail fairing. This light is controlled by the NAV switch located on the EXTERNAL
LIGHTS panel to control the wing navigation lights
Secondary Light - One secondary navigation light is located in the tail cone and is
part of the combined rear strobe/navigation light unit. The bulb portion of the
combined rear strobe/ navigation light unit is the navigation light. The lower
portion of the unit is the strobe light. This navigation light is controlled by the
NAV switch (located on the EXTERNAL LIGHTS panel) which controls the wing
navigation lights
When the NAV switch is selected the primary light will illuminate. Switchover
from the primary to the secondary light system due to a navigation light failure is
achieved automatically by means of the navigation light control/indication unit
STROBE LIGHTS
The anticollision light system consists of two redundant systems, one wing tip/tail
mounted and one fuselage mounted. One white anticollision strobe light is located on
each wing tip next to the navigation lights and one on the tail cone of the airplane.
Page 31
Bombardier Global Express - Lighting
WING/TIP TAIL MOUNTED STROBES
The wing strobe lights and the rear strobe light together comprise one system.
Strobe Light
OFF
ON
O
GX_15_038
STROBE
EXTERNAL LIGHT PANEL
The flashing of the three white strobe lights is synchronized and simultaneous, and are
used as the main system on the airplane.
OFF
ON
O
GX_15_039
STROBE
EXTERNAL LIGHT PANEL
The lights are white in color and are controlled by the STROBE on/off switch located
on the EXTERNAL LIGHTS panel.
Page 32
Bombardier Global Express - Lighting
FUSELAGE-MOUNTED STROBES
The red/white anticollision strobe lights are located at the top and bottom of the
fuselage. The upper strobe light and the lower strobe light together comprise one
system. The flashing of the two lights is synchronized and simultaneous. These lights
can be selected white or red through a WHT/OFF/RED switch located on the
EXTERNAL LIGHTS panel. The red strobe light is incorporated in the fuselagemounted lights for ground operational purposes to minimize unfavorable effects on the
crew and outside personnel during ground handling.
The fuselage mounted white anticollision system is used as a backup system on the
airplane.
WHT
OFF
O
ON
GX_15_040
BEACON
EXTERNAL LIGHTS PANEL
BEACON LIGHT
Page 33
Bombardier Global Express - Lighting
WING INSPECTION LIGHTS
One wing inspection light is mounted on each side of the airplane to provide
illumination of the wing leading edges that are critical with respect to ice
accumulation.
OFF
ON
O
GX_15_041
WING INSP
WING INSPECTION LIGHT
EXTERNAL LIGHT PANEL
These lights are controlled by the WING INSP on/off switch located on the
EXTERNAL LIGHTS panel.
LOGO LIGHTS (IF INSTALLED)
Space provisions are available for the installation of logo lights, to illuminate a
customer logo painted on the vertical stabilizer.
LOGO LIGHTS
OFF
ON
O
GX_15_042
LOGO
EXTERNAL LIGHTS PANEL
LOGO LIGHT
The logo lights can be controlled by a LOGO on/off switch located on the
EXTERNAL LIGHTS panel.
Page 34
Bombardier Global Express - Lighting
EMERGENCY LIGHTING
Emergency lights are provided to illuminate escape routes in case of an emergency
evacuation. The external emergency lights are located in the following areas:
On the fuselage adjacent to the passenger door
Two over the right wing
GX_15_043
•
•
LEGEND
EMERGENCY LIGHT LOCATION
Details/illustrations of the interior ferry kits are not covered in this training guide. An
interior emergency lighting system (ferry kit) for the airplane consists of:
•
Two emergency dome lights
An exit locating and marking signs system (ferry kit) for the airplane consists of:
•
•
Two exit signs
Two exit locator signs
All fixed emergency lights are controlled by an ON/OFF/ARM switch on the PASS
SIGNS/EMER LTS panel, or automatically if the system is armed and the DC ESS
BUS power fails. The electrical power for all emergency lights is supplied by four
self-contained battery power supply units.
Page 35
Bombardier Global Express - Lighting
EMERGENCY LIGHTING CONTROL
The emergency lights are controlled by the ON/OFF/ARM switch located on the PASS
SIGNS/EMER LTS panel. A second switch for emergency lights control can be
installed as an option, at the flight attendant position.
EMER LTS Switch
ON – Turns ON all emergency lights.
OFF – Removes power from the emergency lights.
ARM – Emergency lights will come ON when there is
no power to the DC essential bus.
ON
OFF
A
AUTO
EMER LIGHTS
SEAT BLTS
ON
OFF
A
AUTO
Page 36
ON
OFF
A
ARM
GX_15_044
PASS SIGNS
NO SMKG
Bombardier Global Express - Lighting
EXTERNAL EMERGENCY LIGHTING
Exterior emergency exit lights are positioned adjacent to the emergency exits to assist
in evacuation of the airplane.
EMER LIGHTS
ON
OFF
A
ARM
GX_15_045
PASS SIGNS/EMER LTS Panel
EMERGENCY LIGHT
LEGEND
Direction of lighting
OVERWING EMERGENCY EXIT LIGHTS
One overwing emergency light is installed over the right wing to illuminate the exit
area, the wing, and the ground along the escape route(s).
A second light is installed on the right hand side in the mid fuselage to illuminate the
exit area, the wing, and the ground along the escape route.
Page 37
Bombardier Global Express - Lighting
AFT FUSELAGE EMERGENCY LIGHTS
Two emergency lights are installed on the left and right lower aft fuselage. These
lights are used to illuminate the aft wing and ground areas along the escape route from
the wing exits.
EMER LIGHTS
GX_15_046
ON
OFF
A
ARM
PASS SIGNS/EMER LTS Panel
EMERGENCY LIGHTS
LEGEND
Direction of lighting
PASSENGER DOOR EMERGENCY LIGHT
One emergency light is installed in proximity to the passenger door to provide
illumination of the door stairway and the ground area at the foot of the stairway.
EMERGENCY LIGHT
ON
OFF
A
ARM
LEGEND
Direction of lighting
PASS SIGNS/EMER LTS Panel
Page 38
GX_15_047
EMER LIGHTS
Bombardier Global Express - Lighting
PASSENGER DOOR (FUSELAGE/WING) GROUND LIGHTING
One emergency light is installed on the right lower section of the passenger door
assembly. The light is directed aft along the forward fuselage ground area and wing.
ON
OFF
A
ARM
GX_15_048
EMER LIGHTS
PASS SIGNS/EMER LTS Panel
LEGEND
Direction of lighting
EMERGENCY LIGHT
FLIGHT COMPARTMENT FLASHLIGHTS
GX_15_049
One flashlight is located on each side of the flight compartment to be used in an
abnormal or emergency condition.
Each flashlight is automatically activated when removed from its retention bracket,
and has a built-in battery/lamp flashing LED indicator monitoring circuit and battery
pack.
Page 39
Bombardier Global Express - Lighting
EICAS MESSAGES
1 . 65
EMER LIGHTS OFF
NAV LIGHTS FAIL
EMER LIGHTS ON
EMER LIGHTS ON
Indicates that the
emergency lights have
automatically activated
(no power on the DC
ESS bus) with the
EMER LTS switch in
the arm position or the
EMER LTS switch is
selected ON.
789
GX_15_050
NAV LIGHTS FAIL
Navigator lights have
failed
EMER LIGHTS OFF
Indicates that the
EMER LTS switch is in
the off position.
Page 40
Bombardier Global Express - Lighting
EMS CIRCUIT PROTECTION
CIRCUIT BREAKER - SYSTEM
GEAR
2/2
NAV
HYD
OIL
ICE
OXYGEN
IND/RECORD
THRUST REV
LIGHTS
M
BRT
STAT
SYS
SYSTEM
BUS
PREV
PAGE
CB - LIGHTS SYSTEM
NEXT
PAGE
CNTL
1/7
TEST
BUS
EMER
CONT
CB - LIGHTS SYSTEM
5/7
AFT MAINT LTS
APU BATT ASCA
IN
PBA BRT/DIM 1 B
DC 1
IN
AREA LTS
AV BATT
IN
PBA BRT/DIM 2 A
BATT
IN
BEACON LT 1
DC 2
IN
PBA BRT/DIM 2 B
DC 2
IN
BEACON LT 2
DC 2
IN
PBA BRT/DIM 3 A
BATT
IN
CB PNL INTG LTS
DC 2
IN
PBA BRT/DIM 3 B
DC 1
IN
COPILOT INTG LTS
DC 1
IN
PILOT INTG LTS
DC ESS
M
DCPC
CB - LIGHTS SYSTEM
2/7
M
CB - LIGHTS SYSTEM
IN
6/7
CTR 1 INTG LTS
DC ESS
IN
R LOGO LT
DC 2
IN
CTR 2 INTG LTS
BATT
IN
R NOSE LDG LT
DC 2
IN
CTR 3 INTG LTS
DC 2
IN
R TAXI LT
AC 4
IN
EMER LTS
DC ESS
IN
R WING LDG LT
AC 4
IN
FLOOD LTS
DC ESS
IN
SEAT BELT SIGN
BATT
IN
FLOOR/EYE LTS
DC 2
IN
STAIR LTS
AV BATT
IN
M
CB - LIGHTS SYSTEM
FWD MAIN LTS
AV BATT
L LOGO LT
3/7
M
CB - LIGHTS SYSTEM
7/7
IN
TAIL STROBE LTS
DC 1
IN
DC 1
IN
WING INSPECT LTS
DC 1
IN
L NOSE LDG LT
DC 1
IN
WING STROBE LTS
DC 1
IN
L TAXI LT
AC 1
IN
L WING LDG LT
AC 1
IN
LIGHT DETECTOR
DC 1
M
DCPC
IN
CB - LIGHTS SYSTEM
4/7
MAP LTS
BATT
IN
NAV LTS
DC 2
IN
NO SMOKING SIGN
BATT
IN
OBHD 1 INTG LTS
BATT
IN
OVHD 2 INTG LTS
DC 1
IN
PBA BRT/DIM 1 A
BATT
M
Page 41
M
GX_15_051
CIRCUIT BREAKER