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The aft Copilot Lighting Control Panel has three (3) rotary rheostat controls
for pedestal and console lighting:
(1) AFT PED PNL rotary selector controls illumination intensity of the
instruments, displays, indicators and edge lighting on the aft
pedestal panel.
(2) AFT PED DIG rotary selector controls illumination intensity of the
digital displays in the pedestal panel.
(3) R CONSOLE rotary selector controls illumination intensity of the
instruments, displays, indicators and edge lighting on the right
console panel.
F. Dome Light:
A cockpit dome light is mounted in the ßight compartment headliner aft of
the overhead console. The dome light provides general area illumination
for the ßight compartment, and is controlled by a dedicated switch adjacent
to the light.
A second dome light is often installed as optional equipment, placed in the
headliner just aft of the cockpit in the vestibule area, providing general area
illumination for a jumpseat occupant.
G. Map Lights:
Each pilot control yoke has an integrated map light in the control column
located below the control wheel. The map lights are individually controlled
by a switch on the aft side of each inboard arm of the yoke.
Additional map lights are frequently installed adjacent to the gasper air
outlets above the cockpit side windows. A map light may also be Þtted into
the aft cockpit headliner, near the dome light, for use by a jumpseat
occupant.
3. Controls And Indications:
A. Circuit Breakers (CBs):
The ßight compartment lighting system is protected by the following circuit
breakers:
Circuit Breaker CB Panel Location Power Source
L FLT PNL / GLRSHLD P A-7 ESS DC
L CONSOLE FLOOD P A-10 L MAIN DC
L CONSOLE PWR SUPPLY P D-1 L MAIN DC
R FLT PNL / GLRSHLD P B-7 R MAIN DC
R CONSOLE FLOOD P B-10 R MAIN DC
R CONSOLE PWR SUPPLY P E-1 L MAIN DC
PEDESTAL P A-8 L MAIN DC
AFT PED PWR SUPPLY #1 P E-2 L MAIN DC
OPERATING MANUAL
2A-33-00 PRODUCTION AIRCRAFT SYSTEMS
Page 8
May 30/02
Revision 7
Circuit Breaker CB Panel Location Power Source
AFT PED PWR SUPPLY #2 P E-3 L MAIN DC
OVHD / PED FLOOD LTS P A-9 L MAIN DC
OVHD PNL PRI P B-9 ESS DC
FLOOD LTS OVERRIDE P A-6 ESS DC
DOME LT P B-6 ESS DC
WARN LTS TEST P G-1 ESS DC
STBY INSTR P B-8 EMER DC
4. Limitations:
There are no operational limitations for the ßight compartment lighting system as
of this revision.
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-33-00
Page 9
May 30/02
Revision 7
OPERATING MANUAL
THIS PAGE IS INTENTIONALLY LEFT BLANK.
2A-33-00 PRODUCTION AIRCRAFT SYSTEMS
Page 10
May 30/02
Pilot Side Console Light
Controls (Forward,
Airplanes 1000 through
1456)
Figure 1
OPERATING MANUAL
2A-33-00
Page 11 / 12
May 30/02
Pilot Side Console Light
Controls (Forward,
Airplane 1457 and
Subsequent)
Figure 2
OPERATING MANUAL
2A-33-00
Page 13 / 14
May 30/02
Copilot Side Console Light
Controls (Forward,
Airplanes 1000 through
1456)
Figure 3
OPERATING MANUAL
2A-33-00
Page 15 / 16
May 30/02
Copilot Side Console Light
Controls (Forward,
Airplane 1457 and
Subsequent)
Figure 4
OPERATING MANUAL
2A-33-00
Page 17 / 18
May 30/02
Pilot and Copilot Side
Console Light Controls
(Aft, Airplanes 1000
through 1456 Only)
Figure 5
OPERATING MANUAL
2A-33-00
Page 19 / 20
May 30/02
2A-33-30: Passenger Compartment Lighted Panels And Signs System
1. General Description:
The basic GIV airplane is equipped with the basic circuitry and switch controls for
installing FASTEN SEAT BELT and NO SMOKING ordinance signs in the
passenger compartment. Each airplane interior is customized with various seating
arrangements, convenience compartments (lavatories and galleys) and
bulkheads. The placement of the NO SMOKING and FASTEN SEAT BELT signs
is dependent upon the conÞguration of the passenger compartment, thus only
basic wiring provisions are made for the ordinance signs.
The placement of emergency exit signs is likewise limited by the conÞguration of
the passenger compartment because signs must be placed in highly visible
locations, with view unobstructed by cabin components. For basic airplane
certiÞcation, only the required EXIT signs are installed: over the main entrance
door and at the overwing exits. Other emergency exit signs are installed after
completion of the cabin interior, and include multiple installations pointing out the
　
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