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light installations at the aft lavatory service panel, oxygen service panel,
water service panel and on the forward external electrical access panel.
The refueling panel light (and other service panel lights if installed)
operates from the 28V DC Essential DC bus in order that it may be
powered by the airplane batteries only. A proximity switch installed in the
panel door opens when the door is unlatched, completing the circuit to
power the light. Integrated into the circuit is a SERVICE DOORS
annunciation on the cockpit EICAS display whenever the panel is open.
3. Controls and Indications:
(See Figure 8.)
OPERATING MANUAL
2A-33-00 PRODUCTION AIRCRAFT SYSTEMS
Page 30
May 30/02
Revision 7
A. Circuit Breakers (CBs):
The exterior lighting system is protected by the following CBs:
Circuit Breaker Name CB Panel Location Power Source
NAV / INSP LTS XFMR P C-6 (1)
C-8 (2)
L MAIN 115V AC φA
TAXI LTS XFMR P D-6 (1)
F-10 (2)
115V AC φB
L LDG LT CONT P E-6 (1)
D-7 (2)
L MAIN 28V DC
R LDG LT CONT P F-6 (1)
F-7 (2)
R MAIN 28V DC
L LDG LT PWR P C-7 L MAIN 115V AC φA
R LDG LT PWR P D-7 (1)
E-7 (2)
R MAIN 115V AC φB
STROBE LTS CONT P E-7 (1)
F-8 (2)
R MAIN 28V DC
BOT A/C LT P F-7 (1)
D-6 (2)
R MAIN 28V DC
NAV LTS P C-8 (1)
E-8 (2)
L MAIN 28V AC φA
NAV / INSP LTS CONT P D-8 L MAIN 28V DC
STROBE LTS P E-8 (1)
F-9 (2)
R MAIN 115V AC φA
TOP A/C LT P F-8 (1)
C-6 (2)
R MAIN 115V AC φC
WING INSP LTS P C-9 (1)
E-9 (2)
L MAIN 28V AC φA
TAXI LTS CONT P D-9 (1)
C-9 (2)
L MAIN 28V DC
UTILITY LTS P E-9 (1)
D-9 (2)
ESS 28V DC
BOT A/C LT GND OPER P F-9 (1)
E-6 (2)
ESS 28V DC
L TAXI LT PWR P C-10 R MAIN 28V AC φB
CTR TAXI LT PWR P D-10 R MAIN 28V AC φB
R TAXI LT PWR P E-10 R MAIN 28V AC φB
WHEEL WELL LTS P F-10 (1)
F-6 (2)
ESS 28V DC
BCN LTS CONT P F-7 (3)
D-6 (4)
R MAIN 28V DC
BCN LTS P F-8 (3)
C-6 (4)
R MAIN 115V AC φC
BOT BCN GND OPER P F-9 (3)
E-6 (4)
ESS 115V AC
LOGO LTS P C-5 (5) R MAIN 115V AC φC
PYLON LTS P D-5 (5) R MAIN 28V DC
WING TIP FLD LTS P E-5 (5) L MAIN 28V DC
WING TIP TAXI LTS P K-14 (6) R MAIN 28V AC φB
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-33-00
Page 31
May 30/02
Revision 7
NOTE(S):
(1) SN 1000, 1002-1017
(2) SN 1001, 1018 and subs
(3) SN 1000, 1002-1017 having ASC 10
(4) SN 1001, 1018 and subs having ASC 10
(5) SN 1280 and subs
(6) SN 1000-1279 having ASC 1
B. Advisory (Blue) CAS Messages:
CAS Message Cause or Meaning
SERVICE DOORS One or both of the following service doors is open:
• Tail compartment access door
• Refuel compartment access door (SN 1156 and subs)
4. Limitations:
A. Flight Manual Limitations:
Ground operation of landing lights is limited to Þve (5) minutes.
OPERATING MANUAL
2A-33-00 PRODUCTION AIRCRAFT SYSTEMS
Page 32
May 30/02
Revision 7
Exterior Lights Location
Figure 7
OPERATING MANUAL
2A-33-00
Page 33 / 34
May 30/02
Cockpit EXTERIOR LTS
Panel / Nose Wheel
Switch Panel
Figure 8
OPERATING MANUAL
2A-33-00
Page 35 / 36
May 30/02
2A-33-60: Emergency Lighting System
1. General Description:
The external emergency lighting system facilitates safe evacuation of the airplane
during an emergency in darkness or low visibility. The system is composed of the
following elements:
• Overwing Exit Lights
• Underwing Exit Lights
• Main Entrance Door Emergency Lighting
• Emergency Lighting Battery Packs
• Emergency Lighting Control Switches
2. Description of Subsystems, Units and Components:
A. Overwing Exit Lights:
There are three exit lights on each side of the airplane, installed in the
fuselage below the emergency exit windows. A light is located at the
forward, mid and aft wing root area to illuminate the top of the wing surface
as an aid in airplane evacuation.
B. Underwing Exit Lights:
An exit light positioned forward of the leading edge of the wing on each
side of the airplane illuminates the area beneath the wing. The light
facilitates judging the distance from the wing surface to the area below for
airplane occupants evacuating using the emergency exit windows.
C. Main Entrance Door Emergency Lighting:
Automatic activation of the main entrance door emergency lighting is
　
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