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DIM BRT
MFD PFD
DIM BRT
DIM BRT
DOME
DIM BRT
CB PANELS
DIM BRT
DOME
DIM BRT
GSHLD/R SIDE
MFD PFD
DIM BRT
DIM BRT
CB PANELS
LIGHTING
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 16-01-05
FLIGHT COMPARTMENT LIGHTING (Cont)
STANDBY INSTRUMENT LIGHTING
The standby instrument lights are designed to supply lighting to the three standby instruments. When left main bus power
to the cockpit lights is lost, power to the standby lights is automatically switched to the right essential bus.
These standby instruments are as follows:
- Standby compass
- Standby instrument
- Clock
CFO1601002_023
STANDBY COMPASS
3
STANDBY INSTRUMENT CLOCK
DIM
BRT
LIGHT
UNIT
STD
CAGE BARO
BRT
DIM
10
10
8 100
200
300
900
140
160
180
200
220
1013 hPa
29.92 in
FLT
RST
CHR
GPS/
MAN
MODE
FLT
CHR
HR
DAY
MIN
MIN
MONTH
SEC
YR
UTC
LOC
A
A
B
C
B C
LIGHTING
Volume 2 Flight Crew Operating Manual Sep 13/2004
16-01-06 CSP 100-6 REV 1
FLIGHT COMPARTMENT LIGHTING (Cont)
CHART HOLDER AND MAP/READING LIGHTS
Chart holders are mounted on the control yokes, and the lights are integral to the chart holders.There are overhead lights
that shine downward onto the crew lap area for map/reading lighting.
Individually controlled reading lights are installed in the overhead panel. Light intensity is adjusted by a dimmer knob
above each unit.
FLASHLIGHTS
Flashlights are installed in holders behind the pilot’s and copilot’s seats, below the circuit breaker panels. Flashlights are
also located in the lavatory area of the cabin.
CFO1601002_020
FLIGHT
COMPARTMENT
FLASHLIGHT
LIGHTING
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 16-01-07
EMERGENCY LIGHTING
DESCRIPTION
Emergency lighting contributes to the safe exit of passengers during an emergency. The emergency lighting system consists
of the following:
- Exit signs
- Ceiling emergency floodlights
- Floor emergency floodlights
- Exterior emergency lights
COMPONENTS AND OPERATION
Emergency lights are powered by two independent rechargeable battery packs that provide 15 minutes of power. The lights
are controlled by a switch on the LIGHTING control panel. During an emergency, exterior emergency lights will provide
illumination of the aircraft’s immediate area. When the battery switch is ON and the EMER LTS switch is OFF, an EMER
LIGHTS OFF (C) message is displayed. When the EMER LTS switch is selected to ON, the emergency lights illuminate
and the amber EMER LIGHTS ON (C) message is displayed. When the switch is in the ARM position and the 28 VDC
R MAIN BUS power is lost, all interior and exterior emergency lights illuminate automatically.
CFO1601002_022
EXTERIOR
EMERGENCY
LIGHT
FLOOR LEVEL
EMERGENCY
EXIT SIGN
EMERGENCY
EXIT SIGN
CABIN
OVERHEAD
EMERGENCY
LIGHT
FLOOR
TRACK
LIGHTING
EXTERIOR
EMERGENCY
LIGHT
EMERGENCY
EXIT SIGN
01
02
05
FLOOR
TRACK
LIGHTING
FLOOR
TRACK
LIGHTING
06
07
FLOOR LEVEL
EMERGENCY
EXIT SIGN
03
04
01
02
E
X
I
T
E
X
I
T
EXIT
EXIT
03
04
05
06
07
LIGHTING
Volume 2 Flight Crew Operating Manual Sep 13/2004
16-01-08 CSP 100-6 REV 1
EXTERNAL LIGHTS
The following external lights make the aircraft visible to other aircraft and controllers:
- Anti-collision strobe lights
- Wing tip anti-collision strobe lights (optional)
- Logo lights (optional)
- Navigation lights
- Rotating beacons
COMPONENTS AND OPERATION
The wing inspection lights are mounted on the either side of the fuselage to visually inspect the wing for ice formation.
The navigation lights allow visual tracking as well as orientation or position of an airplane relative to an observer. The wing
tip navigation lights utilize a dual light system for increased dispatch reliability. This consists of a primary, and secondary
unit under the same lens in each wing tip. If the primary navigation light fails, the secondary light will illuminate when the
NAV switch located on the right secondary power center (right avionics rack circuit breaker panel) is selected. The tail navigation
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