Wing Ice Inspection Lights; Navigation Lights; Anticollision Strobe Lights And Beacon Lights; Emergency Lights - BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual

WING ICE INSPECTION LIGHTS

Wing ice inspection lights are mounted in both
sides of the fuselage just above the wing. They
are controlled with the WING switch located
on the overhead external lighting panel (Figure
3-6). Power is supplied by DC bus 1.
MISC LTS
BOARDING DOME
OFF OFF
ON ON
LANDING LTS
NOSE
LEFT
OFF OFF
ON
EXTERNAL LTS
NAV
WING
OFF OFF
ON
Figure 3-6. External Lighting
Control Panel

NAVIGATION LIGHTS

Dual unit navigation lights are mounted in the
left and right wingtips, tail cone, and vertical
stabilizer bullet. The lights are powered by AC
bus 1 via a step-down transformer and are
controlled with the NAV switch on the over-
head lighting panel.
ANTICOLLISION STROBE
LIGHTS AND BEACON LIGHTS
Anticollision strobe lights are integral with each
navigation light except in the vertical stabilizer
bullet. The wingtip lights are powered by DC bus
2 and the tail cone light by DC bus 1. There are
also two red beacon lights (not on green
airplanes), one on the top of the vertical stabilizer
and another on the lower fuselage. They are
powered by DC bus 1 and DC bus 2. Control is
with the ANTI-COLLISION light switch located
on the overhead lighting panel (Figure 3-6). The
switch has three positions which are
BCN/STROBE, OFF, and BEACON. In the
BEACON position only the rotating beacons are
powered. The BCN/STROBE position routes
power to the strobe lights and the beacons.
3-6 CL 601-3A/R
STBY
COMP
SERVICE
DIM
OFF
OFF OFF
ON
ON
ON
RECOG/
RIGHT
TAXI LT
OFF OFF
ON ON ON
OVERHD
PANEL
ANTI COLL
OFF
ON ON
BRT
OFF
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
CL-600-2B16 PILOT TRAINING MANUAL

EMERGENCY LIGHTS

Four emergency lights are provided to illu-
minate escape routes during emergency evac-
uation. There are three lights in the fuselage
above the right wing and one light on the left
side just forward of the main entrance door.
Two battery packs independently supply
power. Emergency lighting is controlled from
the emergency lighting panel on the copilot's
side console (Figure 3-7). The switch labeled
"EMERGENCY LIGHTING" has three posi-
tions: ON, OFF, and ARM.
Figure 3-7. Emergency Lighting Control
In the ARM position , the system charges the
battery packs and automatically illuminates the
emergency lights if DC essential power (charg-
ing supply) fails.
When positioned to ON, the battery packs do
not charge and the lights illuminate, along
with a white light labeled "EMER LTS ON"
located next to the switch.
Positioning the switch to OFF causes the emer-
gency lighting system to deenergize and the
amber EMER LTS OFF light to illuminate.
This light warns the crew that the emergency
lights will not be activated automatically.
To prevent automatic illumination on shut-
down, the EMERGENCY LIGHTING switch
must be turned off while AC power is still
available to power the DC essential bus. (AC
power is converted by essential TRU 1 and 2
to feed the DC essential bus.)
EMERGENCY LIGHTING
ARM
EMER EMER
OFF
LTS LTS
OFF ON
ON
L t é e
L t d .