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alternating sequence with the right landing and nose lights. The pulselite control unit operates the
pulsing sequence at 45 times per minute.
Wing Landing/Taxi Lights
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.
FGF1610_005
LANDING/TAXI LIGHTS
EXTERNAL LIGHTS PANEL
LANDING
L WING NLG R WING
OFF OFF OFF
STEADY
PULSE
STEADY
PULSE
STEADY
PULSE
Nose Gear Landing Lights
Two sealed 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.
EXTERNAL LIGHTS PANEL
LANDING LIGHTS
FGF1610_006
LANDING
NLG
OFF
STEADY
PULSE
LIGHTING
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
16−10−27
EXTERNAL LIGHTS CONTROL PANEL (CONT'D)
Nose Gear Landing Lights (Cont’d)
The nose gear landing lights illuminate when the switch is selectedto the ON or PULSE position
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 for in flight
recognition lights.
EXTERNAL LIGHTS PANEL
LANDING/TAXI LIGHTS
GF1610_034
TAXI/RECOG
OFF
ON
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.
GF1610_035
EXTERNAL LIGHTS PANEL
PRIMARY WING
NAVIGATION LIGHT
SECONDARY WING
NAVIGATION LIGHT
WING TIP
LENSE COVER
NAV
OFF
ON
LIGHTING
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
16−10−28
EXTERNAL LIGHTS CONTROL PANEL (CONT'D)
Wing Navigation Lights (Cont’d)
When the NAV switch is selected, the primary lights on each wing illuminate. Switch over 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.
Tail Navigation Lights
Two white navigation lights (primary and secondary) are located at the aft extremity of the airplane
(fin and tail cone).
GF1610_036
PRIMARY TAIL
NAVIGATION LIGHT
EXTERNAL LIGHTS PANEL
SECONDARY TAIL
NAVIGATION/STROBE LIGHT
(COMBINED)
STROBE LIGHT
(LOWER RING STYLE BULB)
NAVIGATION LIGHT
(BULB)
NAV
OFF
ON
· Primary Light − One primary navigation light is located on the trailing edge at the tail fairing.
This light is controlled by the “NAV” switch (which also controls the wing navigation lights)
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 lower portion of the unit is the strobe
light. The bulb portion of the combined rear strobe/navigation light unit is the navigation 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 on ground, the secondary light will illuminate for
approximately 30 seconds then, switch over to primary light control. Switch over from the
primary to the secondary light system due to a navigation light failure is achieved
　
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