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LANDING
LANDING/TAXI LIGHTS L WING NLG R WING
PULSE PULSE PULSE
OFF OFF
OFF STEADY STEADY STEADY
EXTERNAL LIGHTS PANEL
Nose Gear Landing Lights
FGF1610_005
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.
LANDING LIGHTS
LANDING
NLG
PULSE
OFF STEADY
EXTERNAL LIGHTS PANEL
FGF1610_006
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
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.
LANDING/TAXI LIGHTS
TAXI/RECOG
OFF ON
EXTERNAL LIGHTS PANEL
Wing Navigation Lights
GF1610_034
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.
PRIMARY WING NAVIGATION LIGHT
WING TIP
LENSE COVER
NAV SECONDARY WING
NAVIGATION LIGHT
OFF ON
EXTERNAL LIGHTS PANEL
Volume 2
GF1610_035
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
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 back-up (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).
STROBE LIGHT
(LOWER RING STYLE BULB)
PRIMARY TAIL NAVIGATION LIGHT
NAVIGATION LIGHT (BULB) SECONDARY TAIL
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