国内精品♨️_公主的红肚兜_.手.动.输.入.网.址.联.系.客.服.人.员.lanan_shell
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. When the NAV switch is selected, the primary lights on each wing illuminate. Switchover 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. NAV OFF ON O GX_15_036 Primary Wing Navigation Light Secondary Wing Navigation Light Wing Tip Lens Cover EXTERNAL LIGHTS PANEL For Training Purposes Only Sept 04 15-31 P I LOT T R A I N I N G GU I D E LIGHTING TAIL NAVIGATION LIGHTS Two white navigation lights (primary and secondary) are located at the aft extremity of the airplane (fin and tail cone). • Primary Light - One primary navigation light is located on the trailing edge at the tail fairing. This light is controlled by the NAV switch 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 bulb portion of the combined rear strobe/ navigation light unit is the navigation light. The lower portion of the unit is the strobe 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 the primary light will illuminate. Switchover from the primary to the secondary light system due to a navigation light failure is achieved automatically by means of the navigation light control/indication unit STROBE LIGHTS The anticollision light system consists of two redundant systems, one wing tip/tail mounted and one fuselage mounted. One white anticollision strobe light is located on each wing tip next to the navigation lights and one on the tail cone of the airplane. GX_15_037 EXTERNAL LIGHTS PANEL SECONDARY TAIL STROBE/NAVIGATION LIGHT PRIMARY TAIL NAVIGATION LIGHT NAV OFF ON O 15-32 For Training Purposes Only Sept 04 P I LOT T R A I N I N G GU I D E LIGHTING WING/TIP TAIL MOUNTED STROBES The wing strobe lights and the rear strobe light together comprise one system. The flashing of the three white strobe lights is synchronized and simultaneous, and are used as the main system on the airplane. The lights are white in color and are controlled by the STROBE on/off switch located on the EXTERNAL LIGHTS panel. STROBE OFF ON O GX_15_038 EXTERNAL LIGHT PANEL Strobe Light STROBE OFF ON O EXTERNAL LIGHT PANEL GX_15_039 For Training Purposes Only Sept 04 15-33 P I LOT T R A I N I N G GU I D E LIGHTING FUSELAGE-MOUNTED STROBES The red/white anticollision strobe lights are located at the top and bottom of the fuselage. The upper strobe light and the lower strobe light together comprise one system. The flashing of the two lights is synchronized and simultaneous. These lights can be selected white or red through a WHT/OFF/RED switch located on the EXTERNAL LIGHTS panel. The red strobe light is incorporated in the fuselagemounted lights for ground operational purposes to minimize unfavorable effects on the crew and outside personnel during ground handling. The fuselage mounted white anticollision system is used as a backup system on the airplane. BEACON OFF WHT ON O GX_15_040 EXTERNAL LIGHTS PANEL BEACON LIGHT 15-34 For Training Purposes Only Sept 04 P I LOT T R A I N I N G GU I D E LIGHTING WING INSPECTION LIGHTS One wing inspection light is mounted on each side of the airplane to provide www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：庞巴迪挑战者手册9
