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EICAS Messages................................................................................................................16-01-13
May 06/2005 Flight Crew Operating Manual Volume 2 REV 2 CSP 100-6
16-00-01
AIRCRAFT LIGHTING
INTRODUCTION
The Challenger 300 lighting system provides interior and exterior illumination of the aircraft. In addition, lights provide information and guidance to passengers in normal and emergency situations.
The lighting systems includes:
-Flight compartment lighting
-Emergency lighting
-Passenger compartment lighting
-Service compartment lighting
-Entrance lighting
-External lighting
The flight compartment and external lighting is selected from the lighting control panels located on the center pedestal and along the flight crew side panels.
Passenger compartment lighting consist of indirect LED lighting and adjustable reading lights placed in the overhead pas-senger service unit (PSU).
Emergency lights are controlled from the flight deck. When armed, they illuminate automatically when R MAIN BUS pow-er has been lost (total loss of generated electrical power). Emergency lighting is provided to the emergency power supply units and are designed to last a minimum of ten minutes at critical ambient conditions, such as low temperature.
EICAS messages display the status of the emergency lights and passenger signs.
FLIGHT COMPARTMENT LIGHTING
DESCRIPTION
The cockpit lighting provides illumination of all control panels and instruments installed in the flight compartment that are not otherwise illuminated by their own integral lighting system or display. They include the following:
-Cockpit Dome Light
-Cockpit Stowage Light
-Flight Crew Reading Lights
-Integral Lighting System
COMPONENTS AND OPERATION COCKPIT LIGHTING
The cockpit dome light sub-system consists of one light unit. The cockpit dome light is mounted in the overhead fascia panel of the cockpit for general illumination of the cockpit and the cockpit entrance area.
One cockpit stowage light is used to illuminate the cockpit stowage box, and it is mounted on the aft end of the center ped-estal. The switch for this light is activated by the stowage door, so that the light illuminates only when the door is open.
Two flight crew reading lights are provided to illuminate the pilot and copilot’s lap area. They are recessed in the headliner on each side of the cockpit, to avoid head impact to the pilots.The light can be rotated up to + 30°. It includes a built-in shutter with an ON/OFF position and continuous light intensity adjustment from bright to dim.
The integral lighting system is divided into four control zones as follows:
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Zone 1 - Pilot panel and part of glareshield
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Zone 2 - Center pedestal
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Zone 3 - Copilot panel and part of the glareshield
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本文链接地址：庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-灯光(2)
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