曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
GSHLD/R SIDE
Dimming the right hand side panel and the copilot DCP is controlled via this potentiometer.
MFD — PFD
Display units have internal lighting, and the intensity is controlled by the MFD/PFD potentiometer.
CB PANELS
This potentiometer controls the intensity of lighting to the pilot and copilot circuit breaker panels.
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
16-01-04 FLIGHT COMPARTMENT LIGHTING (Cont) STANDBY INSTRUMENT LIGHTING
The standby instrument lights are designed to supply lighting to the three standby instruments. When left main bus power to the cockpit lights is lost, power to the standby lights is automatically switched to the right essential bus.
These standby instruments are as follows: -Standby compass -Standby instrument -Clock
LIGHT
UNIT
STANDBY COMPASS
A
BRT
DIM
STANDBY INSTRUMENT CLOCK
B
C
CFO1601002_023
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
16-01-05 FLIGHT COMPARTMENT LIGHTING (Cont)
CHART HOLDER AND MAP/READING LIGHTS
Chart holders are mounted on the control yokes, and the lights are integral to the chart holders.There are overhead lights that shine downward onto the crew lap area for map/reading lighting.
Individually controlled reading lights are installed in the overhead panel. Light intensity is adjusted by a dimmer knob above each unit.
FLASHLIGHTS
Flashlights are installed in holders behind the pilot’s and copilot’s seats, below the circuit breaker panels. Flashlights are also located in the lavatory area of the cabin.
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
16-01-06 EMERGENCY LIGHTING
DESCRIPTION
Emergency lighting contributes to the safe exit of passengers during an emergency. The emergency lighting system consists of the following:
-Exit signs
-Ceiling emergency floodlights
-Floor emergency floodlights
-Exterior emergency lights
COMPONENTS AND OPERATION
Emergency lights are powered by two independent rechargeable battery packs that provide 15 minutes of power. The lights are controlled by a switch on the LIGHTING control panel. During an emergency, exterior emergency lights will provide illumination of the aircraft’s immediate area. When the battery switch is ON and the EMER LTS switch is OFF, an EMER LIGHTS OFF (C) message is displayed. When the EMER LTS switch is selected to ON, the emergency lights illuminate and the amber EMER LIGHTS ON (C) message is displayed. When the switch is in the ARM position and the 28 VDC R MAIN BUS power is lost, all interior and exterior emergency lights illuminate automatically.
01
02
03
04
E X I T
E X I T
EXIT
EXIT
CFO1601002_022
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
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(4)
| 
