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
VIDEO SYSTEM — The LCD monitors are capable of displaying movies or other pre-recorded media. Components con-sist of a single channel DVD player and two 15 inch flat screen monitors. One is installed on the aft side of the left forward wardrobe cabinet and the other is installed on the forward side of the right aft cabin partition. Also installed is a chime/ page-audio/video amplifier. An Airshow 400 or 4000 system is included as part of the entertainment center. The Airshow 4000 offers enhanced graphics, cockpit monitor, and interface to telephone or satellite systems. Refer to the applicable Airshow Operator’s Manual for further system description.
LAVATORY
The lavatory is located in the aft cabin with the sink, mirror, storage compartment, soap dispenser, electrical outlet and or-dinance signs for occupants on the left side. On the right side is an electric flushing toilet with timer and overboard servic-ing, storage area, tissue and trash drawer. Access to the aircraft oxygen bottle(s) is also in this area behind an upper closeout panel. Fire extinguisher storage is also provided behind the closeout panel.
The toilet switch panel is located on the left side of the right lavatory partition. The switches control the toilet flush, reading light, upwash lighting, mirror light, and a lav call that is annunciated in the cockpit and galley.
Overboard service is connected to the toilet to enable service from outside the aircraft. The connector uses a standard airline service cart. The service instruction placard is installed in the lavatory servicing compartment.
Feb 22/2006 Flight Crew Operating Manual Volume 2 REV 5 CSP 100-6
01-05-07 CARGO BAY DOOR
DESCRIPTION
The cargo bay door is a plug-type door and is located forward of the left engine nacelle. The cargo door opens inward and upward to the overhead position above the doorway.
The cargo door is accessible from inside the aircraft through the passenger compartment but is not certified as an emergency exit.
COMPONENTS AND OPERATION
The cargo door assembly consists of a direct-coupled inner and outer handle, trigger-lock mechanism, fore and aft locking pin, balance springs and cables, and a roller/track assembly.
To open the door from inside the aircraft, raise the spring loaded cover on the center of the handle and push the handle towards the door pane and turn the handle clockwise. To open the cargo door from outside the aircraft, push the trigger-lock in the outer handle to release the handle from the recess in the door. Rotate the handle 90° counterclockwise to retract the locking pins and open the door inward. As the door moves inward, the rollers engage into the door tracks allowing the door to be lifted and latched in the overhead position. A balance spring/cable assembly on each side of the door takes the weight off of the door as the door is lifted into the overhead position.
Volume 2 Flight Crew Operating Manual Sep 14/2005 CSP 100-6 REV 4
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-飞机概述 Airplane General(14)
|
