|
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
FGF0110_010
Rev 12, Aug 14, 2006 Flight Crew Operating Manual Volume 2
COPILOT'S SIDE CONSOLE
1
2.
Headset Panel 6
3.
Oxygen Mask/Regulator
5.
Cockpit Voice Recorder
6.
Cockpit Printer (If installed)
GF0110_029
Indicates Chapter in which information on item may be found.
Volume 2 Flight Crew Operating Manual Rev 12, Aug 14, 2006
AIRPLANE DOORS
The airplane is equipped with the one passenger door (which serves as an emergency exit), one overwing emergency exit, one baggage compartment door, one rear fuselage equipment bay door and several service doors and panels.
The door warning system provides the flight crew with a visual indication (EICAS), when any of the following exterior doors/exits are opened or incorrectly latched:
.
Passenger door.
.
Cargo door.
.
Aft equipment bay door.
.
Left or right emergency exit.
Description and operation of the emergency features of the wing emergency exits are in this manual Chapter 8, EMERGENCY EQUIPMENT.
The door warning system also provides the flight crew with a visual indication (EICAS), when any of the landing gear doors are not in their commanded position. Description and operation of the landing gear doors are in this manual Chapter 15, LANDING GEAR.
PASSENGER DOOR
The passenger door is the main entrance /exit for passengers as well as the flight crew and is located on the left side of the airplane, aft of the flight compartment. The door is a mechanically balanced airstair with an attached door. The door assembly which opens outwards and downwards, turns on two brackets attached to each side of the airstairs and hinge points in the fuselage. Handrails are attached to each side of the airstairs and the fuselage. They extend and retract as the door opens and closes.
The door operation is power assisted with a cable system and a DC electric motor. The door locking mechanism is capable of operations from inside and outside the airplane. A single operation from either handle will unlock the door and lift it clear of its latching mechanism.
The door opens under a controlled descent through a tension spring arrangement and mechanical damping using a pulley and cable mechanism.
The door is normally closed from inside or outside of the airplane through an electrical actuator. The door can also be manually closed without electrical power.
A hinged flap (vent flap) opens in the exterior surface of the door to protect against pressurization of the fuselage, to an unsafe level, until the door is closed and locked.
The door locks have proximity switches to display an EICAS indication of closed and locked.
Lights are provided in each step riser to illuminate the steps. Door lighting automatically shuts-off when the passenger door closes.
Rev 12, Aug 14, 2006 Flight Crew Operating Manual Volume 2
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
本文链接地址：庞巴迪环球5000公务机机组操作手册 Bombardier Global-空调和增压(20)
| 
