返回首页

庞巴迪挑战者605公务机机组操作手册 CL605-AURAL_and_VISUAL_WARNING_SYSTEM(11)

时间:2011-10-26 21:46来源:蓝天飞行翻译 作者:公务机
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
  
.
Stall warning;

.
Terrain avoidance warnings (TAWS);

.
Overspeed;

.
Trim clacker;

.
Takeoff configuration warnings;

.
Autopilot cavalry charge;

.
Landing gear horn;

.
Altitude alert C-chord;

.
Vertical track alert; and

.
SELCAL – this aural is sounded twice, then silenced.

 

Aural Warning Testing
The AURAL WARN TEST switch, located on the miscellaneous panel, is used to test the audio outputs of the DCUs. The switch is spring-loaded to the neutral position, and must be held in the 1 or 2 position to enable the test to operate. While held in either position, the aural and voice warnings are sounded sequentially.


 AURAL/VISUAL WARNING SYSTEM Description  Vol. 2  03.10.27 
Oct 05/06 


Miscellaneous Panel Figure 03.10.22

Aural Warning Disable
An aural warning disable panel, located on the copilot’s side console, includes two guarded switch/lights, one for each DCU. The switches are used to disable the aural warning function of a DCU should it become inoperative, thereby preventing false aural alerts. The terrain awareness warning system (TAWS) and traffic collision avoidance system (TCAS) aural warnings cannot be disabled by this function.

AUDIO WARNING Panel
Figure 03.10.23


Reversionary Control
Reversionary control includes automatic and manually-operated reversion functions, to ensure that EICAS data continually remains available to the crew.
The automatic reversionary function monitors the operation of the MFD on which the EICAS page is shown. Should this MFD fail, the system automatically reconfigures the opposite MFD to show the EICAS page.
The crew can also manually manage display configuration via the EICAS selector and the L (R) DISPLAYS selectors on the reversionary control panel.


 AURAL/VISUAL WARNING SYSTEM Description  Vol. 2  03.10.28 
Oct 05/06 


EICAS Selector
The EICAS selector positions are; BOTH PFD’s, L MFD and R MFD. The selector is normally in the L MFD position. This locks the left MFD into a split window configuration, placing the EICAS page in the upper window.
Similarly, if the selector is moved to the R MFD position, the right MFD is locked into a split window configuration, with the EICAS page in the upper window.
Placing the selector to the BOTH PFD’s position causes any display, currently configured as a PFD, to include EICAS data. As a result, the display shows flight, navigation and EICAS data in a compressed format.

EICAS Selector moved to Right MFD
Figure 03.10.24

 

 AURAL/VISUAL WARNING SYSTEM Description  Vol. 2  03.10.29 
Oct 05/06 


EICAS Selector moved to BOTH PFD’s Figure 03.10.25
 
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605公务机机组操作手册 CL605-AURAL_and_VISUAL_WARNING_SYSTEM(11)
 

------分隔线----------------------------