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庞巴迪挑战者605公务机机组操作手册 CL605-飞行操纵 FLIGHT_CONTROLS(10)

时间:2011-10-28 11:47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
  

CONTROLS AND INDICATORS
Primary and secondary flight controls and indicators are accessible from both pilot seats. Warning, caution, advisory and status messages are presented on the EICAS page and on the FLIGHT CONTROLS synoptic page.


 FLIGHT CONTROLS Description  Vol. 2  10.10.20 
Oct 05/06 


Pitch, Roll and Yaw Controls
Figure 10.10.13

 

 FLIGHT CONTROLS Description  Vol. 2  10.10.21 
Oct 05/06 


Trim Controls
Figure 10.10.14

 

 FLIGHT CONTROLS Description  Vol. 2  10.10.22 
Oct 05/06 


Flap and Spoiler Controls
Figure 10.10.15

 

 FLIGHT CONTROLS Description  Vol. 2  10.10.23 
Oct 05/06 


Stall Protection System
Figure 10.10.16

 

 FLIGHT CONTROLS Description  Vol. 2  10.10.24 
Oct 05/06 


EICAS Flight Controls Indications (Ground Spoilers)
Figure 10.10.17

 

 FLIGHT CONTROLS Description  Vol. 2  10.10.25 
Oct 05/06 


EICAS Flight Controls Indications (Flight Spoilers)
Figure 10.10.18

 

 FLIGHT CONTROLS Description  Vol. 2  10.10.26 
REV 1, Dec 21/06 


EICAS Flight Controls Indications (Flaps)
Figure 10.10.19

 

 FLIGHT CONTROLS Description  Vol. 2  10.10.27 
Oct 05/06 


EICAS Flight Controls Indications (Trim)
Figure 10.10.20

 

 FLIGHT CONTROLS Description  Vol. 2  10.10.28 
Oct 05/06 


EICAS Flight Controls Indications (Aileron, Elevator, Rudder)
Figure 10.10.21

 

 FLIGHT CONTROLS Description  Vol. 2  10.10.29 
Oct 05/06 

 

Flaps are not set at 20° with the aircraft in takeoff
mode.
Spoilers are not stowed with the aircraft in takeoff
mode.

Pitch trim is not set in the green band with the aircraft in takeoff mode
One or both ailerons have a jammed power control unit.

The left or right altitude compensation circuit of the stall protection computer
has failed.
Indicates >5 degrees difference between left and right elevator surface

position.
Either both flap motors are overheated or the flaps have failed.
Flight spoilers are deployed with either the radio altitude between 10’ – 300’ or

Left and/or right detent mechanism has failed (displays on ground only, unless
there is a loss of system 1 and 2 hydraulic pressure).
Ground spoilers are inoperative.
Ground spoilers are not stowed and the radio altitude is greater than 10’.
 
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