• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 12:29来源:蓝天飞行翻译 作者:admin
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

 Item 8: Aileron scale
 Item 9: SEC computer operation
 Item 10: Horizontal stabilizer hydraulic pressure
 Item 11: Elevator (right) hydraulic pressure
 Item 12: Elevator (right) electrical status
 Item 13: Elevator (right) scale
 Item 14: Elevator (right) position

 1EFF : ALL 1 31-67-27Page 1 1 1 Aug 01/05 1 1 1CES 1


 SD - F/CTL Page: Display of the Parameters 1 to 23
 Figure 001

R 1EFF : 106-149, 303-399, 401-499, 1 31-67-27Page 2 1 1 Aug 01/05 1 1 1CES 1


 SD - F/CTL Page: Display of the Parameters 1 to 23
 Figure 002

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-67-27Page 3 1201-299, 301-302, 1May 01/05 1 1 1CES 1


 Item 15: Rudder scale Item 16: Rudder trim position Item 17: Rudder position Item 18: Rudder hydraulic status Item 19: Trimmable horizontal stabilizer position Item 20: Elevator (left) Item 21: Trimmable horizontal stabilizer control Item 22: ELAC operation Item 23: Aileron indication (left) The symbols related to these indications are described hereafter:
 A. Item 1: Spoilers status indication R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 003)
 **ON A/C ALL

 (1)
 Case 1 The spoiler is represented out and green, when the spoiler status is transmitted correctly from the FCDC bus, the spoiler is extended and available, also from the FCDC bus.

 (2)
 Case 2 The spoiler is represented in and green, when the spoiler status is transmitted correctly from the FCDC bus, the spoiler is retracted and available, also from the FCDC bus.

 (3)
 Case 3 The spoiler is represented out and amber when the spoiler status is transmitted correctly from the FCDC bus, the spoiler is extended and faulty, as transmitted from the FCDC bus.


 1EFF : ALL 1 31-67-27Page 4 1 1 Aug 01/05 1 1 1CES 1


 F/CTL Page - Display of the Parameters: SPOILERS and HYDRAULIC PRESSURE

 Figure 003 
R 1EFF : 1 1 1CES  106-149, 303-399, 401-499,  1 111 31-67-27 Page 5 Aug 01/05

 

 (4)
 Case 4 The spoiler is represented in and amber when the spoiler status is transmitted correctly from the FCDC bus, the spoiler is retracted and faulty, as transmitted from the FCDC bus.

 (5)
 Case 5 The spoiler is replaced by amber XX when the spoiler status is transmitted as not valid from the FCDC bus, or the information is not transmitted correctly from the FCDC bus.


 B. Item 2: Hydraulic system pressure indication

R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 003)
 **ON A/C ALL
 Case 1 The letter which represents the hydraulic system is normally displayed in green. Case 2 It is displayed in amber when the related pressure is lower than 1450 PSI or when the FWC has transmitted a low press to the DMC. Case 3 The letter is not displayed when the information is not transmitted correctly to the DMC.
 C. Item 3: Spoilers status (right)
 Refer to the item 1 (left spoilers) as the same principles apply.
 D. Item 4: FCDC Message A LAF DEGRADED message is displayed in amber when the FCDC transmits a fault of the LAF function: LAF advisory, LAF degraded aileron, LAF degraded spoiler. It is not displayed when neither of these is valid or when the information is not available from the FCDC bus.
 1EFF : ALL 1 31-67-27Page 6 1 1 Aug 01/05 1 1 1CES 1


 E. Item 5: Aileron position

R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 004)
 **ON A/C ALL
 Item (A)
 A pointer moving along a fixed scale represents the aileron position. It
 is normally diplayed in green.
 It is displayed in amber when there is a low pressure of the relevant
 hydraulic systems, or when an aileron fault is transmitted from both
 hydraulic systems concerned.

 F. Item 6: Servo control hydraulic pressure

R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 004)
 **ON A/C ALL
 Item (D)
 Two normally green letters represent the hydraulic systems involved (e.g.
 GREEN and BLU), they are diplayed in amber when the relevant pressure is
 lower than 1450 PSI, as transmitted by the SDAC.
 They are not displayed when the pressure value is not transmitted
 correctly by the SDAC.

 1EFF : ALL 1 31-67-27Page 7 1 1 Aug 01/05 1 1 1CES 1


 F/CTL Page - Display of the Parameters: AILERON POSITION and F/CTL COMPUTER

 STATUS
 Figure 004 
R 1EFF :  106-149, 303-399, 401-499,  1  31-67-27 Page 8 
1  1  Aug 01/05
 1  1
 1CES  1
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM 指示/记录系统 8(105)