• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 13:44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

 1EFF : 301-399, 1 27-21-00Page 517 1 1 May 01/05R 1 1 1CES 1


 (6) Adjustment of the Force Transducer Unit (FTU) (56).
 (a)
 Install the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (51) on the input lever of the cable tension regulator (57). If you cannot engage the rigging pin (51) freely, adjust the lenght of the FTU (56), as follows:

 (b)
 Install the FTU PROTECTION TOOL (98A27103500000):

 (c)
 Install the FTU PROTECTION TOOL (98A27103500001): 1 Engage the upper and lower web (62) between the FTU (56) and


 1_ Engage the upper and lower web (64) between the FTU (56) and
 the tension regulator (57).
 2_ Install the bolt (63) and tighten.

_ the bellcranck (61).
 2 Install the bolt (63) and tighten.
_
 (d) Adjust the FTU (56): 1 Cut and discard the lockwires.
_ 2 Loosen the nuts (72) and (75) and disengage the lockwashers
_
 (71) and (74). 3 Turn the rod body (73) until you can engage the rigging pin.
_
 4 Engage the lockwashers (71) and (74) and TORQUE the nut (72)

_ to 1.2 m.daN (106.19 lbf.in) and the nut (75) to 0.5 m.daN
 (44.24 lbf.in). Do not safety at this time.
 (e)
 Remove the FTU PROTECTION TOOL (98A27103500000).

 (f)
 Remove the FTU PROTECTION TOOL (98A27103500001).

 (g)
 Safety the nuts with lockwire corrosion resistant steel dia 0.8 mm (0.03 in.).

 (h)
 Remove the rigging pin (51) from the input lever of the cable tension regulator (57).

 (i)
 Remove the rigging pin (51) from the connection relay of the F/O rudder pedals.


 1EFF : 301-399, 1 27-21-00Page 518 1 1 May 01/05R 1 1 1CES 1


 **ON A/C ALL
 Subtask 27-21-00-820-057
 B. Adjustment of the Cable Tension
 (1) Adjust the tension of the cables (Ref. TASK 27-21-00-820-002). NOTE : After the adjustment, remove the rigging pins.
____
 NOTE : If you cannot adjust the control cables, do a visual

____ inspection on the pulleys and the tension regulator. If they are in good condition, replace the control cables (Ref. TASK 27-21-61-000-001) (Ref. TASK 27-21-61-400-001).
 Subtask 27-21-00-820-058
 C. Adjustment of the Rear Mechanical Control
 (Ref. Fig. 503/TASK 27-21-00-991-005, 504/TASK 27-21-00-991-012)

 (1)
 Install the PIN - RIGGING (98D27207547000) or RIGGING PIN SET (98D27207516000) (42) on the cable quadrant (24).

 (2)
 Install the PIN - RIGGING (98D27207548000) or RIGGING PIN SET (98D27207516000) (40) on the mixer (41) of the artificial feel unit.

 (3)
 Install the control rod (25) (Ref. TASK 27-21-00-840-001). You must be able to install the bolts of the rod (25) easily. If not, do these operations :

 (a)
 Cut and remove the lockwire from the nuts of the rod (25).

 (b)
 Loosen the nuts.

 (c)
 Release the lockwashers.

 (d)
 Adjust the length of the rod (25) until you can push the bolts in freely.

 (e)
 Engage the lockwashers.

 (f)
 Tighten the nuts.

 (g)
 Make sure that the adjustment is correct after you have tightened the nuts.

 


 1EFF : ALL 1 27-21-00Page 519 1 1 May 01/05R 1 1 1CES 1


R  Rudder Mechanical Control Figure 503/TASK 27-21-00-991-005
 1EFF : 1 1 1CES  ALL  1 111 27-21-00 Page 520 Aug 01/04

 

R  Rudder Mechanical Control Figure 504/TASK 27-21-00-991-012
 1EFF : 1 1 1CES  ALL  1 111 27-21-00 Page 521 Aug 01/04

 

 (h) Safety the nuts with MISCELLANEOUS (Material No. 19-010).
 (4)
 Adjust the rudder trim (Ref. TASK 27-22-00-820-001).

 (5)
 Adjust the yaw damper (Ref. TASK 27-26-00-820-001).

 (6)
 Install the PIN - RIGGING (98D27207546000) or RIGGING PIN SET (98D27207516000) (39) on the output bellcrank of the lower servocontrol (21). You must install and remove the rigging pin (39) easily. If not, do these operations :

 (a)
 Cut and remove the lockwire from the nuts of the rod (23).

 (b)
 Loosen the nuts.

 (c)
 Release the lockwashers.

 (d)
 Adjust the length of the rod (23) until you can install and remove the rigging pin (39) freely.

 (e)
 Engage the lockwashers.

 (f)
 Tighten the nuts.

 (g)
 Make sure that the adjustment is correct after you have tightened the nuts.

 (h)
 Safety the nuts with MISCELLANEOUS (Material No. 19-010).
 
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 FLIGHT CONTROLS 飞行操纵1(142)