• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 14:21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

 (h)
 675DB for the right spoiler 3.

 (i)
 675EB for the right spoiler 4.


 (j) 675GB for the right spoiler 5. Subtask 27-64-00-865-062
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
 Subtask 27-64-00-863-058
 D. Pressurize the hydraulic system that relates to the spoiler you adjust.
 (1)
 For the spoiler 1 or 5, pressurize the Green hydraulic system (Ref. TASK 29-23-00-863-001).

 (2)
 For the spoiler 2 or 4, pressurize the Yellow hydraulic system (Ref. TASK 29-24-00-863-001).

 (3)
 For the spoiler 3, pressurize the Blue hydraulic system (Ref. TASK 29-10-00-863-003).


R 1EFF : 151-199, 401-499, 1 27-64-00Page 536 1 1 Aug 01/05 1 1 1CES 1


 4. Procedure
_________
 (Ref. Fig. 501A/TASK 27-64-00-991-001-A, 502/TASK 27-64-00-991-006, 503/TASK
 27-64-00-991-002)
 Subtask 27-64-00-220-054
 A. With a feeler gauge, measure the clearance X between the underside of the spoiler trailing edge and the upper surface of the flap. The clearance X must be:
 (1) For the spoiler 1: X=3.5 +0 +1.5 mm (0.1377 +0.0000 +0.0590 in.)
 NOTE : You must do this measurement at the trailing edge of the
____ spoiler (not titanium extension plate).
 (2) For the spoiler 2: X=2 +0.5 -0.5 mm (0.0787 +0.0196 -0.0196 in.)
 NOTE : You must do this measurement:
____
 -
at the trailing edge of the spoiler (not titanium extension plate).

 -
at the outboard end of the spoiler.


 (3) For the spoilers 3 and 4: X=-2 +0.5 -0.5 mm (-0.0787 +0.0196 -0.0196 in.)
 NOTE : You must do this measurement at the closest point (point where
____ the gap between the spoiler and the flap is the smallest).
 (a)
 Adjustment of the interference X without tool. To get the negative clearance do as follows:

 (b)
 Adjustment of the interference X with the SPOILER POSITION CHECK TOOL (98D27603000001).


 1_ Adjust the servocontrol (Ref. Para. B) in order to measure:
 X = 2 +0.5 -0.5 mm (0.0787 +0.0196 -0.0196 in.).
 2_ Adjust the servocontrol again (Ref Para. B) by half a turn
 clockwise in order to get the negative clearance.

 1 Install the SPOILER POSITION CHECK TOOL (98D27603000001) as
_ follows: - on the upper surface of the wing - on the trailing edge of the spoiler
R 1EFF : 151-199, 401-499, 1 27-64-00Page 537 1 1 Aug 01/05 1 1 1CES 1


 - on the axis of the servocontrol.
 2_ Read the position of the spoiler.
 3_ Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 (98D27803000000).
 4_ Extend the flaps (Ref. TASK 27-50-00-866-008).
 NOTE : Put the flap and slat control lever to the position 1.____
 5_ Read the new position of the spoiler .
 The difference of positions gives the negative clearance X.
 6_ Retract the flaps (Ref. TASK 27-50-00-866-009).
 7_ Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 (98D27803000000).
 8_ If necessary, adjust the servocontrol (Ref. Para. B).

 (4) For the spoiler 5: X=0 +0 +0.5 mm (0.0000 +0.0000 +0.0196 in.)
 NOTE : You must do this measurement at the closest point (point where
____ the gap between the spoiler and the flap is the smallest).
 (a) Adjustment of the clearance X without tool. To get the clearance do as follows:
 1 Adjust the servocontrol (Ref. Para. B) in order to measure:
_ X = 4 +0 +0.5 mm (0.1574 +0.0000 +0.0196 in.).
 2 Adjust the servocontrol again (Ref. Para. B) by half a turn
_ clockwise in order to get the clearance.
 (b) Adjustment of the clearance X with the SPOILER POSITION CHECK TOOL (98D27603000001).
 1 Install the SPOILER POSITION CHECK TOOL (98D27603000001) as
_ follows: - on the upper surface of the wing - on the trailing edge of the spoiler - on the axis of the servocontrol.
 2 Read the position of the spoiler.
_
R 1EFF : 151-199, 401-499, 1 27-64-00Page 538 1 1 Aug 01/05 1 1 1CES 1 Subtask 27-64-00-820-054


 3_ Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 (98D27803000000).
 4_ Extend the flaps (Ref. TASK 27-50-00-866-008).
 NOTE : Put the flap and slat control lever to the position 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 FLIGHT CONTROLS 飞行操纵6(116)