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时间:2011-04-11 09:17来源:蓝天飞行翻译 作者:航空
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

 S 866-278

 (29)
 Let the flow become stable for one minute and write this flow as


 flow No. 12. Flow No. 12__________GPM
 S 866-279
 (30)
 Put the speedbrake lever in the full aft position.

 S 866-465

 (31)
 Turn the control wheel 30 to 40 degrees clockwise of the neutral position.


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 29-11-00
 ALL  ú ú 01 Page 671 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 S 976-280
 (32) Let the flow become stable for one minute and write this flow as
 flow No. 13. Flow No. 13__________GPM
 S 866-281
 (33)
 Put the control wheel in the neutral position.

 S 976-282

 (34)
 Subtract flow No. 13 from flow No. 12 and write this flow as flow No. 13A.


 Flow No. 12__________GPM
 Flow No. 13__________GPM
 Flow No. 13A__________GPM
 NOTE:____ Flow No. 13A is the internal leakage other than the null
 leakage of the control valve for spoiler package No. 8.

 S 976-283
 (35) Add flow No. 9B, flow No. 11A, and flow No. 13A.  Write this flow as flow No. 13B.
 Flow No. 9B__________GPM Flow No. 11A__________GPM Flow No. 13A__________GPM Flow No. 13B__________GPM
 S 976-284
 (36) Subtract flow No. 13B from flow No. 6A and write this flow as flow No. 13C.
 Flow No. 6A__________GPM Flow No. 13B__________GPM Flow No. 13C__________GPM
 NOTE: Flow No. 13C is the null leakage of the control package
____ for the right central lateral control.
 S 866-285
 (37) Put the speedbrake lever in the full forward position.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-00
 ALL  ú ú 01 Page 672 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 866-676
 WARNING:_______ MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LE AND TE
 FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP
 CONTROL LEVER.  WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL
 MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP
 CONTROL LEVER.

 (38)
 Retract the trailing edge flaps (AMM 27-51-00/201).

 S 866-288

 (39)
 Put the ALT FLAPS arming switch in the off position.

 S 086-289

 (40)
 Remove the control wheel protractor and adapter.

 S 866-290

 (41)
 Release the pressure in hydraulic system No. 4 (AMM 29-11-00/201).

 S 086-291

 (42)
 If the system demand pump was used as a pressure source, remove the flowmeter:

 (a)  
Remove the flowmeter from the pressure line on the demand pump.

 (b)  
Connect the pressure line to the pressure port on the demand pump.

 (c)  
Put the system HYD PUMPS DEMAND switch on the P5 overhead panel in the ON position.

 (d)  
Examine the pressure port connection on the demand pump for leakage.

 (e)  
Put the system HYD PUMPS DEMAND switch in the OFF position.

 (f)  
Repair the cause of any leakage from the pressure connection on the demand pump.


 S 086-292
 (43)
 If a hydraulic service cart was used a pressure source, disconnect the hydraulic service cart:

 (a)  
Disconnect the pressure line on the hydraulic service cart from the system No. 4 pressure module.

 (b)  
Disconnect the return line on the hydraulic service cart from the system No. 4 return module.


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 29-11-00
 ALL  ú ú 01 Page 673 ú Jun 18/01
 
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本文链接地址:747-400 AMM 飞机维护手册 液压 HYDRAULIC 1(74)