29-11-00
ALL ú ú 01 Page 639 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 866-113
(17)
Turn the control wheel clockwise 30 to 40 degrees.
S 976-114
(18)
Let the flow become stable for one minute and write this flow as
flow No. 10. Flow No. 10__________GPM
S 866-115
(19)
Put the speedbrake lever in the full aft position.
S 866-438
(20)
Turn the control wheel to a position 30 to 40 degrees counterclockwise of neutral.
S 976-116
(21)
Let the flow become stable for one minute and write this flow as
flow No. 11. Flow No. 11__________GPM
S 976-117
(22) Subtract flow No. 11 from flow No. 10 and write this flow as flow No. 11A.
Flow No. 10__________GPM
Flow No. 11__________GPM
Flow No. 11A__________GPM
NOTE:____ Flow No. 11A is the internal leakage for other than the
null leakage of the control valves for spoiler packages 2 and
3.
S 866-118
(23)
Turn the control wheel to a position 30 to 40 degrees clockwise of neutral.
S 976-119
(24)
Let the flow become stable for one minute and write this flow as
flow No. 12. Flow No. 12__________GPM
S 866-120
(25)
Put the control wheel in the neutral position.
S 866-439
(26)
Put the speedbrake lever in the full forward position.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-11-00
ALL ú ú 01 Page 640 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
S 976-121
(27) Subtract flow No. 12 from flow No. 7 and write this flow as flow No. 12A.
Flow No. 7__________GPM
Flow No. 12__________GPM
Flow No. 12A__________GPM
NOTE:____ Flow No. 12A is the internal leakage other than the null
leakage of the control valves for spoiler packages 10 and 11.
S 866-122
(28)
Turn the control wheel to a position 75 to 78 degrees clockwise of neutral.
S 976-123
(29)
Let the flow become stable for one minute and write this flow as
flow No. 13. Flow No. 13__________GPM
S 866-124
(30)
Turn the control wheel to the full clockwise position.
S 976-125
(31)
Let the flow become stable for one minute and write this flow as
flow No. 14. Flow No. 14__________GPM
S 866-126
(32)
Put the control wheel in the neutral position.
S 976-127
(33)
Subtract flow No. 14 from flow No. 13 and write this flow as flow
No. 14A. Flow No. 13__________GPM Flow No. 14__________GPM
Flow No. 14A__________GPM
NOTE: Flow No. 14A is the null leakage of the left central-lateral
____ control package.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-11-00
ALL ú ú 01 Page 641 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 液压 HYDRAULIC 1(61)