• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-11 09:07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

Engine Fuel Feed System Simplified Schematic
Figure 6 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-22-00
 ALL  ú ú 01 Page 24 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL


EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-22-00
 ALL  ú ú 04 Page 25 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (2)  Obtain a direct tank-to-engine fuel flow using main tank boost
 (3)  pumps. (a) Check that the applicable FUEL CONTROL switch on the control stand is in RUN position. (b) Check that FUEL X FEED switches on the fuel management control module are in closed position (flowbar extinguished). (c) Set MAIN boost pump switches to ON.Obtain fuel crossfeed from any main tank to adjacent engine or engines. (a) Check that applicable FUEL CONTROL switch(es) on the control stand are in RUN position. (b) Set appropriate FUEL X FEED switches to OPEN (flowbar on switch will illuminate), depending on which boost pumps are operating and engine(s) receiving fuel.
 NOTE:____ Crossfeed valves for main tanks No. 2 and No. 3 will not
 open if airplane is on the ground with flaps extended.
 (4)  (c) Set MAIN boost pump switches to ON.Obtain fuel from the center wing tank for engine fuel feed. (a) Check that applicable FUEL CONTROL switch(es) on the control stand are in RUN position. (b) Set appropriate FUEL X FEED switch(es) in open position (flowbar will illuminate) for fuel flow to desired engine(s).
 NOTE:____ Crossfeed valves for main tanks No. 2 and No. 3 will not
 open if airplane is on the ground with flaps extended.
 (5) (6)  (c) Set CTR override/jettison pump switches to ON.Set boost pump and override/jettison pump switches to OFF to terminate engine fuel feed system operation.Set FUEL CONTROL switch(es) to CUTOFF.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-22-00
 ALL  ú ú 04 Page 26 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

FLOW BAR SHOWS FUEL FLOW

FLOW BAR SHOWS THAT THE VALVE IS OPEN
FLOW BAR SHOWS THAT THE PUMP IS ON AND THERE IS FUEL FLOW
 E45457
Figure 7

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-22-00
 ALL  ú ú 08 Page 27 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
ENGINE FUEL FEED SYSTEM
COMPONENT  SHT 102 FIG.  QTY  ACCESS/AREA  REFERENCE 
ACTUATOR - VALVE, NO. 1 ENGINE FUEL SHUTOFF,  1  1  521EB, L LEADING EDGE TO FRONT  28-22-01
 V13  SPAR 
ACTUATOR - VALVE, NO. 1 FUEL CROSSFEED, V45 1  1  L LEADING EDGE TO FRONT SPAR  28-22-02 
ACTUATOR - VALVE, NO. 2 ENGINE FUEL SHUTOFF,  1  1  L LEADING EDGE TO FRONT SPAR 28-22-01 
V14 
ACTUATOR - VALVE, NO. 2 FUEL CROSSFEED, V46 1  1  L LEADING EDGE TO FRONT SPAR  28-22-02 
ACTUATOR - VALVE, NO. 3 ENGINE FUEL SHUTOFF, 1  1  R LEADING EDGE TO FRONT SPAR  28-22-01 
V15 
ACTUATOR - VALVE, NO. 3 FUEL CROSSFEED, V47  1  1  R LEADING EDGE TO FRONT SPAR  28-22-02 
ACTUATOR - VALVE, NO. 4 ENGINE FUEL SHUTOFF, 1  1  621EB, R LEADING EDGE TO FRONT  28-22-01 
V16  SPAR 
ACTUATOR - VALVE, NO. 4 FUEL CROSSFEED, V48  1  1  R LEADING EDGE TO FRONT SPAR 28-22-02 
ADAPTER - VALVE, NO. 1 ENGINE FUEL SHUTOFF  1  1  LEADING EDGE TO FRONT SPAR OUTBD MAIN TANK, 521EB, L 552EB, L FRONT SPAR TO MID SPAR  28-22-09 
 
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 燃油 FUEL 2(71)