(b)
Associated bleed air valves are closed.
(c)
Fluid to associated engine driven hydraulic pump is shut off.
(d)
Associated engine and spar fuel valves are closed.
(4)
After pulling a fire switch handle, rotating it discharges the extinguishing agent into the appropriate engine. Rotating the handle counterclockwise discharges one bottle, rotating it clockwise discharges the other bottle. Decreasing bottle pressure, by discharge or leakage, activates the pressure switch which illuminates the appropriate amber BTL DISCH light located below the fire switch handles on P5. The appropriate EICAS message also appears.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
26-21-00
ALL ú ú 05 Page 6 ú Feb 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
FLIGHT COMPARTMENT
Squib Test Module
Figure 4
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
26-21-00
ALL ú ú 01 Page 7 ú Jun 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(5)
Fire extinguishing agent can be discharged to either engine from bottle A or bottle B or both. If both containers are discharged into one engine compartment, no extinguishing agent will be available to the other engine compartment. Extinguisher tubing runs from the bottles along the forward wing spar to each engine. Extinguishing agent discharges from outlet nozzles in the forward and aft sections of the engines.
B.
Squib Test Module
(1)
The squib test module checks the integrity of extinguisher bottle squibs and firing circuit. Pressing the test 1 or 2 switch sends a signal to the appropriate extinguisher bottle squib discharge cartridge. The test 1 switch checks bottle A squibs for all four engines, and the test 2 switch checks bottle B squibs for all four engines. If the squib and circuit are operative, the ENG 1, 2, 3 and 4 lights (green) on the squib test module will illuminate.
C.
Pressure Switch Test
(1)
Manually activating the bottle pressure switch by pushing the button or turning the ground hex key will test the discharge light circuit continuity. The amber BTL A (or B) DISCH light will illuminate and the appropriate EICAS message appears on the EICAS display indicating a successful test.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
26-21-00
ALL ú ú 04 Page 8 ú Oct 10/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
FAULT ISOLATION/MAINT MANUAL
ENGINE FIRE EXTINGUISHING SYSTEM
COMPONENT 102 FIG. SHT QTY ACCESS/AREA AMM REFERENCE
BOTTLE - 26-21-03
ENG FIRE EXT, M228,M229 2 2 510, LEFT WING LEADING EDGE
ENG FIRE EXT, M230,M231 2 2 610, RIGHT WING LEADING EDGE
CIRCUIT BREAKER - FLT COMPT, P6
FIRE EXT ENG 1 & 3 BTL A, C32 6H3 *
FIRE EXT ENG 1 & 3 BTL B, C31 6H1 *
FIRE EXT ENG 2 & 4 BTL A, C34 6H4 *
FIRE EXT ENG 2 & 4 BTL B, C33 6H2 *
LIGHT - BTL A DISCH ENG 1 & 2, (L1) 1 1 FLT COMPT, P5, FIRE CONTROL *
MODULE, M7326
LIGHT - BTL B DISCH ENG 1 & 2, (L2) 1 1 FLT COMPT, P5, FIRE CONTROL *
MODULE, M7326
LIGHT - BTL A DISCH ENG 3 & 4, (L5) 1 1 FLT COMPT, P5, FIRE CONTROL *
MODULE, M7326
LIGHT - BTL B DISCH ENG 3 & 4, (L6) 1 1 FLT COMPT, P5, FIRE CONTROL *
MODULE, M7326
LIGHT - ENG 1 SQUIB BTL A AND B, (L1) 1 1 FLT COMPT, P461, SQUIB TEST *
MODULE, M7327
LIGHT - ENG 2 SQUIB BTL A AND B, (L2) 1 1 FLT COMPT, P461, SQUIB TEST *
MODULE, M7327
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 防火 FIRE PROTECTION 2(50)