747-400 AMM 飞机维护手册 指示/记录系统 2(111)

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 5)  The following events will initialize the display with a compacted-full format. a) Initial power application. b) In-flight shut down of any engine. c) Loss of display control selection capability.
 6)  When reverting to multiple EICAS DU operation, the main display is initialized with a primary format and the auxiliary display is initialized with a secondary-full format.
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 31-61-00
 ALL  ú ú 18 Page 90B ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
INTEGRATED DISPLAY SYSTEM
COMPONENT  FIG. 102 SHT  QTY  ACCESS/AREA  REFERENCE 
CIRCUIT BREAKERS - 1 FLT COMPT, P7 
EFIS CONT L, C10168  1 7F11 * 
EFIS CONT R, C10171  1 7F16  *
EIU C, C10175  1 7F10  * 
EIU L, C10174  1 7F9  * 
EIU R, C10176  1 7F15  * 
LWR EICAS, C10172  1 7F14  * 
ND L, C10167  1 7F12  * 
ND R, C10170  1 7F17  * 
PFD L, C10166  1 7F13  * 
PFD R, C10169  1 7F18  * 
FMCS CDU R, C10328 FMCS CDU L, C10327 CIRCUIT BREAKERS - (REF 34-61-00, FIG. 101) UPR EICAS, C10173  1 7F8  * 
CONTROL - CAPT ND BRIGHTNESS, R2268  1  1 FLT COMPT, P72  31-61-09 
CONTROL - CAPT PFD BRIGHTNESS, R2267  1  1 FLT COMPT, P72  31-61-09 
CONTROL - F/O ND BRIGHTNESS, R2270  1  1 FLT COMPT, P72  31-61-09 
LOADER - (REF 34-61-00, FIG. 101) LIGHT - (REF 33-12-00, FIG. 101) AIRBORNE DATA, M7996 F/O MASTER CAUTION/WARNING, S1926 CAPT MASTER CAUTION/WARNING, S1925 CONTROL - F/O PFD BRIGHTNESS, R2269  1  1 FLT COMPT, P72  31-61-09 
MODULE - CAPT DISPLAY TRANSFER, M7992  1  1 FLT COMPT, P1-3  31-61-06 
MODULE - CAPT SOURCE SELECT, M7991  1  1 FLT COMPT, P1-1  31-61-07 
MODULE - F/O DISPLAY TRANSFER, M7994  1  1 FLT COMPT, P3-3  31-61-06 
MODULE - F/O SOURCE SELECT, M7995  1  1 FLT COMPT, P3-1  31-61-07 
PANEL - CAPT EFIS CONTROL, M7354  1  1 FLT COMPT, P10  31-61-03 
PANEL - EICAS CONTROL/FMC SWITCH, M7993  1  1 FLT COMPT, P2-4  31-61-04 
PANEL - EICAS DISPLAY SELECT, M7355  1  1 FLT COMPT, P10  31-61-05 
PANEL - F/O EFIS CONTROL, M7364  1  1 FLT COMPT, P10  31-61-03 
SENSOR - L REMOTE LIGHT, M3488  1  1 31-61-08 
SENSOR - R REMOTE LIGHT, M3489  1  1 31-61-08 
UNIT - AUXILIARY EICAS DISPLAY, M7346  1  1 FLT COMP, P9  31-61-02 
UNIT - CAPT ND DISPLAY, M7350  1  1 FLT COMP, P1-2  31-61-02 
UNIT - CAPT PFD DISPLAY, M7349  1  1 FLT COMP, P1-2  31-61-02 
UNIT - C EFIS/EICAS INTERFACE, M7352  2  1 117AL, MAIN EQUIP CTR, E2-6  31-61-01 
UNIT - L EFIS/EICAS INTERFACE, M7353  2  1 117AL, MAIN EQUIP CTR, E2-6  31-61-01 
UNIT - R EFIS/EICAS INTERFACE, M7351  2  1 117AL, MAIN EQUIP CTR, E2-6  31-61-01 
UNIT - F/O ND DISPLAY, M7348  1  1 FLT COMPT, P3-2  31-61-02 
UNIT - F/O PFD DISPLAY, M7347  1  1 FLT COMPT, P3-2  31-61-02 
UNIT - (REF 34-61-00, FIG. 101) R CONTROL DISPLAY, M7440 L CONTROL DISPLAY, M7439 C CONTROL DISPLAY, M7441 UNIT - MAIN EICAS DISPLAY, M7345  1  1 FLT COMPT, P2-2  31-61-02 

* SEE WDM EQUIPMENT LIST
Integrated Display System - Component Index
Figure 101

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 31-61-00
 ALL  ú
 ú  02  Page 101
 ú  Apr 10/89 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
SEE
CAPT DISPLAY TRANSFER MODULE, M7992
SEE
J SHT 5
CAPT BRIGHTNESS CONTROLS, R2267 AND R2268
SEE
N SHT 7
CAPT SOURCE SELECT MODULE, M7991
SEE
L SHT 6
CAPT PFD, M7349 SEE
C CAPT ND, M7350
SEE SEE
　
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