747-400 AMM 飞机维护手册 液压 HYDRAULIC 2(129)

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ENGINE DRIVEN PUMP FOR SYSTEM THE NO. 3 HYDRAULIC  HYDRAULIC SYSTEM IS NOT CORRECT FOR THE CONDITION OF THE AIRPLANE THE ENGINE DRIVEN PUMP FOR THE NO. 3  29-11-05-00 29-11-31-00 29-11-39-00  (FIG. 112)
NO. 3 HYDRAULIC SYSTEM EDP SHUTOFF VALVE FOR THE  THE EDP SHUTOFF VALVE FOR THE NO. 3 HYDRAULIC SYSTEM IS NOT CORRECT FOR THE CONDITION OF THE AIRPLANE  29-11-39-00  (FIG. 113) 
DEMAND PUMP FOR THE NO. 3 HYDRAULIC SYSTEM  THE DEMAND PUMP FOR THE NO. 3 HYDRAULIC SYSTEM IS NOT CORRECT FOR THE CONDITION OF THE AIRPLANE  29-11-39-00 29-11-31-00 29-11-18-00 29-11-17-00  (FIG. 114) 

Hydraulic Synoptic Display
Figure 101 (Sheet 1)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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747-400 FAULT ISOLATION/MAINT MANUAL
(FIG. 103) DISPLAY SYMBOL HYDRAULIC SYNOPTIC  DESCRIPTION (TABLE 102) HYDRAULIC SYNOPTIC DISPLAY  CORRECTION ACTION FAULT CODE AMM (POSSIBLE FDE) REFERENCE 
DIGITAL READOUTS NO. 3 HYDRAULIC SYNOPTIC  READOUTS ARE NOT CORRECT FOR THE CONDITION OF THE AIRPLANE THE NO. 3 HYDRAULIC SYNOPTIC DIGITAL  29-11-03-00 29-11-09-00 29-11-10-00 29-11-35-00 29-11-39-00 29-17-03-00  (FIG. 115) 
ENGINE DRIVEN PUMP FOR SYSTEM THE NO. 4 HYDRAULIC  HYDRAULIC SYSTEM IS NOT CORRECT FOR THE CONDITION OF THE AIRPLANE THE ENGINE DRIVEN PUMP FOR THE NO. 4  29-11-49-00 29-11-27-00 29-11-32-00 28-11-40-00  (FIG. 116) 
EDP SHUTOFF VALVE FOR THE NO. 4 HYDRAULIC SYSTEM  HYDRAULIC SYSTEM IS NOT CORRECT FOR THE CONDITION OF THE AIRPLANE THE EDP SHUTOFF VALVE FOR THE NO. 4  29-11-40-00 29-11-48-00  (FIG. 117) 
HYDRAULIC SYSTEM DEMAND PUMP FOR THE NO. 4  SYSTEM IS NOT CORRECT FOR THE CONDITION OF THE AIRPLANE THE DEMAND PUMP FOR THE NO. 4 HYDRAULIC  29-11-19-00 29-11-20-00 29-11-32-00 29-11-40-00 29-11-48-00  (FIG. 118) 
DIGITAL READOUTS NO. 4 HYDRAULIC SYNOPTIC  CONDITION OF THE AIRPLANE READOUTS ARE NOT CORRECT FOR THE THE NO. 4 HYDRAULIC SYNOPTIC DIGITAL 29-11-04-00 29-11-11-00 29-11-12-00 29-11-36-00 29-11-40-00 29-11-48-00 29-17-04-00  (FIG. 119) 
FOR THE NO. 1 HYDRAULIC AUXILIARY AC MOTOR PUMP SYSTEM  NO. 1 HYDRAULIC SYSTEM IS NOT CORRECT THE AUXILIARY AC MOTOR PUMP FOR THE FOR THE CONDITION OF THE AIRPLANE  29-11-47-00 29-11-37-00 29-11-13-00  (FIG. 120) 
AUXILIARY AC MOTOR PUMP FOR THE NO. 4 HYDRAULIC SYSTEM  THE AUXILIARY AC MOTOR PUMP FOR THE NO. 4 HYDRAULIC SYSTEM IS NOT CORRECT FOR THE CONDITION OF THE AIRPLANE  29-11-29-00 29-11-40-00 29-11-48-00  (FIG. 121) 

Hydraulic Synoptic Display
Figure 101 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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747-400 FAULT ISOLATION/MAINT MANUAL
IS AUX SWITCH DEM PUMP  PRESSURE EDP IS LOW  IS LOW SYSTEM PRESSURE  SYMBOL DISPLAYED  COLOR SYMBOL 
YES YES NO YES  YES NO N/A YES  YES N/A N/A NO  AUX ON AUX ON AUX OFF AUX ON  WHITE AMBER CYAN WHITE 

AUXILIARY AC MOTOR PUMPS

IS ON SWITCH DEM PUMP  SWITCH DEM PUMP IS AUTO  PRESSURE DEM PUMP IS LOW  DEM PUMP IS RUNNING  SYMBOL DISPLAYED  SYMBOL COLOR 
YES NO NO NO NO YES  NO NO YES YES YES NO  NO YES NO YES N/A N/A  N/A N/A YES YES NO N/A  DEM ON DEM ON DEM ON DEM AUTO DEM AUTO DEM OFF  WHITE AMBER WHITE AMBER CYAN AMBER 

DEMAND PUMPS

Hydraulic Synoptic Display Symbol Logic Tables
Figure 102

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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747-400
FAULT ISOLATION/MAINT MANUAL

AUXILIARY AC MOTOR PUMP STATUS (AUX ON)
ANALOG HYDRAULIC LEVEL INDICATOR
　
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