ADVANCE TO NEXT STEP FOR YES/ADV
Ground Test - LRU - 04 MCP (Steps 27-31)
Figure 21 (Sheet 2)
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MAINTENANCE MANUAL
2) Step 26 - Action message 04 TURN VERT SPD DN - DSPLY DEC? instructs the operator to rotate the vertical speed control toward DN and verify that the vertical speed display decreases in value.
3) Step 27 - Action message 04 TURN ALT SEL CCW - DSPLY DEC? instructs the operator to rotate the altitude select control counterclockwise and verify that the altitude display decreases in value.
4) Step 28 - Action message 04 TURN ALT SEL CW - DSPLY INC? instructs the operator to rotate the altitude select control clockwise and verify that the altitude display increases in value.
5) Step 29 - Message 04 TEST COMPLETE is displayed when the 04 MCP test routine has ended. The completed test is exited and enters ground test select when either the YES/ADV or NO/SKIP switch is pressed. On entering the ground test select routine, the display shows the next ground test listed on the front panel.
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FAULT ISOLATION/MAINT MANUAL
MAINTENANCE MONITOR
* SEE THE WDM EQUIPMENT LIST
GUN 001-050,052-999
2 GUN 051
Maintenance Monitor - Component Index
Figure 101
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FAULT ISOLATION/MAINT MANUAL
MAINTENANCE CONTROL DISPLAY PANEL, M168
SEE A
MAIN EQUIPMENT CENTER
MAIN EQUIPMENT
ACCESS DOOR, 119BL
CENTER ACCESS DOOR, 119BL MAIN EQUIPMENT CENTER
MAINTENANCE CONTROL DISPLAY PANEL, M168
A
Maintenance Monitor - Component Location
Figure 102 (Sheet 1)
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FAULT ISOLATION/MAINT MANUAL
FLIGHT COMPARTMENT
MCDP REMOTE CONTROL PANEL CONNECTOR D41101J (FORWARD SIDE OF P61 PANEL)
Maintenance Monitor - Component Location
Figure 102 (Sheet 2)
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MAINTENANCE MONITOR - ADJUSTMENT/TEST
_____________________________________
TASK 22-41-00-715-001
1. Operational Test - MCDP_______________________
A. General
(1) The Maintenance Control and Display Panel (MCDP) is found in the main equipment center. Do the procedures that follow to test the MCDP and use the flight faults displays and ground tests.
B. Equipment
(1) Remote Control Unit, Maintenance Control Display Panel - A22001-22 (preferred); A22001-15 (optional).
C. References
(1)
24-22-00/201, Electrical Power - Control
(2) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：757 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 2(179)
