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MODULE - SPOILER CONTROL NO. 2 LEFT, M531  1  1  119BL, MAIN EQUIP CTR E3-1  27-09-00 
MODULE - SPOILER CONTROL NO. 2 RIGHT, M534  1  1  119BL, MAIN EQUIP CTR E4-1  27-09-00 
MODULE - SPOILER CONTROL NO. 3 LEFT, M532  1  1  119BL, MAIN EQUIP CTR E3-1  27-09-00 
MODULE - SPOILER CONTROL NO. 3 RIGHT, M535  1  1  119BL, MAIN EQUIP CTR E4-1  27-09-00 
MODULE - STABILIZER TRIM/ELEV ASYM LIMIT LEFT, M524  1  1  119BL, MAIN EQUIP CTR E3-1  27-09-00 
MODULE - STABILIZER TRIM/ELEV ASYM LIMIT RIGHT, M525 MODULE - YAW DAMPER LEFT, M522 MODULE - YAW DAMPER RIGHT, M523 (FIM 22-21-00/101) (FIM 22-21-00/101)  1  1  119BL, MAIN EQUIP CTR E4-1  27-09-00 

* SEE THE WDM EQUIPMENT LIST

GUN NA349 GUN NB061-999
Control System Electronics Unit - Component Index
Figure 101

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757
FAULT ISOLATION/MAINT MANUAL

 

Control System Electronics Unit - Component Location
Figure 102 (Sheet 1)

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757
FAULT ISOLATION/MAINT MANUAL

(-104) (-201)POWER SUPPLY MODULE

Control System Electronics Unit - Component Location (Detail from Sht 1)
Figure 102 (Sheet 2)

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757
FAULT ISOLATION/MAINT MANUAL

BOEING
CW SB
XDCR XDCR

RESET
MODULE
PCA FAULT

PCA RVDT EXCITM
FUSES
(0.3A)

26V AC HI 26V AC LO
CAUTION
CAUTION
(-100 SERIES) (-200 SERIES) SPOILER CONTROL MODULEC
Control System Electronics Unit - Component Location (Detail from Sht 1)
Figure 102 (Sheet 3)

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757 FAULT ISOLATION/MAINT MANUAL

STABILIZER TRIM/ELEVATOR ASYMMETRY MODULE

 

RUDDER RATIO CHANGER MODULE
(EXAMPLE)

Control System Electronics Unit - Component Location (Details from Sht 1)

Figure 102 (Sheet 4)

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757 MAINTENANCE MANUAL
 FLIGHT CONTROL SYSTEM ELECTRONICS UNIT (CSEU) - MAINTENANCE PRACTICES
_____________________________________________________________________
 1.  General
_______
 A.  This procedure has a removal, installation and installation test task for these flight control system electronics unit (CSEU) modules (referred to as modules):
 (1)  
The CSEU Power Supply Modules M536, M537, M538, M539

 (2)  
The Spoiler Control Modules M530, M531, M532, M533, M534, M535

 (3)  
The Stabilizer Trim/Elevator Asymmetry Limit Modules M524, M525 (referred to as the SAM)
　
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本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊(cè) 飛行操縱 FLIGHT CONTROLS 1(50)