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 CHAPTER 29 - HYDRAULIC POWER
 TABLE OF CONTENTS
_________________ Chapter
 Section
 Subject_______  Subject_______ 
Adjustment/Test System Test - Overheat Lights for the Hydraulic Pumps System Test - Temperature Indication for the Hydraulic Reservoir Fluid
 SWITCH - LEFT (L) AND RIGHT (R) ENGINE-DRIVEN PUMP (EDP) CASE DRAIN TEMPERATURE 29-32-01
 Removal/Installation TRANSMITTER - RESERVOIR  29-32-03
 TEMPERATURE
 Removal/Installation HYDRAULIC FLUID QUANTITY  29-33-00
 INDICATING SYSTEM
 Description and Operation General 
Component Details EICAS Display Quantity Monitor Unit Quantity Transmitter Quantity Warning Lights Remote Quantity Indicator Sight Glasses Operation Functional Description Component Location Component Index Component Location Adjustment/Test System Test - Quantity Indicating System for the Hydraulic Fluid MONITOR UNIT - HYDRAULIC FLUID  29-33-51
 QUANTITY
 Removal/Installation TRANSMITTER - HYDRAULIC FLUID  29-33-01
 QUANTITY
 Removal/Installation 

Page
501 501
508
401
401
1 1115111155101
501 501
401
401
EffectivityALL
ALLALLALL
ALLALL
ALLALL

 29-CONTENTS

 GUN Page 10 Mar 20/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 CHAPTER 29 - HYDRAULIC POWER
 TABLE OF CONTENTS
_________________
 Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
 HYDRAULIC RESERVOIR PRESSURE 29-35-00
 INDICATION SYSTEM

 Description and Operation 1 ALL General 1 Component Details 1
 EICAS Display 1 Reservoir Pressure Switch 1 Reservoir Pressure Warning 1
 Light
 Component Location 101 ALL Component Index Component Location
 Adjustment/Test 501 ALL
 System Test - Pressure 501
 Indication for the Hydraulic
 Reservoir

 SWITCH - HYDRAULIC RESERVOIR 29-35-01 PRESSURE Removal/Installation 401 ALL

 29-CONTENTS

 GUN Page 11 Mar 20/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

1.

2.

3.

757 MAINTENANCE MANUAL
 HYDRAULIC POWER - DESCRIPTION AND OPERATION
___________________________________________
General
_______
 A.  Three separate hydraulic systems provide fluid at 3000 psi to operate the airplane systems shown in figure 1. The hydraulic systems are identified as left, right, and center.
 B.  High pressure lines and critical return lines are made from titanium. Aluminum is used for non-critical return lines and steel tubing is used in fire zones. Hydraulic tubing is color coded by system. The left system is coded red, right is green, and center is blue.
　
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