FWD
(THE RIGHT WHEEL WELL IS OPPOSITE) LEFT WHEEL WELL 
FWD  D
TRANSMITTER, TS5193 FLUID TEMPERATURE 

(TS5195) IN THE LEFT (RIGHT) SYSTEM
HYDRAULIC RESERVOIR IN THE LEFT (RIGHT) SYSTEM E
Hydraulic Fluid Temperature Indicating System - Component Location Figure 102 (Sheet 3)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 
FAULT ISOLATION/MAINT MANUAL 
ACCESS DOOR, 197KL, 
FOR THE CENTRAL 
HYDRAULIC SERVICE 
CENTER 
SEE  F 
HYDRAULIC 
RESERVOIR 
IN THE CENTER 
SYSTEM 
SEE  G 
FWD 
AFT LEFT WING-TO-BODY FAIRING

FWD
CENTRAL HYDRAULIC SERVICE CENTER F
FWD
FLUID TEMPERATURE TRANSMITTER, TS5194, IN THE CENTER SYSTEM
HYDRAULIC RESERVOIR IN THE CENTER SYSTEM
G
Hydraulic Fluid Temperature Indicating System - Component Location Figure 102 (Sheet 4)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 HYDRAULIC FLUID TEMPERATURE INDICATING SYSTEM - ADJUSTMENT/TEST
_______________________________________________________________
 1.  General_______
 A.  This procedure has two tasks. One task is a system test of the overheat lights for the hydraulic pumps. The other task is a system test of the temperature indication system for the hydraulic reservoir.
 TASK 29-32-00-735-001
 2.  System Test - Overheat Lights for the Hydraulic Pumps_____________________________________________________
 A.  References
 (1)  
AMM 06-41-00/201, Fuselage Access Doors and Panels

 (2)  
AMM 06-43-00/201, Engine and Nacelle Strut Access Doors and Panels

 (3)  
AMM 24-22-00/201, Electrical Power

 (4)  
AMM 32-00-15/201, Landing Gear Door Locks

 (5)  
AMM 32-00-20/201, Landing Gear Downlocks

 (6)  
AMM 78-31-00/201, Thrust Reverser System

 B.  Access
 (1)  
Location Zones
 143/144 MLG Wheel Well
 197 Wing to Body-Aft Lower Half (Left)
 211/212 Control Cabin
 434/444 Nacelle Strut - Aft Fairing

 (2)  
Access Panels 197KL Central Hydraulic Service Center 434AL/444AL Hydraulics Installation

 C.  Prepare for the System Test
 S 865-002
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 495-003

 (2)  
Make sure the downlocks are installed on the nose and main landing gear (AMM 32-00-20/201).

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