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A

757
MAINTENANCE MANUAL

 B. Consumable Materials
 (1)  D00153 Hydraulic Fluid, Fire Resistant -BMS 3-11

 C. 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 - Control

 (4)  
AMM 36-00-00/201, Pneumatic - General

 (5)  
AMM 78-31-00/201, Thrust Reverser System

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

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

 E. Procedure
 S 862-002
 WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT
_______ THE OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (1)  
Do this procedure: Thrust Reverser Deactivation for Ground
 Maintenance (AMM 78-31-00/201).

 S 012-003

 (2)  
For the left system, open the access panel 434AL for the hydraulic bay in the aft strut (AMM 06-43-00/201).

 S 012-005

 (3)  
For the right system, open the access panel 444AL for the hydraulic bay in the aft strut (AMM 06-43-00/201).

 S 492-008

 (4)  
For the left or right systems, make sure the downlocks are installed on the nose and main landing gear (AMM 32-00-20/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-00
 ALL  ú ú 01 Page 205 ú Jan 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

ENGINE STRUT HYDRAULIC BAY
SEE B
AFT LEFT WING TO BODY FAIRING
SEEA
PRESSURE CONNECTION FOR GROUND POWER FOR THE LEFT (RIGHT) HYDRAULIC SYSTEM
FILTER MODULE FOR THE LEFT (RIGHT) ENGINE-DRIVEN PUMP PRESSURE/CASE DRAIN (REF)
　
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