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29-11-00
ALL ú ú 01 Page 204 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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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