S 866-449
(5)
Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
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29-11-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
TASK 29-11-00-206-450
5. Differential Pressure Indicators Inspection for the Case Drain Filters of the_____________________________________________________________________________ Alternating Current Motor Pumps (ACMP) and the Engine-Driven Pumps (EDP) and
____________________________________________________________________________ for the Return Filters in the Left, Right, and Center Hydraulic Systems.
_______________________________________________________________________
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 29-11-01/401, Left and Right System Alternating Current Motor Pump (ACMP)
(4)
AMM 29-11-02/401, Center System Alternating Current Motor Pump (ACMP)
(5)
AMM 29-11-05/401, Engine-Driven Pump (EDP)
(6)
AMM 29-11-13/401, Center System Return Filter Module and Components
(7)
AMM 29-11-15/401, Left and Right System Return Filter Module and Components
(8)
AMM 29-11-17/401, Left and Right System Engine-Driven Pump (EDP) Pressure and Case Drain Filter Module and Components
(9)
AMM 29-11-18/401, Left and Right System Alternating Current Motor Pump (ACMP) Pressure and Case Drain Filter Module and Components
(10)
AMM 29-11-19/401, Center System Alternating Current Motor Pump (ACMP) Pressure and Case Drain Filter Module and Components
(11)
AMM 32-00-15/201, Main Gear Door Locks
(12)
AMM 32-00-20/201, Landing Gear Downlocks
(13)
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)
434/444 Nacelle Strut - Aft Fairing
730/740 Main Landing Gear and Doors
(2)
Access Panels
197KL Central Hydraulic Service Center
434AL/444AL Hydraulic Bay
C. Procedure
S 496-451
(1) Make sure the downlocks are installed on the nose and main landing gear (AMM 32-00-20/201).
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