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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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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