S 715-364
(19) Stop the left engine (AMM 71-00-00/201).
D. Put the Airplane Back to Its Usual Condition
S 095-365
WARNING: OBEY THE REMOVAL PROCEDURE FOR THE DOOR LOCKS.
_______ THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(1)
Remove the door locks from the landing gear doors and close the doors (AMM 32-00-15/201).
(2)
Remove electrical power if it is not necessary (AMM 24-22-00/201).
S 845-366
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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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS - INSPECTION/CHECK
___________________________________________________________________
1. General_______
A. This procedure has these tasks:
(1)
Main Hydraulic Systems Inspection
(2)
Differential Pressure Indicators Inspection for the Pressure Filters of the Alternating Current Motor Pumps (ACMP), the Power Transfer Unit (PTU) and the Left Engine-Driven Pump (EDP) and Bearing Wear Indicator Inspection for the PTU.
(3)
Differential Pressure Indicator Inspection for the Pressure Filter of the Right Engine-Driven Pump (EDP)
(4)
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.
(5)
Differential Pressure Indicator Inspection for the Case Drain Filter of the Power Transfer Unit (PTU)
(6)
Hydraulic System External Leakage Check
(7)
Hydraulic System PCA Initial Leakage Check
(8)
Hydraulic System Gross Internal Leakage Check
(9)
Hydraulic System Elevator and Rudder Power Control Actuators (PCAs) Internal Leakage Check (This Includes the Elevator and Rudder PCA Monitoring System)
(10)
Hydraulic System ACMP Check Valves Internal Leakage Check
(11)
Full Hydraulic System Internal Leakage Check and Isolation of Components with High Leakage.
TASK 29-11-00-206-001
2. Main Hydraulic Systems Inspection_________________________________
A. References
(1)
AMM 06-41-00/201, Fuselage Access Doors and Panels
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本文链接地址：757 AMM 飞机维护手册 液压 CHAPTER 29 - HYDRAULIC POWER 1(90)
