返回首页
当前位置: 主页 > 航空资料 > 机务资料 >

757-200 MAINTENANCE MANUAL SUPPLEMENT Part II 维护手册补充

时间:2011-11-09 15:23来源:蓝天飞行翻译 作者:航空 点击:
  

Aviation Partners Boeing
757-200 MAINTENANCE MANUAL SUPPLEMENT  Part II
Part II
Practices and Procedures
757-200

Aviation Partners Boeing 757-200 
MAINTENANCE MANUAL SUPPLEMENT 
 Part II
TABLE OF CONTENTS
 Title  Chapter
 Flight Controls  27
 Fuel  28
 Lights  33
 Wings  57 

Aviation Partners Boeing
757-200 MAINTENANCE MANUAL SUPPLEMENT  Part II
CHAPTER 27 – FLIGHT CONTROLS
Table of contents
Subject Section Page
Speedbrake Autostow System General 27-62-00 1 DDG Maintenance Procedures 27-62-09 901
Speedbrake Load Alleviation System MMEL 27-20 (DDG) Preparation - 27-62-09 902 MMEL 27-20 (DDG) Restoration -  27-62-09 903
Speedbrake Autostow System Adjustment/Test 27-62-00 501
1.
Spoiler Panel Rigging and SPEEDBRAKE Handle Force Check

2.
SAC Installation and Light Check

3.
AUTOSTOW System Ground Check

4.
Spoiler AUTOSTOW and System Rigging

5.
Override SPEEDBRAKE Handle Forces Check

6.
Autostow System and Airplane System Interface Check


7. Automatic Ground SPEEDBRAKE Functional Test Removal/Installation 27-62-01 401
1.
Autostow Actuator

2.
Autostow Mechanism Tension Spring

3.
Speedbrake Autostow Controller (SAC)


Aviation Partners Boeing 757-200 MAINTENANCE MANUAL SUPPLEMENT  Part II
CHAPTER 27 – FLIGHT CONTROLS
Speedbrake Autostow System

A. General
This procedure has the following tasks for sustaining the Speedbrake Autostow System for 757-200 airplanes with winglets:
(1)
DDG maintenance procedures.

(2)
System functional tests.

(3)
Component replacement checks.


For scheduled periodic maintenance of the Speedbrake Autostow System, see supplement AP57.2-0604 to MPD D622N001.
For component removal, rigging, and functional testing of the basic speedbrake system, see AMM 27-62-01-401. 
For the Speedbrake Autostow System, the speedbrake control system has an additional cam and roller mechanism installed below the flight control stand in the flight deck. The mechanism has an electrically powered actuator that moves a cam in the mechanism. The actuator is controlled by a “SPEEDBRAKE AUTOSTOW CONTROLLER” (SAC), installed in the electronics bay. 
The SAC receives inputs from the following systems:
.
FMC Data Bus

.
ADIRU Data Bus

.
Flap Position Switches

.
 Air/Ground Logic


Aviation Partners Boeing
757-200 MAINTENANCE MANUAL SUPPLEMENT  Part II
Flight Controls
DDG Maintenance Procedures
A. General
This procedure has maintenance tasks for the Master Minimum Equipment List (MMEL) maintenance requirements as shown in the Supplemental Dispatch Deviations Procedure Guide (DDPG), document AP57.2-0612.  These tasks are used to prepare the airplane for flight with certain systems/components inoperative.
 
中国航空网 www.aero.cn
民航翻译 www.aviation.cn
本文链接地址:757-200 MAINTENANCE MANUAL SUPPLEMENT Part II 维护手册补充
 

------分隔线----------------------------