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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
. Flap Position Switches
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. www.aero.cn 航空翻譯 www.aviation.cn 本文鏈接地址：757-200 MAINTENANCE MANUAL SUPPLEMENT Part II 維護(hù)手冊(cè)補(bǔ)充
