FUSE - (SYSTEM B OR STANDBY SYSTEM) LEADING EDGE FLAP AND SLAT HYDRAULIC
Removal/Installation SEAL DOOR - KRUEGER FLAP TO NACELLE AND STRUT
Maintenance Practices Adjustment Removal/Installation
Seal Door
Seal Door Spring
SLATS - LEADING EDGE
Removal/Installation
Inspection/Check
SWITCH - LEADING EDGE SLAT UP Removal/Installation Chapter SectionSubject_______ Page____ Effectivity
27-81-51401 ALL401
401409405
27-81-11401 ALL27-81-61
401 ALL27-81-14
201 ALL210201201206
27-81-21401 ALL601 ALL
27-81-45401 [*]
[*] AIRPLANES WITH THE LEADING EDGE SLAT UP SWITCH
VALVE - LEADING EDGE FLAP AND 27-81-81
SLAT CONTROL
Removal/Installation 401 ALL
Adjustment/Test 501 ALL
Adjustment - Control Valve 501
Test - Control Valve 504
VALVE - LEADING EDGE FLAP FLOW 27-81-71
LIMITING
Removal/Installation 401 ALL
27-CONTENTS
BEJ Page 23 Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS
_________________ Chapter
Section
Subject_______ Subject_______ Page____
VALVE - LEADING EDGE STANDBY 27-81-91
DRIVE SHUTOFF
Maintenance Practices 201
Removal/Installation Motor 205
Removal/Installation Valve 201
Test - Standby Drive Shutoff 206
Valve
LEADING EDGE AUTOSLAT SYSTEM 27-83-00
Description and Operation 1
General 1
Computers - Autoslat 2
Indication - Flight Deck, 6
Autoslat
Sensors - Angle of Airflow 1
Valve - Autoslat 7
Operation 7
[*] AIRPLANES WITH AUTOSLAT COMPUTER P/N 65-52818
Description and Operation 1
General 1
Computer - Stall Management 1
Indication - Flight Deck, 5
Autoslat
Valve - Autoslat 5
Operation 5
[*] AIRPLANES WITH STALL MANAGEMENT COMPUTER P/N 65-52822
Trouble Shooting 101 [*] AIRPLANES WITH AUTOSLAT COMPUTER P/N 65-52818
Trouble Shooting 101 [*] AIRPLANES WITH STALL MANAGEMENT COMPUTER P/N 65-52822
Adjustment/Test 501 Operational Test 501 System Test 504
[*] AIRPLANES WITH AUTOSLAT COMPUTER P/N 65-52818
Adjustment/Test 501 Operational Test 501 System Test 505
[*] AIRPLANES WITH STALL MANAGEMENT COMPUTER P/N 65-52822Effectivity
ALL
CONFIG 1 [*]
CONFIG 2 [*]
CONFIG 1 [*]CONFIG 2 [*]CONFIG 1 [*]
CONFIG 2 [*]
27-CONTENTS
BEJ Page 24 Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL CHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS
_________________
Chapter
Section
Subject_______ Subject_______ Page____ Effectivity___________
COMPUTER - LEADING EDGE AUTOSLAT 27-83-11
Removal/Installation 401 [*]
[*] AIRPLANES WITH AUTOSLAT COMPUTER P/N 65-52818
Adjustment/Test 501 [*] [*] AIRPLANES WITH AUTOSLAT COMPUTER P/N 65-52818
SOLENOID - AUTOSLAT CONTROL 27-83-31
VALVE
Removal/Installation 401 ALL
VALVE - AUTOSLAT CONTROL 27-83-21
Removal/Installation 401 ALL
POSITION INDICATING SYSTEM - 27-88-00
LEADING EDGE FLAP AND SLAT
Description and Operation 1 ALL
General 1
Indicator - Leading Edge Flap 7
and Slat Position
Module - Leading Edge Flap and 1
Slat Position Indication
Panel - Leading Edge Devices 7
Annunciator
Sensors - Proximity 1
Operation 7
Trouble Shooting 101 ALL
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本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(9)
