DRUM - AILERON CONTROL WHEEL Removal/Installation Adjustment/Test Inspection/Check Chapter SectionSubject_______ Page____ Effectivity
27-11-001 ALL147
131310
107
13
71316
101 ALL201 ALL201
205
501 ALL501539536
534
52227-11-54401 ALL
27-11-11401 ALL601 ALL801 ALL
27-11-51401 ALL501 ALL601 ALL
27-CONTENTS
BEJ Page 3 Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CHAPTER 27 - FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
Subject
_______
LINKAGE - AILERON POWER CONTROL
UNIT Removal/Installation Inspection/Check Approved Repairs
MECHANISM - AILERON ARTIFICIAL
FEEL, CENTERING AND TRIM Removal/Installation Adjustment/Test Inspection/Check
MECHANISM - AILERON TRANSFER Removal/Installation MODULE - AILERON/RUDDER TRIM CONTROL Removal/Installation Check - Rudder Trim Knob and Light Plate
Removal/Installation -Aileron/Rudder Trim Control Module
Removal/Installation -Rudder Trim Indicator Removal/Installation -Trim Control Switches Test - Trim Control Switches
PANEL AND SEALS - BALANCE Removal/Installation Inspection/Check
QUADRANT - AILERON BODY
Removal/Installation
Inspection/Check
QUADRANT - AILERON WING
Removal/Installation
Inspection/Check
RODS - AILERON TAB CONTROL Removal/Installation Inspection/Check
TAB - AILERON BALANCE
Removal/Installation
Inspection/Check
UNIT - AILERON POWER CONTROL Removal/Installation Adjustment/Test Chapter SectionSubject_______ Page____ Effectivity
27-11-14401 ALL601 ALL801 ALL
27-11-81401 ALL501 ALL601 ALL
27-11-61401 ALL27-11-94
401 ALL408
401
405
403
407
27-11-31401 ALL601 ALL
27-11-91401 ALL601 ALL
27-11-24401 ALL601 ALL
27-11-34401 ALL601 ALL
27-11-21401 ALL601 ALL
27-11-71401 ALL501 ALL
27-CONTENTS
BEJ Page 4 Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ____ Effectivity_______ Page ___________
WHEEL - AILERON CONTROL 27-11-41 Removal/Installation 401 ALL
RUDDER 27-20-00
______ RUDDER AND RUDDER TRIM CONTROL 27-21-00 SYSTEM Description and Operation 1 ALL General 1 Actuator - Rudder Trim 10 Actuator - Standby Rudder 14 Crank - Rudder Pedal 6 Adjustment Mechanism - Rudder Feel and 11 Centering Mechanism - Rudder Trim 10 Control Pedals - Rudder 4 Quadrant - Rudder Aft Control 6 Rudder 4 Torque Tube - Rudder Control 6 Unit - Rudder Power Control 11 Valve - Standby Rudder 14 Actuator Shutoff Operation 16 Trouble Shooting 101 ALL Maintenance Practices 201 ALL Pressurization - Rudder 201 Hydraulic Systems A and B Remove the Pressure - Rudder 205 Hydraulic Systems A, B Adjustment/Test 501 ALL Rudder Trim Control System 524 Test ACTUATOR - RUDDER TRIM 27-21-87 Removal/Installation 401 ALL ACTUATOR - STANDBY RUDDER 27-21-24 Removal/Installation 401 ALL Adjustment/Test 501 ALL Inspection/Check 601 ALL CRANK - RUDDER PEDAL ADJUSTMENT 27-21-41 Removal/Installation 401 ALL
27-CONTENTS
BEJ Page 5 Nov 12/99
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 ____ Effectivity_______ Page ___________
FUSE - RUDDER HYDRAULIC 27-21-95 Removal/Installation 401 [*]
[*] AIRPLANES WITH A RUDDER HYDRAULIC FUSE (FOR HYDRAULIC SYSTEM B)
HINGES - RUDDER 27-21-21 Removal/Installation 401 ALL
INDEX PLATE - RUDDER 27-21-17 Removal/Installation 401 ALL
PEDALS - RUDDER 27-21-31 Removal/Installation 401 ALL
QUADRANT - RUDDER AFT 27-21-61 Removal/Installation 401 ALL Inspection/Check 601 ALL
QUADRANT - RUDDER FORWARD 27-21-51 Removal/Installation 401 ALL Inspection/Check 601 ALL
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