EffectivityALL
ALLALLALLALL
ALLALL
27-CONTENTS
BEJ Page 8 Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
_______
Inspection/Check HINGES - ELEVATOR Adjustment/Test MECHANISM - ELEVATOR NEUTRAL SHIFT Removal/Installation MECHANISM - ELEVATOR TAB CONTROL Removal/Installation MODULE - ISOLATION VALVES
HYDRAULIC Removal/Installation Adjustment/Test
PANELS - ELEVATOR BALANCE Removal/Installation Adjustment/Test Inspection/Check
PITOT-STATIC SYSTEM - ELEVATOR
Maintenance Practices Flushing Pitot-Static System Drainage
Inspection/Check System Test PLATES - ELEVATOR INDEX Removal/Installation QUADRANT - ELEVATOR FORWARD CONTROL Removal/Installation SEALS - ELEVATOR Adjustment/Test
TABS - ELEVATOR
Removal/Installation
Inspection/Check
TUBE - ELEVATOR INPUT TORQUE Removal/Installation
TUBE - ELEVATOR OUTPUT TORQUE Removal/Installation Inspection/Check
TUBE - FEEL SYSTEM PITOT Removal/Installation
UNIT - ELEVATOR POWER CONTROL Removal/Installation Adjustment/Test Inspection/Check Chapter SectionSubject_______ Page____ Effectivity
601 ALL27-31-21501 ALL27-31-91
401 ALL27-31-34401 ALL27-31-84
401 ALL501 ALL
27-31-41401 ALL501 ALL601 ALL
27-31-17201 ALL201203
20327-31-81401 ALL27-31-61
401 ALL27-31-44501 ALL
27-31-31401 ALL601 ALL
27-31-71401 ALL
27-31-74401 ALL601 ALL
27-31-94401 ALL
27-31-14401 ALL501 ALL601 ALL
27-CONTENTS
BEJ Page 9 Nov 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ___________
UNIT - FEEL AND CENTERING 27-31-64
Removal/Installation 401 ALL
Inspection/Check 601 ALL
VALVES - MANUAL ISOLATION 27-31-87
Removal/Installation 401 ALL
STALL WARNING SYSTEM 27-32-00
Description and Operation 1 CONFIG 1 [*] General 1 Computer - Digital Stall 5
Warning
Sensor - Angle of Airflow 1
Shaker - Control Column 9
Switch - Self Test 9
Transmitter - Flap Position 1
Operation 9
[*] AIRPLANES WITH DIGITAL STALL WARNING COMPUTER P/N 65-52819
Description and Operation 1 CONFIG 2 [*] General 1 Computer - Stall Management 4 Sensor - Angle of Airflow 1 Shaker - Control Column 7 Switch - Self Test 6 Transmitter - Flap Position 1 Operation 7
[*] AIRPLANES WITH STALL MANAGEMENT COMPUTER P/N 65-52822
Trouble Shooting 101 CONFIG 1 [*] [*] AIRPLANES WITH DIGITAL STALL WARNING COMPUTER P/N 65-52819
Trouble Shooting 101 CONFIG 2 [*] [*] AIRPLANES WITH STALL MANAGEMENT COMPUTER P/N 65-52822
Adjustment/Test 501 CONFIG 1 [*] [*] AIRPLANES WITH DIGITAL STALL WARNING COMPUTER P/N 65-52819
Adjustment/Test 501 CONFIG 2 [*] Operational Test 501 System Test 502
[*] AIRPLANES WITH STALL MANAGEMENT COMPUTER P/N 65-52822
27-CONTENTS
BEJ Page 10 Nov 15/98
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 ___________
COMPUTER - DIGITAL STALL WARNING 27-32-41 Removal/Installation 401 [*] [*] AIRPLANES WITH DIGITAL STALL WARNING COMPUTER P/N 65-52819
COMPUTER - STALL MANAGEMENT 27-32-42
Removal/Installation 401 [*]
[*] AIRPLANES WITH STALL MANAGEMENT COMPUTER P/N 65-52822
MODULE - STALL WARNING TEST 27-32-21 Removal/Installation 401 ALL SENSOR - ANGLE OF AIRFLOW 27-32-11 Removal/Installation 401 CONFIG 1 [*] [*] AIRPLANES WITH DIGITAL STALL WARNING COMPUTER P/N 65-52819
Removal/Installation 401 CONFIG 2 [*] [*] AIRPLANES WITH STALL MANAGEMENT COMPUTER P/N 65-52822
Inspection/Check 601 ALL
SHAKER - CONTROL COLUMN 27-32-31
Removal/Installation 401 ALL
HORIZONTAL STABILIZERS 27-40-00
______________________ HORIZONTAL STABILIZER TRIM CONTROL 27-41-00 SYSTEM
Description and Operation 1 ALL
General 1
Assembly - Stabilizer 7
Jackscrew and Gearbox
Indicator - Stabilizer 7
Position
Mechanism - Stabilizer Forward 5
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