Effectivity[*]
[*][*]
22-CONTENTS
BEJ Page 6 Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CHAPTER 22 - AUTOFLIGHT TABLE OF CONTENTS
_________________ Chapter
Section
Subject_______ Subject_______ Page____
DIGITAL FLIGHT CONTROL SYSTEM 22-11-01
Description and Operation 1
General 1
Actuator - Mach Trim 21
Actuators - Autopilot 17
Annunciator - Autoflight 16
Status
Annunciator - Flight Mode 15
Computer - Flight Control 9
Distribution - DFCS Power 25
Indicator - Electronic 16
Attitude Director
Operation - DFCS 42
Panel - Mode Control 10
Sensor - Angle of Airflow 23
Sensors - Position and Neutral 19
Shift
Servo - Stabilizer Trim 20
Switches - Pressure and Limit 24
Switches and Annunciators 21
System - Altitude Alert 34
System - Mach Trim 29
System - Speed Trim 31
System - Stabilizer Trim 36
Transducer - Control Wheel 16
Steering (CWS) Force
Transmitters - Flap Position 24
Unit - AFC Accessory or 15
Integrated Flight System
Accessory
[*] AIRPLANES WITH EFIS
Trouble Shooting 101
[*] AIRPLANES WITH EFIS
Adjustment/Test 501
Operational Test 502
Rigging Test 548
System Test 515
[*] AIRPLANES WITH EFIS
SENSOR - ANGLE OF AIRFLOW (Ref
27-32-11)
Effectivity[*]
[*][*]
22-CONTENTS
BEJ Page 7 Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CHAPTER 22 - AUTOFLIGHT
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
ACTUATOR - AUTOPILOT AILERON 22-11-25 Removal/Installation 401 ALL Adjustment/Test 501 ALL
ACTUATOR - AUTOPILOT ELEVATOR 22-11-26 Removal/Installation 401 ALL Adjustment/Test 501 ALL
ANNUNCIATOR - AUTOFLIGHT STATUS 22-11-32 Servicing 301 [*] [*] AIRPLANES WITH EFIS
Removal/Installation 401 [*] [*] AIRPLANES WITH EFIS
ANNUNCIATOR - DFCS 22-11-35 Removal/Installation 401 [*] [*] AIRPLANES WITHOUT EFIS
Adjustment/Test 501 [*] [*] AIRPLANES WITHOUT EFIS
COMPUTER - DIGITAL FLIGHT 22-11-33
CONTROL SYSTEM (MACH TRIM,
SPEED TRIM) SYSTEM
Maintenance Practices 201 ALL Removal/Installation 401 ALL Adjustment/Test 501 ALL
LIMITER - AILERON FORCE 22-11-13 Removal/Installation 401 [*] [*] AIRPLANES WITH MECHANICAL AILERON FORCE LIMITER
Adjustment/Test 501 [*] [*] AIRPLANES WITH MECHANICAL AILERON FORCE LIMITER
LINKAGE - AUTOPILOT AILERON 22-11-25 ACTUATOR Inspection/Check 601 ALL LINKAGE - AUTOPILOT ELEVATOR 22-11-26 ACTUATOR Inspection/Check 601 ALL
PANEL - DFCS MODE CONTROL 22-11-34 Maintenance Practices 201 ALL Removal/Installation 401 ALL Adjustment/Test 501 ALL
22-CONTENTS
BEJ Page 8 Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CHAPTER 22 - AUTOFLIGHT
TABLE OF CONTENTS
_________________
Chapter Section
Subject_______ Subject ____ Effectivity_______ Page ___________
SENSOR - AILERON POSITION 22-11-29 Removal/Installation 401 ALL Adjustment/Test 501 ALL
SENSOR - ANGLE OF AIRFLOW 22-11-38 Adjustment/Test 501 ALL
SENSOR - ELEVATOR NEUTRAL SHIFT 22-11-14 Removal/Installation 401 ALL Adjustment/Test 501 ALL
SENSOR - ELEVATOR POSITION 22-11-30 Removal/Installation 401 ALL Adjustment/Test 501 ALL
SENSOR - SPOILER POSITION 22-11-27 Removal/Installation 401 ALL Adjustment/Test 501 ALL
SENSOR - STABILIZER POSITION 22-11-31 Removal/Installation 401 ALL Adjustment/Test 501 ALL
SERVO - AUTOPILOT STABILIZER 22-11-81 TRIM Removal/Installation 401 [*] [*] AIRPLANES WITH AUTOPILOT TRIM SERVO
Adjustment/Test 501 ALL
SWITCH - AUTOPILOT DISENGAGE 22-11-41 Removal/Installation 401 ALL Adjustment/Test 501 ALL
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 1(3)
