CHAPTER 22
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AUTO FLIGHT
TABLE OF CONTENTS
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SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ RUDDER TRIM COMPUTATION 22-62-00 ADJUSTMENT/TEST 501 ALL Operational Test of the Rudder 501 ALL Trim Function
CONTROL SWITCH - RUDDER TRIM 22-62-11
REMOVAL/INSTALLATION 401 ALL Removal of the RUD TRIM Control 401 ALL Switch (9CC) Installation of the RUD TRIM 405 ALL Control Switch (9CC)
PUSHBUTTON SWITCH - RUDDER TRIM/ RESET 22-62-12
REMOVAL/INSTALLATION 401 ALL Removal of the RUD TRIM/RESET 401 ALL Pushbutton Switch (8CC) Installation of the RUD TRIM/RESET 405 ALL Pushbutton Switch (8CC)
INDICATOR - RUDDER TRIM 22-62-21
REMOVAL/INSTALLATION 401 ALL Removal of the Rudder Trim 401 ALL Indicator (17CC) Installation of the Rudder Trim 405 ALL Indicator (17CC)
YAW DAMPER COMPUTATION 22-63-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL System Description 1 ALL Composition 1 ALL Architecture 1 ALL Interface 4 ALL Operation 4 ALL Principle 4 ALL Structure of Yaw Damper 6 ALL Control-Law Operating Logic 8 ALL Monitoring of Yaw Damper 8 ALL Function Test Procedure 11 ALL Computer 11 ALL Servo-Actuator 11 ALL
YAW DAMPER COMPUTATION 22-63-00
ADJUSTMENT/TEST 501 ALL Operational Test of the Yaw Damper 501 ALL Function
CHAPTER 22__________
AUTO FLIGHT
TABLE OF CONTENTS_________________
SUBJECT_______ CH/SE/SU________ C_ PAGE EFFECTIVITY____ ___________
CONFIGURATION AND OPERATIONAL SPEED 22-64-00
COMPUTATION
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
System Description 2 ALL
Presentation of Characteristic 2 ALL
Speed Data
Definition and Symbols 5 ALL
Operation 8 ALL
Speed Computation Principle 8 ALL
Computation of Aerodynamic 15 ALL
Flight-Path Angle (Gamma-a) and
Potential Flight-Path Angle
(Gamma-T)
Computation of Alpha Floor 15 ALL
Protection
Rudder Trim Position 15 001-049, 051-099
101-105, 151-199
201-299,
Rudder Trim Position and Rudder 21 106-149, 301-399
Travel Limiter 401-499,
Windshear Warning 21 ALL
Low Energy Warning 28 ALL
ENGAGEMENT AND INTERNAL MONITORING 22-65-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
System Description 1 ALL
Operation 2 ALL
Connection with FLT CTL/FAC 2 ALL
Pushbutton Switches
Global Internal Monitoring of 2 ALL
the Computer
Monitoring of Peripherals 8 ALL
Monitoring of Internal Power 17 ALL
Supplies
Monitoring of Sensors 19 ALL
Safety Tests 19 ALL
FLIGHT AUGMENTATION COMPUTER (FAC) 22-66-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 1 ALL
System Description 1 ALL
Description 1 ALL
22-CONTENTS Page 7
Aug 01/05
R
CES
CHAPTER 22
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AUTO FLIGHT
TABLE OF CONTENTS
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SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Software Organization 6 ALL
FLIGHT AUGMENTATION COMPUTER (FAC) 22-66-00
DEACTIVATION/REACTIVATION 401 ALL
Deactivation of the FAC 2 401 ALL Refer to the MMEL TASK: 401 ALL 22-66-01-B)
Reactivation of the FAC 2 403 ALL Refer to the MMEL TASK: 403 ALL 22-66-01-B)
COMPUTER - FLIGHT AUGMENTATION (FAC) 22-66-34
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