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22-11-00  AFDS -FUNCTIONAL DESCRIPTION -WARNING AND ANNUNCIATION  98.36  BEJ ALL 
INTRODUCTION 
22-11-00  AFDS -FUNCTIONAL DESCRIPTION -WARNING AND ANNUNCIATION  98.39  BEJ ALL 
-PFD AND ND DISPLAYS 
22-11-00  AFDS -FUNCTIONAL DESCRIPTION -WARNING AND  98.43  BEJ ALL 
ANNUNCIATIONS -EICAS DISPLAYS 
22-11-00  AFDS -SPECIAL FUNCTIONS  98.46  BEJ ALL 
22-11-00  AFDS -LRU TESTS  98.49  BEJ ALL 
22-11-00  AFDS -SYSTEM TESTS  98.53  BEJ ALL 
22-31-00  THRUST MANAGEMENT COMPUTING SYSTEM (TMCS) - 1  BEJ ALL 
INTRODUCTION 
22-31-00  TMCS -GENERAL DESCRIPTION  5  BEJ ALL 
22-31-00  TMCS -FLIGHT DECK COMPONENT LOCATIONS  8  BEJ ALL 
22-31-00  TMCS -MAIN EQUIPMENT CENTER COMPONENT LOCATIONS  10  BEJ ALL 
22-31-00  TMCS -INTERFACES -1  13  BEJ ALL 
22-31-00  TMCS -INTERFACES -2  18  BEJ ALL 
22-31-00  TMCS -A/T SERVO MOTOR  20  BEJ ALL 
22-31-00  TMCS -A/T ARM, A/T MODE, AND THRUST LEVER SWITCHES  22  BEJ ALL 
22-31-00  TMCS -PRIMARY FLIGHT DISPLAY -OPERATION  25  BEJ ALL 
22-31-00  TMCS -EICAS DISPLAY -OPERATION  29  BEJ ALL 

22-CONTENTS
Page 4
D633W101-BEJ
Jan 05/2002

CHAPTER 22
Autoflight

CH-SC-SU  Subject  Page  Effectivity 
22-31-00  TMCS -AUTOTHROTTLE FLIGHT PROFILE  33  BEJ ALL 
22-31-00  TMCS -A/T OPERATION -TAKEOFF  36  BEJ ALL 
22-31-00  TMCS -A/T OPERATION -VNAV CLIMB  38  BEJ ALL 
22-31-00  TMCS -A/T OPERATION -VNAV CRUISE  40  BEJ ALL 
22-31-00  TMCS -A/T OPERATION -VNAV DESCENT  42  BEJ ALL 
22-31-00  TMCS -A/T OPERATION -FLIGHT LEVEL CHANGE  44  BEJ ALL 
22-31-00  TMCS -A/T OPERATION -SPEED  46  BEJ ALL 
22-31-00  TMCS -A/T OPERATION -GO-AROUND  48  BEJ ALL 
22-31-00  TMCS -A/T OPERATION -FLARE RETARD  50  BEJ ALL 
22-31-00  TMCS -TMCF FUNCTIONAL DESCRIPTION -INTRODUCTION  53  BEJ ALL 
22-31-00  TMCS -TMCF FUNCTIONAL DESCRIPTION -AUTOTHROTTLE  57  BEJ ALL 
CONTROL LAWS 
22-31-00  TMCS -TMCF FUNCTIONAL DESCRIPTION -THRUST LIMIT  62  BEJ ALL 
CALCULATION 
22-31-00  TMCS -TMCF FUNCTIONAL DESCRIPTION -ENGAGE LOGIC  64  BEJ ALL 
22-31-00  TMCS -FUNCTIONAL DESCRIPTION -A/T SERVO MOTOR  66  BEJ ALL 
22-31-00  TMCS -TMCF FUNCTIONAL DESCRIPTION -BITE AND FAULT  69  BEJ ALL 
MONITORING 
22-31-00  TMCS -SYSTEM TESTS  72  BEJ ALL 
22-31-00  TMCS -LRU REPLACEMENT TESTS  74  BEJ ALL 

22-CONTENTS
Page 5
D633W101-BEJ
Jan 05/2002

AUTOPILOT FLIGHT DIRECTOR SYSTEM -INTRODUCTION

General
The autopilot flight director system (AFDS) has two purposes. These purposes are:
*
To automatically control the airplane attitude

*
To supply indications so the flight crew can manually control the airplane attitude.

The flight crew uses the mode control panel (MCP) to select the mode of operation.
Autopilot
The autopilot controls the airplane attitude through:
*
Takeoff (flight director only)

*
Climb

*
Cruise

*
Descent

*
Approach

*
Go-around

*
Autoland.

The autopilot commands go to the primary flight computers (PFCs) to operate the flight control surfaces.
EFFECTIVITY BEJ ALL
Flight Director
When the flight director switches are on, the flight director command bars show on the primary flight displays (PFDs). The flight crew uses the flight director bars as guides to control the attitude of the airplane.
Abbreviations and Acronyms
*
A/P -autopilot

*
ACE -actuator control electronics

*
ADIRU -air data inertial reference unit

*
AFDC -autopilot flight director computer

*
AFDS -autopilot flight director system

*
AGS -air/ground system

*
AIMS -airplane information management system

*
alt -altitude

*
ASCPC -air supply cabin pressure controller

*
BAP -bank angle protect

*
BDA -backdrive actuator

*
bkdrv -backdrive

　
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