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results.
S LRU Rigging -- Used to initiate the LRU programing procedure.
S System Parameters -- Displays airplane system parameters.
S ATA Index -- Displays list of ATA chapter numbers for all aircraft and avionics
systems.
S LRU Index/Operations -- Displays a list of LRUs and is used to select any associated
test or rigging procedure.
S MDC Setup -- Used to set aircraft identification and clock. Also used to load files.
S Configuration Data -- Used to access the configuration of the integrated avionics
processor system (IAPS) computers and to check the MDC version information.
S FCC Diagnostic -- Displays instructions to put flight control system into diagnostic
mode.
AURAL/VISUAL INDICATING AND Vol. 1 02--40--4
RECORDING
Maintenance Data Computer REV 1, Jan 13/03
Flight Crew Operating Manual
CSP C--013--067
Maintenance Main Menu EICAS Page
Figure 02---40---2
Maintenance Main Menu Page
Multifunction Display
AURAL/VISUAL INDICATING AND Vol. 1 02--40--5
RECORDING
Maintenance Data Computer REV 1, Jan 13/03
Flight Crew Operating Manual
CSP C--013--067
MDC Fault Indication
Figure 02---40---3
Status Page
MDC FAULT status (white)
Indicates that a fault has been
detected in the MDC.
AURAL/VISUAL INDICATING AND Vol. 1 02--40--6
RECORDING
Maintenance Data Computer REV 1, Jan 13/03
Flight Crew Operating Manual
CSP C--013--067
B. Data Loader Unit
The data loader unit is located in the top of the forward entrance compartment.
Through the download function from the MENU page, the unit enables the transfer of
data files, between DOS-compatible diskettes and applicable aircraft systems. The
data loader unit provides the capability to format disks, read directories and read/write
files. <1018>
Data Loader Unit <1018>
Figure 02---40---4
Diskette Eject
Used to eject
diskette from
disk drive.
FAIL Indicator (red)
POWER Indicator (green) Indicates disk drive failure.
Indicates that power to disk
drive is available.
Drive In--Use Indicator
Indicates that data are
being read from or
written to diskette.
Disk Drive
Used to upload / download
MDC / FMS data
Data Loader Unit
NOTE
Indicators are not dimmable.
C. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Maintenance Data Loader DATA LOAD DC BUS 1 1 H10
Data
Computer MDC IAPS L AFCS
/ MDC
BATTERY
BUS 2 P6
Vol. 1 03--00--1
AUTOMATIC FLIGHT CONTROL SYSTEM
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
CHAPTER 3 --- AUTOMATIC FLIGHT CONTROL SYSTEM
Page
TABLE OF CONTENTS 03--00
Table of Contents 03--00--1
INTRODUCTION 03--10
Introduction 03--10--1
FLIGHT CONTROL AND GUIDANCE 03--20
Flight Control and Guidance 03--20--1
Flight Director 03--20--2
Synchronization 03--20--7
Flight Mode Annunciator 03--20--8
Lateral Modes of Operation 03--20--9
Vertical Modes of Operation 03--20--12
Altitude Alert System 03--20--16
System Circuit Breakers 03--20--18
AUTOPILOT 03--30
Autopilot 03--30--1
LIST OF ILLUSTRATIONS
FLIGHT CONTROL AND GUIDANCE
Figure 03--20--1 Flight Control Panel -- Layout 03--20--1
Figure 03--20--2 Flight Director -- Schematic 03--20--3
Figure 03--20--3 Flight Director -- Controls and Indications 03--20--5
Figure 03--20--4 Course Pointer Control and Indication 03--20--6
Figure 03--20--5 FD Synchronization 03--20--7
Figure 03--20--6 Flight Mode Annunciator 03--20--8
Figure 03--20--7 AFCS EICAS Indications 03--20--17
AUTOPILOT
Figure 03--30--1 Autopilot -- Schematic 03--30--2
Figure 03--30--2 Autopilot -- General 03--30--3
Figure 03--30--3 Autopilot -- Controls 03--30--4
Figure 03--30--4 Autopilot -- PFD Flags 03--30--6
Figure 03--30--5 Autopilot -- EICAS Messages 03--30--7
Vol. 1 03--00--2
AUTOMATIC FLIGHT CONTROL SYSTEM
Table of Contents Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
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Vol. 1 03--10--1
AUTOMATIC FLIGHT CONTROL SYSTEM
Introduction Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
1. INTRODUCTION
The automatic flight control system (AFCS) provides integration of the autopilot and flight
director systems. The system consists of two interlinked flight control computers, an
autopilot, two yaw dampers, automatic elevator trim control and assorted servos and
actuators.
The flight control computer receives mode selections from the flight control panel and sensor
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