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Flight Crew Operating Manual
CSP C--013--067
The autopilot can be disengaged manually by any of the following:
S Pushing either AP/SP DISC switch on the control wheels
S Pushing the AP ENG switch on the flight control panel
S Lowering the AP DISC switch-bar on the flight control panel (a red line becomes visible)
S Operating either stabilizer trim switch on the control wheels
S Pressing either TOGA switch on the thrust levers
S Pressing the yaw damper DISC pushbutton on the yaw damper panel
Disengagement of the autopilot causes a cavalry charge aural alert and the AP indication on
the primary flight display (PFD) to turn red. The autopilot disengage warning will
automatically cancel, after approximately two repetitions of the cavalry charge, when a
disengagement is mutually induced.
Automatic disengagement of the autopilot occurs:
S If both yaw dampers are disengaged or fail
S If a failure condition is detected by the FCC monitoring circuits
S If a stall warning occurs
S During windshear avoidance procedures
The autopilot is automatically disengaged two seconds after a windshear warning (if the
autopilot has not already been disengaged). During those two seconds, the autopilot will
follow the windshear commands.
In the event that the autopilot is disengaged due to a system fault, pressing the AP/SP DISC
switch or either TOGA switch will cancel the red flashing AP indication on the PFD and
silence the aural warning.
The automatic flight control system monitors both axes of the autopilot when engaged. If a
control surface is detected to be significantly out of trim, an indication will appear on the PFD
and a caution message will be displayed on the EICAS primary page to indicate in which
direction that the control surface is out of trim.
Vol. 1 03--30--6
AUTOMATIC FLIGHT CONTROL SYSTEM
Autopilot REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Autopilot --- PFD Flags <1015>
Figure 03---30---4
Primary Flight Display
Pilot’s and Copilot’s Instrument Panels
Aileron Mistrim Indicator (yellow)
Iindicates that the ailerons are in a
mistrim condition, when the autopilot
is engaged.
Elevator Mistrim Indicator (yellow)
Indicates that the horizontal stabilizer
is in a mistrim condition, when the
autopilot is engaged.
Vol. 1 03--30--7
AUTOMATIC FLIGHT CONTROL SYSTEM
Autopilot REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Autopilot --- EICAS Messages <1001>
Figure 03---30---5
AP PITCH TRIM caution (amber)
Indicates that autopilot pitch trim has failed.
Primary Page
Vol. 1 03--30--8
AUTOMATIC FLIGHT CONTROL SYSTEM
Autopilot REV 1, Jan 13/03
Flight Crew Operating Manual
CSP C--013--067
THIS PAGE INTENTIONALLY LEFT BLANK
Vol. 1 05--00--1
COMMUNICATIONS
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
CHAPTER 5 --- COMMUNICATIONS
Page
TABLE OF CONTENTS 05--00
Table of Contents 05--00--1
INTRODUCTION 05--10
Introduction 05--10--1
AUDIO INTEGRATING SYSTEM 05--20
Audio Integrating System 05--20--1
Audio Control Panels 05--20--1
Ground Crew Interphone 05--20--5
Attendant’s Handset 05--20--6
Passenger Address System 05--20--8
Intercom Control Panel 05--20--8
Passenger Service Units 05--20--9
System Circuit Breakers 05--20--9
ANNOUNCEMENT AND BOARDING MUSIC SYSTEM 05--25
Announcement and Boarding Music System <1035> 05--25--1
System Circuit Breakers 05--25--2
RADIO COMMUNICATION SYSTEM 05--30
Radio Communication System 05--30--1
Radio Tuning Unit 05--30--1
Backup (Standby) Tuning Unit 05--30--4
System Circuit Breakers 05--30--5
LIST OF ILLUSTRATIONS
AUDIO INTEGRATING SYSTEM
Figure 05--20--1 Passenger Address System Interface Diagram 05--20--2
Figure 05--20--2 Audio Control Panel 05--20--3
Figure 05--20--3 Pilot’s Control Wheel(Copilot’s opposite) 05--20--4
Figure 05--20--4 GND Crew Interphone 05--20--5
Figure 05--20--5 Attendant’s Handset 05--20--7
Figure 05--20--6 CKPT Intercom Control Panel 05--20--9
ANNOUNCEMENT AND BOARDING MUSIC SYSTEM
Figure 05--25--1 Announcement and Boarding Music System <1035> 05--25--2
Vol. 1 05--00--2
COMMUNICATIONS
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
RADIO COMMUNICATION SYSTEM
Figure 05--30--1 VHF Communication Interface 05--30--2
Figure 05--30--2 Radio Tuning Unit 05--30--3
Figure 05--30--3 BackupTuning Unit 05--30--4
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