曝光台 注意防骗
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positions.
Rudder pedals override disconnects the autopilot.
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AUTO FLIGHT SYSTEM CONTROL AND INDICATING - THRUST LEVERS, SIDE STICKS & RUDDER PEDALS
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AUTO FLIGHT SYSTEM CONTROL AND INDICATING
RESETS
The FMGC, FAC, FCU and MCDU resets are possible in the
cockpit.
Depending on the computer (1 or 2), the circuit
breakers are located either on the overhead circuit
breakers panel 49VU or on the rear circuit breakers
panel 121VU.
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AUTO FLIGHT SYSTEM CONTROL AND INDICATING
RMPs
The Radio Management Panels (RMPs) are located on the
center pedestal near Multipurpose Control and Display
Units 1 and 2.
The RMPS are used for navaid standby selection.
EWD/SD
The Engine/Warning Display (EWD) and the System Display
(SD) are located on the main instrument panel.
The EWD displays AFS warning messages.
The SD displays AFS information such as inoperative
systems on the STATUS page or landing capabilities
availability.
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AUTO FLIGHT SYSTEM CONTROL AND INDICATING
ATTENTION GETTERS
The attention getters are located on the glareshield
panel on the Capt and F/O sides.
The MASTER CAUTION and/or the MASTER WARNING are
activated when an AFS disconnection occurs.
The AUTOLAND warning is activated when a problem occurs
during final approach in automatic landing.
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22 - AUTO FLIGHT SYSTEM
22-00-00 BASIC OPERATIONAL PRINCIPLES
CONTENTS:
General
Data Base Loading
Power-up Test FD Engagement
MCDU Initialization
A/THR Engagement
AP Engagement
Self Examination
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BASIC OPERATIONAL PRINCIPLES
GENERAL
This sequence describes the operational use of the
Flight Management and Guidance Computers (FMGCs) in a
normal operation with a total availability of the
concerned functions.
The short-term pilot orders are entered through the
Flight Control Unit (FCU). The long-term pilot orders
are entered through the Multipurpose Control and
Display Unit (MCDU).
Four key-words for the control principle and both types
of guidance are to be kept in mind in order to avoid
handling errors.
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