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‐ during approach, from 1 300 ftto 50 ft
In both situations, the aircraft must be in configuration 1, 2, 3 or FULL.
WINDSHEAR DETECTION PRINCIPLES
Applicable to: ALL
The FACs generate the windshear warning whenever the predicted energy level for the aircraft falls
below a predetermined threshold.
In computing this energy level prediction, the FACs use data from different sources. From ADIRS
comes data such as vertical speed, air and ground speeds and slope ; from other sources come such
derived parameters as total slope, longitudinal wind gradient, and vertical wind.
The FACs express this energy level as an angle of attack and compare it with an angle-of-attack
threshold above which windshear conditions are most likely and pilot action is required.
GUIDANCE
Applicable to: ALL
In windshear conditions, flight guidance acts on specially adapted FD pitch orders received from the
speed reference system (SRS). The pilot must set go around thrust immediately (which also triggers
the FD SRS mode), and follow the pitch order to execute the optimum escape maneuver.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT AUGMENTATION
WINDSHEAR DETECTION FUNCTION
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OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT AUGMENTATION
CONTROLS AND INDICATORS
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FAC ENGAGEMENT
Applicable to: ALL
Refer to DSC-27-10-20-D YAW CONTROL - GENERAL
RUDDER TRIM OPERATION
Applicable to: ALL
Refer to DSC-27-10-20-D YAW CONTROL - GENERAL
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT AUGMENTATION
CONTROLS AND INDICATORS
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AIRCRAFT SYSTEMS
AUTO FLIGHT - AOC FUNCTIONS
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AIRCRAFT SYSTEMS
AUTO FLIGHT - AOC FUNCTIONS
PRELIMINARY PAGES - TABLE OF CONTENTS
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TABLE OF CONTENTS......................................................................................................................................1/2
GENERAL............................................................................................................................................................1/8
FLIGHT PLAN INITIALIZATION FUNCTION........................................................................................................1/8
TAKEOFF DATA FUNCTION............................................................................................................................. 3/8
WIND DATA FUNCTION.................................................................................................................................... 4/8
FLIGHT REPORTS............................................................................................................................................. 5/8
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - AOC FUNCTIONS
PRELIMINARY PAGES - TABLE OF CONTENTS
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - AOC FUNCTIONS
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GENERAL
Applicable to:
,
,
MSN,,,,
The FMS AOCS function gives an interface between a ground station and one onboard FMGC,
allowing data transmission between these two computers via the ACARS Management Unit or the
ATSU.
Two different sets of message can be exchanged:
UPLINK messages from the ground station. They consist in reception of data requested or directly
sent to the crew.
DOWNLINK messages from the FMGC (master). They consist in reports or requests sent to the
ground station.
The FMGS/ACARS or FMGS/ATSU interface enables the following AOC capabilities.
‐ F-PLN initialization (flight plan and performance data)
‐ Takeoff data
‐ Wind data
‐ Flight reports
‐ Broadcast data
Crews can send message using ACARS FUNCTION pages or relevant MCDU pages.
Only one FMGC talks to the ground station. This FMGC is called FMGC “master”.
GENERAL SCRATCHPAD MESSAGES
NOT XMITTED TO ACARS: A crew request or report was sent to the ground but the
communication was not established or not acknowledged.
　
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