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in the F-PLN and the aircraft is 30 s before the deceleration point to the
precomputed HOLD SPEED.
DECELERATE White This message is displayed if the thrust is not reduced when passing the top
of descent and the aircraft is above the descent profile.
MORE DRAG White DES mode is engaged, idle is selected, and either:
‐ The aircraft is above the vertical profile and the predicted intercept point
of the theoretical profile is at less than 2 nm from the next ALT CSTR, or
‐ In auto speed control and the aircraft enters a speedbrake decelerating
segment.
VERT DISCON AHEAD Amber DES mode is engaged and:
‐ A TOO STEEP path exists on the next leg
‐ The aircraft is less than 30 s from the TOO STEEP path.
SPECIAL MESSAGES (FMA COLUMNS 2 AND 3)
Applicable to:
,
,
MSN,,,,
The third line displays three types of messages:
‐ It gives first priority to Flight Control messages
‐ It gives second priority to vertical Flight Management messages
‐ It gives last priority to EFIS reconfiguration messages.
DISPLAY COLOR MEANING
MAN PITCH TRIM ONLY Red Displayed in case of loss of L+R elevators.
USE MAN PITCH TRIM Amber F/CTL are in direct law.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
FLIGHT MODE ANNUNCIATOR (FMA)
A318/A319/A320/A321 FLEET DSC-22_30-100 P 11/12
FCOM 19 AUG 10
Continued from previous page
DISPLAY COLOR MEANING
CHECK APP SEL White The aircraft is in cruise at less than 100 nm from the Top of Descent or in
descent or in approach and:
‐ A non-ILS approach has been selected
‐ An ILS frequency is tuned on the MCDU RAD NAV page.
SET MANAGED SPD White The SPEED target is selected but a preselected SPEED does not exist for
the next flight phase.
SET GREEN DOT SPD White The aircraft is in Engine Out mode and the SPEED target is selected. This
message is displayed if the FCU selected speed is:
≤ Green Dot -10 kt, or
≥ Green Dot +10 kt, except in ALT* and ALT mode.
SET HOLD SPD White The aircraft is in selected SPEED control, a Holding pattern is inserted
in the F-PLN and the aircraft is 30 s before the deceleration point to the
precomputed HOLD SPEED.
DECELERATE White This message is displayed if the thrust is not reduced when passing the top
of descent and the aircraft is above the descent profile.
MORE DRAG White DES mode is engaged, idle is selected, and either:
The aircraft is above the vertical profile and the predicted ‐ intercept point
of the theoretical profile is at less than 2 nm from the next ALT CSTR, or
‐ In auto speed control and the aircraft enters a speedbrake decelerating
segment.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
FLIGHT MODE ANNUNCIATOR (FMA)
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-22_30-100 P 12/12
FCOM 19 AUG 10
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT AUGMENTATION
Intentionally left blank
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT AUGMENTATION
PRELIMINARY PAGES - TABLE OF CONTENTS
A318/A319/A320/A321 FLEET DSC-22_40-PLP-TOC P 1/2
FCOM 19 AUG 10
DSC-22_40-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
DSC-22_40-10 GENERAL
GENERAL............................................................................................................................................................1/2
DSC-22_40-20 YAW FUNCTIONS
YAW DAMPING.................................................................................................................................................. 1/2
RUDDER TRIM................................................................................................................................................... 1/2
RUDDER TRAVEL LIMITATION.........................................................................................................................1/2
DSC-22_40-30 FLIGHT ENVELOPE FUNCTION
GENERAL............................................................................................................................................................1/6
PFD SPEED SCALE MANAGEMENT..................................................................................................................1/6
ALPHA-FLOOR PROTECTION.......................................................................................................................... 3/6
LOW- ENERGY WARNING................................................................................................................................ 4/6
　
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