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or cruise if selected speed is active. It is not displayed if
managed speed is active.
SET HOLD SPEED
(also displayed on PFD)
II/A
(W)
This instruction appears when the aircraft is in selected
speed, the pilot has inserted a hold in the flight plan, the
aircraft is 30 s or less from the point where it must start
decelerating toward hold speed, and the selected speed
differs from the hold speed by more than 5 kt.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT MANAGEMENT
CONTROLS AND INDICATORS - MCDU - MESSAGES
A318/A319/A320/A321 FLEET DSC-22_20-50-20-30 P 7/8
FCOM 19 AUG 10
Continued from previous page
MESSAGE TYPE/COLOR CONDITIONS
SET VFTO
􀀋″RDS􀀃FQDDM􀀃CNS″􀀃chrok􀁄xdc􀀃nm
PFD)
II/A
(W) This message appears when the following conditions are all
met :
‐ Engine-out condition
‐ Climb phase
‐ Aircraft in selected speed mode
‐ FCU-selected speed equal to or greater than green-dot
speed +10 kt, and ALT* or ALT not active, or FCU-selected
speed equal to or less than green-dot speed -10 kt.
SPECIF NDB UNAVAIL II/A The NDB to be autotuned (specified for a NDB approach) has
been deselected.
SPECIF VOR-D UNAVAIL
(also displayed on ND)
II/A The VOR, VOR-DME, or VORTAC to be autotuned (specified
for an RNAV or VOR approach) has been deselected.
SPD ERROR AT WPTXX II/W In lateral managed flight, the system predicts that the aircraft
will miss a speed constraint by more than 10 kt. When the
prediction changes to bring the miss within 5 kt, the message
is cleared.
SPD LIM EXCEEDED II/A The aircraft is more than 300 ft below the speed limit altitude
and more than 10 kt over the speed limit.
STEP ABOVE MAX FL II/W The pilot has entered a step altitude that is above the
predicted maximum altitude.
STEP DEFINED AT WPTXX II/W The system has a step in it and the step prediction page is
called up at a revise point other than that where the step is
defined.
STEP DELETED II/W A step has been deleted due to :
‐ an engine out or
‐ the insertion of another step or
‐ a prediction that the step cannot be flown (too near the top
of descent).
STORED ROUTE FULL I/W The system already contains three pilot-defined routes. (Only
three are allowed.)
SYSTEM RNP IS XX.X �� II/A Displayed when the RNP value, manually entered in the
PROG page is larger than the RNP value associated with
the current flight area (FMGS default value, Refer to 99
Duref Cible FCOM). It is also displayed when the RNP value
associated to the current flight area becomes smaller than the
manually entered RNP value.
TAKEOFF DATA UPLINK ��
(ACARS msg)
II/W A takeoff data message is received.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT MANAGEMENT
CONTROLS AND INDICATORS - MCDU - MESSAGES
A318/A319/A320/A321 FLEET DSC-22_20-50-20-30 P 8/8
FCOM 19 AUG 10
Continued from previous page
MESSAGE TYPE/COLOR CONDITIONS
TMPY F-PLN EXISTS I/W The flight crew has selected any LS key (except ERASE
or INSERT) or attempted a flight planning operation on
the secondary flight plan while the system is displaying a
temporary flight plan.
TIME CSTR DELETED �� II/W A time constraint is deleted automatically, or the flight crew
enters a second time constraint, deleting the first one.
TIME CSTR EXISTS �� I/W The crew attempts to clear an ETT (estimated takeoff time)
computed by the FMGS.
TIME ERROR AT WPTXX �� II/W While the aircraft is not airborne, or is airborne and in NAV
mode, the FMGC predicts that it will miss a time constraint by
more than two minutes.
TIME TO EXIT II/A The aircraft must leave holding immediately to satisfy fuel
reserve requirements. (Extra fuel is zero).
TOO STEEP PATH AHEAD II/A The system displays this message in cruise phase if the
aircraft is within 150 nm of its destination or in descent or
approach phase and in NAV mode and the descent profile
contains a segment that is too steep.
TUNE BBB FFF.FF II/A The system cannot autotune the VOR for approach or position
because of a manual VOR selection.
UNKNOWN PROGRAM PIN II/W The system has been unable to initialize because of an
incompatible or undefined aircraft pin program combination
(A/C type, engine type, VMO/MMO parity) in the FMGC
software.
UPLINK INSERT IN PROG ��
(ACARS msg)
II/W Displayed when an uplink message is currently inserted in the
　
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