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is entered, an aural warning “minimums,
minimums” is heard when the DH is reached.
If MDA is entered, the digits in the PFD altitude
window turn amber when the aircraft is below
this altitude.
LDG CONF (4R, 5R)
The pilot can choose the flap landing
configuration here. By default, FULL is
selected (written in big characters) and CONF
3 is selectable (shown with a *).
This choice determines the content of the
landing check-list that will display the
required flap configuration when the aircraft is
close to land.
Note that if you select the CONF 3, you will still
have a GPWS warning “too low, flaps” when
the aircraft gets close to the ground. To avoid
this, press the GPWS flap button on the
overhead (refer to the system section for more
information about the GPWS).
NEXT PHASE (6R)
Displays the PERF GO AROUND page.
F, S, O Speeds
In the center of the page, the F, S and Green
Dot speeds are displayed. They can be
calculated only when the Gross Weight (GW) is
defined (INIT B page). They can not be
modified by the crew.
PERF GO AROUND PAGE
This page lets the crew set the aircraft ready
for a possible go around.
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Airbus Series Vol.1
92 For Microsoft Flight Simulator use only. Not for use in real aviation.
THR RED/ACC (5L)
Like on the PERF TAKE OFF page, this field
lets the crew select the thrust reduction
altitude and the acceleration altitude in case of
a go around. Remember that the acceleration
altitude must be equal or greater than the
thrust reduction altitude.
ENG OUT ACC (5R)
This is the altitude at which you should
accelerate if an engine is out.
F, S, O Speeds
In the center of the page, the F, S and Green
Dot speeds are displayed. They can be
calculated only when the Gross Weight (GW) is
defined (INIT B page). They can not be
modified by the crew.
FUEL PRED PAGE
This page is accessible by pressing the FUEL
PRED key on the MCDU. It allows you to enter
flight information like on the INIT B page. It is
especially useful if you forgot to enter data in
the INIT B page and the engines are started
(the INIT B page is accessible only when the
engines are stopped).
AT (1L)
This is a reminder of the destination airport. It
is not modifiable by the crew.
GW / CG (3L)
This field contains the Gross Weight and the
center of gravity. The gross weight information
is mandatory, so amber boxes appear here if
this information is not available.
RTE RSV / % (4L)
This field is exactly the same as the one shown
on the INIT B page.
FINAL / TIME (5L)
This field is exactly the same as the one shown
on the INIT B page.
EXTRA / TIME (6L)
This field is exactly the same as the one shown
on the INIT B page.
Refer to the INIT B page section for more
information about these fields.
EFOB (1R)
This is the fuel prediction at destination. It is
not modifiable by the crew.
FOB (3R)
This field allows the crew to enter a FOB (Fuel
On Board) quantity. You should be very
cautious when enter a value here because it
can make the fuel predictions wrong. It can be
used only when engines are stopped. As soon
as engines are started, the FOB information is
acquired from the fuel sensors again.
In addition, you have the ability to define how
the FOB quantity is computed:
- FF + FQ: the fuel flow and the fuel quantity
sensors are used
- FF: the fuel flow sensors are used only
- FQ: the fuel quantity sensors are used only
CRZ TEMP/TROPO (4R)
This field displays the temperature at the
cruise altitude and the tropopause altitude.
Both values can be modified by the crew.
PROG PAGE
The PROG page is a multifunction page.
The title is composed of the current flight
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phase (TO for takeoff, CLB, CRZ, DES or APPR)
and the flight number.
CRZ (1L)
This field displays the current cruise altitude.
The crew can modify this value to change the
cruise altitude during the flight (it is the only
way to do this as the INIT page is not
accessible during the flight).
This field is empty when the aircraft is in
descent or approach phase.
SEND POS (2L)
Pressing this key sends a position report.
UPDATE AT (3L)
This field allows the crew to update the IRS
position with a navaid position. This function is
not implemented in this aircraft because its
position is updated by the GPS.
　
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