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CAUTION The characteristic speeds displayed on the MCDU (green dot, F, S, VLS) are
computed from the ZFW and ZFWCG entered by the crew on the MCDU.
Therefore, this data must be carefully checked (Captain’s responsibility).
‐ The flight crew should insert the weights after completing all other insertions. This is to avoid
cycles of prediction computations at each change in flight plan, constraints, etc.
‐ If ZFW and ZFWCG are unavailable, it is acceptable to enter the expected values in order to
obtain predictions. Similarly, the flight crew may enter the expected fuel on board, if refueling
has not been completed at that time.
‐ If ZFW, ZFWCG, and BLOCK FUEL are inserted, the FM will provide all predictions, as well as
the EXTRA fuel, if any.
Applicable to: ALL
TAKEOFF DATA INSERTION (PERF TAKEOFF SD page):
* V1, VR, V2.........................................................................................................................INSERT
* FLX TO TEMP................................................................................................................... INSERT
* THR RED/ACC altitude......................................................................................... SET or CHECK
For noise abatement procedure, the crew must set the acceleration altitude at, or above, 3 000 ft,
and adjust the values according to local noise abatement regulations.
* ENG OUT ACC altitude.........................................................................................SET or CHECK
* FLAPS/THS reminder........................................................................................................ INSERT
* TO SHIFT.......................................................................................................................AS RQRD
Enter the takeoff SHIFT distance, if takeoff is to be from an intersection. This is essential for
position updating at takeoff and, consequently, for navigation accuracy.
Applicable to:
MSN,,,
RNP INSERTION(PROG PAGE):
* RNP....................................................................................................................... SET or CHECK
For RNP AR departure, check or insert the RNP.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - COCKPIT PREPARATION
A318/A319/A320/A321 FLEET PRO-NOR-SOP-06 P 17/22
FCOM 19 AUG 10
Applicable to: ALL
CLIMB, CRUISE, DESCENT, SPEED PRESELECTION
* PRESET SPEEDS..........................................................................................................AS RQRD
If the flight is cleared for a close-in turn or close-in altitude constraint, the flight crew may preselect
green dot speed on the PERF CLB page. Once the CLB phase is active, the preselected speed
will be displayed in the FCU speed window and on the PFD (blue symbol). Once the turn is
completed or the altitude cleared, the pilot will resume the managed speed profile by pressing the
SPD selector on the FCU.
Similarly the pilot may select a CRZ MACH number on the PERF CRZ page (constant CRZ Mach
segment, for example). When the CRZ phase is active, the preselected CRZ MACH number will
be displayed in the FCU speed window and on the PFD. When ECON MACH number may be
resumed, the crew presses the FCU SPD selector.
In either of the above cases, the pilot may cancel the CLB or CRZ preselected SPD/MACH prior to
activating the related phase, by selecting ECON on the PERF CLB or CRZ pages.
SPD LIM is defaulted to 250 kt below 10 000 ft in the managed speed profile. This may be either
cleared or modified on the VERT REV page at the origin (or a climb waypoint).
GLARESHIELD
Applicable to: ALL
LIGHTING
Glareshield integral light selector and flood light pb-sw.....................................................AS RQRD
Applicable to:
EFIS CONTROL PANEL
BARO REF.................................................................................................................................SET
Set QNH (or QFE) on the EFIS control panel ‐ and on the standby altimeter
‐ Check barometer settings and altitude indications on the PFD and standby altimeter.
(Tolerance limits are given in Refer to PRO-SUP-34-B FLIGHT INSTRUMENT TOLERANCES
- GENERAL).
* FD.............................................................................................................................. CHECK ON
* ILS................................................................................................................................ AS RQRD
Note: Do not engage the autothrust on ground, as it may generate the AUTO FLT A/THR OFF
warning at engine start.
A318/A319/A320/A321 FLIGHT CREW
　
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