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maximum reverse thrust.
Do not hold the nose wheel off the ground.
‐ If necessary, the maximum reverse thrust can be used until the aircraft is fully stopped.
‐ If the runway length is limiting, apply the brakes before lowering the nose gear onto the runway,
but be prepared to apply back stick to counter the nose down pitch produced by the brakes
application. (The strength of this pitching moment will depend on the brake torque attainable on
the slippery runway).
‐ Maintain directional control with the rudder as long as possible, use nose wheel steering with care.
‐ When the aircraft is at taxi speed, follow the recommendations for taxiing.
Note: If there is snow, visibility may be reduced by snow blowing forward at low speeds if
reversers are not cancelled.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ADVERSE WEATHER - FLUID CONTAMINATED RUNWAY
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A318/A319/A320/A321 FLEET PRO-SUP-91-50 P 4/4
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
LESS PAPER IN THE COCKPIT
A318/A319/A320/A321 FLEET PRO-SUP-92 P 1/8
FCOM 19 AUG 10
INTRODUCTION
Applicable to: ALL
The Less Paper Cockpit (LPC) concept consists of a complete set of software tools, designed to :
‐ Improve access to pilot’s operational information, and simplify some of their tasks.
‐ Reduce the quantity of paper documents in the cockpit, and replace them with electronic ones,
enabling quicker and easier updates, while improving information retrieval.
The applicable areas include Performance and Weight and Balance computations, in addition
to technical operational documentation (FCOM, MEL, Operations Policy Manual..). This section
addresses the procedures corresponding to the modules which are already available.
The various modules are linked via F.O.V.E. (Flight Operations Versatile Environment), which is
designed to provide an interface between the various modules by enabling :
‐ Inter-module communication
‐ Software compatibility management
‐ Software version management
‐ Integrity control between data and the software versions
‐ Update management
‐ Context management
Each airline may choose to install one or several modules, each of which is able to work
independently.
GENERAL
Applicable to: ALL
LPC PROGRAM AND REFERENCE VERSION NUMBER UPDATING
Each pilot should check that the version of F.O.V.E, installed on their PC, corresponds to the latest
updated version provided by their airline’s Flight Operations.
POWER SUPPLY
Check that each available PC is electrically-supplied.
PC STOWAGE DURING TAKEOFF AND LANDING
Pilot PCs should be unplugged and stowed during takeoff and landing.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
LESS PAPER IN THE COCKPIT
A318/A319/A320/A321 FLEET PRO-SUP-92 P 2/8
FCOM 19 AUG 10
LPC TAKEOFF MODULE
Applicable to: ALL
GENERAL
The takeoff module is designed to provide aircraft takeoff performance, based on actual daily
environmental conditions, just prior to flight. It allows straightforward computations, and provides
the best takeoff performance for the given conditions.
Applicable to: ALL
TAKEOFF PERFORMANCE TASKSHARING
The tasksharing policy for data computation, and introduction in the MCDU is consistent with the
currently applicable policy, as per the SOP :
One pilot performs the computation, then introduces the resulting data in the MCDU.
The other pilot checks the :
‐ Computation by using the PC to verify that the entered data is correct.
‐ Data entered in the MCDU.
Data entry and computation are generally done by the PF, and checked by the PNF. These tasks
can be swapped, as per company policy, or as circumstances dictate. For instance, during taxi,
data entry and computation should be done by the PNF, since the PF is busy taxiing the aircraft.
The PF will then have to perform the check, by stopping the aircraft or, if a stop is not possible, by
transferring command to the other pilot.
Applicable to:
COCKPIT PREPARATION
TAKEOFF DATA COMPUTATION
The PF checks that the version of F.O.V.E, available on the PC, is the applicable one. (The
applicable version is indicated on the computerized F-PLN, or other document, as per airline
policy).
The PF enters the data, then shows the screen to the PNF for data confirmation.
If the Weight and Balance module is to be used:
Use the pilot’s PC to compute the ZFCG and ZFW:
The computed values will be automatically fed to the takeoff performance module.
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