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2. The FADEC includes a keep-out zone, which is designed to avoid steady state
operation inside a N1 range between 60 % and 74 % due to fan flutter phenomenon.
This can result in discontinuous EPR increase during thrust setting (Refer to
DSC-70-20 FUNCTIONS ).
DIRECTIONAL CONTROL......................................................................................... USE RUDDER
At 130 kt (wheel speed), the connection between nosewheel steering and the rudder pedals
is removed. Therefore, in strong crosswinds, more rudder input will be required at this point to
prevent the aircraft from turning into the wind.
CHRONO...............................................................................................................................START
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - TAKEOFF
A318/A319/A320/A321 FLEET PRO-NOR-SOP-12 P 3/10
FCOM 19 AUG 10
PFD/ND................................................................................................................................... SCAN
1. Check the FMA on the PFD. The following modes are displayed: MAN TOGA (or MAN FLX xx)
/SRS/RWY (or blank) / A/THR (in blue).
Note: If an ILS that corresponds to the departure runway is tuned, RWY mode appears. If
not, no lateral mode appears until the aircraft lifts off.
2. Check the FMS position on the ND (aircraft on runway centerline).
Note: If GPS PRIMARY is not available, check the FMS position update.
FMA.............................................................................................................................. ANNOUNCE
Applicable to:
,
,
MSN
THRUST SETTING
�� If the crosswind is at or below 20 kt and there is no tailwind:
THRUST LEVERS................................................................................................. FLX or TOGA
‐ To counter the nose-up effect of setting engine takeoff thrust, apply half forward stick until
the airspeed reaches 80 kt. Release the stick gradually to reach neutral at 100 kt.
‐ PF progressively adjusts engine thrust in two steps:
• from idle to about 50 % N1 (1.05 EPR).
• from both engines at similar N1 to takeoff thrust.
▪ Once the thrust levers are set to FLX or TOGA detent, the captain keeps his hand on
the thrust levers until the aircraft reaches V1.
�� In case of tailwind or if crosswind is greater than 20 kt:
THRUST LEVERS................................................................................................. FLX or TOGA
‐ PF applies full forward stick.
‐ PF sets 50 % N1 (1.05 EPR) on both engines then rapidly increases thrust to about 70 %
N1 (1.15 EPR) then progressively to reach takeoff thrust at 40 kt ground speed, while
maintaining stick full forward up to 80 kt. Release stick gradually to reach neutral at 100 kt.
‐ Once the thrust levers are set to FLX or TOGA detent, the captain keeps his hand on the
thrust levers until the aircraft reaches V1.
Note: ENG SD page replaces WHEEL SD page on the ECAM lower display.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - TAKEOFF
A318/A319/A320/A321 FLEET PRO-NOR-SOP-12 P 4/10
FCOM 19 AUG 10
DIRECTIONAL CONTROL......................................................................................... USE RUDDER
At 130 kt (wheel speed), the connection between nosewheel steering and the rudder pedals
is removed. Therefore, in strong crosswinds, more rudder input will be required at this point to
prevent the aircraft from turning into the wind.
CHRONO...............................................................................................................................START
PFD/ND................................................................................................................................... SCAN
1. Check the FMA on the PFD. The following modes are displayed: MAN TOGA (or MAN FLX xx)
/SRS/RWY (or blank) / A/THR (in blue).
Note: If an ILS that corresponds to the departure runway is tuned, RWY mode appears. If
not, no lateral mode appears until the aircraft lifts off.
2. Check the FMS position on the ND (aircraft on runway centerline).
Note: If GPS PRIMARY is not available, check the FMS position update.
FMA.............................................................................................................................. ANNOUNCE
Applicable to:
, ,
MSN
BEFORE REACHING 80 KT

　
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