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�� In stabilized approach conditions, the flare height is approximately 40 ft:
FLARE ...................................................................................................................... PERFORM
ATTITUDE................................................................................................................... MONITOR
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - LANDING
A330/A340 FLEET PRO-NOR-SOP-22 P 12/16
FCOM 19 AUG 10
The PNF should monitor the attitude, and call out:
“PITCH PITCH”, ‐ if the pitch angle reaches 7.5 °
‐ “BANK BANK”, if the bank angle reaches 7 °.
THRUST lever ........................................................................................................................... IDLE
If autothrust is engaged, it automatically disconnects when the pilot sets all thrust lever to the IDLE
detent.
In manual landing conditions, the “RETARD” callout is triggered at 20 ft Radio Altitude (RA), in
order to remind the pilot to retard the thrust lever.
Note: If one or more thrust lever remain above the IDLE detent, ground spoilers extension is
inhibited.
Ground clearance
‐ Avoid flaring high
‐ A tailstrike occurs, if the pitch attitude exceeds 11 ° (landing gear compressed), 16 ° (landing
gear extended)
‐ A wingtip or engine scrape occurs, if the roll angle exceeds 17 °.
Applicable to:
AT TOUCHDOWN
REV.......................................................................................................................................... PULL
‐ Pull to reverse idle at main landing gear contact (not before)
‐ When REV green is indicated on ECAM, select MAX REV
‐ An interlock system on thrust reversers 1 and 4 prevents the two corresponding thrust lever
from being increased above idle reverse, until both 1 and 4 thrust reverser doors are fully open.
Select immediately thrust reversers 2 and 3
‐ In the case of an engine 2 or 3 failure, the flight crew should use the remaining thrust reversers
‐ If the airport regulations restrict the use of thrust reversers, select and maintain the thrust lever
in reverse idle position until taxi speed is reached
‐ Lower the nosewheel without undue delay
‐ The PNF continues to monitor the attitude
‐ Braking may begin before the nosewheel has touched down, if required for performance
reasons. However, when comfort is the priority, the flight crew should delay braking until the
nosewheel has touched down.
‐ During rollout, the flight crew should avoid sidestick inputs (either lateral or longitudinal).
If directional control problems are encountered, the flight crew should reduce thrust to reverse
idle until directional control is satisfactory.
‐ After reverse thrust is selected, the flight crew must perform a full stop landing.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - LANDING
A330/A340 FLEET PRO-NOR-SOP-22 P 13/16
FCOM 19 AUG 10
GROUND SPOILERS ......................................................................................CHECK/ANNOUNCE
Check that the ECAM WHEEL page displays the ground spoilers extended after touchdown.
If no ‐ ground spoilers are extended:
• Verify and confirm that all thrust lever are set to IDLE or REV detent
• Set all thrust reverser lever to REV MAX, and fully press the brake pedals.
Note: If ground spoilers are not armed, ground spoilers extend at reverser thrust selection.
REVERSERS ...................................................................................................CHECK/ANNOUNCE
Check that the ECAM E/WD page displays that the reverse deployment is as expected (REV
green).
DIRECTIONAL CONTROL.................................................................................................. ENSURE
‐ Use rudder pedals for directional control
‐ Do not use nose wheel steering control handle before reaching taxi speed.
BRAKES........................................................................................................................... AS RQRD
Monitor the autobrake, if it is on. When required, brake with the pedals.
Note: If no ground spoilers are extended, the autobrake is not activated.
DECELERATION.............................................................................................. CHECK/ANNOUNCE
The deceleration is felt by the flight crew, and confirmed by the speed trend on the PFD. The
deceleration may also be confirmed by the DECEL light (if autobrake is on).
Applicable to: ,
AT TOUCHDOWN
REV.......................................................................................................................................... PULL
　
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