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· ILS course not checked at "LAND" green.
· Autopilot not disengaged at end of roll out.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.02.21 Page 4
REV 21 MAY 98
NORMAL OPERATION BRIEFINGS
PRECISION APPROACHES
CAT II - CAT III
CHAP02\21
01 - TRAINING OBJECTIVE
· To land the aircraft in a safe manner.
· To decelerate the aircraft after landing using appropriate combination of reverse thrust and
manual or auto wheel brakes.
02 - SCHEDULE
Briefing duration : 10 minutes
03 - EQUIPMENT
DOC references :
· FCOM 1.32.30 (Brakes and anti-skid)
· FCOM 1.70.70 (Thrust reverser system)
· FCOM 3.01.40 (Limitations)
· FCOM 3.03.18 (SOPs)
· FCOM 3.03.22 (SOPs)
· FCOM 3.04.27 (Supplementary techniques)
04 - INSTRUCTOR’S ACTIONS
Briefing of the following key points.
MAIN
· Flare at correct height.
· Crosswind landing technique.
· Awareness of possible tailstrike (especially A321).
· Selection of idle thrust and standard use of reverse thrust.
· Normal use of autobrake system and related indications.
· Manual braking and directional control techniques.
· Brake and reverser limitations.
· Actions in case of abnormal braking behavior.
· Conditions for spoiler deployment.
SECONDARY
· Flight controls flare mode.
· Possible pitch up with spoiler deployment.
· Brake and anti-skid indications on SD WHEEL page.
· Recommendations for use of autobrakes.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.02.22 Page 1
REV 21 MAY 98
NORMAL OPERATION BRIEFINGS
LANDING
- LANDING AND STOPPING THE A/C -
CHAP02\22
05 - TRAINEES’ ACTIONS
As a basic rule for all approaches, no later than 1 000 ft AGL, the PF should have one hand
on the THRUST LEVERS and the other one on the side stick. This should apply regardless
of AP - ATHR selection.
During the final visual segment of the approach it is very important not to over control with
the sidestick. The aircraft will maintain pitch and roll attitudes resisting any atmospheric
disturbance until 50 ft when landing mode becomes active (FCOM 3.04.27 [Supplementary
Techniques - Flight Controls]). Landing mode is only a pitch mode and roll control is the
same as normal law until the wheels are on the ground.
At approximately 20 ft the aircraft should be progressively flared and the thrust levers
selected to idle. Due to the engagement of landing mode in pitch it is necessary to make a
progressive pull on the sidestick in order to increase the pitch angle in the flare. The ’Retard’
call at 20 ft is a reminder to retard the thrust levers to idle if they have not already been
retarded.
For crosswind landing techniques read the briefing given in FCOM bulletin number 21 (blue
pages in FCOM 3).
At touch down the ground spoilers will deploy automatically which may give a slight pitch up.
Automatic ground spoiler deployment will occur with both main landing gear compressed or
with one MLG on the ground and reverse thrust selected (FCOM 1.27.10 [Flight Controls -
Ground Spoiler Control]). Ground spoiler deployment will enable autobrake operation (if
selected). The green DECEL light on the AUTO/BRK panel enable the crew to monitor
whether the selected rate of deceleration is achieved.
Tailstrike occurs (A320) at 13.5 or 11.5 (landing gear compressed), so pitch attitude should
be monitored in the flare (see FCOM bulletin 22). FCOM 3.03.22 (SOPs Landing) contains
information on pitch and roll limits.
Autobrake should normally be used for landing, however on long dry runways it will not be
necessary. Only LO or MED should be used for landing. If landing on a short or slippery
runway MED autobrake should be selected and then use appropriate manual braking to stop
the airplane.
The normal method of disarming the autobrake is by even pressure on both brake pedals.
The auto brake may also be disconnected by action on the respective AUTO/BRK pb (not
recommended as both pilots should be heads up during the landing roll) or by pushing down
the speedbrake control lever. Autobrake should be disconnected before 20 kt is reached.
Max reverse (or idle reverse depending on airport regulations or airline policy) should be
selected immediately after main gear touchdown. PNF should monitor spoiler deployment
(ECAM WHEEL page), operation of reverse thrust (E/WD) and the operation of autobrake
(green decel light on AUTO/BRK panel) and notify PF of any non normal indications.
A319/A320/A321
　
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