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Set the go around altitude on the FCU.
Applicable to: ,
, MSN,
AT GREEN DOT SPEED
FLAPS 1...............................................................................................................................ORDER
FLAPS 1..............................................................................................................................SELECT
At high weights, if the green dot speed is close to VFE ‐ NEXT, the crew may select a lower
speed
‐ FLAPS 1 should be selected more than 3 nm before the FAF (Final Approach Fix).
Note: The ECAM automatically displays the STATUS page, if it is applicable, and if the flight
crew has not already selected a system page manually.
‐ Check deceleration toward “S” speed
‐ The aircraft must reach, or be established on, the glideslope with FLAPS 1 and S speed at, or
above, 2 000 ft AGL.
‐ If the aircraft speed is significantly higher than S on the glideslope, or if the aircraft does not
decelerate on the glideslope, extend the landing gear to slow it down. It is also possible to use
speed brakes. However, the flight crew should be aware that the use of speed brakes causes
an increase in VLS.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - ILS APPROACH
A318/A319/A320/A321 FLEET PRO-NOR-SOP-18 P 6/12
FCOM 19 AUG 10
TCAS �� ......................................................................................................................TA or TA/RA
The FAA recommends selecting TA only mode:
‐ In case of known nearby traffic, which is in visual contact
‐ At particular airports, and during particular procedures, identified by an Operator as having a
significant potential for unwanted or inappropriate resolution advisories (closely-spaced parallel
runways, converging runway, low terrain along the final approach...).
FMA........................................................................................................... CHECK and ANNOUNCE
LOC CAPTURE..................................................................................................................MONITOR
The flight crew must always monitor the capture of LOC beam. During the capture phase, the
associated deviation indications on the PFD and ND must indicate movement towards the center
of the scale.
G/S CAPTURE...................................................................................................................MONITOR
�� If above the glideslope:
V/S mode........................................................................................................................SELECT
FCU ALTITUDE............................................................................. SET ABOVE A/C ALTITUDE
Do not reach VFE to avoid reversion to OP CLB.
Note: 1. When reaching VFE, the AP maintains VFE and reduces the V/S without MODE
REVERSION.
2. If the aircraft intercepts the ILS above the radio altimeter validity range (no radio
altitude indication available on the PFD), CAT 1 is displayed on the FMA. Check that
the FMA displays the correct capability for the intended approach, when the aircraft is
below 5 000 ft.
GO-AROUND ALT....................................................................................................................... SET
Set the go around altitude on the FCU.
Applicable to: ALL
AT 2 000 FT AGL (MINIMUM)
FLAPS 2...............................................................................................................................ORDER
FLAPS 2..............................................................................................................................SELECT
Check ‐ deceleration towards F speed
‐ If the aircraft intercepts the ILS glideslope below 2 000 ft AGL, select FLAPS 2 at one dot below
the glideslope
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - ILS APPROACH
A318/A319/A320/A321 FLEET PRO-NOR-SOP-18 P 7/12
FCOM 19 AUG 10
‐ If the aircraft speed is significantly higher than S on the glide slope, extend the landing gear in
order to slow down the aircraft. The use of speed brakes is not recommended
‐ When the speed brakes are deployed, extending the flaps beyond FLAPS 1 may induce a
slight roll movement, and in calm conditions a small lateral control asymmetry may remain until
disturbed by a control input or by an atmospheric disturbance.
Applicable to: ALL
WHEN FLAPS ARE AT 2
LDG GEAR DOWN................................................................................................................ORDER
L/G lever...................................................................................................................SELECT DOWN
　
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