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stabilization height:
The aircraft is on the correct ‐ lateral and vertical flight path
‐ The aircraft is in the desired landing configuration
‐ The thrust is stabilized, usually above idle, to maintain the target approach speed along the
desired glide path
‐ No excessive flight parameter deviation.
If the aircraft is not stabilized on the approach path in landing configuration, at 1 000 ft above airfield
elevation in instrument conditions, or at 500 ft above airfield elevation in visual conditions, or as
restricted by Operator policy/regulations, the flight crew must initiate a go-around, unless they think
that only small corrections are necessary to rectify minor deviations from stabilized conditions due,
amongst others, to external perturbations.
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 4/12
FCOM 19 AUG 10
Applicable to:
,
,
MSN,,,,
APPR pb on FCU.......................................................................................................................PRESS
‐ Press the APPR pb, only when ATC cleares the aircraft for the approach. This arms the LOC and
G/S modes
‐ LOC and/or G/S capture modes will engage no sooner than 3 s after being armed.
BOTH APs............................................................................................................................. ENGAGE
When APPR mode is selected, AP1 pb and AP2 pb should be engaged.
Applicable to:
MSN,
AT GREEN DOT SPEED
FLAPS 1...............................................................................................................................ORDER
FLAPS 1..............................................................................................................................SELECT
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.
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
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 5/12
FCOM 19 AUG 10
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
　
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