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‐ The AP disengages.
‐ The FD reverts to its HDG - V/S or TRK - FPA modes.
FAILURE OF LOCALIZER OR GLIDESLOPE TRANSMITTER (WHEN CAPTURED)
‐ The corresponding index is lost.
‐ The LOC and G/S scales flash.
‐ The corresponding FD bar flashes.
The FMA retains the LOC and G/S modes : If the transmitter failure is temporary, the APs are
able to regain these modes. If the failure is long-term, or if it occurs when the aircraft is below
200 ft RA, this allows the aircraft to perform a GO AROUND with one or 2 autopilots engaged.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
SYSTEMS RELATED PROCEDURES - FMS
A318/A319/A320/A321 FLEET PRO-NOR-SRP-01-70 P 21/42
FCOM 19 AUG 10
WARNINGS FOR ILS APPROACH
Applicable to:
,
,
MSN,,,,
AUTOLAND WARNING
With “LAND” or “FLARE” in green on the FMA and at least one AP engaged, the AUTOLAND
red light appears on the glareshield when the aircraft is below 200 ft RA and one of the following
events occurs :
‐ The autopilots are lost, or
‐ The aircraft gets too far off the beam (LOC or G/S flash on PFD), or
‐ Loss of LOC signal above 15 ft, or loss of glide signal above 100 ft (transmitter or receivers).
‐ The difference between both radio altimeter indications is greater than 15 ft.
When the Autoland light comes on, Autoland must be discontinued (Refer to
PRO-NOR-SRP-01-70 FAILURES AND ASSOCIATED ACTIONS BELOW FT DURING A
CAT II APPROACH,
Refer to PRO-NOR-SRP-01-70 FAILURES AND ASSOCIATED ACTIONS BELOW FT CAT
III WITH DH,
Refer to PRO-NOR-SRP-01-70 FAILURES AND ASSOCIATED ACTIONS BELOW FT FOR
CAT III WITHOUT DH).
WARNING OF EXCESSIVE BEAM DEVIATION
This warning is a flashing of the LOC and G/S scales on the PFD and ND ROSE ILS. It occurs
whenever :
‐ G/S deviation is greater than 1 dot (above 100 ft RA).
‐ LOC deviation is greater than 1/4 dot (above 15 ft RA).
WARNING ASSOCIATED WITH ILS "LANDING CAPABILITY"
Any downgrading in the aircraft’s capability for automatic approach and landing sounds a
triple-click aural warning.
FAILURE OF BOTH LOCALIZER AND GLIDESLOPE RECEIVERS
The PFD and ND (rose ILS mode) display red LOC and G/S flags (if the ILS pushbutton has
been pressed green). LOC and G/S scales disappear from the PFD.
If LOC or G/S modes are engaged and at least one AP/FD is engaged
‐ The AP disengages.
‐ The FD reverts to its HDG - V/S or TRK - FPA modes.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
SYSTEMS RELATED PROCEDURES - FMS
A318/A319/A320/A321 FLEET PRO-NOR-SRP-01-70 P 22/42
FCOM 19 AUG 10
FAILURE OF LOCALIZER OR GLIDESLOPE TRANSMITTER (WHEN CAPTURED)
The ‐ corresponding index is lost.
‐ The LOC and G/S scales flash.
‐ The corresponding FD bar flashes.
Above 200 ft RA, if the transmitter failure lasts less than 7 s, the FMA retains the LOC and G/S
modes (or the LAND mode) and the APs are able to regain these modes. If the failure lasts
longer than 7 s, the AP disengages and the FD reverts to its basic modes. Below 200 ft RA, if
the transmitter failure occurs, the AUTOLAND warning appears, indicating that the crew must
perform a GO AROUND (if insufficient visual references) with one or 2 APs engaged.
FAILURES AND ASSOCIATED ACTIONS ABOVE 1 000 FT FOR CAT II OR CAT III
Applicable to: ALL
FAILURE
(for multiple failures, the
most limiting applies)
ACTION TO BE PERFORMED
ABOVE 1 000 ft LANDING CATEGORY
ONE ENGINE OUT Complete ECAM procedure. CAT III SINGLE
LANDING CAPABILITY DECREASE Try to recover As displayed on FMA
LOSS OF A/THR Switch AP, and try to reengage CAT II
(if A/THR not recovered)
NOSE WHEEL STEERING CAT III SINGLE
(DH = 50 ft)
Disengage AP at touch down
ANTI SKID CAT III SINGLE
Disengage AP at touch down
AMBER "CHECK ATT" ON TWO
PFDs
Check with standby horizon, use switching
to recover (no switching below 1 000 ft)
AMBER "CHECK HDG" ON TWO
PFDs AND TWO NDs
Check with standby compass, use
switching to recover (no switching below
1 000 ft)
RED "HDG" ON ONE PFD AND ONE
ND
RED "ATT" ON ONE PFD
RED "SPD" ON ONE PFD
DIAGONAL LINE ON ONE PFD AND
ONE ND
Use switching to recover (no switching
below 1 000 ft)
CAT III SINGLE
(if the warning disappears)
CAT I
(if not)
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
SYSTEMS RELATED PROCEDURES - FMS
　
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