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Autothrust disconnects.
�� At touchdown :
CHECK that “ROLL OUT” appears on the FMA.
�� At the end of the rollout :
Disconnect the autopilot.
If the flight crew does not disconnect the AP at the end of the rollout, and uses the nosewheel
steering handwheel to taxi the aircraft off the runway, the following will occur :
The AP will try to steer the aircraft back to the runway centerline, ‐ if the nosewheel steering
handwheel is released and the aircraft heading is less than 20 ° off the runway centerline.
‐ The AP will automatically disconnect, if the aircraft heading is 20 ° or more off the runway
centerline.
Applicable to: ALL
MANUAL LANDING
�� at DH
DISCONNECT the autopilots. SPEED mode remains engaged.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
SYSTEMS RELATED PROCEDURES - FMS
A330/A340 FLEET PRO-NOR-SRP-01-70 P 5/38
FCOM 19 AUG 10
�� At 20 ft “RETARD” automatic call out comes up
MOVE the thrust levers to IDLE if they are not there already. (The autothrust disconnects).
�� At touch down
“ROLL OUT” appears on the FMA and the yaw bar comes up on the PFD.
Note: The retard call out is only a reminder when a manual landing is performed.
Applicable to: ALL
STANDARD ILS AUTOMATIC APPROACH
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
SYSTEMS RELATED PROCEDURES - FMS
A330/A340 FLEET PRO-NOR-SRP-01-70 P 6/38
FCOM 19 AUG 10
Applicable to: ALL
EARLY SELECTION OF APPROACH MODE LOC - G/S
Pressing the APPR pushbutton arms LOC and G/S.
The RA signal is not valid above 8 200 ft AGL (TRT) or 5 000 ft AGL (Collins),
�� If the aircraft is cleared for an ILS approach when it is higher than 8 000 ft AGL or
5 000 ft AGL (Collins), proceed as follows :
PRESS the APPR pushbutton on the FCU.
�� When aligned on the localizer check LOC and G/S engagement :
CAT 1 is displayed on FMA. (Radio altimeters not yet valid).
Check that the FMA displays the correct capability for the intended approach when the aircraft
is below 5 000 ft AGL.
Applicable to: ALL
GLIDE SLOPE INTERCEPTION FROM ABOVE
If the aircraft is above the glide slope, the system will not capture the G/S automatically.
The pilot must bring the aircraft onto the glide slope beam, and selects an appropriate V/S to
intercept it. Refer to the PSL PRO NOR SOP.
Applicable to: ALL
DATA LOCK
When the aircraft reaches 700 ft RA with APPR mode (LOC and G/S) armed or engaged, the ILS
frequency and course are frozen in the receiver.
This function (ILS tune inhibit) is available when at least one AP/FD is engaged. Any attempt to
change ILS frequency or CRS through the MCDU or RMP does not affect the receiver.
If the speed is managed, the system does not accept any modifications the flight crew may enter
on the PERF APPR page (surface wind, selected landing configuration, or VAPP) for speed
guidance purposes below this altitude.
When the aircraft reaches 400 ft RA, LAND mode engages. The flight crew can disengage this
mode only by engaging the GO AROUND mode.
Applicable to: ALL
USE OF RMPS FOR ILS/DME
If both FMGCs fail, the flight crew can use the RMPs (Radio Management Panels 1 and 2) for
back up tuning. Either RMP controls ILS. Prior to select an ILS frequency on one of the RMPs, the
flight crew has to select “NAV” button from RMP1 and RMP2.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
SYSTEMS RELATED PROCEDURES - FMS
A330/A340 FLEET PRO-NOR-SRP-01-70 P 7/38
FCOM 19 AUG 10
Applicable to:
LOCALIZER (LOC) BEAM CAPTURE
The flight crew must always monitor the capture of a LOC beam. During this evolution, the PFD
and ND must indicate that associated deviation indications move toward the centre of the scale.
To avoid performing a false capture, the flight crew must be careful not to arm the LOC too early.
The following graph shows the angle of interception versus distance to the runway threshold that
ensures that the aircraft will not overshoot the axis by more than one and a half dot.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
SYSTEMS RELATED PROCEDURES - FMS
A330/A340 FLEET PRO-NOR-SRP-01-70 P 8/38
FCOM 19 AUG 10
The capture begins when the deviation is two dots or less. It is programmed to line the aircraft up
on the beam with a single overshoot, even if the intercept angle is large.
Note: ICAO requires loc beam to ensure a normal capture within 10 nm and +/- 35 ° of the
course centerline. Some current ILS systems just meet the requirement and are subject
　
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