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AP engagement is indicated by the lighting of the corresponding FCU pushbutton, and by the
appearance of AP1 (or 2) on the PFD’s FMA.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
AUTOPILOT (AP)
A330/A340 FLEET DSC-22_30-30 P 2/4
FCOM 19 AUG 10
AP DISENGAGEMENT
Applicable to: ALL
AP1 or 2 disengages when:
‐ The flight crew presses the takeover pb on the sidestick
‐ The flight crew presses the corresponding AP pb on the FCU
‐ The flight crew pushes on the sidestick harder than a certain threshold. (Disengagement through
rudder pedals is only active on ground)
‐ The other AP is engaged, except when localizer/glideslope modes are armed or engaged, or
rollout or go-around mode is engaged
‐ The thrust levers are set above the MCT detent and the aircraft is on ground
‐ In a non-precision approach, with FINAL APP mode engaged, the aircraft reaches:
• The MDA/MDH -50 ft (if entered), or 400 ft AGL (if no MDA/MDH is entered), or
• The Missed Approach Point (MAP), depending on which one comes first.
‐ One of the engagement conditions is lost.
Furthermore, in normal law with all protections available, the AP will disconnect if:
‐ High speed protection is active
‐ Angle-of-attack􀀃protection􀀃is􀀃active􀀃(α􀀃prot􀀃+1􀀃°􀀃is􀀃reached)􀀃
‐ Pitch attitude exceeds 25 ° up, or 13 ° down, or bank angle exceeds 45 °.
The standard way for the flight crew to disengage the AP is to press the takeover pb on the sidestick.
When AP is OFF, the associated FCU pushbutton goes off, and the AP1 (or 2) disappears from the
PFD’s FMA
AP WARNINGS
Applicable to: ALL
When the AP is disengaged, the system warns the flight crew:
If the flight crew disengages it with the takeover pb on the sidestick, ‐ the warnings are temporary
‐ If the disengagement results either from a failure, from the flight crew pushing the pushbutton on
the FCU, or from a force on the sidestick, the visual and audio warnings are continual.
AP DISENGAGEMENT
TAKEOVER pb
on SIDESTICK BY OTHER MEANS
MASTER
WARNING light Flashing red during 3 s maximum Flashing red
CONSEQUENCE
ECAM AP OFF red message
9 s maximum AUTO FLT AP OFF red warning
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
AUTOPILOT (AP)
A330/A340 FLEET DSC-22_30-30 P 3/4
FCOM 19 AUG 10
Continued from previous page
AP DISENGAGEMENT
TAKEOVER pb
on SIDESTICK BY OTHER MEANS
AUDIO
Cavalry charge
0.5 s minimum
1.5 s maximum
Continuous cavalry charge
1.5 s minimum
CLR pb on ECAM
CONTROL PANEL Extinguished Illuminated
MASTER
WARNING light
‐ Extinguishes Master Warning
light
‐ Erases ECAM warning
‐ Stops audio if pressed within
1.5 s
‐ Extinguishes Master Warning
light
‐ Stops audio after 1.5 s
CLR pb on ECAM
CONTROL PANEL No effect
‐ Extinguishes CLR pb
‐ Erases ECAM message
‐ Calls status
ACTION
TAKEOVER pb
‐ Extinguishes Master Warning
light
‐ Erases ECAM warning
‐ Stops audio if pressed within
1.5 s
‐ Extinguishes Master Warning
light
‐ Stops audio after 1.5 s
ECAM STATUS MESSAGE NO YES
AUTOLAND WARNING
Applicable to: ALL
The autoland red warning flashes in LAND mode when the radio altitude goes below 200 ft and:
‐ The aircraft gets too far off the beam (LOC or GLIDE), or
‐ Both glide slope transmitters or receivers fail, or
‐ Both localizer transmitters or receivers fail, or
‐ Both radio altimeters differ from more than 15 ft, or
‐ Both autopilots fail.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
AUTOPILOT (AP)
Intentionally left blank
A330/A340 FLEET DSC-22_30-30 P 4/4
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
SPEED/MACH CONTROL
A330/A340 FLEET DSC-22_30-40 P 1/4
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
In flight, either the AP/FD pitch control or the autothrust may acquire and hold a target speed or
Mach number, according to the engaged modes.
The speed control is:
‐ Managed when the target comes from the FMGES
‐ Selected when the target comes from the SPD/MACH FCU window.
MANAGED SPEED/MACH TARGET
Applicable to: ALL
When the speed target is managed, the SPD/MACH window of the FCU shows dashes, and the
　
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