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thrust, regardless of the thrust levers positions. This protection is available from liftoff to 100 ft RA
in approach.
The following indications are then provided:
‐ A-FLOORontheFMAandontheEWD,aslongasαfloorconditionsaremet
‐TOGALKontheFMA,whentheaircraftleavestheαfloorconditions.
TOGA thrust is then frozen.
A-FLOOR and TOGA LK are displayed in green, and outlined with a flashing amber box.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
AUTOTHRUST
A330/A340 FLEET DSC-22_30-90 P 21/22
FCOM 19 AUG 10
In order to cancel ALPHA FLOOR or TOGA LK thrust, disconnect the A/THR.
Note: ALPHA FLOOR is inhibited:
‐ In case of engine failure, with the flaps extended
‐ In case of engine failure, with derated TO selected
‐ Below 100 ft at landing
‐ Above M 0.53.
ALPHA FLOOR protection is lost in case of an A/THR failure.
CAUTION The system may consider an engine to be failed when this engine’s Thrust Lever
Angle (TLA) is below 5 °, and the TLA of other engine is above 5 °. Therefore,
ALPHA FLOOR may be inhibited.
In manual thrust control, when simultaneously moving both thrust levers back to
about the IDLE position, and in order to avoid undue ALPHA FLOOR inhibition,
check that both levers are well aligned and that no TLA is below 5 °.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
AUTOTHRUST
Intentionally left blank
A330/A340 FLEET DSC-22_30-90 P 22/22
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
FLIGHT MODE ANNUNCIATOR (FMA)
A330/A340 FLEET DSC-22_30-100 P 1/10
FCOM 19 AUG 10
FLIGHT MODE ANNUNCIATOR (FMA)
Applicable to:
GENERAL
The Flight Mode Annunciator (FMA) located on the top of the PFDs reflects the status of the
A/THR, the AP/FD vertical and lateral modes, the approach capabilities and the AP/FD-A/THR
engagement status.
A white box is displayed for 10 s around each new annunciation.
Applicable to: ,
GENERAL
The Flight Mode Annunciator (FMA) located on the top of the PFDs reflects the status of the
A/THR, the AP/FD vertical and lateral modes, the approach capabilities and the AP/FD-A/THR
engagement status.
A white box is displayed for 10 s around each new annunciation. The white box display time may
be increased to 15 s in some mode reversion cases associated with a triple click aural warning.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
FLIGHT MODE ANNUNCIATOR (FMA)
A330/A340 FLEET DSC-22_30-100 P 2/10
FCOM 19 AUG 10
Applicable to: ALL
THE THREE LEFT COLUMNS
The engaged modes are displayed in green on the first line.
The armed modes are displayed in blue or in magenta on the second line.
Modes armed because of a constraint are displayed in magenta.
Special messages, are displayed on the third line:
First priority is given ‐ to messages related to flight controls:
• "MAN PITCH TRIM ONLY" flashing red during 9 s then steady
• "USE MAN PITCH TRIM" pulsing amber during 9 s then steady.
‐ With lower priority messages related to FMGES.
Applicable to:
THE FOURTH COLUMN
Displays approach capabilities in white.
DH or MDA/MDH is displayed in blue.
Note: The DH or MDA/MDH is rounded off to the nearest 10 ft.
Applicable to: ,
THE FOURTH COLUMN
Displays approach capabilities in white.
DH or MDA/MDH is displayed in blue.
Note: The DH or MDA/MDH value on the FMA is not rounded off : The exact value appears on
the FMA, and is the same value as the one inserted in the MCDU PERF APPR page.
Applicable to: ALL
THE FIFTH COLUMN
Displays the engagement status of AP, FD and A/THR in white.
Displays a box around FD for 10 s in case of automatic FMGEC switching.
Displays A/THR in blue when autothrust is armed but not active.
Note: The FMGES synchronizes A/THR modes, AP/FD modes and landing capability to
provide identical information on both PFDs.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT GUIDANCE
FLIGHT MODE ANNUNCIATOR (FMA)
A330/A340 FLEET DSC-22_30-100 P 3/10
FCOM 19 AUG 10
AUTOTHRUST ANNUNCIATIONS (FMA COLUMN 1)
Applicable to: ,
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 2(66)