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models for the A340, or on a single engine model for the A330.
ENGINE-OUT IN APPROACH PHASE
Applicable to: ALL
• The aircraft maintains approach speed (VAPP).
• “LVR MCT” flashes on the Flight Mode Annunciator.
• The PERF APPR page appears, showing the “EO CLR*” prompt.
• The PROG page displays the engine-out maximum altitude (EO REC MAX).
PROCEDURE
MOVE the thrust lever(s) for the live engine(s) to the MCT detent.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT MANAGEMENT
OTHER FUNCTIONS - ENGINE OUT
A330/A340 FLEET DSC-22_20-60-40 P 10/10
FCOM 19 AUG 10
SELECT a suitable flight mode as for an all engine approach.
CAUTION Below maneuvering speed (F, S, Green Dot), the autopilot or flight director
(AP/FD) cannot order a bank angle greater than 15 °. Above maneuvering speed,
normal AP/FD bank angle is available.
ENGINE-OUT IN GO-AROUND PHASE
Applicable to: ALL
The results and procedures for takeoff phase apply, however the displays do not show the
engine-out SID.
Note: If ALT* engages out of SRS mode, and an engine-out occurs simultaneously, an airspeed
loss may be encountered during the altitude capture.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT MANAGEMENT
OTHER FUNCTIONS - SECONDARY FLIGHT PLAN
A330/A340 FLEET DSC-22_20-60-50 P 1/4
FCOM 19 AUG 10
SECONDARY FLIGHT PLAN
Applicable to:
The secondary flight plan (SEC F-PLN) is an alternative flight plan which can be activated when
required.
With respect to the secondary flight plan, you can :
‐ Construct it independently
‐ Copy it from the active flight plan.
‐ Delete it completely.
‐ Activate it as primary flight plan using ACTIVATE SEC prompt.
‐ The screen displays the “ACTIVATE SEC” prompt in flight :
• when the heading (track) mode is engaged, or
• when the navigation mode is engaged if the active legs of the primary and secondary flight
plans are common.
‐ The screen displays the “INIT” prompt if the secondary flight plan is not a copy of the active flight
plan.
The secondary flight plan sequences with the active flight plan when it is a copy of the active.
The navigation display shows the secondary flight plan in white.
In PLAN mode use the slew keys to review it (as you would for the primary flight plan).
PREDICTIONS
The FMGS computes predictions using the same performance methods and performance factor
as for the active flight plan. However, it predicts pseudo-waypoints only for display the MCDU, and
not for the Navigation Display (ND).
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT MANAGEMENT
OTHER FUNCTIONS - SECONDARY FLIGHT PLAN
A330/A340 FLEET DSC-22_20-60-50 P 2/4
FCOM 19 AUG 10
USE OF SECONDARY FLIGHT PLAN
The crew may use the secondary flight plan in the following situations :
• When an alternate takeoff runway is probable
• To plan a diversion
• To prepare the next flight
• To compare predictions and evaluations.
SECONDARY FLIGHT PLAN
Applicable to: ,
The secondary flight plan (SEC F-PLN) is an alternative flight plan which can be activated when
required.
With respect to the secondary flight plan, you can :
Construct it independently (it can ‐ be created while a temporary exists).
‐ Copy it from the active flight plan.
‐ Delete it completely.
‐ Activate it as primary flight plan using ACTIVATE SEC prompt.
‐ The screen displays the “ACTIVATE SEC” prompt in flight :
• when the heading (track) mode is engaged, or
• when the navigation mode is engaged if the active legs of the primary and secondary flight
plans are common.
‐ The screen displays the “INIT” prompt if the secondary flight plan is not a copy of the active flight
plan.
The secondary flight plan sequences with the active flight plan when it is a copy of the active.
The navigation display shows the secondary flight plan in white.
In PLAN mode use the slew keys to review it (as you would for the primary flight plan).
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT MANAGEMENT
OTHER FUNCTIONS - SECONDARY FLIGHT PLAN
A330/A340 FLEET DSC-22_20-60-50 P 3/4
FCOM 19 AUG 10
PREDICTIONS
The FMGS computes predictions using the same performance methods and performance factor
as for the active flight plan. However, it predicts pseudo-waypoints only for display the MCDU, and
not for the Navigation Display (ND).
　
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