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‐ The system automatically calls up the current performance page, which has the EO CLR
(engine-out clear) prompt displayed in the 1R field (except during takeoff, before the diversion
point is reached).
If the crew presses the EO CLR, the 2 engine predictions and performance will be restored.
Reverting back to one engine-out performance is not possible, unless the system detects a new
EO condition. Therefore, the pilot should not press the EO CLR key, if an actual engine-out is
detected.
‐ In the descent and approach phases, the system automatically restores two-engine predictions.
The descent mode is available.
It is not permitted to use the autopilot to perform non precision approaches in engine-out in the
following modes : FINAL APP, NAV V/S, NAV/FPA. Only FD use is authorized.
FLIGHT MANAGEMENT PART
Applicable to:
The managed target speeds is immediately set to a value that ‐ depends upon the flight phase.
‐ All preselected speeds entered in the MCDU are deleted.
‐ Step climb (or step descent), if entered, is deleted.
‐ The time constraint is deleted.
‐ The PROG page shows the engine-out maximum recommended (EO MAX REC) altitude.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT MANAGEMENT
OTHER FUNCTIONS - ENGINE OUT
A318/A319/A320/A321 FLEET DSC-22_20-60-50 P 2/14
FCOM 19 AUG 10
‐ The system automatically calls up the current performance page, which has the EO CLR
(engine-out clear) prompt displayed in the 1R field (except during takeoff, before the diversion
point is reached).
If the crew presses the EO CLR, the 2 engine predictions and performance will be restored.
Reverting back to one engine-out performance is not possible, unless the system detects a new
EO condition. Therefore, the pilot should not press the EO CLR key, if an actual engine-out is
detected.
‐ In the descent and approach phases, the system automatically restores two-engine predictions.
The descent mode is available.
It is not permitted to use the autopilot to perform non precision approaches in engine-out in the
following modes : FINAL APP, NAV V/S, NAV/FPA. Only FD use is authorized.
FLIGHT MANAGEMENT PART
Applicable to:
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‐ The managed target speeds is immediately set to a value that depends upon the flight phase.
‐ The following pilot entries are deleted : preselected speeds, steps, time constraints.
‐ No predictions are available for the ALTN flight plan, and the associated fields are dashed. The
default MIN DEST FOB value (ALTN + FINAL) will be subsequently affected.
‐ Predictions on the secondary flight plan are lost, if it is a copy of the active flight plan.
‐ The PROG page shows the engine-out maximum recommended (EO MAX REC) altitude.
‐ The system automatically calls up the current performance page, which has the EO CLR
(engine-out clear) prompt displayed in the 1R field (except during takeoff, before the diversion
point is reached).
If the crew presses the EO CLR, the 2 engine predictions and performance will be restored.
Reverting back to one engine-out performance is not possible, unless the system detects a new
EO condition. Therefore, the pilot should not press the EO CLR key, if an actual engine-out is
detected.
In the descent and approach phases, ‐ the system automatically restores two-engine predictions.
The descent mode is available.
It is not permitted to use the autopilot to perform non precision approaches in engine-out in the
following modes : FINAL APP, NAV V/S, NAV/FPA. Only FD use is authorized.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT MANAGEMENT
OTHER FUNCTIONS - ENGINE OUT
A318/A319/A320/A321 FLEET DSC-22_20-60-50 P 3/14
FCOM 19 AUG 10
FLIGHT GUIDANCE PART
Applicable to:
‐ All selected modes remain available (the “HDG/TRK”, “V/S”, and “OPEN” modes, for example).
‐ In the speed reference system (SRS) mode, the takeoff speed target is V2, or the current speed if
it is higher. The magenta triangle indicates V2 in all cases.
‐ The system limits autopilot (AP) and flight director (FD) bank angles during takeoff and approach
phases as follows :
• 15 ° when the aircraft speed is below the maneuvering speeds (F, S, or Green Dot speed) -10 kt
• Then linear increase to 25 ° up to maneuvering speeds (F, S, or Green Dot speed) -3 kt
• 25 ° above maneuvering speeds (F, S, or Green Dot speed) -3 kt.
Note: The engine-out bank angle limits apply, when the FG part of the FMGS has detected
an engine-out. It cannot be cleared by the crew through the MCDU E.O CLEAR
　
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