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prompt.
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 but no more than V2 + 15. The magenta triangle indicates V2 in all cases. The GO
Around speed target is VAPP, or the current speed if higher, limited to VLS + 15 kt.
‐ 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
prompt.
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 4/14
FCOM 19 AUG 10
FLIGHT GUIDANCE PART
Applicable to:
,
,
MSN,,
4538,,
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 but no more than V2 + 15. The magenta triangle indicates V2 in all cases. The GO
Around speed target is VAPP, or the current speed if higher, but limited to VLS + 15 kt.
‐ 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)
• Normal AP/FD bank angle above maneuvering speed.
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
prompt.
AUTOTHRUST
Applicable to: ALL
The system extends the active range of the active engine from idle to maximum continuous thrust
(MCT instead of CL thrust).
The Flight Mode Annunciator requests maximum continuous thrust on the live engine at a time that
depends on when the engine-out occurs.
ENGINE-OUT CONDITIONS
Applicable to:
The FMGS considers the aircraft to be in an engine-out condition, when one of the following
conditions is present and the aircraft has commenced takeoff or is in flight :
‐ One engine master switch off, or
‐ N2 below idle, or
‐ One thrust lever angle is below 5 ° with the other above 22 °, or
‐ The FADEC shows an engine fault.
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 5/14
FCOM 19 AUG 10
ENGINE-OUT CONDITIONS
Applicable to:
,
,
MSN,,
4538,,
The FMGS considers the aircraft to be in an engine-out condition, when one of the following
conditions is present and the aircraft has commenced takeoff or is in flight :
One engine master switch off for CFM engines, one engine ‐ shut down for IAE engines,
‐ N2 below idle, or
‐ One thrust lever angle is below 5 ° with the other above 22 °, or
‐ The FADEC shows an engine fault.
ENGINE-OUT SID
Applicable to:
GENERAL
An engine-out standard instrument departure (EOSID), when defined in the database, is always for
a specific runway. It is indicated on the bottom line of the SID page for that runway, and you can
select it manually.
The pilot can review the SID either by selecting the PLAN mode on the navigation display (solid
yellow line), or by selecting it on the SID page. In the latter case, the navigation display shows the
SID as a temporary flight plan.
The last point, if any, that is common to both the SID and engine-out SID is called the diversion
point (DP).
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 6/14
FCOM 19 AUG 10
Applicable to:
,
,
MSN,,
4538,,
GENERAL
An engine-out standard instrument departure (EOSID), when defined in the database, is always for
a specific runway. It is indicated on the bottom line of the SID page for that runway, and you can
　
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