05 - TRAINEES’ ACTIONS (END)
SINGLE ENGINE GO-AROUND
The go-around is essentially the same as on 2 engines, the pitch target is now 12°5. Apply rudder to compensate for the increase in thrust and keep the b target centered. FMA will indicate GA TRK, think about aircraft navigation with respect to terrain. Flap retraction and acceleration will take place in level flight at acceleration altitude. As this is a go-around, target speed is the memorized approach speed or the speed at engagement of go-around, becoming green dot at acceleration altitude.
b  TARGET
The side slip indicator (yellow) gives the same indications as traditional slip ball. The b target (blue) replaces the side slip indicator on the PFD when there is engine power asymmetry and CONF 1, 2 or 3 is set [see FCOM 1.27.20 (Flight Controls - Normal law)]. When the b target is centered, total drag is minimized even though there is a small amount of side slip
The calculation of b target is a trade off between drag produced by deflection of control surfaces, and airframe drag produced by a slight side slip. This is better than a traditional ball as rudder deflection, aileron deflection, spoiler deployment and aircraft body angle are all taken into incount.

06 - COMPLETION STANDARDS
.  
Makes correct decision to continue the take-off.

.  
Ensures minimum deviation from runway centerline.

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Establishes correct pitch attitude at rotation with wings level and b target centered.

.  
Accurately follows flight director and ensures correct FCU selections.

.  
Maintains speed, V2 +5 kt/-0 kt during second segment.

.  
Adheres to engine-out vertical profile maintaining acceleration altitude
+200 ft/-0 ft.

.  
Follows EOSID, emergency turn procedure, ATC instructions or required heading +/- 10.

.  
Respects task sharing.

07 - COMMON ERRORS
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Over rotation to high pitch attitude.

.  
b Target not fully centered.

.  
ECAM non-reversible actions carried out without proper crew confirmation.

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SID, EOSID or ATC instructions not accurately followed.

.  
Poor maintenance and monitoring of required track.

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Lack of task sharing discipline during manual flight (FCU actions).

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Not trimming the rudder.

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Not rotating to correct pitch attitude on go-around.

.  
To ensure continued safe flight following loss of all engine generators.

.  
To carry out ECAM procedure strictly respecting task sharing requirements.

.  
To perform a safe approach and landing using raw data information and degraded flight control laws.

A319/A320/A321 FLIGHT CREW TRAINING MANUAL  ABNORMAL OPERATION BRIEFINGS OPERATING TECHNIQUES  1.03.10  Page 8 
REV 21  MAY 98 

A319/A320/A321 FLIGHT CREW TRAINING MANUAL  ABNORMAL OPERATION BRIEFINGS EMER ELEC CONFIG - ALL ENGINE GENERATORS FAULT - 1.03.24  Page 1 
REV 21  MAY 98 

02 - SCHEDULE
Briefing duration : 20 minutes
03 - EQUIPMENT
DOC references :
.  
QRH 02.02 to 02.05 (Systems remaining)

.  
FCOM 03.02.24 (Elec emerg CONF)

.  
QRH 2.08 & FCOM 03.02.28 (Fuel gravity feeding)

.  
Briefing note - ECAM use in case of failures

.  
Briefing note - ILS raw data approach

.  
Briefing note - Use of FPV

04 - INSTRUCTOR’S ACTIONS
Briefing of the following key points.
　
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