.
QRH 2.21 (Overweight landing)

.
FCOM 1.27.20 (Sideslip target)

.
FCOM 3.02.10 (Operating techniques)

.
FCOM 3.02.26 (Engine fire)

.
FCOM 3.02.70 (Engine fail)

.
FCOM 4.04.30 (EOSID) if applicable

.
FCOM 4.05.30 (Engine Out Procedure)

04 - INSTRUCTOR’S ACTIONS
Briefing of the following key points :
MAIN
.
GO/STOP decision making.

.
Aircraft control on the ground and at rotation.

.
Roll control, sideslip target and "Fly by wire" characteristics.

.
Pitch attitude and speed control.

.
Specific task sharing procedures.

.
Confirmation of non-reversible items with ECAM actions.

.
Engine-out profile.

SECONDARY

.
A/P engagement / Rudder trim.

.
EOSID activation.

.
Availability and use of TOGA.

.
FD roll limit below green dot speed.

A319/A320/A321 FLIGHT CREW TRAINING MANUAL  ABNORMAL OPERATION BRIEFINGS OPERATING TECHNIQUES  1.03.10  Page 4 
REV 21  MAY 98 

05 - TRAINEES’ ACTIONS
ENGINE FAILURE
After detecting an engine failure, PNF is to call "engine failure", without identifying which engine has failed.
TOGA power is available, but should only be applied when required by PF. This is because the increase in power may cause directional control difficulties when at light weights and low speeds.
PF should maintain runway centerline with rudder, visually or with assistance of the PFD yaw bar (if available). At VR, rotate smoothly to 12°5 nose up and centralize blue b target (see below for explanatory note) with rudder. Adjust pitch attitude and monitor speed trend arrow (minimum speed V2) until SRS has stabilized. The change over from yellow side slip index to blue b target may not occur instantaneously. Use rudder trim to neutralize rudder pedal pressure. When a positive climb has been achieved, call for retraction of the gear. Use autopilot if it is available.
PNF should closely monitor the aircraft’s flight path, cancel warnings and identify the failure when appropriate. Note when a positive climb has been established and announce accordingly. Retract gear on command.
Once well clear of the ground, minimum 400 ft, the ECAM actions may be started. It is not necessary to rush into doing the ECAM drills and 400 ft is the MINIMUM altitude at which commencement of ECAM drills should be considered. The priority is to ensure that the aircraft is climbing, stabilized and is flying in a safe direction. Do not get too distracted with ECAM. Furthermore, ECAM should be interrupted when necessary to allow both pilots to monitor level-off, configuration changes etc.
It is important to determine whether the engine has suffered a flameout or has structural damage. The action of putting the start switch to ignition confirms the relight attempt being made by the FADEC. If a flameout has occurred, then a relight (QRH 2.18) may be considered at a later stage when aircraft has been cleaned up and a safe flight path established.
There must be no movement of thrust lever, master switch or fire pb without positive confirmation from both pilots.
A319/A320/A321 FLIGHT CREW TRAINING MANUAL  ABNORMAL OPERATION BRIEFINGS OPERATING TECHNIQUES  1.03.10  Page 5 
REV 21  MAY 98 

05 - TRAINEES’ ACTIONS(CONT’D)
ENGINE FIRE
Should an engine fire develop, follow the general series of actions described above. However, the ECAM drill should be commenced as soon as is practicable (though not below 400 ft). Be aware that the engine may still be developing a significant amount of thrust until the engine master switch is placed to off. Consider the use of autopilot to reduce workload. The ECAM will count down the seconds to initial agent discharge and the time period between discharges.
　
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