ENGINE FAILURE AFTER V1 / GO AROUND
CAPTAIN FIRST OFFICER / PNF
"Engine Fail" "Engine Fail"
"Go"
"Continuous Relight" Select Continuous Relight "Continuous Relight"
VR "Rotate"
Rotate to 12.50. Apply rudder on side of live engine to keep wings level. Apply rudder progressively on the side where control wheel is defected to get control wheel neutral.
"Positive climb"
"Gear up" Select gear up
“Bank 15” Select Bank limit 15
Min 250’, AP 1 in CMD "CMD 1"
In case of Flex T/O, Go around thrust may be set by pressing TOGA on TRP or Manually advancing Throttle lever.
"400 ft"
Aircraft stabilized. "ECAM actions" Carry out ECAM actions.
Affected throttle idle. “ 1/ 2 Throttle idle”
(Guards the good engine throttle & monitors thrust.)
“1 / 2 fuel lever off”.
“Affected Fuel lever off”
(Guards good engine fuel lever ) Checks good engine fuel lever is guarded.
Checks no immediate relight on failed engine** and selects No 1/2 fuel lever off.
"If damage", continue ECAM actions, till 1st agent discharge.
Call ATC "Air India............No. 1/2 Eng failure, following S.I.D*, will require level acceleration at ______ ft” (MSA)
“start APU” Starts APU.
" Speed 250, Alt hold "
(done by PF if AP in CMD/by PNF if Manual flying.)Note: As soon as SRS / go around mode is lost be prepared to trim rudder as AP yaw damper compensation is lost. “MSA”
"F speed"
"Flaps O" "Flap 0 Selected, Moving"
."Flaps O"
Maintain Slats 15 at S speed, if conditions exist for immediate turn back "S Speed"
If immediate turn back is not decided upon, "Slats retract"
"Slats selected, moving"
"Slats retracted"
At Green dot speed on Standby ASI
" Lvl. Change, Green dot speed, MCT, bank Normal"
A THR pb - Push to engage.
Inform ATC “Resuming Climb”
Note: As soon as slats retract AP rudder compensation is lost, be prepared to hold rudder and trim.
"Continue ECAM Actions till status." Carry out ECAM actions till ‘STATUS’ appears.
" After take-off C/L." Carryout After take-off C/L.
“Engine fail check list” Carries out engine fail checklist from QRH.
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