Flight Instructors Training Procedures _revised AIC_x

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ix. Raise the landing gear and flap. Select “zero
thrust” on the idling engine.
x. Adopt Vyse and re-trim.
xi. Complete engine shutdown checklist
(simulated).
xii. Repeat entire exercise (i) to (xi) at Vyse minus
10 knots IAS.
Note: The climb performance and the
significance of achieving at least the safety
speed at lift-off before entering a positive
climb.
ii. Asymmetric committal height. i. Lookout.
ii. Establish the aeroplane into a descent with
landing gear and landing flap lowered.
iii. Set “zero thrust” on one engine.
iv. Adopt a typical approach airspeed (below Vyse
) for the aeroplane type.
v. At a nominated altitude of at least 100 agl.
adopt the missed approach procedure.
Apply take-off power on the operating engine.
Raise the flaps to optimum and once
established in a positive rate of climb, raise
the gear and the rest of the flaps.
9. ENGINE FAILURE DURING THE TAKE-
OFF PHASE
i.
Engine Failure During Take-off
Note: This demonstration may only be
shown providing ample distance is available
and the take-off surface is suitable for firm
braking action to be applied.
Note the altitude loss between initiating the
missed approach procedure and establishing
a positive rate of climb.
vi. Repeat the above demonstration commencing
at Vyse , and note the smaller height loss
involved between applying power and
climbing away.
Note: The importance of selecting a safe
height below which a missed approach should
not be initiated, and the value of maintaining
at least Vyse until this height is reached on an
asymmetric approach. This height should not
be below 300 ft agl.
i. Pre take-off checks completed.
ii. Take-off briefing/review – indicating specific
wording and content for a particular take-off.
iii. Commence normal take-off.
i. ATC liaison.
ii. Shortly after full power/thrust has been
applied, close one throttle to simulate engine
failure.
iii. Immediate Actions:
a. Simultaneously close the throttle of the
operating engine.
b. Maintain direction by use of the rudder
and if necessary differential braking
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