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Flight Instructors Training Procedures _revised AIC_x

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ii.<br />

iii.<br />

Varying the power/thrust at a constant<br />

airspeed.<br />

High power/thrust and low speed.<br />

Varying the power/thrust at a constant<br />

airspeed.<br />

Lower power/thrust and high speed.<br />

4. CRITICAL SPEED<br />

Note:<br />

Propeller will not be feathered during this<br />

demonstration.<br />

,<br />

deflection if yaw is to be prevented.<br />

i. Maintain Vyse and close one throttle.<br />

ii. Maintain balance and wings level.<br />

iii. Select climb power on the operative engine.<br />

Note:<br />

a. More rudder deflection will be required<br />

to maintain balance.<br />

b. More aileron defection will be required<br />

to keep the wings level.<br />

iv. Return to twin engine straight and level flight<br />

at cruise power/thrust and speed.<br />

v.<br />

Note: A reduction of airspeed or an increase<br />

of power will result in an increase of control<br />

deflection to maintain balance with the wings<br />

level.<br />

The largest amount of control deflection and<br />

force will be required at a low airspeed and<br />

high power setting<br />

i. From straight and level flight place the<br />

aeroplane in a trimmed descent at cruising<br />

speed and with a low power/thrust setting.<br />

ii. Follow through on the light controls.<br />

iii. Partially reduce the power/thrust of one<br />

engine and note:<br />

Symptoms of asymmetry are less marked,<br />

leading to the possibility of partial power<br />

failure going unnoticed during a descent with<br />

low power/thrust settings.<br />

iv. Continue to reduce the power/thrust to idling<br />

on the selected engine and note:<br />

Even when one engine fails completely the<br />

visual feel and instrument “asymmetric<br />

symptoms” are not very apparent, during a<br />

high airspeed and low power/thrust<br />

configuration.<br />

v. Return to twin engine straight and level flight<br />

at cruising power/thrust.<br />

i. Lookout.<br />

ii. Complete HASELL checks.<br />

iii. Place the aeroplane in straight and level flight<br />

at approximately 3000’ agl. for an aeroplane<br />

with non turbo-charged engines.<br />

iv. Raise the aeroplane’s nose and reduce<br />

airspeed to Vyse. Select maximum permitted<br />

RPM and manifold pressure on both engines.<br />

v. Gradually close the left throttle and move the<br />

mixture control to idle cut-off whilst<br />

maintaining balance, heading and wings level.<br />

Slowly raise the aeroplane’s nose and allow<br />

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