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Flight Instructors Training Procedures _revised AIC_x

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v. Demonstrate – that by taking off power in a<br />

spiral the height lost in recovery can be<br />

minimised. Applying power for the climb<br />

away, take care not to exceed the engine<br />

limitations.<br />

2. EFFECT OF AIRSPEED<br />

Demonstrate the effect of airspeed on the<br />

controls at low and high speeds at a constant<br />

power setting, i.e. throttle closed. For high<br />

speed demonstration, descend at best glide<br />

speed plus 30%; then descend at best glide<br />

speed for low speed demonstration.<br />

3. EFFECT OF SLIP STREAM<br />

Demonstrate the effect on the controls at a<br />

high power setting, climbing at best angle of<br />

climb and then at a reduced power setting at<br />

the same speed whilst descending.<br />

)+<br />

increases, low nose attitude and high rate of<br />

descent occurs – spiral dive.<br />

v. Recovery from spiral descent:<br />

a. Close throttle fully.<br />

b. Simultaneously co-ordinated<br />

movement of rudder and control<br />

column to opposite side of spiral.<br />

c. Centralise ailerons and rudder when<br />

wings are level with horizon, balancing<br />

with rudder.<br />

d. Recover from dive − ease back on<br />

control column.<br />

e. When the nose moves through the<br />

horizon, apply climb power.<br />

RUDDER:-<br />

i. Primary effect – yaw with secondary roll.<br />

ii. Further effect from being banked, is slip and<br />

yaw leading to increased bank and spiral<br />

descent due to weather cocking effect.<br />

iii. Recovery as for spiral dive.<br />

Note: this exercise is to demonstrate the correct<br />

use of the flight controls:<br />

Change.<br />

Check.<br />

Hold.<br />

HIGH AIRSPEED:-<br />

i. Firm feel.<br />

ii. Increased effectiveness of controls.<br />

Relatively small movements result in large<br />

changes in attitude.<br />

LOW AIRSPEED:-<br />

i. Reduced feel.<br />

ii. Reduced control effectiveness especially<br />

aileron. Large control movements result in<br />

small changes of attitude.<br />

REDUCED SLIP STREAM:-<br />

i. Reduced feel.<br />

ii. All controls relatively ineffective. Large<br />

movement for comparatively small changes<br />

of attitude.<br />

INCREASED SLIP STREAM:-<br />

i. Firmer feel on rudder and elevator. Ailerons<br />

unchanged.<br />

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