Flight Instructors Training Procedures _revised AIC_x

6. Adverse Aileron Yaw:
i. Newton’s Law – for each action there is an equal and opposite reaction.
ii. Lift/Drag relationship.
iii. Total Drag graph to indicate the effect of speed on induced drag reason for
demonstration at low speed.
iv. Pressure distribution around a wing. Reason for use of:
a. Differential ailerons.
b. Frise ailerons.
v. Use of rudder during aileron application for balance.
7. Discuss the further effects of:
i. Elevators – none.
ii. Ailerons – continuous roll, turn, slip, weathercock, resulting in spiral
dive.
iii. Rudder – continuous yaw, skid roll, turn, resulting in spiral dive.
8. Recovery from a spiral dive:
i. Power – throttle closed.
ii. Wings level and balance.
iii. Nose position – attain climb attitude.
iv. Power – open throttle as required.
9. Discuss the effects of:
i. Airspeed.
ii. Slipstream.
iii. Power changes – couples, torque and slipstream effects.
iv. Flaps – movement of centre of pressure, downwash over tailplane, total drag increase
and dragline lowered – resulting in pitching moment.
v. Undercarriage.
10. Working of the trimmer – discuss.
11. Engine controls:
i. Throttle.
ii. Pitch.
iii. Mixture – operation and idle cut off.
iv. Carburettor Heat.
v. Cowl flaps.
vi. Primer – correct priming (over priming – danger of fire.)
vii. Ventilation and cabin heat.
viii. Radio stack.
3. DESCRIPTION OF AIR EXERCISE
a. APPLICABLE PROCEDURES AND CHECKLISTS
b. AIRCRAFT HANDLING TECHNIQUES:-
DEMONSTRATION OBSERVATION
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NOTE:
A/C responds continuously until control is returned to
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