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Flight Instructors Training Procedures _revised AIC_x

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16. THE GYROSCOPIC EFFECTS OF THE PROPELLER WITH POWER ON<br />

Where the propeller turns clockwise as viewed from the cockpit, an increase in power during<br />

the spin will cause the spin to flatten if spinning to the left and to pitch nose down if spinning to<br />

the right.<br />

17. EFFECT OF FLAP<br />

Discuss the effect of flap on the spin.<br />

18. EFFECT OF MASS AND BALANCE<br />

Discuss the effect of mass and balance distribution on the spin.<br />

3. DESCRIPTION OF AIR EXERCISE<br />

a. APPLICABLE PROCEDURES AND CHECKLISTS<br />

b. AIRCRAFT HANDLING TECHNIQUES:-<br />

DEMONSTRATION OBSERVATION<br />

1. THE STUDENT’S FIRST SPIN<br />

i. The considerations are the same as those for<br />

the student’s first stall, so the first spin should,<br />

therefore, be done at the end of the lesson<br />

preceding that on which spinning is to be taught.<br />

This spin should consist of not more than two<br />

turns. To give the student as little time for<br />

thought and worry it helps if he is kept busy with<br />

flying the aircraft and doing all the necessary<br />

actions right up to the moment of the entry.<br />

2.<br />

i.<br />

SPINS FROM STRAIGHT AND LEVEL<br />

FLIGHT<br />

Demonstrate spins in both directions (lead with<br />

rudder in direction of intended spin).<br />

,,<br />

i. Lookout.<br />

ii. Complete pre-stall checks (HASSELL).<br />

iii. Inspection turn.<br />

iv. No a violent manoeuvre.<br />

v. Ease of recovery.<br />

vi. Check position frequently in relation to<br />

landmarks during the exercise.<br />

i. Lookout.<br />

ii. Pre-stall checks (HASELL).<br />

iii. Entry:<br />

a. As for normal power-off stall.<br />

b. Just prior to the stall, simultaneously<br />

apply full rudder in the direction of the<br />

desired spin and move the control<br />

column fully back.<br />

c. Ensure throttle fully closed.<br />

d. Carb heat as required.<br />

iv. In the spin:<br />

a. Ailerons neutral.<br />

b. Rudder – full on.<br />

c. Control column – fully back.<br />

Note:<br />

a. High rate of descent – altimeter/VSI.<br />

b. Direction of turn needle – position of<br />

ball.<br />

c. No continuous increase in airspeed.<br />

!"#$ %# &"" '$ #

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