Flight Instructors Training Procedures _revised AIC_x

1. EFFECT OF FLYNG CONTROLS
i Demonstrate the primary effect of each control
. from straight and level flight at cruise power.
(Momentary Application).
ii. Demonstrate the primary effects in a banked
attitude.
iii. Adverse aileron yaw. Set power applicable to
aircraft type.
a. Demonstrate from straight and level
flight at slow speed, rolling the aircraft
with ailerons only (Hold rudder pedals
neutral).
b. Repeat the exercise using rudder to
counteract the effect of adverse aileron
yaw (co-ordinated turn).
iv. Demonstrate the further effects from straight
and level flight, at cruise power. (At this stage
do not allow the spiral to develop in too steep
an attitude as this may lead to air sickness
and may also frighten the pupil).
)*
neutral position. Smooth progressive control
movements desired.
ELEVATORS:-
i. Lookout.
ii. Fore and aft movement of the control
column.
iii. Direction of nose movement relative to
aircraft.
iv. Airspeed changes.
v. Direction of nose movement relative to the
horizon.
AILERONS:-
i. Lookout.
ii. Lateral movement of the control column.
iii. Direction of wing movement relative to the
aircraft.
iv. Direction of nose movement relative to the
horizon/turning.
RUDDER:-
i. Lookout.
ii. Rudder pedal movements.
iii. Nose movement – yawing.
Relationship of the rate and amount of movement of
the flying controls to the movement of the aircraft.
The effect is in relation to the aircraft axis and not the
horizon.
i. Lookout.
ii. Select reference point on horizon.
iii. Apply aileron input.
iv. Note that nose yaws initially to the opposite
side of the roll.
ELEVATORS – No further effect.
AILERONS:-
i. Lookout.
ii. Primary effect – roll and turn.
iii. Further effect from being banked, is slip and
yaw, leading to increased bank and spiral
descent due to weather cocking effect.
iv. Note: Angle of bank steepens, airspeed
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