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Flight Instructors Training Procedures _revised AIC_x

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1. AIM<br />

DEFINITION<br />

SIDE SLIPPING<br />

An aircraft may be considered to be side slipping when it’s flight path is at an angle to the heading<br />

of the aircraft’s nose and is achieved by a cross-controlled condition of flight applied during a<br />

straight glide or gliding turn.<br />

According to the definition there are three definite types of sideslip which have to be discussed,<br />

namely:<br />

i. Nose yawed.<br />

ii. Slipping turns.<br />

iii. Nose straight.<br />

WHAT THE INSTRUCTOR IS TO TEACH<br />

i. Discuss the aerodynamic principles involved.<br />

ii. The air exercise briefing:<br />

a. Applicable <strong>Procedures</strong> and Check lists.<br />

b. Aircraft handling techniques:- Demonstration and Observation.<br />

c. Considerations of Airmanship and engine handling.<br />

d. Similarity to previous exercises.<br />

e. De-briefing after flight.<br />

WHY IT IS BEING TAUGHT<br />

To accustom the student pilot to side slipping the aircraft, and instil confidence in handling the<br />

aircraft with Maximum deflection of the flight controls, and to have a complete understanding of the<br />

theory which eventually determines:<br />

i. The aircraft configuration.<br />

ii. The IAS – attitude relationship (position of static vent).<br />

iii. The effect of ailerons and rudder.<br />

iv. The effect of wind (head, tail and crosswind.)<br />

HOW THE EXERCISE APPLIES TO FLYING<br />

i To get rid of excess height during an approach.<br />

ii Crosswind landing.<br />

iii Engine fire – to divert flames and smoke from cabin.<br />

iv Flap failure.<br />

2. PRINCIPLES INVOLVED<br />

i. Forces in a glide.<br />

ii. Forces in a turn.<br />

iii. Newton’s laws.<br />

iv. Forces during a side slip.<br />

v. Lift/drag relationship.<br />

vi. Wind effect – crosswind and gradient.<br />

vii. Airspeed indicator errors.<br />

viii. Effect of flaps – downwash over elevator and rudder reduces effective.<br />

*<br />

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