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Flight Instructors Training Procedures _revised AIC_x

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. Mass.<br />

c. Drag.<br />

d. Power.<br />

3. DESCRIPTION OF AIR EXERCISE<br />

a. APPLICABLE PROCEDURES AND CHECKLISTS<br />

b. AEROPLANE HANDLING TECHNIQUES:-<br />

DEMONSTRATION OBSERVATION<br />

1. SLOW ROLL (AXIAL) i. Look out.<br />

ii. Complete aerobatic checks – HASELL.<br />

iii. Set climb power if C.S.U. is fitted.<br />

iv. Set trimmers for straight and level flight.<br />

v. Select a line feature and reference point ±45°<br />

to the right of the line feature (i.e. to execute a<br />

barrel roll to the left side).<br />

vi. To enter barrel roll, do a wing-over onto the<br />

selected reference point to the right of the line<br />

feature.<br />

vii. In the dive – check engine RPM if fixed pitch<br />

propeller is fitted.<br />

viii. Ease out of dive just before target speed for<br />

the manoeuvre is attained – ensure that wings<br />

are level with the horizon on selected reference<br />

point.<br />

ix. If fixed pitch propeller is fitted, apply full power<br />

as nose rises above the horizon.<br />

x. Simultaneously, apply aileron to the left to<br />

produce the roll, balancing with rudder, whilst<br />

maintaining a backward pressure on the control<br />

column (elevators) to ensure the aeroplane<br />

spirals round the selected line feature.<br />

xi. To keep rate of roll constant, aileron deflection<br />

will vary with speed – ensure that wings are<br />

level with the horizon when inverted at the 90°<br />

reference point.<br />

xii. Observe engine limitations in inverted flight.<br />

xiii. Adjust elevators to assist in maintaining a<br />

smooth roll – avoiding negative “g”.<br />

xiv. Continue until wings are about to become level<br />

and then smoothly centralize the controls.<br />

xv. Barrel roll should be completed at the same<br />

point on the horizon and at the same target<br />

speed, where the manoeuvre was commenced<br />

– check with line feature.<br />

xvi. Reduce power to that required.<br />

xvii. Minimum height for the aeroplane to be at an<br />

even keel 2000ft agl.<br />

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