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Flight Instructors Training Procedures _revised AIC_x

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. Effect of momentum during recovery.<br />

vi. DISCUSS:<br />

With reference to applicable aeroplane type, discuss the planes of movement and application<br />

of previously mentioned principles to slow rolls at lower and higher speeds.<br />

vii. ADVERSE CONDITIONS AND CORRECTION<br />

a. Aileron overbalance.<br />

b. Aileron snatch.<br />

c. Airframe limitations in roll (Manoeuvre Envelope) and possible consequences.<br />

viii. FACTORS AFFECTING THE SLOW ROLL<br />

a. Torque.<br />

b. Slipstream.<br />

c. 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 reference point ± 45° to one side.<br />

vi. Wing-over to the reference point.<br />

vii. Dive until the recommended speed for the<br />

manoeuvre is achieved – check RPM if fixed<br />

pitch propeller is fitted.<br />

viii. Raise nose to just above the horizon (±20°),<br />

apply full power and check climb attitude<br />

before rolling.<br />

ix. Smoothly but firmly apply aileron in direction of<br />

roll and some rudder in the same direction to<br />

compensate for adverse aileron yaw.<br />

x. As aeroplane rolls to the vertical, apply top<br />

rudder as necessary and whilst applying<br />

aileron to control rate of roll, move control<br />

column forward.<br />

xi. Whilst inverted, use rudder to keep straight on<br />

reference point, apply maximum aileron if<br />

necessary and ensure control column forward<br />

to prevent nose dropping below the horizon.<br />

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

xiii. As the aeroplane rolls to the vertical again,<br />

apply top rudder to prevent “scooping” and<br />

whilst continuing to apply full aileron, move the<br />

control column rearwards.<br />

xiv. When the straight and level attitude is once<br />

again reached, set power to that required.<br />

xv. Aim to obtain a constant rate of roll.<br />

xvi. Minimum height for the aeroplane to be on an<br />

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