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Flight Instructors Training Procedures _revised AIC_x

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4. EFFECT OF TRIM<br />

i. The student maintains a constant attitude<br />

while each trimmer is moved in turn. The<br />

student then adjusts the trimmers until the<br />

control forces are removed. Use cruise<br />

power.<br />

ii. Effect of power changes on trim.<br />

5. EFFECT OF THROTTLE, PROPELLER<br />

CONTROL AND MIXTURE CONTROL<br />

)<br />

ii. Larger rudder and elevator effectiveness.<br />

Smaller movements for comparatively large<br />

changes of attitudes. Ailerons unchanged.<br />

(The feel of ailerons is a good indication of<br />

airspeed).<br />

i. Increasing load on rudder or elevator.<br />

ii. Sense of trim control movements.<br />

iii. Adjustment to relieve control forces.<br />

iv. Thus aircraft remains in the selected<br />

attitude when accurately trimmed.<br />

NOTE:<br />

Demonstrate that the initial adjustment to the aircraft<br />

attitude should be made by the primary controls and<br />

that the trimmers should then be adjusted until no<br />

force is required on the controls to maintain attitude:-<br />

Change, Check, Hold and Trim. During this<br />

demonstration, ensure that the student has his hands<br />

and feet resting lightly on the controls, otherwise he<br />

may fail to identify the zero force trim setting.<br />

i. Lookout.<br />

ii. Note nose attitude and heading.<br />

iii. Reduce power to 55%.<br />

iv. Maintain nose attitude and heading.<br />

v. Note increased back pressure required on<br />

control column to maintain nose attitude.<br />

vi. Note rudder input required for balanced<br />

flight<br />

vii. Re-trim elevator and rudder.<br />

viii. Regain cruise power and repeat sequences<br />

(i.-vii.) above.<br />

EFFECT OF THROTTLE:-<br />

i. Sense of throttle movement.<br />

ii. Boost (power) changes.<br />

iii.<br />

EFFECT OF PROPELLER CONTROL:-<br />

i. Sense of control movement.<br />

ii. R.P.M. changes.<br />

iii. At very low boost settings, the throttle<br />

controls the RPM as well as the boost and<br />

the propeller control is relatively ineffective.<br />

EFFECT OF MIXTURE CONTROL:-<br />

i. At high altitudes engines run rough when<br />

the mixture is too rich.<br />

ii. Too lean a mixture will cause an RPM drop.<br />

iii. If leaned off further, the engine will surge<br />

and cut out.<br />

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