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VB: Aircraft Contro Instructor: CCPL G. Fleming
13

AVB 5: Aircraft Control - CCPL Fleming - 27 AUG

Jan 19, 2015

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Page 1: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG

AVB: Aircraft ControlInstructor: CCPL G. Fleming

Page 2: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG

AVB: Aircraft Control

• Identify the following control surfaces:a. Aileronb. Rudderc. Elevatord. Trim Tab

• List the Primary effects of the elevator, rudder and aileron flight controls on aircraft movement in flight about the longitudinal, lateral and normal (vertical) axes.

Page 3: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG

Aileron

• They control the lateral (ROLL) movement of the aircraft.• To bank an aeroplane the control column is moved to the left

or right. This moves the ailerons,• Ailerons are situated at the trailing edge of the wings

normally at the outer edge near the wing tips.• To bank to the left, the left aileron goes up causing a decrease

in lift on the left wing, at the same time the right side aileron goes down causing an increase in lift and the aeroplane will bank to the left.

• This is the primary effect; the secondary effect is to cause YAW, as during a bank the nose will have a tendency to slip sideways.

Page 4: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG
Page 5: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG

Rudder

• The rudder controls the directional (YAW) movement and is controlled through the rudder pedals.

• This is the primary effect of rudder movement, the secondary effect is to produce a roll as yawing of the nose to one side will cause the outer wing to speed up,

• Increased lift is the result and a consequent slight rolling.

Page 6: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG
Page 7: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG

Elevator

• The elevators control the lateral (PITCH) of the aircraft.

• The up and down movement of the nose is known as PITCH

• It can be controlled by the movement of the control column backwards and forwards, thereby moving the elevator

• Altering the aerodynamic force produced by the tailplane and changing the pitch of the aeroplane.

Page 8: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG

Trim Tab

• The elevator trim tab is located on the trailing edge of the elevator,

• It is operated by a trim wheel between the front seats.

• It allows the aircraft to be flown with little pressure on the control column.

Page 9: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG
Page 10: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG
Page 11: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG

Questions?

Page 12: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG

Quiz

• What is the primary and secondary effect of the rudder?

• What is the primary and secondary effect of the ailerons?

• Where can I find the trim wheel?

Page 13: AVB 5: Aircraft Control - CCPL Fleming - 27 AUG