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Principles of Flight Chapter 3 – Stability and Control
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Page 1: Principles of Flight Chapter 3 – Stability and Control.

Principles of Flight

Chapter 3 – Stability and Control

Page 2: Principles of Flight Chapter 3 – Stability and Control.

Stability

An Aircraft must be stable in flight in order to perform well

Also we must be able to control the aircrafts movement.

Page 3: Principles of Flight Chapter 3 – Stability and Control.

Yaw

Aircraft turns left or right

Page 4: Principles of Flight Chapter 3 – Stability and Control.

Controlling - Yaw

Using the rudder pedals the pilot moves the rudder left or right to change the aircrafts direction.

Page 5: Principles of Flight Chapter 3 – Stability and Control.

Pitch

Aircrafts noses Up or Down

Page 6: Principles of Flight Chapter 3 – Stability and Control.

Controlling - Pitch

Moving the stick forwards/back lifts or lowers the aircrafts nose by generating more or less lift at the tail

It uses Elevators to do this

Page 7: Principles of Flight Chapter 3 – Stability and Control.

Roll

Aircraft “twists”

Page 8: Principles of Flight Chapter 3 – Stability and Control.

Controlling - Roll

Moving the stick left/right rolls the aircraft by generating more lift on one side.

It does this by moving flaps known as Ailerons

Page 9: Principles of Flight Chapter 3 – Stability and Control.

Trimming

When an aircraft pitches involuntarily it needs to be trimmed.

Small flaps mounted on the Elevators called “Trimming tabs” jut out from the elevators to increase the camber.

Aileron and Rudder trimming is the same

Page 10: Principles of Flight Chapter 3 – Stability and Control.

Flaps

Flaps increase wing camber and/or area

Page 11: Principles of Flight Chapter 3 – Stability and Control.

Flaps

Flaps allow aircraft to fly safely at slow speeds

They are mounted on the inside of the wings and can hinge down to increase lift at slow speeds

Page 12: Principles of Flight Chapter 3 – Stability and Control.

Slats

Like flaps at the front of the wingThey slide out of the leading edge and

are used at low speedPositioned on leading edge of the wing