Aircraft Stability

Front

The type of aircraft rotation in the lateral axis is

Back

Pitch

Front

The flight control that helps in controlling the pitching of aircraft is ......................... and located on .........................

Back

elevator and horizontal stabiliser, elevator,horizontal stabiliser, elevator & horizontal stabiliser

Front

Aircraft rotation around the longitudinal axis is

Back

Roll

Front

The flight control surface used to roll an aircraft is/are the ............................ located on the ...........................

Back

Ailerons, wings, Ailerons and wings, Ailerons & wings

Front

The yawing rotation of an aircraft is around the

Back

Vertical Axis

Front

Yawing of an aircraft is accomplished with the ............................ located on the ..........................

Back

Rudder and vertical stabiliser

Front

Turbulent air on the wing is

Back

disrupted airflow on the wing

Front

Two types of stability of an aircraft

Back

Static stability and Dynamic stability, Dynamic stability and static stability, Static and Dynamic, Dynamic and Static

Front

The reliability of the aircraft to respond to the pilot’s commands while carrying out manoeuvres

Back

Controllability