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Which Force does Thrust oppose

Drag (correct)

Lift

Weight

None of above

Which motion is along lateral axis of aircraft

Roll

Pitch (correct)

Yaw

None of above

Which control surface is primary

Slats

Flaps

Spoilers

Rudder (correct)

Which of the statements is false

Cambered aerofoil helps create low pressure area at the bottom of the aerofoil Signup and view all the answers

When two aircraft are approaching head on, which rule applies

Both would alter heading to starboard Signup and view all the answers

Which of the statements is true

If I see an aircraft with its red navigation light to the left and green navigation light to the right then the aircraft is going away from me Signup and view all the answers

Which of these primary control surfaces move in opposite directions

Ailerons Signup and view all the answers

Which of these statements is true

Slats are located at forward end of wings Signup and view all the answers

Which of these aircraft parts are used to reduce vortex rings

Winglets Signup and view all the answers

Which of these statements is true

Basic parts of an aircraft are fuselage , Wings , Tail or empennage and landing gear Signup and view all the answers

Secondary part which helps power up a system before engines are started is

APU Signup and view all the answers

A pilot wears how many stripes on the shoulder

Four Signup and view all the answers

Which law of Newton comes in force in Thrust

Third Signup and view all the answers

Where is the maximum lift generated with all other factors equal

Mumbai Signup and view all the answers

Select the right answer

To generate more lift, Flaps, Elevators and Ailerons are pulled down so as to increase the camber. Signup and view all the answers

Which law states that higher the velocity of air, lower would be the low pressure area

Bernoulis Signup and view all the answers

Which statement is false

Drag increases with increase in angle of attack and increase in lift Signup and view all the answers

Which of the statements is true

As the angle of attack increases beyond the optimum for lift, the drag component increases beyond the lift component and aircraft stalls ie loses height rapidly which is catastrophic at lower levels close to the ground. Signup and view all the answers