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The aircraft is established in a normal-law climb. Immediately after the pilot releases the sidestick to neutral, the flight controls will:

Correct! Wrong!

The aircraft is in level flight and the normal law is active. With the sidestick released and airspeed slowed by 20 kt, the flight controls will:

Correct! Wrong!

The sidestick inputs result in adjusting:

Correct! Wrong!

Maximum operating altitude with slats and/or flaps extended is:

Correct! Wrong!

In normal law, the aircraft is established in a 20-degree left turn, to maintain the altitude. The pilot:

Correct! Wrong!

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All flight controls are:

Correct! Wrong!