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Performancemedium#612

For a Class A aeroplane, the minimum second segment climb gradient with one engine inoperative is:

A

1.2%

B

2.4%

Correct

C

1.5%

D

3.0%

Explanation

CS-25 requires a minimum 2.4% climb gradient during the second segment (gear up, takeoff flaps, OEI) for twin-engine aircraft.

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