What is the maximum G loading for Flaps Retracted?

What is the maximum G loading for Flaps Retracted?

• A. 2.5 G
• B. 2.0 G
• C. 3.0 G
• D. 1.5 G

Answer: (A)

In clean configuration, the airplane’s structure is built to tolerate a defined maximum positive load factor, which is 2.5 g. This value represents the greatest gust or maneuver load the airframe can safely withstand with the flaps retracted, without risking structural damage. Therefore, the maximum G loading for Flaps Retracted is 2.5 g. Values higher than this would exceed the certified limit and could stress the airframe, while lower figures would not reflect the actual certified limit.

In clean configuration, the airplane’s structure is built to tolerate a defined maximum positive load factor, which is 2.5 g. This value represents the greatest gust or maneuver load the airframe can safely withstand with the flaps retracted, without risking structural damage. Therefore, the maximum G loading for Flaps Retracted is 2.5 g. Values higher than this would exceed the certified limit and could stress the airframe, while lower figures would not reflect the actual certified limit.