What is the maximum load factor for asymmetric configuration with gear and flaps extended?

• A. +2.5 Gs
• B. +4.7 Gs
• C. +7 Gs
• D. +0 Gs

Answer: (A)

The maximum load factor for an aircraft in an asymmetric configuration with the landing gear and flaps extended is +2.5 Gs. This is established based on the aircraft's design limitations to ensure structural integrity and safety. When the aircraft is in an asymmetric state, particularly with landing gear and flaps extended, it is more vulnerable to aerodynamic forces, which can affect performance and handling.

The load factor indicates how much additional gravitational force the aircraft can safely withstand compared to normal earth gravity. Exceeding this limit can lead to structural failure or unrecoverable flight conditions. The +2.5 Gs limit is set considering the potential for adverse flight characteristics and loss of control that can accompany fuel asymmetry or other discrepancies in lift between the wings.

In this context, the higher load factor options are not applicable, as they do not account for the reduced structural integrity associated with an extended flap configuration and landing gear, which inherently limits the aircraft's performance. Understanding the implications of these limits is crucial for safe operating conditions and effective flight management.