What is the negative maximum maneuvering load factor at Vne?

What is the negative maximum maneuvering load factor at Vne?

• A. -2.2
• B. -1.0
• C. -2.0
• D. -0.5

Answer: (A)

Limit load factors are the airframe’s certified tolerances for maneuvers, describing the forces the airplane can safely withstand in both directions. Vne is the speed beyond which the airframe must still be able to handle its published limit loads. For this aircraft, the negative (downward) maneuvering limit at Vne is -2.2 g, so the airframe is designed to endure downward loading up to 2.2 g during maneuvers at that speed. This value sets the safety boundary for push-down maneuvers or aggressive descents without risking structural overstress. The other options don’t match the aircraft’s published downward limit, which is why -2.2 g is the correct figure.

Limit load factors are the airframe’s certified tolerances for maneuvers, describing the forces the airplane can safely withstand in both directions. Vne is the speed beyond which the airframe must still be able to handle its published limit loads. For this aircraft, the negative (downward) maneuvering limit at Vne is -2.2 g, so the airframe is designed to endure downward loading up to 2.2 g during maneuvers at that speed. This value sets the safety boundary for push-down maneuvers or aggressive descents without risking structural overstress. The other options don’t match the aircraft’s published downward limit, which is why -2.2 g is the correct figure.