What are the flight load factors with flaps up?

What are the flight load factors with flaps up?

• A. +4.4g, -1.76g
• B. +3.5g
• C. +4.2g, -1.5g
• D. +3.8g, -1.2g

Answer: (A)

The flight load factors describe the maximum vertical loads the airframe is designed to carry in flight. For a Cessna 152 with flaps up, the published limit load factors are +4.4 g in the positive direction and -1.76 g in the negative direction. This means you should not exceed these g-values during maneuvers or gusts to avoid structural overstress. The other options present values that do not match the flaps-up configuration, or mix in figures from different configurations, so they aren’t the correct limits for flaps up.

The flight load factors describe the maximum vertical loads the airframe is designed to carry in flight. For a Cessna 152 with flaps up, the published limit load factors are +4.4 g in the positive direction and -1.76 g in the negative direction. This means you should not exceed these g-values during maneuvers or gusts to avoid structural overstress. The other options present values that do not match the flaps-up configuration, or mix in figures from different configurations, so they aren’t the correct limits for flaps up.