Which of the following describes a result of higher density altitude?

Higher density altitude results in a decrease in air density, which significantly impacts aircraft performance. As density altitude increases, the air becomes less dense, which means that the aircraft engine produces less power, the propeller is less effective, and the wings generate less lift. This reduction in lift and power leads to a slower climb rate because the aircraft will struggle to gain altitude as effectively as it would at lower density altitudes.

The other choices do not accurately reflect the consequences of higher density altitude. For instance, increased takeoff weight capacity is typically a characteristic of lower density altitudes because the aircraft can support a heavier weight more effectively with denser air. Better ground maneuverability and lower stall speeds also relate to more favorable flying conditions found at lower density altitudes, where conditions support greater lift and control responsiveness. Thus, the correct statement pertains directly to the compromised climb performance experienced at higher density altitudes.