What is the calculated density altitude based on the given conditions?

To calculate density altitude, one needs to understand its relationship to pressure altitude and temperature. Density altitude represents the altitude at which the air density is equal to the standard atmosphere at a given temperature.

The process includes determining the pressure altitude, which is typically determined from the altimeter setting, and correcting it based on the difference between the actual air temperature and the standard temperature for that altitude. If the actual temperature is warmer than the standard temperature, the density altitude increases.

In the case where the calculated density altitude is given as 4,097 feet, this would suggest that the pressure altitude, combined with temperature adjustments, results in a density altitude that accounts for the reduction in air density due to the higher temperature.

This particular value would be reached by properly applying the formulas and considerations for altitude and temperature. A density altitude of 4,097 feet means that the air is less dense than it would be at the standard atmospheric conditions, which affects aircraft performance, such as engine power, lift, and climb rates.

In flight operations, understanding density altitude is crucial, especially in hot environments or at higher elevations, as it directly influences aircraft performance characteristics. The other options, while plausible, do not fit as accurately into the necessary calculations that would yield the