Determine the total distance required to land with standard OAT, pressure altitude of 10,000 feet, weight of 2,400 lbs, calm wind component, and a 50 ft obstacle.

To determine the total distance required to land, various factors must be considered, including the aircraft's weight, altitude, environmental conditions like temperature and pressure, and the presence of obstacles.

In this scenario, we have a pressure altitude of 10,000 feet and standard OAT (Outside Air Temperature), which means the temperature is around 5 degrees Celsius at that altitude. This combination can lead to a longer landing distance compared to lower elevations, primarily due to the thin air affecting lift and drag.

The specified weight of 2,400 lbs is also key, as heavier aircraft require more distance to decelerate after landing due to the increased momentum. With no wind component, the landing performance is more consistent since crosswinds or headwinds can affect distances significantly.

When a 50-foot obstacle is present, the landing distance increases further as the aircraft must be able to clear that height while also ensuring sufficient runway is available to come to a complete stop effectively.

The total landing distance often includes a baseline landing roll plus required additional distance to clear any obstacles and account for any margin needed for safety. The value of approximately 1,925 feet as the total distance reflects the calculated requirements according to standard landing performance charts specific to the aircraft type being considered,