Determine the total distance required to land with an outside air temperature of 90°F, pressure altitude of 3,000 feet, weight of 2,900 lbs, headwind component of 10 knots, and a 50 ft obstacle.

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

In this scenario, the outside air temperature is 90°F, which affects the aircraft's performance because higher temperatures generally decrease air density and can increase the landing distance due to reduced lift and engine efficiency. The specified pressure altitude of 3,000 feet also contributes to decreased air density, further impacting the aircraft's performance.

The weight of 2,900 lbs plays a crucial role, as a heavier aircraft requires a longer distance to land due to its increased energy and the need for more lift at lower speeds. In addition, the headwind component of 10 knots can help reduce the landing roll by providing additional lift and reducing the aircraft's groundspeed upon touchdown.

Considering the requirement to clear a 50 ft obstacle means that the landing distance must also include the distance required to descend and clear this obstacle safely.

Factoring in all these elements, calculations or established performance charts specific to the aircraft type would show that the total distance required to land under these conditions totals 1,725 feet. This figure considers the necessary adjustments for temperature and altitude, aircraft weight, and the effects of the