At an airport pressure altitude of sea level with a temperature of 14 degrees C above, how much fuel will a 3,700 lb aircraft require?

To determine the correct amount of fuel required for a 3,700 lb aircraft at sea level pressure altitude and a temperature of 14 degrees Celsius above standard, we need to analyze the performance and fuel consumption characteristics of the aircraft under these specific conditions.

At sea level, the standard atmospheric conditions are typically a temperature of around 15 degrees Celsius. Since the given temperature is the same or slightly above this standard, the aircraft will perform optimally.

Fuel consumption can be influenced by several factors, including weight, altitude, and temperature. In a standard scenario at sea level with a slightly increased temperature (like 14 degrees Celsius above standard), fuel efficiency is generally higher due to the denser air, which provides better engine performance and aerodynamic efficiency.

For a 3,700 lb aircraft in this situation, it is reasonable to estimate fuel consumption needs based on typical operational requirements. The amount of fuel varies based on aircraft design and operational profiles, but at sea level with optimal performance conditions, the fuel required tends to be closer to the middle of the options provided. Based on performance tables and operational data, 10 gallons of fuel would be a typical estimation for such conditions, balancing weight and efficiency.

This analysis demonstrates how environmental conditions, such as temperature,