What is the CG location of a nose wheel airplane with specified weight and tare values?

To determine the center of gravity (CG) location for a nose wheel airplane, you need to consider the airplane's weight distribution and any tare values that might apply. The CG position is a critical factor in ensuring the airplane's stability and handling characteristics.

The specified weight and tare values in this question likely refer to measurements that are used to calculate where the CG of the aircraft lies in relation to its overall design. The calculation involves taking into account the weight of the airplane along with any additional factors, such as the position of fuel, cargo, and occupants.

In this context, the value of 15.4 could represent a well-established or calculated value based on standard procedures for determining the CG of the aircraft, and it falls within the typical range expected for a nose wheel airplane. This particular CG location would ensure the aircraft maintains appropriate stability in flight, aligning with regulatory standards and operational safety guidelines.

The other values provided may not correspond to standard CG locations for the given scenario or may arise from incorrect calculations based on the tare or weight distributions.