Based on weight and balance calculations, if front seat occupants weigh 340 lb, rear seat occupants weigh 295 lb, fuel is 44 gal, and baggage is 56 lb, how is the airplane loaded?

To determine how the airplane is loaded based on weight and balance calculations, it is essential to calculate the total weight and the center of gravity (CG) position.

First, add together the weights of the front seat occupants, rear seat occupants, fuel, and baggage:

• Front seat occupants: 340 lb

• Rear seat occupants: 295 lb

• Fuel: Since fuel weighs approximately 6 lb per gallon, 44 gallons would be 44 * 6 = 264 lb.

• Baggage: 56 lb

Now, summing these weights:

340 lb (front) + 295 lb (rear) + 264 lb (fuel) + 56 lb (baggage) = 955 lb total weight.

Next, we need to compare this total weight with the airplane's maximum allowable weight. If the airplane's maximum weight limit is above 955 lb, then the aircraft is not overweight.

For the CG calculation, you would typically multiply each weight by its respective arm (distance from the reference point, usually the leading edge of the wing or another specified point) to find a total moment. Then, you would total the moments and divide by the total weight to find the CG. If the CG falls within