I'm confident I have it right. The empty plane bit has an ARM back from the leading edge. The weight at that point is the entire weight of the empty plane with 2.9L of unusable fuel. ARM x Weight = Moment. Total moments / total weight gives the CG.
Empty weight determination
The empty weight of an aircraft includes all operating equipment that has a fixed location and is
actually installed in the airplane. It includes the weight of the painted airplane, accumulator, standard and optional equipment, full engine coolant, hydraulic fluid, brake fluid, oil and unusable
fuel 2.9 l. The aircraft is weighed without crew, fuel and baggage.
Anyway if you guys are calculating W&B before each flight then your opinion is more important to me than the expert (ex is a hasbeen and spurt is a drip under pressure) who learned it from a book.