Weight & fuel

Weight & balance

Loaded weight, moment, centre of gravity and %MAC against the envelope.

Empty aircraftWeightArm

Front seatsWeightArm

Rear seatsWeightArm

BaggageWeightArm

FuelWeightArm

LEMAC (arm)MAC length

Total weight: —
Centre of gravity: —
% MAC: —

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How it works

CG = Σ(weight × arm) ÷ Σweight. %MAC = (CG − LEMAC) ÷ MAC × 100. Load the real arms and limits from the AFM/POH.

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