6-4
6.3 Loaded weight and balance calculations via diagram
Determine empty aircraft weight and empty aircraft centre of gravity position (see
chapter 6.2).
Subtract the centre of gravity position shift increment for each individual item (crew,
luggage, fuel) on the graduated scale.
Sum up so determined increments and add them to the empty aircraft CG.
The total gives the aircraft centre of gravity position at the chosen payload of each
item given in % MAC and must fit within the allowed centre of gravity position range
(22
– 32,5 % MAC).
