Flight and Operations Manual of ATEC 321 Faeta ultralight aircraft with Rotax 912 iS Sport
ATEC v.o.s. Libice nad Cidlinou, Czech Republic Page 45 of 56
8.6. Useful load, weight sheet
Useful load is the weight difference between the maximum take-off weight and the empty weight
determined by weighing.
When the aircraft empty weight is kg, the useful load is kg.
Aircraft weight and centre of gravity sheet, fuel tanks 2 x 50 L, take-off weight 472,5 kg
If above listed limits are kept, the centre of gravity is situated in permitted position range.
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