Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 iS
ATEC v.o.s., Libice nad Cidlinou, Czech Republic
Page 47 of 59
8.7.
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 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
kg
Fuel amount
100 L
75 L
50 L
25 L
10 L
Max. weight of crew
CG position in % bMAC
Min. weight of crew
CG position in % bMAC
Max. weight of luggage
Max. weight of crew
CG position in % bMAC
If above listed limits are kept, the centre of gravity is situated in permitted position range.
8.8.
Maximum Useful Load of the Luggage Compartment
Maximum useful load of the luggage compartment is 20 kg. This load is limited by the weight of the crew
according to following weight sheet. For calculation of the max. useful load, an extreme option for max.
rear CG is considered at each given weight of the crew.
Never exceed this load! An overloading of the rear CG may be caused in an extreme situation!