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 43 of 56
8.1. Introduction
Weight, useful load and centre of gravity data are described in this chapter.
8.2. Empty Weight
The empty weight is the weight of fully equipped, ready to operate aircraft, excluding fuel and crew.
Empty weight is a total sum of all weight values measured under all undercarriage wheels
simultaneously.
The empty weight of the aircraft is
kg
8.3. Maximum Take-off Weight
The maximum take-off weight defined by the Manufacturer and Czech UL 2 regulation is
472,5 kg
Never exceed the maximum take-off weight!
8.4. Centre of Gravity (CG) Range
CG of the empty aircraft % of MAC
Permitted range of the CG in flight 27 - 36 % of MAC
Operation over this range is prohibited!
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