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9.1. Introduction
The weight, useful weight and centre of gravity information is described in this chapter.
9.2. Empty Weight
The weight of aircraft full equipped, without fuel and pilot. It is weighed as a total weight of
all wheels weights.
The empty weight of the ATEC 212 SOLO including ROTAX 912 UL 80 HP and standard
equipment with / without rescue system is
……………………………… kg
9.3. Maximum take-off weight
300 315 kg
Never exceed the maximum take-off weight
9.4. Centre of gravity range
The aircraft CG including the pilot of 75 kg without fuel is
32,6 % of MAC
The flight range of CG specified by manufacturer is
28 – 36% of MAC
Operation over this range is prohibited