Shark UL - 6.1. Weight and Center of Gravity Determination for Flight

Page 6-3
Flight manual UL aircraft
6.1. WEIGHT AND CENTER OF GRAVITY
DETERMINATION FOR FLIGHT
Weight limits are described in section 2 of this manual.
Permitted centre of gravity range for airplane ready to fly (including
fuel, crew and baggage) is: 16 - 34%
When the airplane is occupied according to the following table, the
limits can be met for airplane with an empty weight of 290 325 kg
and center of gravity between 15 to 20%.
Front seat max
Rear seat max
Bggage max
solo
110 kg
0
25 kg
2 + baggage
110 kg
69 kg
10 kg
2 max
110 kg
88 kg
0
These weights are limited by the rear center of gravity and lower weight of
empty airplane, so it is possible to increase these limits for a particular
airplane according to the specific weighting data of the individual airplane.
Airplane seriál number:
Empty plane weight
kg
CG of empty plane
% BSAT
Front seat max
Rear seat max
Bggage max
solo
110 kg
0
25 kg
2 + baggage
110 kg
kg
10 kg
2 max
110 kg
kg
0