Shark UL - 2.6. Weight Limits

Page 2-5
Flight manual UL aircraft
2.6. WEIGHT LIMITS
Empty weight: standard version (kg)
290 kg
Empty weight: fully equiped (kg)
320 kg (max 325 kg)
Max. take-off weight:
NO Ballistic Recovery System installed (kg)
450 kg
Max. take-off weight:
Ballistic Recovery System installed (kg)
472,5 kg
Max. crew weight:
calculated for max take-off weight (kg)
177 kg
Min. crew weight: (kg)
55 kg
Max. crew weight: rear seat (kg)
95 kg
Max. one pilot weight: (kg)
110 kg
Max. weight in baggage compartment (kg)
- for solo flight from front seat
25 kg
Max. weight in baggage compartment (kg)
10 kg
MAXIMAL CREW WEIGHT (kg)
depends on fuel and baggage quantity
Fuel tank
filling

Fuel gauge
indication 
full
3/4
1/2
1/4
30 min
of flight
Fuel quantity
in liters 
100
75
50
25
5
kg
72
54
36
18
3,6
Baggage
weight

Max: 10 kg
½ : 5 kg
Without baggage
Max. crew weight has to be written indelibly for specific measured weight of airplane.
WARNING:
Do not exceed these weight limits. Pay attention to fuel quantity,
especially when 2 persons are on board.
DO NOT EXCEED maximum take-off weight.