Shark 600 - Fuel Tank Capacity; Other Limitations

FLIGHT MANUAL
SHARK 600
Section 2
Limitations
2024-02-25
Rev. B
Doc. No.: SHARK600_MA_075
2-11
2.11.2 Fuel Tank Capacity
Fuel Tank Type
Standard
Long Range
Capacity each tank
50 liters
13.2 US gal
75 liters
19.8 US gal
Total Fuel capacity
100 liters
26.4.US gal
150 liters
39.6 US gal
Unusable Fuel
1 liter
2.12 Other Limitations
Maximum Demonstrated Cross Wind
Component
12 kts
6 m/s
Maximum Demonstrated Head Wind
Component
30 kts
15m/s
Maximum Outside Temperature
50°C
Minimum Outside Temperature
-25°C
CAUTION
Heavy rain or excessive moisture can cause decrease of airplane
performance. Increase take-off and landing speeds by 10 km/h.