Shark 600 - 1.6 Engine

FLIGHT MANUAL
SHARK 600
Section 1
General
2024-02-25
Rev. B
Doc. No.: SHARK600_MA_075
1-7
Vertical Stabilizer
Area: ....................................................... 1.062 m
2
Rudder Area: .......................................... 0.335 m
2
Landing Gear
Track: ...................................................... 1.694 m
Wheel Base: ............................................ 1.48 m
1.6 Engine
Rotax 912 ULS Engine, 4 Cylinder, 4-Stroke, Horizontally Opposed,
Liquid Cooled Cylinder Heads, Air Cooled Cylinders.
Propeller is driven via an integrated Reduction Gear.
Reduction Ratio: ..................................... 2.43 : 1
Displacement;......................................... 1.352 liters
Output Power: ........................................ 73.5 kW / 100hp @ 5800
rpm
1.7 Propeller
Two-bladed Variable Pitch Propeller, manufactured by Woodcomp
and Neuform:
• In-flight electrically adjustable (Woodcomp SR 3000 2WN)
• In-flight hydraulically adjustable (Woodcomp KW20W)
• In-flight electrically adjustable (Neuform TXR2-V-70)