Shark 600 - Powerplant

FLIGHT MANUAL
SHARK 600
Section 7
Airplane Description
2024-02-23
Rev. C
Doc. No.: SHARK600_MA_075
7-33
7.9 Powerplant
Engine
Rotax 912 A3. 4 cylinder, 4 stroke engine, horizontally opposed,
liquid cooled cylinder heads, air cooled cylinders.
Propeller is driven through an integrated reduction gear.
Technical data
Performances figures are valid for standard conditions (MSA/ISA).
Engine Model
912 ULS D.C.D.I.
Engine power
Max. 5 min.:
69.0 kW (95 hp) @5500 RPM
73.5 kW (100 hp) @5800 RPM
Torque
128 Nm @ 5100 RPM
Maximum speed
5800 RPM
Bore:
84.0 mm
Stroke:
61.0 mm
Cylinder capacity:
1352.0 cm
3
Compression ratio:
10,5:1
Ignition:
DUCATI double CDI
Ignition timing:
4° to 1000 RPM / above 26°
Sparking plugs:
ROTAX part no. 297 940
Generator output:
250 W DC @ 5500 RPM
Voltage:
13,5 V