Shark UL - 7.7.1. Technical Data

Page 7-17
Flight manual UL aircraft
7.7.1. Technical data
Performances for standard conditions (MSA/ISA).
Engine Model
912 ULS D.C.D.I.
Engine power
69,0 kW (95,0 hp) at 5500 RPM
Max. 5 min.:
73,5 kW (100,0 hp) at 5800 RPM
Torque
128 Nm at 5100 RPM
Maximum speed
5800 RPM
Bore:
84,0 mm
Stroke:
61 mm
Cilinder 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 at 5 500 RPM
Voltage:
13,5 V
OPERATING FILLING:
Fuel:
Natural 95 or AVGAS 100 LL
Olej:
API SF or SG, 100LL, not synthetic oil
Coolant:
50% BASF Glysantin-Antikorrosion / 50%
water
WEIGHT- engine
Standard engine with gearbox i=2,43
56,6 kg (124,8 lb.)
Oil cooler 886 029
0,5 kg
Radiator 995 697
1,0 kg
Slip clutch
1,0 kg
Fuel pump incl. pipes
0,2 kg
Vacuum pump
0,8 kg
External alternator 40 A/ 12 V DC
3,0 kg
Rectifier
0,1 kg