Engine Limitations; Rotax 912Uls - Skyleader 200 Pilot Operating Handbook

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2.4.

Engine limitations

2.4.1. Rotax 912ULS

Specifications stated in this article are not complete.
For more information, see engine Operator's Manual.
KP 2U POH 05/2022
R912ULS
Takeoff RPM
Max. RPM
Iddle RPM
Oil pressure
Oil temperature
Coolant temperature
Exgaust gas
Fuel pressure
Fuel consumption
The engine have no airwothiness certificate and it could fail at any time !!
The pilot of the ULL aircraft is responsible for any consequences of the engine failure !!!
Value
5800 1/min
5500 1/min
1400 rpm
max: 7 bar (102 psi), min 0.8 bar (12 psi) below 3500 rpm
normal: 2.0 - 5.0 bar (29-73 psi) above 3500 rpm
min: 50°C (120°F), max 130°C (266°F)
normal: approx. 90 to 110°C (190-230°F)
max: 120°C (248°F)
max: 880°C (1616°F)
min: 0.15 bar (2.2 psi), max 0.4 bar (5.8 psi)
max 0.5 bar (7.26 psi) - for applicate only for fuel pump from
S/N 11.0036
27.0 l/h (7.1 gal/h) at takeoff performance
25.0 l/h (6.6 gal/h) at max. continous performance
18.5 l/h (4.9 gal/h) 75% at max. continous performance