Rotax OM-912 Operator's Manual page 24

Introduction
Table of contents
Effectivity: 912 Series
OM Edition 2 / Rev. 0
2) Operating instructions
The data of the certified engines are based on type certificate of
type 912 A JAR 22 (TC No. EASA.E.121),
912 F/S FAR 33 (TC No. E00051 EN),
JAR-E (TC No. EASA.E.121).
This chapter of the Operators Manual contains the operating limits
that must be observed to ensure the ROTAX aircraft engine and
standard systems operate safely.
Operating limits (912 A/F/UL)
Performance
Speed
Acceleration
Oil pressure
Oil temperature
EGT
Conventional coolant
Waterless coolant
Engine start temperature
Fuel pressure
Power consumption of the hydraulic propeller
governor
Power consumption of the vacuum pump
Power consumption of the external alternator
Deviation from bank angle
Operating limits (912 S/ULS)
Performance
Speed
Acceleration
Oil pressure
Oil temperature
EGT
Conventional coolant
Waterless coolant
Engine start temperature
Fuel pressure
Power consumption of the hydraulic propeller
governor
Power consumption of the vacuum pump
Power consumption of the external alternator
Deviation from bank angle
Operating fluids:
Coolant
Fuel
Lubricants
BRP-Powertrain
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April 01/2010