Rotax 912 ULS 3 - Operating Instructions

Effectivity: 912 Serie BRP-Powertrain page 2-1
OM Edition 2 / Rev. 0 April 01/2010
d04674.fm
2) Operating instructions
Introduction 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).
Table of contents 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.
Subject Page
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
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page 2-2
page 2-2
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page 2-2
page 2-3
page 2-3
page 2-4
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page 2-5
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page 2-6
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page 2-7
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page 2-7
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Operating fluids:
Coolant
Fuel
Lubricants
page 2-8
page 2-8
page 2-9
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