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Rotax 912 Series Installation Manual

Rotax 912 Series
199 pages
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These technical data and the information embodied therein are the property of
BRP-Powertrain GmbH&Co. KG, Austria, acc, BGBI 1984 no. 448, and shall not, without
prior written permission of BRP-Powertrain GmbH&Co. KG, be disclosed in whole or in
part to third parties. This legend shall be included on any reproduction of these data, in
whole or in part. The Manual must remain with the engine/aircraft in case of sale.
Copyright 2012 © - all rights reserved.
ROTAX
®
is a trade mark of BRP-Powertrain GmbH&Co. KG. In the following document
the short form of BRP-Powertrain GmbH&Co. KG = BRP-Powertrain is used.
Other product names in this documentation are used purely for ease of identification and
may be trademarks of the respective company or owner.
Approval of translation has been done to best knowledge and judgement - in any case
the original text in german language is authoritative.
Before starting with engine installation, please read the Installation Manual completely as
it contains important safety relevant information.
WARNING

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Rotax 912 Series Specifications

General IconGeneral
Redline5800 rpm
TBO2000 hours
Displacement1211 cc
Bore79.5 mm
Stroke61 mm
Power Output80 hp (59.6 kW)
Compression Ratio9.0:1
Fuel TypeAvgas 100LL
Ignition SystemDual electronic ignition
Fuel SystemFuel Injected
Oil SystemDry sump
Engine Type4-cylinder, horizontally opposed, 4-stroke

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