Rotax 914 series Installation Manual

These technical data and the information contained therein are property of BRP-Rotax
GmbH&CO. KG and must not be reproduced, neither entirely nor partially, and passed on
to third parties without previous consent in writing by BRP-Rotax GmbH&CO. KG. This text
must be written on every complete or partial reproduction. The Manual must remain with
the engine/aircraft in case of sale.
Copyright 2008 © - all rights reserved
ROTAX
®
is a trademark of BRP-Rotax GmbH&Co.KG. In the following document the short
form BRP-Rotax instead of BRP-Rotax GmbH&Co. KG will be used.
Other names of products used in this book, are used to recognize the familiar and can be
trademarks of corresponding companies or owners.
Approval of translation has been done to best knowledge and judgment in case the original
text in the German language is authoritative.
WARNING
Before starting with engine installation, please read the Installation Manual completely as it
contains important safety relevant information.

Rotax 914 series Specifications

General

Bore	79.5 mm
Stroke	61 mm
Compression Ratio	9.0:1
Cooling System	Liquid-cooled cylinder heads, air-cooled cylinders
Redline	5800 rpm
Engine Type	4-cylinder, 4-stroke
Fuel Type	Avgas 100LL
Oil System	Dry sump
Fuel System	fuel injection
TBO (Time Between Overhauls)	2000 hours
Displacement	1.211 liters (1211 cc)
Power Output	84.6 kW (115 hp) at 5, 800 rpm