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Rotax 914 series Installation Manual

Rotax 914 series
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Effectivity: 914 Series
Edition 2 / Rev. 0
d04274
page 9
July 01/2008
BRP-Rotax
INSTALLATION MANUAL
3) Preface
In this Manual the installation of all ROTAX 914 Series engines is described.
NOTE: ROTAX 914 Series includes 914 F and 914 UL.
Before starting with the engine installation, read this Installation Manual carefully. The Manual
will provide you with basic information on correct engine installation, a requirement for safe
engine operation.
If any passages of the Manual are not completely understood or in case of questions, please,
contact an authorized Distribution- or Service Center for ROTAX engines.
BRP-Rotax GmbH & Co. KG (hereinafter "BRP-Rotax") wish you much pleasure and
satisfaction flying your aircraft powered by this ROTAX
engine.
3.1) Remarks
This Installation Manual is to acquaint the owner/user of this aircraft engine with basic
installation instructions and safety information.
For more detailed information on operation, maintenance, safety- or flight, consult the
documentation provided by the aircraft manufacturer and dealer.
For further information on maintenance and spare part service contact the nearest
ROTAX distributor (see section 3.3).
3.2) Engine serial number
On all enquiries or spare parts orders, always indicate the engine serial number, as the
manufacturer makes modifications to the engine for further development.
The engine serial number is on the top of the crankcase, magneto side.
3.3) ROTAX Authorized Distributors for Aircraft Engines
See latest Operators Manual or in the Internet at the official Homepage
www.rotax-aircraft-engines.com.

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Rotax 914 series Specifications

General IconGeneral
Bore79.5 mm
Stroke61 mm
Compression Ratio9.0:1
Cooling SystemLiquid-cooled cylinder heads, air-cooled cylinders
Redline5800 rpm
Engine Type4-cylinder, 4-stroke
Fuel TypeAvgas 100LL
Oil SystemDry sump
Fuel Systemfuel injection
TBO (Time Between Overhauls)2000 hours
Displacement1.211 liters (1211 cc)
Power Output84.6 kW (115 hp) at 5, 800 rpm

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