Rotax 912 Series Installation Manual

d04918.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
00-00-00
page 1
August 01/2012
Chapter: 00-00-00
GENERAL NOTE
Introduction This section describes the installation of engine type ROTAX 912 Series.
NOTE: The ROTAX 912 Series includes all engines such as the
912 A, 912 F, 912 S, 912 UL and 912 ULS.
Table of contents This chapter of the Installation Manual contains general and safety infor-
mation concerning the operation and maintenance of the aircraft engine.
Subject Page
General note Page 3
Type description
Standard version
Page 4
Page 5
Abbreviations and terms used in this Manual
Conversion table
Page 7
Page 9
Safety notice
Safety information
Instruction
Technical documentation
Page 10
Page 11
Page 13
Page 14

Rotax 912 Series Specifications

General

Redline	5800 rpm
TBO	2000 hours
Displacement	1211 cc
Bore	79.5 mm
Stroke	61 mm
Power Output	80 hp (59.6 kW)
Compression Ratio	9.0:1
Fuel Type	Avgas 100LL
Ignition System	Dual electronic ignition
Fuel System	Fuel Injected
Oil System	Dry sump
Engine Type	4-cylinder, horizontally opposed, 4-stroke