Rotax 912 Series Installation Manual

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INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
10-10-00
page 1
August 01/2012
Chapter: 10-10-00
STORAGE AND INSTALLATION
Introduction
Table of contents This section of the Installation Manual contains state of delivery, trans-
port, storage and aircraft engine installation.

WARNUNG
NOTICE
The stated directives are measures that must be ob-
served during every engine installation to prevent any
accidents and engine damage.
Subject Page
Preparations for engine installation
State of delivery
Unpacking/handling of the engine
Preservation and storage of the engine
Protective coverings
Page 3
Page 3
Page 3
Page 4
Page 5
Engine suspension and installation position
Engine suspension instructions
Attachment points
Definition of attachment points
Permissible installation positions
Page 6
Page 6
Page 8
Page 9
Page 12
Preparations for trial run of engine
Conduct test run
Verification of the throttle lever detent for max.
continuous power
Page 14
Page 14
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