Rotax 912 Series Installation Manual

d04926.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
78-00-00
page 1
August 01/2012
Chapter: 78-00-00
EXHAUST SYSTEM
General note See Fig. 1.
Table of contents This section of the Installation Manual contains information on the
exhaust system of the aircraft engines.

WARNUNG
NOTICE
The exhaust system must be designed by the aircraft
or fuselage manufacturer such that the permissible
loads and bending moments on the points of attach-
ment are not exceeded. The exhaust system may re-
quire additional support.
Subject Page
General notes on the exhaust system Page 3
Exhaust system requirements
Technical data
Page 5
Page 5
Attaching of the exhaust system Page 7
Operating limits
Data for optional components of exhaust system
Page 9
Page 10

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