Rotax 912 Series Operator's Manual

9) Supplement
Topics in this chapter
9.1 Form ....................................................................................................2
See Form
According to the regulation of EASA part 21 A.3 / FAR 21.3 the
manufacturer shall evaluate field information and report to the
authority. In case of any relevant occurrences that may involve
malfunction of the engine, the form on the next page should be
filled out and sent to the responsible ROTAX® authorized
aircraft engines distributor or their independent service center.
NOTE
The form is also available from the official ROTAX® AIRCRAFT
ENGINES Website in electronic version.
Authorized
Distributor
Overview of ROTAX® authorized aircraft engines distributor or
their independent service center.
Refer to the official ROTAX® AIRCRAFT ENGINES Website
www.FLYROTAX.com.
Effectivity: 912 Serie
Edition 4 / Rev. 0
BRP-Rotax Page 9-1
November 01/2016

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