Rotax 912 i series Operator's Manual

Effectivity: 912 i Series BRP-Powertrain page 9-1
OM Edition 1/Rev. 0 January 01/2012
d05698.fm
9) Supplement
Introduction According to the regulation of EASA part 21 A.3 / FAR 21.3 the
manufacturer shall evaluate field information and report to the au-
thority. In case of any relevant occurrences that may involve mal-
function of the engine, the form on the next page should be filled
out and sent to the responsible authorized ROTAX
®
distributor.
NOTE: The form is also available from the official
ROTAX
®
AIRCRAFT ENGINES Website in
electronic version.
www.FLYROTAX.com
Table of content This chapter of the Operators Manual contains the form and the
list of authorized distributors for ROTAX aircraft engines.
Subject Page
Form Page 9-3
Authorized distributors Page 9-5

Rotax 912 i series Specifications

General

Number of Cylinders	4
Max Power	100 hp (73.5 kW)
Max Power Output RPM	5800 rpm
Ignition System	Dual electronic ignition
Oil System	Dry sump, forced lubrication with separate oil tank
Reduction Gear Ratio	2.43:1
TBO	2000 hours
Engine Type	4-stroke, horizontally opposed
Displacement	1352 cm³
Bore x Stroke	84 mm x 61 mm
Max Torque	128 Nm
Fuel Type	Avgas 100LL or unleaded automotive gasoline
Fuel System	Electronic fuel injection
Cooling System	Liquid/air-cooled