d04918.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
00-00-00
page 4
August 01/2012
2) Type description
e.g. ROTAX 912
version 2
The type description is made up the following.
Designation
Options Available options (optional equipment) for the engine type mentioned
above:
NOTE: Conversion of the configuration 2/4 to configuration 3 may
be accomplished by ROTAX Authorized Distributors or their
Service Center.
Type
(type)
Zulassung
(certification)
Ausführung
(configuration)
ROTAX
Designation Description
Type 912 4-cyl. horizontally opposed, normal aspirated engine.
Certification A Certified to JAR 22 (TC No. EASA.E.121).
F, S Certified to FAR 33 (TC No. E00051 EN)
JAR-E (TC No. EASA.E.121).
UL, ULS Non-certified aircraft engines.
Configuration 2 Prop shaft with flange for fixed prop.
3
Prop shaft with flange for constant speed propeller
and drive for hydraulic governor for constant speed
propeller.
4 With prop flange for fix pitch propeller, but prepared for
retro-fit of hydraulic governor for constant speed prop
(not supplied by manufacturer anymore.
External
alternator
Vacuum-
pump
Drive for rev counter/
hour meter
Governor
for configuration 2 yes yes yes no
for configuration 3 yes no yes yes
for configuration 4 yes yes yes no
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