Type Description - Rotax 912 Series Operator's Manual

1.7) Type description

e.g.
ROTAX
Designation
Type
Certifica-
tion
Configura-
tion
Suffix
Options
for configura-
tion 2
for configura-
tion 3
Page 1-16
November 01/2016
The type description consists of the following:
912
type
certification
Designation Description
912 4 –cyl. horizontally opposed, normal aspirated
engine
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, Non-certified aircraft engines
ULS
2 Prop shaft with flange for fixed pitch propeller.
3 Prop shaft with flange for constant speed propeller
and drive for hydraulic governor for constant speed
propeller.
–XX Explanation of the type designation suffix, see
SB-912-068
Available options (optional equipment) for the engine type men-
tioned above:
external
alterna-
tor
yes
yes
NOTE
Conversion of the configuration 2 to configuration 3 may be ac-
complished by ROTAX® authorized aircraft engines distributors
or their Independent service centers.
BRP-Rotax
A 2
configuration
vacuum
drive for rev
pump
hour meter
yes
no
-01
Suffix
gover-
nor
counter/
yes no
yes yes
Effectivity: 912 Serie
Edition 4 / Rev. 0