Type Description - Rotax 912 ULS 3 Operator's Manual

1.7) Type description

e.g. 912 A 2
Description
Effectivity: 912 Serie
OM Edition 2 / Rev. 0
The type designation is of the following composition.
ROTAX
Description
Type: 912
Certification: A
F, S
UL, ULS
Configuration: 1
NOTE: This configuration is not available any longer
and will be replaced by configuration 2.
2
3
4
NOTE: This configuration 4 is not available any longer
and will be replaced by configuration 3.
BRP-Powertrain
Configuration
4-cyl. horizontally opposed, nor-
mal aspirated engine
certified to JAR 22
(TC No. EASA.E.121)
certified to FAR 33 (TC No.
E00051 EN)
JAR-E (TC No. EASA.E.121)
non-certified aircraft engines
Prop shaft with flange for fixed
prop, P.C.D 100 mm (3.936 in.).
Prop shaft with flange for fixed
pitch propeller.
Prop shaft with flange for constant
speed propeller and drive for hy-
draulic governor for constant
speed propeller.
Prop flange for fixed pitch propeller
and prepared for retrofit of a hy-
draulic governor for constant
speed propeller.
April 01/2010
page 1-11