Effectivity: 914 Series BRP-Powertrain page 1-11
OM Edition 2 / Rev. 0 April 01/2010
d04473.fm
1.7) Type description
e.g. 914 F 2 The type designation is of the following composition.
Description
Type
(type)
Zulassung
(certification)
Baureihe
(configuration)
ROTAX
Description Configuration
Type: 914 4-cyl. horizontally opposed, turbo-
charged engine
Certification: F certified to FAR 33 (TC No.
E00058 NE)
JAR-E (TC No. EASA.E.122)
UL non-certified aircraft engines
Configuration: 2 Prop shaft with flange for fixed
pitch propeller.
3 Prop shaft with flange for constant
speed propeller and drive for hy-
draulic governor for constant
speed propeller.
4 Prop flange for fixed pitch propeller
and prepared for retrofit of a hy-
draulic governor for constant
speed propeller.
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