Type Description (912 Series) - BRP 912 Series Operator's Manual

1.6) Type description (912 Series)

e.g.
ROTAX
Designation
Type
Certifica-
tion
Configura-
tion
Suffix
Options
for configura-
tion 2
for configura-
tion 3
Effectivity: 912 Series
Rev. 1
The type description consists of the following:
912
type
certification
Designation
912
A
F, S
UL,
ULS
2
3
–XX
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
Description
4 –cyl. horizontally opposed, normal 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 pitch propeller.
Prop shaft with flange for constant speed propeller
and drive for hydraulic governor for constant speed
propeller.
Explanation of the type designation suffix, see
SB-912-068
vacuum
pump
yes
no
-01
Suffix
gover-
drive for rev
nor
counter/
hour meter
yes
yes
Page 1-15
Ed.4/January 01 2023
no
yes