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Rotax 912 Series - Permissible Installation Positions

Rotax 912 Series
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d04919.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
10-10-00
page 12
August 01/2012
2.4) Permissible installation positions
General note See Fig. 4
NOTE: Dimensions are always from zero reference point and the
coordinate system position remains unchanged.
Installation posi-
tions
The following installation position details refer to the aircraft in
parked position (aircraft on ground, ready for take off).
- Engine suitable for propeller in tractor or pusher arrangement
- Installation only with propeller shaft above cylinders
Propeller axis The centres of attachment points L1 and R1 must be on a y2 axis parallel
to the y-axis.
Permissible deviation from parallelism: 
Fig. 4 02454
WARNUNG
NOTICE
The oil system, fuel system and the cooling system are
unsuitable for upside-down/inverted installation of the
engine.
+z
-y
+y
P
-z
L1R1
y2

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