INTERFACE OVERVIEW
Figure 5.8: Attachment points
MECHANICAL INTERFACES
Attachment
Interface Parameter
points
Attachment points
x-axis (in)
y-axis (in)
The aircraft or fuselage manufacturer must design the engine suspension so that it can
Effectivity: 915 i A Series
Edition 0/Rev. 0
INSTALLATION MANUAL
INTERFACE DESCRIPTION
Non-compliance can result in serious injuries or death!
safely carry the maximum occurring operational loads without exceeding the max. al-
lowable forces and bending moments on the engine housing and attachment points.
Tighten all engine suspension screws as specified by the aircraft manufacturer.
BRP-Rotax
Value
L2
105 mm
(-4.13 in.)
m WARNING
R2
L3
615 mm (24.21 in.)
-105 mm
-105 mm
(-4.13 in.)
(-4.13 in.)
72–00–00
December 01 2017
R3
-105 mm
(-4.13 in.)
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