d05165.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 0
10-10-00
Page 9
January 01/2012
2.3) Definition of attachment points
General note See Fig. 5.
Graphic Attachment points
Fig. 5
Non-compliance can result in serious injuries or
death!
The aircraft or fuselage manufacturer must design the
engine suspension so that it can safely carry the max-
imum occurring operational loads without exceeding
the max. allowable forces and bending moments on
the engine housing and attachment points.
Tighten all engine suspension screws as specified by
the aircraft manufacturer.