d04926.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
78-00-00
page 7
August 01/2012
3) Attaching of the exhaust system
General note See Fig. 4.
The shape and configuration of the exhaust system is essentially deter-
mined by the free space available in the aircraft.
Two M8x23 studs are provided on each cylinder for attaching the exhaust
system.
Location of the
studs
NOTE: All dimensions from zero reference point (P).
Coordinates
Location
x axis mm/in y axis mm/in z axis mm/in
Cylinder 1 -160 mm (-6.3 in) -196 mm (-7.72 in) -82 mm (-3.23 in)
-160 mm (-6.3 in) -212 mm (-8.35 in) -113 mm (-4.45 in)
Cylinder 2 -192 mm (-7.56 in) 196 mm (7.72 in) -82 mm (-3.23 in)
-192 mm (-7.56 in) 212 mm (8.35 in) -113 mm (-4.45 in)
Cylinder 3 -408 mm (-16.06 in) -196 mm (-7.72 in) -82 mm (-3.23 in)
-408 mm (-16.06 in) -212 mm (-8.35 in) -113 mm (-4.45 in)
Cylinder 4 -438 mm (-17.24 in) 196 mm (7.72 in) -82 mm (-3.23 in)
-438 mm (-17.24 in) 212 mm (8.35 in) -113 mm (-4.45 in)
Attachment points
Max. permissible forces (safe load) in (N/lb-
force)
on x, y and z axis
1000 N/224.81
Max. permissible bending moment (safe load)
in (Nm) on x, y and z axis
40 Nm/30 ft.lb
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