Exhaust System - Rotax 912 Series Installation Manual

11) Exhaust system

See Fig. 2, 3 and 4.
The shape and execution of the exhaust system is determined essentially by the free
space available in the aircraft.
For attaching, the exhaust system two studs M8x23 are provided on each cylinder.
Location of the studs:
◆ NOTE:
max. allowable forces (limit load) in (N)
max. allowable bending (limit load) in (N)
▲ WARNING: The exhaust system has to be designed by the aircraft or fuselage
Effectivity: 912 Series
Edition 1 / Rev. 0
BRP-Rotax
INSTALLATION MANUAL
location
cylinder 1
cylinder 2
cylinder 3
cylinder 4
All dimension to point of reference (P).
in x,y and z axis
in x,y and z axis
manufacturer such, that the limit loads on the points of attachment will
not by exceeded. Additional support of exhaust system may be
necessary.
coordinates [mm]
x axis y axis z axis
-160 -196
-160 -212
-192 196
-192 212
-408 -196
-408 -212
-438 196
-438 212
points of attachment
1 000
40
-82
-113
-82
-113
-82
-113
-82
-113
09189
02023
page 39
May 01/2007