Rotax 912 Series Maintenance Manual page 405

Re-establish attachment (9) turbocharger bracket engine suspension frame
(not supplied with engine). Tightening torque as specified by the aircraft
manufacturer.
Tightening torque of the M10 screws = 15 Nm (133 in.lb).
Reconnect the two oil lines for turbocharger on the oil pump.
See 79-00-00.
◆ NOTE:
Fit the 4 exhaust bends (3).
◆ NOTE:
The connecting ends (35) of the exhaust manifold must overlap the pleat of the
labyrinth end by at least 5 mm (.197 in.) at each of the 4 exhaust bends. See
Fig. 78-7
■ CAUTION:
Effectivity 912/914 Series
Edition 1 / Rev. 0
BRP-Rotax
Maintenance Manual
If the location of the oil line connection does not correspond with
oil pump housing, correction can be achieved by slightly turning
the turbocharger center section (34)
To make assembly easier, LOCTITE Anti Seize can be applied
on the labyrinth end (36). See Fig. 78-7
All 4 exhaust bends must be fitted free of stress and must not
be damaged during installation.
Fig. 78-7
35
00163
min. 5 mm
(min. 0.179 in.)
36
78-00-00
page 17
May 01/2007