Effectivity 912/914 Series
Edition 1 / Rev. 0
78-00-00
page 17
May 01/2007
d02627
BRP-Rotax
Maintenance Manual
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.
â—† NOTE: 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)
Fit the 4 exhaust bends (3).
â—† NOTE: To make assembly easier, LOCTITE Anti Seize can be applied
on the labyrinth end (36). See Fig. 78-7
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
â– CAUTION: All 4 exhaust bends must be fitted free of stress and must not
be damaged during installation.
min. 5 mm
00163
Fig. 78-7
35
36
(min. 0.179 in.)
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