Superior Vantage Engine O-360 SERIES Maintenance Manual page 36

−
Remove external full flow oil filter. Install
new integral bypass, full flow oil filter by
applying a light coat of Dow Corning #4
or equivalent to the rubber seal at the
base of the new filter. Lightly lubricate
the filter threads and install to the
adapter, applying 192-216 in-lb (16-18 ft-
lb) torque. Install safety wire from oil
filter to adapter.
−
Cut open the used filter and check the
element for metal particles indicative of
engine damage.
lubricating oil.
−
Remove oil suction screen and inspect
the screen carefully for presence of
metal particles that are indicative of
internal engine
thoroughly prior to replacement. Refer
to Lubrication
information.
−
Check oil lines for leaks. Pay particular
attention to connection attachments for
wear from rubbing or vibration and for
dents and cracks.
•
Exhaust System
Check the exhaust port flanges for evidence
of leakage. If they are loose or distorted,
they must be removed and machined flat
before they are reassembled and tightened.
Examine the general condition of the exhaust
manifolds.
•
Cooling System
Check cowling and baffles for secure
attachment or damage.
missing part of the cooling system must be
repaired or replaced before the aircraft
resumes operation.
© March 2006 Superior Air Parts Inc.
Maintenance Manual
O-360 and IO-360 Series Engines
Drain and renew
damage. Clean
Section for further
Any damaged or
•
Cylinders
Check rocker box covers for evidence of oil
leaks. If found, replace gasket and tighten
screws to specified torque. Check cylinders
for evidence of excessive heat, oil or
combustion
discoloration of the cylinder. This condition
indicates possible internal damage to the
cylinder and the source must be determined
and corrected before the aircraft resumes
operation.
•
Carburetor / Fuel Injection System
Check carburetor or fuel injection servo
attaching screws (as appropriate to engine
type) for tightness. Tighten to 40-50 inch-
pounds.
•
Belt and Hoses
Check all belts and hoses for wear. Replace
if worn or damaged. Refer to section 72-10-
00 for alternator belt tension requirements.
2
Scheduled Inspection and Maintenance
gas leakage indicated
05-20-00
by