Teledyne Continental Motors, Inc.
TM
Non-Overhaul Removal and Replacement
IOF-550 Permold Series Engine Maintenance Manual
10-59
1 April 2007
10-6.28. EDI Replacement
EDI installation instructions are dependent upon aircraft make and model. Refer to the
applicable aircraft maintenance manual for EDI location and removal and installation
instructions.
10-6.29. ECP Replacement
ECP installation instructions are dependent upon aircraft make and model. Refer to the
applicable aircraft maintenance manual for ECP location and removal and installation
instructions.
10-7.
Lubrication System Repair
10-7.1. Oil Filter Adapter Stud Replacement
Procedure
1.
Disconnect electrical power to the engine; verify the Ignition Switch is turned OFF.
WARNING
If the power is not turned OFF, a loose or broken wire could
cause the engine to start and the propeller to rotate. As a
precaution, do not stand or allow anyone else to stand within
the arc of the propeller.
2.
Remove the oil filter adapter stud.
3.
Inspect the threads in the adapter housing for damage or cracks. If any thread damage
or crack is evident, remove the adapter housing and install a new adapter housing.
4.
Clean the adapter housing threads thoroughly to remove any remaining thread
adhesive and oil.
5.
Do not apply Loctite at this time. Install the new oil filter adapter stud (Figure 10-50).
(This stud is 1.440-inch (36.6 mm) in length uninstalled.)
6.
Verify the incomplete thread on the new oil filter adapter stud stops at the first thread
in the adapter housing and does not continue into the housing below the minimum
.500-inch (12.7 mm) extension. If the extension is less than .500-inch (12.7 mm),
replace the adapter housing.
Figure 10-50.
Oil Filter Stud Height
