Continental Motors TSIOL-550-C Operation, Maintenance & Installation Manual page 205

NOTE...
Place a support at the load bearing area of aircraft
tail to prevent damage to the airframe.
Crankcase Separation
If the crankcase halves must be separated, remove
the engine from airframe in accordance with the
TSI0L-550-C Overhaul Manual, Form OH-15 and
the airframe manufacturer's instructions.. Engine
disassembly, cleaning,
replacement and assembly must be accomplished in
accordance with the TSI0L-550-C Overhaul Manual,
Form OH-15.
NOTE...
Exercise judgment in determining how far systems
and components should be disassembled.
Any maintenance of engine systems and components
removed from engine must be performed in
accordance with that particular system or component
chapter of this manual.
inspection, repair,
CAUTION...
Dimensional inspection of the crankcase and
crankcase internal components must be performed in
accordance with the
Manual, Form OH-15. Prior to dimensional
inspection, insure that the part conforms with all
visual, fluorescent penetrant, magnetic particle or
ultrasonic inspection requirements.
All crankcase repairs must be performed in
accordance with the TSI0L-550-C Overhaul Manual,
Form OH-15. Any non TCM supplied accessory that
was disassembled for maintenance must be re-
assembled in accordance with the applicable
accessory manufacturer's
maintenance involving crankcase separation will
require an acceptance
determination, reinstallation in airframe and test
flight in accordance with the TSI0L-550-C Overhaul
Manual, Form OH-15.
Crankease/Starter Needle Bearing Installation
If a new crankcase needle bearing has to be installed
in the engine prior to overhaul, use a modified
needle bearing tool and fixture shown in Figures 17-
4 and 17-5 on the following page. Replace the
needle bearing in accordance with the TSI0L-550-C
Overhaul Manual, Form OH-15.
Crankcase
TSI0L-550-C Overhaul
instructions. Any
test, oil consumption
17-5