Teledyne TSIO-360-RB, Maintenance Manual

Page: 39 / 206

5-7
CAUTION ... Failure to properly install the induction air filter will result in unfiltered air being
ingested into the engine which will accelerate engine wear and reduce engine service life.
5. Inspect induction air box for security and deterioration in accordance with the aircraft
manufacturer's instructions.
WARNING
Insure the fuel selector is in the off position prior to servicing fuel filters.
6. Drain the fuel filter and service as required and reinstall in accordance with the aircraft
manufacturer's instructions.
7. Visually inspect engine and nacelle for fuel, oil leaks and other discrepancies.
WARNING
Failure to identify and correct fuel or oil leaks can result in engine/nacelle fire, loss of
engine power, engine failure, bodily injury or death.
8. Drain engine oil (small full flow filter). During engine oil change, oil must be drained into an
appropriate container and disposed of properly. Reinstall oil drain plug with new gasket,
torque to 190 - 210 in. lbs. and safety.
9. Remove oil filter. Inspect filter element. See "Oil Filter Element Inspection, Oil Analysis and
Spectrographic Oil Analysis" at the end of this chapter.
10. Place a thin film of Dow Corning

DC-4 compound on new oil filter gasket. Install new oil
filter. Torque filter to 192 - 216 and safety wire.
11. Inspect all induction system or cylinder drain(s) for clogging or restriction.
12. Inspect ignition leads for chafing, deterioration and proper routing.
13. Visually inspect magnetos for condition. Inspect, repair and adjust as required if magneto
drop or spread was not within published limits.
14. Inspect exhaust system for cracks, excessive leakage, deterioration, loose and missing
brackets, clamps and hardware. Visually inspect turbocharger and associated turbocharger
system components for evidence of oil or exhaust leakage.
15. Correct all discrepancies noted.
WARNING
Operation of a malfunctioning engine can result in additional engine damage, bodily
injury or death.
16. At the completion of any maintenance event the engine must be given a complete and
thorough operational run-up. A test flight will be required if any engine adjustments have
been made which affect flight characteristics or operation; This test flight is require by FAR
91.407.
a. Record all engine parameters.
b. Verify recorded parameters are within the specifications published for the engine and
aircraft.
c. Correct any discrepancies noted during operational run-up prior to returning engine to
service.