5-10
26. Visually inspect magneto pressurization filter for contamination. If filter element is white,
it may be continued in service. If filter element has turned to yellow or red, element is
contaminated and must be replaced. If there is visible moisture present in the filter
canister the magnetos must be removed from the engine, disassembled and inspected
for possible internal contamination and corrosion.
27. Correct any discrepancies noted.
28. Perform post inspection operational run-up. Visually inspect engine and nacelle for fuel
and oil leaks.
29. Correct any discrepancies noted during this inspection prior to returning engine to
service.
SYSTEM DRAIN INSPECTION
.
At each scheduled maintenance interval, perform the following inspection to ensure that
the drain(s) function properly:
WARNING
Do not rotate the propeller or allow any personnel to stand in the area of the
propeller arc while performing the following inspection.
1. Perform a normal engine start priming sequence in accordance with the Aircraft
Manufacturer or STC holder's instructions.
2. Observe the drain location(s) in the engine cowling and make certain that fuel drains
from each.
3. Remove, clean or replace any drain that does not function properly.
500-HOUR INSPECTION
In addition to the items listed for 100-hour inspections, perform the following inspections and
maintenance every 500 hours of engine operation.
1. Magnetos require a thorough, detailed inspection. Refer to the applicable service and
overhaul information published by the manufacturer of the magneto. Magnetos must be
overhauled or replaced at the same intervals as the engine. TCM magnetos (formerly
Bendix) must be overhauled or replaced every four years regardless of total operating hours
since last overhaul or replacement.
2. Engine mounted accessories not supplied by TCM such as alternators, stand-by generators,
etc., may require servicing at specific intervals. Refer to the instructions provided by the
aircraft manufacturer, accessory manufacturer or STC holder for detailed information.
3. TCM gear driven alternators require inspection and testing at 500-hour intervals. Refer to
the applicable alternator manufacturer's instructions. See "Related Publications" in the
Introduction section of this manual.
Summary of Contents for CONTINENTAL L/TSIO-360-RB
Page 8: ...tNTENTIONALLY LEFT BLANK viii OCTOBER 1998 ...
Page 10: ...1 2 Change 2 INTENTIONALLY LEFT BLANK ...
Page 16: ...1 8 Change 2 Figure 1 1 L TSIO 360 RB Top and Front View ...
Page 17: ...1 9 Change 2 Figure 1 2 L TSIO 360 RB Side and Aft View ...
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Page 27: ...3 1 CHAPTER 3 SEALANTS AND LUBRICANTS Sealants Lubricants 3 2 ...
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Page 60: ...6 6 FIGURE 6 1 INSTALLATION DRAWING ...
Page 61: ...6 7 FIGURE 6 1 INSTALLATION DRAWING cont d ...
Page 62: ...6 8 FIGURE 6 1 INSTALLATION DRAWING cont d ...
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Page 87: ...11 3 FIGURE 11 1 INDUCTION AND EXHAUST SYSTEM ...
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Page 141: ...17 7 FIGURE 17 4 STARTER ADAPTER FITS LIMITS ...
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Page 145: ...OIL SUCTION OIL FILTERADAPTER SCREEN BOSS MOUNT FLANGE FIGURE 18 1 ACCESSORY CASE DESCRIPTION ...
Page 149: ...19 3 FIGURE 19 1 LUBRICATION SYSTEM SCHEMATIC ...
Page 151: ...19 5 ACCESSORY CASE INTERNAL VIEW TSIO 360 FIGURE 19 2 OIL PUMP DESCRIPTION TSIO 360 ...
Page 152: ...19 6 ACCESSORY CASE INTERNAL VIEW LTSIO 360 FIGURE 19 3 OIL PUMP DESCRIPTION LTSIO 360 ...
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Page 179: ...OCTOBER 1998 20 1 g ...
Page 183: ...21 3 FIGURE 21 1 CRANKCASE DESCRIPTION ...
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Page 205: ...23 9 FIGURE 23 6 CONSTANT SPEED SEA LEVEL PERFORMANCE CURVE ...
Page 206: ...23 10 FIGURE 23 7 FUEL FLOW VS METERED FUEL PRESSURE ...
Page 207: ...23 11 FIGURE 23 8 FUEL FLOW VS BRAKE HORSEPOWER ...