8-4
8-5
INDEFINITE STORAGE INSPECTION PROCEDURES
1. Aircraft prepared for indefinite storage must have the cylinder dehydrator plugs visually
inspected every 15 days. The plugs must be changed as soon as they indicate other
than a dark blue color. If the dehydrator plugs have changed color in one-half or more of
the cylinders, all desiccant material on the engine must be replaced.
2. The cylinder bores of all engines prepared for indefinite storage must be re-sprayed with
corrosion preventive mixture every 90 days.
8-6
RETURNING AN ENGINE TO SERVICE AFTER STORAGE
1. Remove seals and all desiccant bags.
2. Remove cylinder dehydrators and plugs or spark plugs from upper and lower spark plug
holes.
3. Remove oil sump drain plug and drain the corrosion preventive mixture. Replace drain
plug, torque and safety. Remove oil filter. Install new oil filter torque and safety.
Service the engine with oil in accordance with the manufacturer's instructions.
WARNING
To prevent possibility of serious bodily injury or death, before moving the propeller
accomplish the following:
a. Disconnect all spark plug leads.
b. Verify magneto switches are connected to magnetos, that they are in the
"OFF" Position and "P" leads are grounded.
c. Throttle position "CLOSED."
d. Mixture control "IDLE-CUT-OFF."
e. Set brakes and block aircraft wheels.
f. Insure that aircraft tie-downs are installed and verify that the cabin door latch
is open.
g. Do not stand within the arc of the propeller blades while turning the propeller.
4. Rotate propeller by hand several revolutions to remove preservative oil.
5. Service and install spark plugs and ignition leads in accordance with the manufacturer's
instructions.
6. Service engine and aircraft in accordance with the manufacturer's instructions.
7. Thoroughly clean the aircraft and engine. Perform visual inspection.
8. Correct any discrepancies.
9. Conduct a normal engine start.
10. Perform operational test in accordance with "Operational Inspection," Chapter 1,
Maintenance. .
11. Correct any discrepancies.
12. Perform a test flight in accordance with airframe manufacturer's instructions.
13. Correct any discrepancies prior to returning aircraft to service.
14. Change oil and filter after 25 hours of operation.
Summary of Contents for TSIO-360-RB
Page 11: ...1 5 FIGURE 1 1 Engine Description L TSIO 360 RB ...
Page 12: ...1 6 FIGURE 1 2 ENGINE DESCRIPTION L TSIO 360 RB Cont d ...
Page 13: ...1 7 FIGURE 1 2 ENGINE DESCRIPTION L TSIO 360 RB Cont d ...
Page 14: ...1 8 FIGURE 1 2 ENGINE DESCRIPTION L TSIO 360 RB Cont d ...
Page 15: ...1 9 FIGURE 1 2 ENGINE DESCRIPTION L TSIO 360 RB Cont d ...
Page 25: ...3 1 CHAPTER 3 SEALANTS AND LUBRICANTS Sealants Lubricants 3 2 ...
Page 32: ...4 2 INTENTIONALLY LEFT BLANK ...
Page 54: ...6 2 INTENTIONALLY LEFT BLANK ...
Page 58: ...6 6 FIGURE 6 1 INSTALLATION DRAWING ...
Page 59: ...6 7 FIGURE 6 1 INSTALLATION DRAWING cont d ...
Page 60: ...6 8 FIGURE 6 1 INSTALLATION DRAWING cont d ...
Page 61: ...6 9 FIGURE 6 1 INSTALLATION DRAWING cont d ...
Page 64: ...6 12 INTENTIONALLY LEFT BLANK ...
Page 70: ...7 6 INTENTIONALLY LEFT BLANK ...
Page 82: ...10 2 INTENTIONALLY LEFT BLANK ...
Page 85: ...11 3 FIGURE 11 1 INDUCTION AND EXHAUST SYSTEM ...
Page 94: ...11 12 INTENTIONALLY LEFT BLANK ...
Page 110: ...12 16 INTENTIONALLY LEFT BLANK ...
Page 124: ...14 4 INTENTIONALLY LEFT BLANK ...
Page 128: ...15 4 INTENTIONALLY LEFT BLANK ...
Page 132: ...16 4 INTENTIONALLY LEFT BLANK ...
Page 139: ...17 7 FIGURE 17 4 STARTER ADAPTER FITS LIMITS ...
Page 140: ...17 8 INTENTIONALLY LEFT BLANK ...
Page 143: ...18 3 FIGURE 18 1 ACCESSORY CASE DESCRIPTION ...
Page 147: ...19 3 FIGURE 19 1 LUBRICATION SYSTEM SCHEMATIC ...
Page 149: ...19 5 ACCESSORY CASE INTERNAL VIEW TSIO 360 FIGURE 19 2 OIL PUMP DESCRIPTION TSIO 360 ...
Page 150: ...19 6 ACCESSORY CASE INTERNAL VIEW LTSIO 360 FIGURE 19 3 OIL PUMP DESCRIPTION LTSIO 360 ...
Page 158: ...19 14 INTENTIONALLY LEFT BLANK ...
Page 181: ...21 3 FIGURE 21 1 CRANKCASE DESCRIPTION ...
Page 186: ...21 8 INTENTIONALLY LEFT BLANK ...
Page 194: ...22 8 INTENTIONALLY LEFT BLANK ...
Page 203: ...23 9 FIGURE 23 6 CONSTANT SPEED SEA LEVEL PERFORMANCE CURVE ...
Page 204: ...23 10 FIGURE 23 7 FUEL FLOW VS METERED FUEL PRESSURE ...
Page 205: ...23 11 FIGURE 23 8 FUEL FLOW VS BRAKE HORSEPOWER ...