Lycoming IO-360-N1A Installation And Operation Manual page 66

Oil Grade at Temperatures between 30°F to 90°F (-1°C
to 32°C)
Oil Grade at Temperatures between 0°F to 70°F (-18°C
to 21°C)
Oil Grade at Temperatures below 10ºF (-12ºC)
The correct grade of oil to be used is based on environmental conditions.
If the aircraft is going to be flown into an area that is much warmer or colder than the aircraft is
usually operated in, use a different viscosity of oil.
During operation, if the oil inlet temperatures are near the maximum permitted temperatures, then a
higher viscosity oil can help to decrease the temperatures.
Fuel minimum octane (refer to the latest revision of
Service Instruction No. SI-1070 for any new approved
fuels)
Fuel Injector (Precision)
Fuel Pump
Starter Drive, Ratio to Crankshaft at Bendix
and Rotation
Starter - Sky-Tec or equivalent
Alternator Drive Rotation
Alternator - Hartzell (formerly Kelly Aerospace) or
equivalent
Magnetos (2) Slick
Magneto Drive, Ratio to Crankshaft
and Rotation
Tachometer Drive, Ratio to Crankshaft
and Rotation (Optional)
Freon Compressor Drive
NOTICE: All locations and rotations are as viewed from the anti-propeller end of the engine
unless specified differently.
For any possible additional optional starters and alternators, refer to the latest revision
of Lycoming Service Instruction No. SI-1154.
Appendix A
Page 46
IO-360-N1A Engine Installation and Operation Manual
Table A-1 (Cont.)
IO-360-N1A Engine Specifications
40
30
20
91/96 or 100LL (Aviation Grade)
RSA-5AD1
Diaphragm
16.556:1
Counterclockwise
12 Volt - Geared (Optional)
24 Volt - Geared -(Optional)
Clockwise
12 Volt, 70 Amp (Optional)
24 Volt, 70 Amp (Optional)
4347 (Left)
4370 (Right)
1.000:1
Clockwise
0.5:1
Clockwise
Optional
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40
30, 40 or 20W-40
30 or 20W-30
February 2016