LYCOMING 76 SERIES AIRCRAFT ENGINES Section8
TestProcedure
Let engine stand for ten (10) minutes after which the pro-peller should be turned back and forth through 90 for twelve (12)cycles. Drain the preservative oil.
8-27. Spray the exhaust port and valve of each cylinderwith the piston approximately 1/4 turn before top center of the exhaust stroke using MIL-C-6529 oil, Type 1.
8-28. Spray each cylinder with an airless spray gun(Spraying System Company "Gunjet" model 24A-8395 or equivalent) through the spark plug holes with MIL-
C-6529oil, Type 1. Spray approximately two (2)ounces of oil into each cylinder.
8-29. For all spraying the spray nozzle temperature shall be maintained between 200°F. and 220°F.
NOTE In the event an airless spray gun is not available, it is recommended that a moisture trap be installed in the air line of the conventional spray gun and the oil shall be 200°F. to 220°F. at the nozzle.
8-30. Seal the breather openings with oil and moisture resistant caps or dehydrator plug, P/N 40238 or AN4062-11.
8-31. All accessory drives for which oil seals are providedshall be liberally coated with MIL-C-6529 oil, Type 1, before applying the drive covers.
8-32. Engines shall have spark plugs installed in the bot-tom cylinder location and dehydrator plugs, P/N 40238in-stalled in the upper cylinder location. The ignition harness shall be attached to the spark plugs in the bottom loca-tions and have ignition cable protectors (AN-4060)on the top locations.
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