6-cylinder engine 6A-350-C1

Franklin 60-350-C1 is a six cylinder, four stroke, clockwise rotation, air-cooled, opposed type piston engine, designed for light aircraft operation and used as direct drive power unit.

POWER AND ROTATION:
Take off: 220 hp at 2800 r.p.m.
Max. Continuous: 220 hp at 2800 r.p.m.
COMPRESSION RATIO: 10,5:1
DISPLACEMENT: 350 inch3
RPM MAXIMUM LIMIT: 2800 r.p.m.
RPM IDLE: 750-950 r.p.m.
WEIGHT OF DRY ENGINE: 150 kg