6-cylinder engine 6A-350-C1R

Franklin 60-350-C1R 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. Prepared to work in two-units system.

POWER AND ROTATION:
Take off: 205 hp at 2800 r.p.m.
Max. Continuous: 205 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