Cessna C-310R

SOSU operates one C-310R for multi-engine student training. The 310 has retractable landing gear and two fuel injected six-cylinder engines turning three bladed constant speed propellers.


Specifications:

Engine: Two Continental IO-520-M's producing 285 HP @ 2700 RPM

Max Takeoff Weight: 5500 lbs

Max Cruising Speed (Vno): 183 KCAS