INFORMATION
CESSNA C310B |
The Model 310 is a twin-engined five-seat cabin monoplane. The prototype flew |
| Fuselage | all metal flush-riveted structure |
| Wings | low-wing cantilever monoplane all-metal flush-riveted structure Electrically-operated split flaps Maximum flap depression 45 degrees Wing area 175 sq. ft |
Tail | cantilever monoplane all-metal flush-riveted structure trim tabs on rudder and elevators |
Landing gear | electro-mechanically retractable Cessna-type oleo shock-absorber struts nose gear steerable to 15 degrees castors from 15 to 55 degrees(both directions) |
Powerplant | two 240 h.p. Continental 0-470-M six-cylinder horizontally-opposed air-cooled engines propellers are two-bladed metal constant-speed and full-feathering |
Fuel tanks | two permanently-attached wing-tip tanks Each tank contained a bladder-type fuel cell holding 50 U.S. gallons Each tank had cross-feed capability fitted with an electrical fuel boost pump optional 30 U.S. gallon auxiliary fuel system available in 1956 It consisted of two 15 U.S. gallon rubber fuel-cells which were installed between the wing spars outboard of each engine nacelle and connected to the main fuel system |
Accomodations | Cabin seats five two in front and three on cross bench behind Controlled-heating provided by Stewart-Warner thermostatically controlled blower type heater Large door on starboard side gives access to all seats Baggage compartment aft of cabin has internal and external access Capacity is 200 lbs | Dimensions | span:36 ft length:27 ft 1 in height:10 ft 5 in |
Weights and Loading | empty weight: 2900 lb gross weight: 4700 lb wing loading: 26.2lb/sq ft |
Performance (at 4700 lbs) |
max speed: 232 mph cruise speed: (70%-8000') 213 mph rate of climb (SL): 1660 ft/min rate of climb SE (SL): 415 ft/min service ceiling: 20,500 ft service ceiling SE: 7750 ft cruising range(70%-8500'): 850 sm cruising range aux(70%): 1107 sm |
...CESSNA 310B...
