Cessna 310 II

Performance Specifications
Engine 

Manufacturer: Continental
Model: I0-520-M
Horsepower: 570 hp

 Weights (lbs/kg) 

Gross Weight: 5500/2495
Standard Empty/Equipped Weight (b,c): 3589/1628
Standard Useful Load (a): 1911/867

 Dimensions 

Wing Span (ft/m): 36.9/11.25
Length (ft/m): 31.9/9.74
Height (ft/m): 10.6/3.25
Wing Area (ft2/m2): /16.63
Fuel Capacity (gal/l) 

Usable Fuel: /

 Maximum Speed (kts/kmh) 

TAS at Gross Weight: 207/383

 Cruising Speeds (kts/kmh) 

Normal Cruise Speed 144/267
Cruising Range (nm/km) 

Cruising Range:792/1467
(45 minute reserves at 65% power)

 Stall Speed (kts/kmh) IAS 

Flaps up 77.7/144

 Service Ceiling (ft/m) 

(100 fpm): 19750/6020
SE: 7400/2255
Take-Off Distance (ft/m) 

Total over 50 ft obstacle: /

 Landing Distance (ft/m) 

Total over 50 ft obstacle: /
a. Standard Useful load is ramp weight minus standard equipped weight.
b. The standard empty weight and standard equipped weight are the same.
c. Standard aircraft per marketing.
1978 Prices

Standard Equipped List Price:$ 160,500

PIPER : Archer III | Arrow | Malibu Mirage | Saratoga IIHP | Seminole | Seneca IV | Warrior III |

CESSNA : C 150 | C152 | C 172 | C 182 | C 210 | C 310 |

ROCKWELL : C114A |

MOONEY :