Cessna 310
Overview
The Cessna 310 is a general aviation aircraft manufactured by Cessna, with the profile centered on its personal/training/utility role. It first flew in 1953 and entered service in 1954. Production is recorded as ending in 1980. The listed configuration provides for a crew of 1 and passenger capacity of 5. Power is provided by 2 Continental IO-470 / TSIO-520 engines. Recorded dimensions include length 32 ft, wingspan 36.9 ft, height 10.6 ft. Maximum takeoff weight is listed as 5,500 lb. Listed performance includes cruise speed 167 mph kt. Its ICAO type designator is C310. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
First Flight
1953
Crew
1
Passengers
5
Cruise Speed
167 mph
Specifications
| ICAO Type Code | C310 |
|---|---|
| First Flight | 1953 |
| Introduction Date | 1954 |
| Crew | 1 |
| Passenger Capacity | 5 |
| Length | 32 ft |
| Wingspan / Rotor Diameter | 36.9 ft |
| Height | 10.6 ft |
| Empty Weight | 3200 lb |
| Max Takeoff Weight | 5,500 lb |
| Cruise Speed | 167 mph |
| Engine Manufacturer | Continental |
| Engine Model | IO-470 / TSIO-520 |
| Engine Count | 2 |
Data verification status: Partially Verified