Twin Engine • Cessna • 310, 310A, 310B, 310H, 310R
| Manufacturer | Cessna |
| Model | 310 |
| Category | Twin Engine |
| Variants | 310, 310A, 310B, 310H, 310R |
| Production Years | 1954 – 1981 |
| Seating | 6 seats |
| Typical TTAF | 5,200 hours |
| Markets | United States, Canada, Australia, Mexico, Brazil |
| Price Range | $85K – $425K |
The Cessna 310 is a six-seat, twin-engine aircraft that became one of the most iconic light twins in aviation history. First introduced in 1954, it established itself as a reliable workhorse for personal, business, and charter operations. The aircraft features retractable landing gear, a pressurized cabin option in later models, and robust construction that appeals to both experienced and transitioning pilots. Known for its solid performance, dependable Continental engines, and spacious cabin, the 310 gained widespread adoption among flight schools, air taxi operators, and private owners seeking a capable twin-engine platform. The design emphasizes stability and safety, with symmetrical wing design and excellent single-engine handling characteristics compared to competitors. Its versatility, moderate operating costs relative to larger twins, and strong aftermarket support have kept many examples in active service today. The 310 remains popular in the used aircraft market, valued for both transportation and training purposes.
Maximum Speed: 195 mph
Cruise Speed: 180 mph
Range: 1,200 miles
Service Ceiling: 19,500 feet
Engines: Twin Continental IO-470 (310R)
Maximum Takeoff Weight: 5,100 lbs
Empty Weight: 3,150 lbs
Useful Load: 1,950 lbs
Fuel Capacity: 102 gallons