The Cessna 310 is a low-wing twin-engine monoplane that can accommodate up to six seats in-flight. It was the first aircraft of Cessna powered by twin engines that were put into production after the Second World War.

United States
1954 to: 1980
US$.147 million (1978)
2x Continental IO-470-M
240 horsepower
Max Cruise Speed:
190 knots
352 Km/h
Approach Speed (Vref):
68 knots
Travel range:
870 Nautical Miles
1,611 Kilometers
Fuel Economy:
Service Ceiling:
20,000 feet
Rate of Climb:
1700 feet / minute
8.64metre / second
Take Off Distance:
507 metre - 1,663.37 feet
Landing Distance:
546 metre - 1,791.32 feet
Max Take Off Weight:
2,087 Kg
4,601 lbs
Max Landing Weight:
1,293 Kg
2,851 lbs
Max Payload:
790 Kg
1,742 lbs
Fuel Tank Capacity:
125 gallon
473 litre
Baggage Volume:
1 m3 / 35 ft3
Seats - Economy / General:
5 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
1.2 metre - 3.94 feet
Cabin Width:
1.2 metre - 3.94 feet
Cabin Length:
2.4 metre - 7.87 feet
Exterior Length:
8.3 metre - 27.23 feet
Tail height:
3.25 metre - 10.66 feet
Fuselage Diameter:
1.3 metre - 4.27 feet
Wing Span / Rotor Diameter:
10.7 metre - 35.10 feet
Wing Tips:
No Winglets

On January 3, 1953, the Cessna 310 conducted its maiden flight. In late 1954, deliveries of the aircraft started. Throughout the aircraft’s 28-year production span, it involved numerous improvements and innovations such as engine exhaust thrust augmenter tubes and the fuel storage in tip tanks in earlier versions. In 1964, it was found out that augmenter tubes cause too much noise, so it was opted to change the flow of the engine exhaust under the wing.

The Cessna 310 also developed from a pressure-carbureted engine to a high-power turbocharged engine. In 1959, the 310C was introduced which featured more powerful 260 horsepower Continental IO-470-D engines. In 1960, another version with swept-back vertical tail surfaces was introduced, designated as the 310D. In 1961, the 310F with an extra cabin window on each side was produced. A few more variants of the 310 were produced until 1980.

The Cessna 310 was used both in commercial and military operations. It was used as a charter aircraft for many air taxi businesses in general aviation after World War II. It boasted its speed, low operating cost, and aftermarket modifications like the Short Take-Off and Landing (STOL) kits that made the aircraft in demand throughout the globe for its bush flying capabilities. The aircraft could take-off and land on short runways, while simultaneously carrying a 2,000 pounds of useful load, at speeds that were above the capability of a typical twin-engine piston aircraft.

The 310 were also utilized by the United States Air Force (USAF) in 1957 as a light utility aircraft for transport and administrative support. The USAF acquired 160 L-27As, unmodified version of the 310A, that were changed afterward to U-3A in 1962. From 1960 to 1961, an additional 36 L-27B, military designation for the 310E/310M powered by 260 hp engines were delivered.

The 1956 model of the Cessna 310 has a cruise speed of 178 knots, a range of 870 nautical miles, a service ceiling of 20,000 feet, and a rate of climb of 1,700 feet per minute. It has a maximum take-off weight of 2,087 kg.

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