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Cessna 310

General Aviation and Light Aircraft

The Cessna 310 is an American four-to-six-seat, low-wing, twin-engine piston monoplane that Cessna built from 1954 to 1980, the second twin the company put into production after the T-50. It first flew on 3 January 1953 and deliveries began in late 1954. Early aircraft stored all fuel in tip tanks and used exhaust thrust augmenter tubes, which were replaced in 1964 by exhaust routed under the wing, and the 310G of 1961 introduced the canted wingtip tanks that became common across Cessna twins. The turbocharged 320 Skyknight was developed from the 310F, and the United States military used the type as the L-27, redesignated U-3 after 1962. More than six thousand 310 and 320 aircraft were produced in total.

Facts
Year
1954 1
Engine Class
Piston 1
Status
Out of production 1
Top Speed (km/h)
350 1
Mass (kg)
1293 1
Maximum Mass (kg)
2087 1
Engine
2 x Continental O-470-B horizontally opposed piston engine, 240 hp each 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Source Cessna 310 (Wikipedia)

Of Make

Source Cessna 310 (Wikipedia)
Sources
1. Cessna 310 (Wikipedia)
  • Lead
    The Cessna 310 is an American four-to-six-seat, low-wing, twin-engine monoplane produced by Cessna between 1954 and 1980.
  • Specifications (1956 model 310)
    Powerplant: 2 × Continental O-470-B horizontally opposed piston engine, 240 hp (180 kW) each
  • Specifications (1956 model 310), empty weight
    Empty weight: 2,850 lb (1,293 kg)
  • Specifications (1956 model 310), gross weight
    Gross weight: 4,600 lb (2,087 kg)
  • Specifications (1956 model 310), maximum speed
    Maximum speed: 220 mph (350 km/h, 190 kn)
  • Development
    or more, at speeds that were high for a twin engine piston aircraft.
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