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
Engine Class Top Speed (km/h) Maximum Mass (kg) Engine2 x Continental O-470-B horizontally opposed piston engine, 240 hp each 1 Comparison
Body StyleAircraft (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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