The Cessna 310 is a north american four-to-six-seat, low-wing, twin-engined monoplane produced by Cessna. The aeroplanes entered the light-twin market in late 1954 as the first twin-engined aircraft that Cessna came into production following World War II.
The 310 first flew on January 3, 1953 and included innovative features such as engine exhaust pushed augmenter pontoons through which the exhaust fumes from the aircraft’s reciprocating engine was given to provide additional thrust. The 310 was quickly indexed as a hire aircraft intended for numerous content World War II atmosphere taxi businesses.
The Cessna 310 held extensive advantages over its rivals like the Piper PA-23 regarding speed, inexpensive operating costs and the accessibility to aftermarket modifications such as the Robertson STOL products which managed to get popular for bush traveling by air. The 310 was able to employ short runways while having a useful weight of 910 kg or even more which achieved it an incredibly adaptable aircraft.
In 1957, the United States Naval pilot (USAF) hand picked the Cessna 310 for support as a lumination utility aeroplanes for transportation roles. The USAF bought 160 310A aircraft together with the designation L-27A and nicknamed the aircraft the ‘Blue Canoe’ after it’s special blue and white colour scheme. Even though both the US Armed service and Navy made use of the aircraft underneath different livery, the play name remained.
The official designation of the L-274A was changed to U-3A in 1962. Yet another 36 enhanced 310D chosen L-27B (later U-3B) were delivered over 1960 and 1961 and featured better 260 hp (194 kW) engines and further cabin house windows and pointed nose and swept up and down fin. The 310D of 1960 marked the 1st 310 to feature the swept straight tail.
A advancement the 310F was the turbo charge 320 Skyknight, with TSIO-470-B engines and a 4th cabin side-window. The Skyknight was in production between 1961 and 1969 (the 320D, E and F had been named Exec Skyknight), mainly because it was changed by the comparable Turbo 310
The 310G was released in 1962 and featured the canted wingtip fuel tanks found on most of the Cessna twin-engined products, marketed as stabila-tip storage containers by Cessna because these people were meant to help stability in flight. A single side window changed the rear two window configuration on the 310K of 65, with optionally available three-blade propellers being launched as well. Subsequent developments included the 310Q and the turbo charged T310Q which in turn featured a redesigned rear cabin having a skylight windowpane.
The final production types were the 310R and T310R. The 1975 honda civic 310R had 285 hp (213 kW) Continental IO-520-M or IO-520-MB engines, three-blade propellers while standard, extended nose that contain a suitcases compartment, and 5, five-hundred lb (2, 500 kg) maximum take-off weight. The T310R likewise featured a turbocharged Continental TSIO-520-B or perhaps TSIO-520-BB engine.
Through the years there were several modifications distributed around the 310 to improve overall performance. Aircraft industrial engineer Jack Riley produced a lot of variants pertaining to the plane line such as Riley Rocket 310 as well as the Riley Turbostream 310. Mr Riley substituted the standard Ls 310 hewlett packard (230 kW) engines with 350 horsepower (261 kW) Lycoming TIO-540 engines. These turbocharged intercooled engines had been installed with three-blade Hartzell propellers in a counter-rotating configuration to further enhance performance and single-engine protection. This resulted in a cruising speed of 480 km/h at 18, 000 foot.
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