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The Cessna 172 Skyhawk is an American four-seat, single-engine, high wing, fixed-wing aircraft made by the Cessna Aircraft Company. [2] First flown in 1955, [2] more 172s have been built than any other aircraft. [3] It was developed from the 1948 Cessna 170 but with tricycle landing gear rather than conventional landing gear.
The Cessna 177 (originally Model 341) [3] was designed in the mid-1960s when the engineers at Cessna were asked to create a "futuristic 1970s successor to the Cessna 172". The resulting aircraft featured newer technology such as a cantilever wing lacking the lift struts of previous models, and a new laminar flow airfoil.
Cessna Model A: 1927 70 Single piston engine monoplane utility airplane Cessna Model BW: 13 Single piston engine monoplane utility airplane Cessna CG-2: Glider Cessna CH-1: 1953 ~50 Single piston engine utility helicopter Cessna CH-4: Single piston engine utility helicopter Cessna CR-1: 1 Single piston engine monoplane racer Cessna CR-2: 1930 1
Used in the Cessna 172 I to M models. O-320-E2F 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as E1F but with fixed pitch prop provisions. [4] O-320-E2G 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as E2D but with O-320-A sump and intake pipes. [4] O ...
The model designation nomenclature differs from some other Cessna models with optional retractable gear. For instance, the retractable version of the Cessna 172 was designated as the 172RG and the 177RG , whereas the retractable gear version of the Cessna 182 is the R182. Cessna gave the R182 the marketing name of "Skylane RG". [8]
In 1992, Velocity introduced the "173", also known as the long wing. This model had a longer wing, giving it a lower landing speed. The name was a play on the name of a popular model of Cessna, the Cessna 172, the idea being it is one better. Some flying Velocity planes experienced "deep stall" incidents, where the main wing stalled before the ...
The 1954 model year introduced a 225 hp (168 kW) O-470-J engine and interior refinements. 1956 introduced a 230 hp (172 kW) O-470-K engine with a new air intake duct. Certified on 23 December 1952. 641 (1953), 620 (1954), 891 (1955), and 512 (1956) built. [5] [6] A 1957 Cessna on display at Hullavington Airfield, England. 180A
The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines.Engines in the O-360 series produce between 145 and 225 hp (110 and 170 kW), with the basic O-360 producing 180 hp (130 kW).
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