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The Cessna 150 is a two-seat tricycle gear general aviation airplane that was designed for flight training, touring and personal use. [2] In 1977, it was succeeded in production by the Cessna 152, a minor modification to the original design. The Cessna 150 is the fifth most produced aircraft ever, with 23,839 produced. [3]
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 Single piston engine monoplane racer Cessna CR-3: 1933 1 Single piston engine monoplane racer Cessna CW-6: 1928
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 Lycoming provided not only an increase in engine power over the Cessna 150, but also was more compatible with the newer 100LL low-lead fuel. [1] Cessna 152s produced between 1977 and 1982 were equipped with Lycoming O-235-L2C engines producing 110 hp (82 kW) at 2,550 rpm. This engine still suffered some lead-fouling problems in service.
Data from Global Security [better source needed] General characteristics Crew: one Capacity: three passengers Length: 26 ft 11 in (8.20 m) Wingspan: 35 ft 10 in (10.92 m) Height: 8 ft 10 in (2.69 m) Wing area: 159 sq ft (14.8 m 2) Empty weight: 1,363 lb (618 kg) Gross weight: 2,500 lb (1,134 kg) Powerplant: 1 × Continental IO-360-D 6-cylinder air-cooled horizontally-opposed piston engine, 210 ...
The 175 was designed to fill a niche between the Cessna 172 and the slightly heavier, larger and faster Cessna 182.The engine of the 175, a reduction drive or geared version of the O-300 (Continental GO-300) used in the 172, is rated at 175 hp (130 kW), or 30 hp (22 kW) more than the engine offered in the contemporary 172.
Data from Jane's All The World's Aircraft 1955–56 General characteristics Crew: 1 Capacity: 3 passengers Length: 24 ft 11 + 1 ⁄ 2 in (7.607 m) Wingspan: 36 ft (11 m) Height: 6 ft 7 in (2.01 m) Wing area: 174 sq ft (16.2 m 2) Aspect ratio: 7.46:1 Airfoil: NACA 2412 Empty weight: 1,205 lb (547 kg) Gross weight: 2,200 lb (998 kg) Fuel capacity: 42 US gal (160 L; 35 imp gal) Powerplant: 1 × ...
Cessna thought that a less expensive four-seater aircraft than the existing Cessna 172 would have good market potential. The company designed a simplified four-seat high-wing aircraft using non-tapering wings, extensive use of heavily beaded wing and fuselage skins as well as free-castering nose gear to save weight and decrease the man-hours required for construction.