Cessna · United States · ICAO: C180 · 1953–1981 ·
$13,000 (1957)

The Cessna 180 Skywagon is a four to six-seat general aviation aircraft with conventional landing gear which was produced from 1953 to 1981. Though production has ended, many Skywagons are still operational and used as personal aircraft in utility roles such as bush flying.

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Engine:
1× Continental O-470-U
Engine type:
Piston
Power:
230 hp  ·  172 kW
Wing Tips:
No winglets
Seats:
6
Cabin width:
ft 6 in · 1.06 m
Cabin height:
ft 11 in · 1.20 m
Cabin length:
11 ft 2 in · 3.40 m
Exterior length:
25 ft 9 in · 7.85 m
Tail height:
ft 9 in · 2.36 m
Fuselage diameter:
ft 7 in · 1.10 m
Wing span / rotor:
35 ft 12 in · 10.97 m
Max takeoff weight:
2,800 lb  ·  1,250 kg
Max landing weight:
2,250 lb  ·  1,050 kg
Max Payload:
1,050 lb  ·  450 kg
Fuel capacity:
90 gal  ·  300 L  ·  200 kg  (AvGas)
Max cruise speed:
148 kt  ·  170 mph  ·  274 km/h
Approach speed (Vref):
48 kt  ·  55 mph  ·  89 km/h
Range:
890 nm  ·  1,020 mi  ·  1,650 km
Ceiling:
17,700 ft  ·  5,400 m
Rate of climb:
1,100 ft/min  ·  m/s
Takeoff distance:
1,080 ft  ·  330 m
Landing distance:
1,330 ft  ·  410 m
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The Cessna 180 was introduced in the market as a more powerful aircraft to complement the Cessna 170. After some time, it has been designated as the Cessna 180 Skywagon. On May 26, 1952, the prototype registered N41697 conducted its first flight, piloted by William D. Thompson.

In 1964, Geraldine Mock, the first woman to fly solo around the world, used a 1953 single-engine Cessna 180 registered as N1538C, christened the Spirit of Columbus, and nicknamed Charlie. The trip started on March 19, 1964, in Columbus, Ohio, to April 17, 1964, in Columbus, Ohio, and the Cessna 180 gained recognition around the world. The Cessna factory acquired the aircraft and stored it at the manufacturing plant in Wichita, Kansas after the historical flight. The aircraft is presently on display at the National Air and Space Museum.

The Cessna 180 has an all-metal airframe, constructed of aluminum alloy. It has an external length of 7.85 meters, a height of 2.36 meters, and a fuselage diameter of 1.1 meters. The fuselage is a semi-monocoque structure. The strut-based wings have a wingspan of 10.97 meters and a wing area of 16.2 square meters. The conventional landing gear has a wheelbase of 6.8 meters, with main gear legs made of spring steel, and a steerable tailwheel attached on a steel tube. Aircraft produced from 1953 to 1963 were designed with two side windows, while later models had three side windows. The Cessna 180 can also be fitted with floats and skis.

The aircraft is powered by a Continental O-470-U piston engine with a maximum thrust of 230 horsepower. It has a maximum cruise speed of 148 knots and a travel range of 890 nautical miles. It can fly up to 17,700 feet and can climb at a rate of 1,100 feet per minute. The takeoff distance is 329 meters while the landing distance is 405 meters.

The Cessna 180 has a maximum takeoff and landing weight of 1,270 kg and 1,029 kg, respectively, and a maximum payload of 469 kg.

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