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Cessna 180

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Introduced
  
1953

First flight
  
May 26, 1952

Number of seats
  
6

Engine type
  
Continental O-470

Manufacturer
  
Cessna

Cessna 180 Cessna 180 Skywagon all models Photos AirplanePicturesnet

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The Cessna 180 is a four- or six-seat, fixed conventional gear general aviation airplane which was produced between 1953 and 1981. Though the design is no longer in production, many of these aircraft are still in use as personal aircraft and in utility roles such as bush flying.

Contents

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Development

Cessna introduced the heavier and more powerful 180 as a complement to the Cessna 170. It eventually came to be known as the Skywagon.

Cessna 180 Cessna 180 amp 185 Skywagon pictures technical data history

The prototype Cessna 180, N41697, first flew on May 26, 1952. Cessna engineering test pilot William D. Thompson was at the controls.

Cessna 180 httpsuploadwikimediaorgwikipediacommonsthu

In all its versions, 6,193 Cessna 180s were manufactured. In 1956, a tricycle gear version of this design was introduced as the Cessna 182, which came to bear the name Skylane. Additionally, in 1960, Cessna introduced a heavier, more powerful sibling to the 180, the conventional gear Cessna 185. For a time, all three versions of the design were in production.

Design

Cessna 180 FileN4768B Cessna 180 3832934246jpg Wikimedia Commons

The airframe of the 180 is all-metal, constructed of aluminum alloy. The fuselage is a semi-monocoque structure, with exterior skin sheets riveted to formers and longerons. The strut-braced wings, likewise, are constructed of exterior skin sheets riveted to spars and ribs. The landing gear of the 180 is in a conventional arrangement, with main gear legs made of spring steel, and a steerable tailwheel mounted on a hollow tapered steel tube.

Cessna 180s produced between 1953 and 1963 have two side windows, while 1964 to 1981 models feature three side windows, as they use the same fuselage as the Cessna 185. 180s can be equipped with floats and skis.

Record flight

The Cessna 180 gained recognition as the aircraft chosen by Geraldine Mock, the first woman pilot to successfully fly around the world. The flight was made in 1964 in her 1953 model, the Spirit of Columbus (N1538C), as chronicled in her book Three-Eight Charlie. The Cessna factory obtained the aircraft and kept it at the Pawnee (Wichita, Kansas) manufacturing plant after the epic flight, suspended from the ceiling over one of the manufacturing lines. It is currently on display at the National Air and Space Museum.

Variants

180
Four seat high wing light aircraft powered by a 225 hp (168 kW) Continental O-470-A, O-470-J, or a 230 hp (172 kW) O-470-K engine, landplane gross weight 2,550 lb (1,157 kg) and first certified on 23 December 1952.
180A
Four seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-K, landplane gross weight 2,650 lb (1,202 kg) and first certified on 17 December 1956.
180B
Four seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-K, landplane gross weight 2,650 lb (1,202 kg) and first certified on 22 August 1958.
180C
Four seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-L or O-470-R, landplane gross weight 2,650 lb (1,202 kg) and first certified on 8 July 1959.
180D
Four seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-L or O-470-R, landplane gross weight 2,650 lb (1,202 kg) and first certified on 14 June 1960.
180E
Four seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-L or O-470-R, landplane gross weight 2,650 lb (1,202 kg) and first certified on 21 September 1961.
180F
Four seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-L or O-470-R, landplane gross weight 2,650 lb (1,202 kg) and first certified on 25 June 1962.
180G
Six seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-L or O-470-R, landplane gross weight 2,800 lb (1,270 kg) and first certified on 19 July 1963.
180H
Six seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-L or O-470-R, landplane gross weight 2,800 lb (1,270 kg) and first certified on 17 June 1964.
180I
There was no "I" model Cessna 180.
180J
Six seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-R or O-470-S, landplane gross weight 2,800 lb (1,270 kg) and first certified on 13 October 1972.
180K
Six seat high wing light aircraft powered by a 230 hp (172 kW) Continental O-470-U, landplane gross weight 2,800 lb (1,270 kg) and first certified on 19 August 1976.

Civil

The Cessna 180 is popular with air charter companies and is operated by private individuals and companies.

Military

 Australia

19 Cessna 180s were in service with both the Australian Army and RAAF from 1959 to 1974.

  • Royal Australian Air Force
  • No. 16 Air Observation Post Flight RAAF
  • Australian Army Aviation
  • No. 16 Army Light Aircraft Flight
  • No. 161 (Independent) Reconnaissance Flight – The Australian Army operated a number of Cessna 180s as surveillance aircraft with the 161 Reconnaissance Flight (call sign "Possum") during the Vietnam War.
  •  El Salvador
     Guatemala
     Honduras
  • Honduran Air Force
  •  Israel
  • Israeli Air Force
  •  Khmer Republic
  • Khmer Air Force – operated 2 Cessna 180s.
  • Kingdom of Laos
  • Royal Lao Air Force
  •  Nicaragua
     Philippines
     Thailand
  • Royal Thai Navy
  •  Uruguay
  • Uruguayan Air Force
  • Specifications (1978 Cessna 180 II landplane)

    Data from Cessna

    General characteristics

  • Crew: one
  • Capacity: five passengers
  • Length: 25 ft 9 in (7.85 m)
  • Wingspan: 35 ft 10 in (10.92 m)
  • Height: 7 ft 9 in (2.36 m)
  • Wing area: 174 sq ft (16.2 m2)
  • Empty weight: 1,700 lb (771 kg)
  • Gross weight: 2,800 lb (1,270 kg)
  • Powerplant: 1 × Continental O-470-U , 230 hp (170 kW)
  • Propellers: 2-bladed constant speed, 6 ft 10 in (2.08 m) diameter
  • Performance

  • Maximum speed: 148 kn (170 mph; 274 km/h)
  • Cruise speed: 142 kn (163 mph; 263 km/h)
  • Stall speed: 48 kn (55 mph; 89 km/h)
  • Range: 890 nmi (1,024 mi; 1,648 km)
  • Service ceiling: 17,700 ft (5,400 m)
  • Rate of climb: 1,100 ft/min (5.6 m/s)
  • References

    Cessna 180 Wikipedia


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