The Cessna 185 Skywagon is a six-seat, single-engined, general aviation light aircraft manufactured by Cessna. It first flew as a prototype in July 1960, with the first production model completed in March 1961. The Cessna 185 is a high-winged aircraft with non-retractable conventional landing gear and a tailwheel.
Cessna 185 Skywagon | |
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A Cessna 185 with floats | |
Role | Light utility aircraft |
Manufacturer | Cessna Aircraft Company |
First flight | July 1960 |
Introduction | 1961 |
Status | Active |
Produced | 1961–1985 |
Number built | over 4,400 |
Developed from | Cessna 180 |
Variants | St-Just Super-Cyclone |
Over 4,400 were built with production ceasing in 1985. When Cessna re-introduced some of its most popular models in the 1990s, the tailwheel equipped Cessna 180 and 185 were not put back into production.
The aircraft is basically a Cessna 180 with a strengthened fuselage. The main difference between the two aircraft is the larger vertical fin on the 185 and the 300 hp (224 kW) Continental IO-520-D engine as opposed to the 230 hp (172 kW) Continental O-470-S fitted to the Cessna 180. The exception was that a Continental Motors IO-470-F engine of 260 hp (194 kW) was initially fitted until midway through the 1966 production year. The later model Skywagon II has a factory fitted avionics package.
The Skywagon can also be fitted with floats, amphibious floats, or skis. The AgCarryall variant of the 185 adds a 151-gallon belly chemical tank and removable spray booms for aerial application. It is also possible to fit a cargo pod under the fuselage that can carry an extra 300 lb (136 kg).
The 180 and 185 are widely used in bush flying, the commercial transport of passengers and freight to rudimentary, remote airstrips, lakes and snowfields, primarily in Canada and Alaska.
The Cessna 185 is popular with air charter companies and is operated by private individuals and companies.
As part of the United States Military Assistance Program, Cessna received a contract to supply the United States Air Force with the Skywagon. These were intended for delivery overseas and were designated U-17A and U-17B.
Data from Cessna[27]
General characteristics
Performance
Landplane | Floatplane | Amphibian | |
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Length | 27 ft 0 in (8.23 m) | 27 ft 6 in (8.38 m) | |
Height | 12 ft 2 in (3.71 m) | 12 ft 8 in (3.86 m) | |
Empty weight | 1,745 lb (792 kg) | 1,910 lb (866 kg) | 2,165 lb (982 kg) |
MTOW | 3,320 lb (1,506 kg) | 3,265 lb (1,481 kg) on land 3,100 lb (1,406 kg) on water | |
Max. speed | 136 knots (252 km/h) | 141 knots (261 km/h) | 135 knots (251 km/h) |
Range | 516 nm (957 km) | 503 nm (933 km) | 482 nm (893 km) |
Service ceiling | 16,400 ft (5,000 m) | 15,300 ft (4,700 m) | |
Rate of climb | 960 ft/min (293 m/min) | 970 ft/min (296 m/min) | |
Wing loading | 19.1 lb/ft2 (93.3 kg/m2) | 18.8 lb/ft2 (91.8 kg/m2) |
Related development
Media related to Cessna 185 at Wikimedia Commons