Cessna 185 Skywagon

Cessna 185 Skywagon
Državi	Zda
Vlogo	Lahka letalska letala
Prvi let	julij 1960
Zgrajena	4400+

V Cessna A-185F Skywagon je enomotorno, visokokrilno, šestsedežno lahko letalo, ki ga proizvaja ameriški proizvajalec Cessna Aircraft Company. Gre za razvoj modela Cessna 180, z močnejšim motorjem, večjo kabino in podvozjem zadnjega kolesa. Model A-185F je bil predstavljen leta 1973 in je imel motor Continental IO-520-D z vbrizgavanjem goriva s 300 KM, propeler s tremi lopaticami in hrbtno plavut za boljšo stabilnost. A-185F je imel tudi večji prtljažni prostor, širše zadnje steklo in opcijsko trebušno tovorno palico. A-185F je bil zadnji model Skywagon, ki je bil izdelan, saj je Cessna leta 1985 prekinil linijo. A-185F je priljubljen med bush piloti, ki ga uporabljajo za različne misije, kot so čarterski leti, fotografiranje iz zraka, gašenje požarov, padalstvo in humanitarna pomoč. A-185F ima največjo hitrost 155 vozlov, domet 845 navtičnih milj in zgornjo mejo storitve 17,150 čevljev. A-185F je znan po svoji robustnosti, zanesljivosti in vsestranskosti.

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Cessna A185F Skywagon Walk Around
Photographer	Vladimir Yakubov
Localisation	Hiller Museum Sea Plane Fly-in 2013
Photos	79

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Cessna A-185F Skywagon 09

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General Characteristics (A185F Variant)

The Cessna 185 Skywagon is a rugged, high-wing, single-engine utility aircraft designed for general aviation and demanding operations in remote areas. Introduced as a more powerful version of the Cessna 180, the 185 is famous for its exceptional useful load and conventional (tailwheel) landing gear, making it a favorite among bush pilots and operators requiring short takeoff and landing (STOL) capabilities.

Property	Typical Value (A185F Landplane)
Vlogo	Utility Aircraft / Bush Plane / Light Transport
proizvajalec	Cessna Aircraft Company
Production Years	1961–1985
Posadke	1 pilot
Zmogljivost	Up to 5 passengers (6 total occupants)
Peruti	10.92 m (35 ft 10 in)
Dolžina	7.85 m (25 ft 9 in)
Max Takeoff Weight	1,520 kg (3,350 lb)

Design and Powerplant

Engine: One Continental IO-520-D six-cylinder, fuel-injected, air-cooled piston engine (on later models).
Power Output: 224 kW (300 hp) for takeoff (285 hp continuous).
Propeller: Typically a 2-bladed or optional 3-bladed constant-speed propeller.
Fuselage: All-metal monocoque construction with a high wing and fixed, non-retractable conventional (tailwheel) landing gear.
Versatility: Can be easily converted to various roles, often fitted with floats (seaplane) or skis for operation on water or snow/ice, thanks to its high useful load and power.
Useful Load: The high useful load (up to 1,600+ lb) is a key feature, allowing it to carry substantial cargo or full fuel/passengers simultaneously.

Performance and Key Features

Max Cruise Speed: Up to 269 km/h (167 mph, 145 knots).
Maximum Range: Approximately 1,330 km (720 nautical miles) with standard fuel.
Service Ceiling: 5,230 m (17,150 ft).
Rate of Climb: Approximately 5.1 m/s (1,010 ft/min).
STOL Performance: Known for its short field performance, with a ground roll of approximately 251 m (825 ft) at maximum weight, ideal for unimproved strips.
Cargo: Later models (A185F) included a large baggage area and the option for bubble side windows, a cargo pod (adding 300 lb capacity), or a spray rig (AgCarryall variant).

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