
Cessna 185 Skywagon | |
|---|---|
| Riik | USA |
| Rolli | Kerged kommunaallennukid |
| Esimene lend | Juuli 1960 |
| Ehitatud | 4400+ |
2007 Cessna A-185F Skywagon on ühemootoriline, kõrge tiivaga, kuuekohaline kerge tarbelennuk, mille on tootnud Ameerika tootja Cessna Aircraft Company. See on Cessna 180 mudeli edasiarendus, millel on võimsam mootor, suurem kabiin ja tagaratta maandumisseade. A-185F mudelit tutvustati 1973. aastal ja sellel oli kütuse sissepritsega Continental IO-520-D mootor, millel oli 300 hj, kolme teraga propeller ja seljauim parema stabiilsuse tagamiseks. A-185F-il oli ka suurem pagasiruum, laiem tagaklaas ja valikuline kõhuga kaubakapsel. A-185F oli viimane Skywagoni mudel, mida toodeti, kuna Cessna lõpetas liini 1985. aastal. A-185F on populaarne bush-pilootide seas, kes kasutavad seda erinevateks missioonideks, nagu tšarterlennud, aerofotograafia, tuletõrje, langevarjuhüpped ja humanitaarabi. A-185F maksimaalne kiirus on 155 sõlme, vahemik 845 meremiili ja teeninduslagi 17 150 jalga. A-185F on tuntud oma vastupidavuse, töökindluse ja mitmekülgsuse poolest.
Allikas: Cessna 185 Skywagon Vikipeedias
| Cessna A185F Skywagon Walk Around | |
|---|---|
| Photographer | Vladimir Yakubov |
| Localisation | Hiller Museum Sea Plane Fly-in 2013 |
| Photos | 79 |
Vaata ka:
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) |
|---|---|
| Rolli | Utility Aircraft / Bush Plane / Light Transport |
| Tootja | Cessna Aircraft Company |
| Production Years | 1961–1985 |
| Meeskonna | 1 pilot |
| Võimsuse | Up to 5 passengers (6 total occupants) |
| Tiibade siruulatus | 10.92 m (35 ft 10 in) |
| pikkus | 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).
Vaatamisi : 852


















