Cessna 182 "High-altitude Corridor"

Cessna 182 "High-altitude Corridor"

Cessna 182 "High-altitude Corridor" is essentially a 180 aircraft with a fixed front three-point landing gear. 182 "high-altitude corridor" 1956 made its first flight, 1958 65438+ 10 entered service. The final version has a retractable landing gear. The total delivery of "air corridor" exceeds 22,000.

Name: Cessna 182 "High-altitude Corridor" single-engine piston light aircraft.

Maiden voyage time: 1956

Service time: 1958 65438+ 10 month.

R&D unit: Cessna Aircraft Company.

Aerodynamic layout: straight wing

Number of engines: single engine

Flight speed: subsonic

Crew: 4 people

Captain: 8.5 meters

Span: 10.9 m

Machine height: 2.8m.

Empty weight: 984 kg

Engine: Continental or Laichuan Ming piston engine.

Maximum takeoff weight:1.406kg.

Maximum flight speed: 278 km/h.

Maximum voyage: 1, 896 km

Model evolution

182 initial basic production type. 182c has a swept vertical tail, and a third porthole is added. 182E The rear of the fuselage is shortened, and the panoramic rear window. 182P landing gear strut is steel tube type. With a huge dorsal fin. 182R can be equipped with a turbocharged engine. 182s "high-altitude corridor" 1995, new model. 182T "high-altitude corridor" is an improvement of 200 1. T 182T "turbo high-altitude corridor" turbocharged vehicle. 182R "high-altitude corridor" can be equipped with turbocharged engine. R 182 "High-rise Corridor" RG adopts retractable landing gear with optional turbocharger.

design feature

Inclined strut linear upper wing; Single continental or Laichuan Ming piston engine, Shuang Ye propeller; Swept vertical tail, dorsal tail and lower horizontal tail: fix or retract the landing gear (some models of wheel fairings are stuck).