model s

Aircraft updates are normally the story of larger engines. Even larger always appears to be much better with engines. Who will not want much more surge on takeoff, a steeper climb and more rapidly cruise?

Engine updates do have complications even though. More electric power generally means more gas movement, which suggests more substantial tanks, a lot less beneficial load or a beefier structure which wants much more energy to elevate it and so on.

Cessna would seem to have prevented the engine treadmill by offering the 182 just the correct total of energy from the start. The typical 182 that rolled off the line in 1956 is inside of 5 horsepower of ones coming off the line in 2011.

In point just two engines, the Continental O-470 and Lycoming O-540 account for the engines in the vast greater part of Cessna 182’s flying.

Following are the key versions in Cessna 182 designs. Quite a few of the improvements are related to boosts in gross excess weight. Styles with insignificant variations are omitted. One modify to note is that the “S”model released a fuel injected motor which is additional effective, is not issue to carburetor ice and requires a unique starting up process.

182
Original manufacturing edition with fixed landing gear, 4 put gentle aircraft, run by a 230 hp Continental O-470-L piston motor, gross excess weight 2,550 lb and accredited on 2 March 1956.

182A Skylane
Powered by a 230 hp (172 kW) Continental O-470-L, weight 2,650 lb and licensed on 7 December 1956.

182E Skylane
Run by a 230 hp Continental O-470-L or O-470-R, body weight 2,800 lb and licensed on 27 June 1961.

182N Skylane
Driven by a 230 hp Continental O-470-R or O-470-S, fat 2,950 lb for get-off and 2,800 lb for landing. Licensed on 17 September 1969.

182P Skylane
Driven by a 230 hp Continental O-470-R or O-470-S, body weight 2,950 lb and qualified on 8 October 1971.

182Q Skylane
Driven by a 230 hp Continental O-470-U, gross fat 2,950 lb and qualified on 28 July 1976.

182R
Powered by a 230 hp Continental O-470-U, gross weight of 3,100 lb for acquire-off and 2,950 lb for landing. Licensed on 29 August 1980.

182S Skylane
Run by a gasoline-injected 230 hp Lycoming IO-540-AB1A5 piston motor, gross excess weight of 3,100 lb for choose-off and 2,950 lb for landing. Qualified on 3 Oct 1996.

R182 Skylane RG
Retractable landing gear, powered by a 235 hp (175 kW) Lycoming O-540-J3C5D, gross pounds 3,100 lb and certified on 7 July 1977.

T182
Powered by a turbocharged 235 hp Lycoming -540-L3C5D, gross excess weight of 3,100 lb for acquire-off and 2,950 lb (1,338 kg) for landing. Qualified on 15 August 1980.

T182T Skylane
Powered by a turbocharged and gas-injected 235 hp (175 kW) Lycoming TIO-540-AK1A, gross fat of 3,100 lb for acquire-off and 2,950 lb for landing. Licensed on 23 February 2001.

TR182 Turbo Skylane RG
Retractable landing gear, powered by a turbocharged 235 hp Lycoming O-540-J3C5D, body weight 3,100 lb and certified on 12 September 1978

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