Cessna 182 Skylane
The Cessna 182 Skylane is a four-seat, single-engine, fixed-wing aircraft manufactured by Cessna Aircraft Company from 1956 to 1986. It is a high-wing, strut-braced monoplane with a tricycle landing gear and a single, six-cylinder, air-cooled engine. The Skylane is designed for general aviation, including private flying, flight training, and business transportation.
The Skylane was developed from the Cessna 172 Skyhawk, and it shares many of the same design features. However, the Skylane is larger and more powerful than the Skyhawk, and it has a wider fuselage and a longer wingspan. The Skylane is also equipped with a more powerful engine, which gives it a higher cruise speed and a greater payload capacity.
The Skylane is a versatile aircraft that can be used for a variety of purposes. It is a popular choice for private pilots who want a comfortable and capable aircraft for flying, and it is also used by flight schools for training new pilots. The Skylane is also a popular choice for businesses that need to transport employees or cargo.
The Skylane has a long and successful history, and it remains a popular aircraft today. It is a well-built and reliable aircraft that is easy to fly and maintain. The Skylane is also a very comfortable aircraft, and it is a pleasure to fly.
Here are some of the key features of the Cessna 182 Skylane:
* Four-seat, single-engine, fixed-wing aircraft
* High-wing, strut-braced monoplane
* Tricycle landing gear
* Single, six-cylinder, air-cooled engine
* Cruise speed of 140 mph
* Payload capacity of 1,000 lbs
* Range of 700 miles
The Cessna 182 Skylane is a versatile and capable aircraft that is suitable for a variety of purposes. It is a popular choice for private pilots, flight schools, and businesses. The Skylane is a well-built and reliable aircraft that is easy to fly and maintain. The Skylane is also a very comfortable aircraft, and it is a pleasure to fly.
Cessna 182 Skylane 1974-86 Complete Parts Catalog Manual. This comprehensive parts manual offers detailed illustrations along with complete part numbers for the Cessna 182 Skylane airplane. It contains all you need to know to keep your Cessna 182 Skylane working correctly. You will find that this parts catalog/manual is an indispensable source of detailed information and is the only parts manual you will need for your Cessna 182 Skylane plane. It will help you better understand, care for, service and overall will lower the repair and maintenance cost for your Cessna airplane.
Covers the following Cessna 182 Skywagon Years & Models
1974 - 182 Skylane
1975 - 182 Skylane
1976 - 182 Skylane
1977 - 182 Skylane
1978 - 182 Skylane
1979 - 182 Skylane
1980 - 182 Skylane
1981 - 182 Skylane
1982 - 182 Skylane
1983 - 182 Skylane
1984 - 182 Skylane
1985 - 182 Skylane
1986 - 182 Skylane
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* PDF FORMAT
* Easy navigation and fully searchable allowing you to identify the exact parts needed in the quickest time possible.
*Detailed illustrations, exploded diagrams, drawings.
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File Format: PDF
Printable: Yes
Language: English
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Cessna 182 Model Information
182
Initial production version with fixed landing gear, four place light aircraft, powered by a 230 hp (172 kW) Continental O-470-L piston engine, gross weight 2,550 lb (1,157 kg) and certified on 2 March 1956.[4]
182A Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-L piston engine, gross weight 2,650 lb (1,202 kg) and certified on 7 December 1956.[4]
182B Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-L piston engine, gross weight 2,650 lb (1,202 kg) and certified on 22 August 1958.[4]
182C Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-L piston engine, gross weight 2,650 lb (1,202 kg) and certified on 8 July 1959.[4]
182D Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-L piston engine, gross weight 2,650 lb (1,202 kg) and certified on 14 June 1960.[4]
182E Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-L or O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 27 June 1961.[4]
182F Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-L or O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 1 August 1962.[4]
182G Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-L or O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 19 July 1963.[4]
182H Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 17 September 1964.[4]
182I
There was no "I" model built.[4]
182J Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 20 October 1965.[4]
182K Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 3 August 1966.[4]
182L Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 28 July 1967.[4]
182M Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 19 September 1968.[4] There was also an experimental version of this model with a full cantilever wing.[6]
182N Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-R or O-470-S piston engine, gross weight 2,950 lb (1,338 kg) for take-off and 2,800 lb (1,270 kg) for landing. Certified on 17 September 1969.[4]
182P Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-R or O-470-S piston engine, gross weight 2,950 lb (1,338 kg) and certified on 8 October 1971.[4]
182Q Skylane
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-U piston engine, gross weight 2,950 lb (1,338 kg) and certified on 28 July 1976.[4]
182R
Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-U piston engine, gross weight of 3,100 lb (1,406 kg) for take-off and 2,950 lb (1,338 kg) for landing. Certified on 29 August 1980.[4]
182S Skylane
Four place light aircraft with fixed landing gear, powered by a fuel-injected 230 hp (172 kW) Lycoming IO-540-AB1A5 piston engine, gross weight of 3,100 lb (1,406 kg) for take-off and 2,950 lb (1,338 kg) for landing. Certified on 3 October 1996.[4]
182T Skylane
Four place light aircraft with fixed landing gear, powered by a fuel-injected 230 hp (172 kW) Lycoming IO-540-AB1A5 piston engine, gross weight of 3,100 lb (1,406 kg) for take-off and 2,950 lb (1,338 kg) for landing. Certified on 23 February 2001.[4]
R182 Skylane RG
Four place light aircraft with retractable landing gear, powered by a 235 hp (175 kW) Lycoming O-540-J3C5D piston engine, gross weight 3,100 lb (1,406 kg) and certified on 7 July 1977.[4]
T182
Four place light aircraft with fixed landing gear, powered by a turbocharged 235 hp (175 kW) Lycoming 0-540-L3C5D, piston engine, gross weight of 3,100 lb (1,406 kg) for take-off and 2,950 lb (1,338 kg) for landing. Certified on 15 August 1980.[4]
T182T Skylane
Four place light aircraft with fixed landing gear, powered by a turbocharged and fuel-injected 235 hp (175 kW) Lycoming TIO-540-AK1A piston engine, gross weight of 3,100 lb (1,406 kg) for take-off and 2,950 lb (1,338 kg) for landing. Certified on 23 February 2001.[4]
TR182 Turbo Skylane RG
Four place light aircraft with retractable landing gear, powered by a turbocharged 235 hp (175 kW) Lycoming O-540-J3C5D piston engine, gross weight 3,100 lb (1,406 kg) and certified on 12 September 1978.[4]
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