The Cessna Service Manual offers detailed servicing instructions for the Cessna 182 Skylane 1969-1976 aircraft. The Service repair manual will give you complete step by step information on repair, servicing and preventative maintenance for your Cessna. The manual is highly detailed with photos and illustrations to help guide you through every repair and troubleshooting procedure. This manual contains all you need to know to keep your Cessna 182 working right and is the only service repair manual you will need. It will help you understand, care for, service and lower the repair and maintenance cost for your Cessna 182.

Covers the following Cessna 182 Years & Models
1969 - 182M, A182M SKYLANE
1970 - 182N, A182N SKYLANE
1971 - 182N, A182N SKYLANE
1972 - 182P, A182N SKYLANE
1973 - 182P, A182N SKYLANE
1974 - 182P, A182N SKYLANE
1975 - 182P, A182N SKYLANE
1976 - 182P, A182N SKYLANE

* INSTANT DOWNLOAD NO WAITING
* PDF FORMAT

* Easy navigation allowing you to identify the exact service procedures in the quickest time possible.

*Detailed illustrations, exploded diagrams, drawings.

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File Format: PDF
Pages: 390
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]