**Cessna 180/182 Skylane**
**A Versatile and Enduring Aviation Icon**
The Cessna 180/182 Skylane is a legendary single-engine aircraft renowned for its versatility, reliability, and enduring popularity. First introduced in 1953, the Skylane has undergone continuous improvements and upgrades, establishing itself as a workhorse of the aviation industry.
**Design and Construction:**
The Skylane features a rugged and durable all-metal airframe, constructed from lightweight aluminum alloys. Its high-wing design provides excellent visibility and handling characteristics, while the retractable landing gear enhances aerodynamic efficiency during flight.
**Powerplant:**
At the heart of the Skylane is a powerful six-cylinder Continental O-470 engine, delivering up to 230 horsepower. This proven engine provides reliable power for takeoff, climb, and cruising flight, ensuring ample performance even in challenging conditions.
**Flight Performance:**
The Skylane's performance is impressive, with a maximum speed of over 150 knots (278 km/h) and a cruising speed of around 140 knots (259 km/h). Its range extends to over 800 nautical miles (1,482 km), making it suitable for cross-country trips and extended missions.
**Cabin and Interior:**
The Skylane's spacious cabin accommodates up to four passengers comfortably, with ample headroom and legroom. Its well-appointed interior features adjustable seats, a panel-mounted navigation system, and a comprehensive suite of avionics for enhanced situational awareness and flight control.
**Versatility and Applications:**
The Skylane's versatility is unparalleled, making it a sought-after aircraft for a wide range of applications. Pilots use it for:
* Personal and recreational flying
* Business travel and transportation
* Flight training and instruction
* Aerial photography and surveying
* Law enforcement and surveillance
* Medical evacuation and rescue missions
**Legacy and Impact:**
Since its introduction, the Cessna 180/182 Skylane has sold over 23,000 units worldwide, making it one of the best-selling single-engine aircraft in history. Its enduring popularity is a testament to its exceptional design, performance, and versatility.
Today, the Skylane continues to be a highly valued aircraft among pilots and aviation enthusiasts alike, representing a true icon of the skies.
Cessna 180, 182 Skylane 1953-62 Complete Parts Catalog Manual. This comprehensive parts manual offers detailed illustrations along with complete part numbers for the Cessna 180, 182 Skylane airplane. It contains all you need to know to keep your Cessna 180, 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 180, 182 Skylane plane. It will help you better understand, care for, and overall will lower the repair and maintenance cost for your Cessna airplane.
Covers the following Cessna 180, 182 Skylane Years & Models
1953 - 180
1954 - 180
1955 - 180
1956 - 180, 182
1957 - 180, 182
1958 - 180, 182
1959 - 180, 182
1960 - 180, 182
1961 - 180, 182
1962 - 180
* INSTANT DOWNLOAD NO WAITING
* 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
Pages: 450
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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