CESSNA AIRCRAFT MANUALS 172 The handbook is designed To help you operate your plane with safety and confidence. To more fully acquaint you. POH CESSNA 172P 1984, 14-02691, $50.50. POH CESSNA 172P 1985. CESSNA 172 & SKYHAWK 1957-58 OWNERS MANUAL, 14-00668, $15.95. 1983 Cessna 172Q 180HP 0 results. Items in search results. Cessna 172N 172P 172Q Maintenance Service & Parts Catalog. 1984 Cessna 172Q Cutlass Pilot's. Manual ebooks and get kindle books of cessna 172p poh manual, 1984 cessna 172p skyhawk pilots information manual g s. Digital cessna pilot s operating.
I'm always looking for POHs for my own collection - I reckon the more POHs an instructor can have access to the better. HercFeend- Does Canterbury Aero Club know about this C172P copy?? CB - That scribd has some nice resources - thanks for the link. Dunno why I've never come across it in search before, but you do need to pay - or upload, if you want to download, which is fair enough - share resources. All the Cessna manuals they have I have already, posted here Free POHs (no limits or registrations.trying to build a collection - submissions welcomed, concentrating on Cessna but happy to post anything helpful.
Looking for a C182L if anyone has one, among others. And anything C210 related (left mine at home: If anyone objects I'll take it down, but I reckon shared knowledge=improved safety!!! Thanks Big Pistons, looks like a nice site and a couple I don't have.
I'm trying to spread the word, but keep it quiet if you know what I mean, hehe, but it's a work in progress, happy to help. (Needless I hope to say -for non-commercial and non-operational use only.) Thanks so much to those who've sent private contributions. Betterfromabove - sorry on the validation file, I think I may have removed it recently since I am not in Namibia right now, and can't guarantee the accuracy, it's a magic place to hire and fly, but sorry to say high insurance and poor standards of flight training schools (the former caused by the latter) mean it is quite difficult to arrange. There are four schools who can advise, send me an email message if you want more details, as it's not appropriate to go into that here, but if it's always been a dream I am sure you can make it work.
Contents. Development The Cessna 182 was introduced in 1956 as a variant of the. In 1957, the 182A variant was introduced along with the name Skylane. As production continued, later models were improved regularly with features such as a wider fuselage, swept tailfin with rear 'omni-vision' window, enlarged baggage compartment, higher gross weights, landing gear changes, etc. The 'restart' aircraft built after 1996 were different in many other details including a different engine, new seating design, etc. By mid-2013 Cessna planned to introduce the next model of the 182T, the JT-A, using the 227 hp (169 kW) diesel engine running on with a burn rate of 11 U.S.
Gallons (42 L; 9.2 imp gal) per hour and cruise at 155 kn (287 km/h). Cessna has no timeline for the JT-A and the diesel 172. The normally aspirated, fueled 182 went out of production in 2012, but came back in 2015. Cessna 182s were also built in Argentina by DINFIA (called A182), and by, France, as the F182.
Design The Cessna 182 is an all-metal (mostly aluminum alloy) aircraft, although some parts – such as engine cowling nosebowl and wingtips – are made of fiberglass or thermoplastic material. Its wing has the same platform as the smaller Cessna 172 and the larger 205/206 series; however, some wing details such as flap and aileron design are the same as the 172 and are not like the 205/206 components.
Retractable gear The retractable gear R182 and TR182 were offered from 1978 to 1986, without and with engine turbocharging respectively. The model designation nomenclature differs from some other Cessna models with optional retractable gear. For instance the retractable version of the Cessna 172 was designated as the 172RG, whereas the retractable gear version of the Cessna 182 is the R182.
Cessna gave the R182 the marketing name of 'Skylane RG'. The R182 and TR182 offer 10-15% improvement in climb and cruise speeds over their fixed gear counterparts or, alternatively, 10-15% better fuel economy at the same speeds at the expense of increased maintenance costs and decreased gear robustness. The 1978 R182 has a sea level climb rate of 1140 fpm and cruising speed (75% BHP) at 7,500 feet (2,300 m) of 156 KTAS at standard temperature. The landing gear retraction system in the Skylane RG uses hydraulic actuators powered by an electrically driven pump. The system includes a gear position warning that emits an intermittent tone through the cabin speaker when the gear is in the retracted position and either the throttle is reduced below approximately 12' MAP (manifold pressure) or the flaps are extended beyond 20 degrees. In the event of a hydraulic pump failure, the landing gear may be lowered using a hand pump to pressurize the hydraulic system. The system does not, however, allow the landing gear to be manually retracted.
Variants 182 Initial production version with fixed landing gear, four-seat light aircraft, powered by a 230 hp (172 kW) piston engine, gross weight 2,550 lb (1,157 kg) and certified on 2 March 1956. 182A Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,650 lb (1,202 kg) and certified on 7 December 1956. 182B Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,650 lb (1,202 kg) and certified on 22 August 1958. 182C Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,650 lb (1,202 kg) and certified on 8 July 1959. 182D Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,650 lb (1,202 kg) and certified on 14 June 1960.
182E Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) or O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 27 June 1961. 182F Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) or O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 1 August 1962. 182G Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) or O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 19 July 1963. 182H Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,800 lb (1,270 kg) and certified on 17 September 1964.
182J Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,800 lb (1,270 kg) and certified on 20 October 1965. 182K Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,800 lb (1,270 kg) and certified on 3 August 1966. 182L Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,800 lb (1,270 kg) and certified on 28 July 1967. 182M Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,800 lb (1,270 kg) and certified on 19 September 1968.
There was also an experimental version of this model with a full cantilever wing. 182N Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) 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.
182P Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) or O-470-S piston engine, gross weight 2,950 lb (1,338 kg) and certified on 8 October 1971. 182Q Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight 2,950 lb (1,338 kg) and certified on 28 July 1976. 182R Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) piston engine, gross weight of 3,100 lb (1,406 kg) for takeoff and 2,950 lb (1,338 kg) for landing.
Certified on 29 August 1980. This variant, along with the 182Q, can alternatively be equipped with the burning Diesel engine. 182S Skylane Four-seat light aircraft with fixed landing gear, powered by a 230 hp (172 kW) 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. 182T Skylane Four-seat light aircraft with fixed landing gear, powered by a fuel-injected 230 hp (172 kW) piston engine, gross weight of 3,100 lb (1,406 kg) for take-off and 2,950 lb (1,338 kg) for landing. It was certified on 23 February 2001 and, as of July 2015, it is the only variant in production. R182 Skylane RG Four-seat light aircraft with retractable landing gear, powered by a 235 hp (175 kW) piston engine, gross weight 3,100 lb (1,406 kg) and certified on 7 July 1977.
T182 Four-seat light aircraft with fixed landing gear, powered by a turbocharged 235 hp (175 kW), 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. T182T Skylane Four-seat light aircraft with fixed landing gear, powered by a turbocharged and fuel-injected 235 hp (175 kW) piston engine, gross weight of 3,100 lb (1,406 kg) for take-off and 2,950 lb (1,338 kg) for landing.
Cessna 172p Specifications
Certified on 23 February 2001. TR182 Turbo Skylane RG Four-seat light aircraft with retractable landing gear, powered by a 235 hp (175 kW) piston engine, gross weight 3,100 lb (1,406 kg) and certified on 12 September 1978. T182JT-A Turbo Skylane JT-A Four-seat light aircraft with fixed landing gear, powered by a 227 hp (169 kW) diesel engine, it burns 11 U.S. Gallons (42 L; 9.2 imp gal) per hour of fuel and cruises at 156 kn (289 km/h). The model was first flown in May 2013, and as of July 2015, FAA certification is on hold indefinitely. Originally introduced as the Turbo Skylane NXT, Cessna changed the name to avoid confusion with the Remos NXT. Robertson STOL 182 An aftermarket 182 conversion certified in 1967 that changes the shape and controls and lowers the stall speed below 35 mph (56 km/h).
Operators Civil users The 182 is used by a multitude of civil operators, cadet organizations and flight schools worldwide. Government operators Belgium. Canada. – one, sold in 2010 United States. United States Air Force Auxiliary / – Used for inland and coastal search and rescue, homeland security support, and airborne communications repeater service. 27 used as equipped with optical, infrared and cellphone equipment Military operators.
Army Aviation. – 5 × L-182, retired 1970. Early model 182 between the 1950s and early 1980s. Cessna website lists 22,336 Skylanes delivered up to 2007 plus 901 Turbo Skylanes delivered up to 2007. It does not indicate whether these numbers include the retractable-gear 182s, which are no longer in production and therefore are not discussed on their webpage.
It also does not (as of 14 May 2009) list the 2008 delivery totals. Fred George (May 2017).
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Retrieved 2 December 2011. Civil Air Patrol. Retrieved 1 October 2012. With 118 glass cockpit Cessna 182 Skylanes now in CAP’s fleet, more and more CAP aircrews are benefiting from Cessna’s state-of-the-art Garmin G1000 flight equipment. Star Tribune. Archived from on 2 June 2015. Retrieved 2 June 2015.
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'General Aviation marches into its second century'., May 2000, Vol. External links Wikimedia Commons has media related to. at Airliners.net. at PilotFriend.com.