|
|more users=
|produced=1956–1985,<br />1996–2012,<br />2015–present
|number built=
|number built=over 23,237+<ref>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, so are not discussed on their webpage. It also does not (as of 14 May 2009) list the 2008 delivery totals.</ref>
|variants with their own articles=
|developed from=[[Cessna 180]]
==Development==
The Cessna 182 was introduced in 1956 as a [[tricycle gear]] variant of the [[Cessna 180|180]]. In 1957, the 182A variant was introduced, alongfollowed withby a deluxe version the namefollowing year known as the '''Skylane'''.<ref name="Phillips" /> 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.{{citation needed|date=December 2020}}
By mid-2013, Cessna planned to introduce the next model of the 182T, designated the JT-A, using the {{convert|227|hp|kW|0|abbr=on}} [[SMA SR305-230]] diesel engine running on [[Jet-A]] with a burn rate of {{convert|11|u.s.gal}} per hour and cruise at {{convert|155|kn|km/h|0|abbr=on}}.<ref name=aopa2012>{{cite journal|journal=AOPA Pilot|title=Jet A for your Skylane|author=Thomas B Haines|date=October 2012}}</ref><ref name="Grady22Jul12">{{cite news|url = http://www.avweb.com/news/airventure/EAAAirVenture2012_CessnaUnveilsJetAEngineForSkylane_207018-1.html|title = Cessna Unveils Jet A Engine For Skylane|access-date = 24 July 2012|last = Grady|first = Mary|date = 22 July 2012| work = AVweb}}</ref> Cessna has no timeline for the JT-A.<ref name=avw2015-05>{{cite web |first=Paul |last=Bertorelli |url=http://www.avweb.com/blogs/insider/Has-Cessna-Suddenly-Grown-Cold-on-Diesel-224068-1.html |title=Has Cessna Suddenly Grown Cold On Diesel? |work=AVweb|agency=Aviation Publishing Group |date=12 May 2015 |access-date=13 May 2015 }}</ref> The normally aspirated, [[avgas]]-fueled 182 went out of production in 2012, but came back in 2015.<ref name=fly2015-05-14>{{cite news |first=Stephen |last=Pope |url=http://www.flyingmag.com/aircraft/pistons/gas-powered-cessna-182-back-production |title=Gas-Powered Cessna 182 Back in Production |work=[[Flying (magazine)|Flying]] |date=14 May 2015 |access-date=16 May 2015 }}</ref><!--old sources prediction the future <ref name=aopa2012/><ref name="Grady22Jul12"/> -->
===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 and the 177RG , whereas the retractable gear version of the Cessna 182 is the R182. Cessna gave the R182 the marketing name of "Skylane RG".<ref name="3A13">{{cite web|url = http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/084b5675182d8714862575f6006d1bf4/$FILE/3A13%20Rev%2069.pdf|title = TYPE CERTIFICATE DATA SHEET NO. 3A13 Revision 69|access-date = 23 March 2010|last = Federal Aviation Administration|author-link = Federal Aviation Administration|date = April 2009|archive-date = 1 February 2010|archive-url = https://web.archive.org/web/20100201153302/http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/084b5675182d8714862575f6006d1bf4/$FILE/3A13%20Rev%2069.pdf|url-status = dead}}</ref>
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 ft/min and cruising speed (75% BHP) at {{convert|7500|ft|m}} of 156 KTAS at standard temperature.<ref name="1978 R182 POH">{{cite book | author = Cessna Aircraft Company | title = Pilot's Operating Handbook, Skylane RG, 1978 Model R182 |date=October 1977 }}</ref>
==Variants==
''Cessna has historically used [[Model year|model years]] similar to U.S. auto manufacturers, with sales of new models typically starting a few months prior to the actual calendar year.''
;182
:Initial production version withbuilt fixedonly landingfor gear,the four-seat1956 lightmodel year. aircraft, poweredPowered by a carbureted {{convert|230|hp|kW|0|abbr=on}} [[Continental O-470|Continental O-470-L]] piston engine, gross weight {{convert|2550|lb|kg|0|abbr=on}}. and certifiedCertified on 2 March 1956. 844 built.<ref name="Phillips" /><ref name="3A13" /><ref name=":0">{{Cite web |last=Frank |first=John M. |date=April 11, 2012 |title=182 Model History |url=https://cessna.org/wp-content/uploads/2019/07/182hist-1.pdf |access-date=June 5, 2024 |website=Cessna Pilots Association}}</ref>
;182A Skylane
:Introduced for the 1957 model year with manual flaps, redesigned landing gear for improved ground handling, and an increased gross weight of {{convert|2650|lb|kg|0|abbr=on}}. A deluxe version was introduced for the 1958 model year as the '''Skylane''' with full exterior paint, wheel fairings, and an improved engine cowling with the exhaust stack moved to the right to improve engine cooling. Certified on 7 December 1956. 1713 total built; 911 (1957) and 802 (1958).<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-L piston engine, gross weight {{convert|2650|lb|kg|0|abbr=on}} and certified on 7 December 1956<ref name="3A13" />
;182B Skylane
:Four-seat1959 lightmodel aircraftyear with fixeda landingmore gear,streamlined poweredcowling bywith acowl carburetedflaps, {{convert|230|hp|kW|0|abbr=on}}a Continentalnew O-470-Linstrument pistonpanel enginecover, grossand weightimproved {{convert|2650|lb|kg|0|abbr=on}}ventilation. and certifiedCertified on 22 August 1958. 802 built.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
;182C Skylane
:1960 model year with a redesigned swept vertical tail and smaller wing root fillets. The cabin was also redesigned with more headroom, molded plastic control wheels, and a third cabin window. Certified on 8 July 1959. 650 built, plus four largely identical '''L-19L''' models for the [[Canadian Army]].<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-L piston engine, gross weight {{convert|2650|lb|kg|0|abbr=on}} and certified on 8 July 1959<ref name="3A13" />
;182D Skylane
:1961 model year with a key start switch, cam-lock cowling fasteners, and decreased landing gear height. Certified on 14 June 1960. 591 built.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-L piston engine, gross weight {{convert|2650|lb|kg|0|abbr=on}} and certified on 14 June 1960<ref name="3A13" />
;182E Skylane
:Four-seat1962 lightmodel aircraftyear with fixeda landingcut geardown rear fuselage with "Omni-Vision" rear windows, poweredelectric by"Para-Lift" flaps, a carburetedredesigned horizontal stabilizer, elevator and rudder trim tabs, a new tailcone and wingtips, and {{convert|65|gal|L||abbr=on}} [[neoprene]] fuel bladders. Wheel fairings, which were previously exclusive to the deluxe Skyhawk model, were made standard of the 182E. Power was provided by a {{convert|230|hp|kW|0|abbr=on}} Continental O-470-L or O-470-R piston engine, and gross weight was increased to {{convert|2800|lb|kg|0|abbr=on}}. and certifiedCertified on 27 June 1961. 826 built.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
;182F Skylane
:1963 model year with minor refinements including magnesium rudder peddles. Certified on 1 August 1962. 635 built.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-L] or O-470-R piston engine, gross weight {{convert|2800|lb|kg|0|abbr=on}} and certified on 1 August 1962.<ref name="3A13" />
;182G Skylane
:1964 model year with redesigned rear and aft cabin windows for improved visibility. Certified on 19 July 1963. 786 built.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-L or O-470-R piston engine, gross weight {{convert|2800|lb|kg|0|abbr=on}} and certified on 19 July 1963<ref name="3A13" />
;182H Skylane
:1965 model year with new propeller spinner, increased horizontal stabilizer span, and one-piece windshield. Certified on 17 September 1964. 840 built.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-R piston engine, gross weight {{convert|2800|lb|kg|0|abbr=on}} and certified on 17 September 1964<ref name="3A13" />
;182J Skylane
:1966 model year with magnesium control wheels and new door latches. Certified on 20 October 1965. 941 built, plus 56 shipped to Argentina as the '''A182J'''.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-R piston engine, gross weight {{convert|2800|lb|kg|0|abbr=on}} and certified on 20 October 1965.<ref name="3A13" />
;182K Skylane
:1967 model year with short-stroke [[oleo strut]] nose gear, increased vertical stabilizer tip length, and "Omni-Flash" rotating beacon. Certified on 3 August 1966. 880 built, plus 40 shipped to Argentina as the '''A182K'''.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-R piston engine, gross weight {{convert|2800|lb|kg|0|abbr=on}} and certified on 3 August 1966.<ref name="3A13" />
;182L Skylane
:1968 model year with new boom microphone, pre-select flap controls, and relocated flight instruments. Certified on 28 July 1967. 820 built, plus 20 shipped to Argentina as the '''A182L'''.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-R piston engine, gross weight {{convert|2800|lb|kg|0|abbr=on}} and certified on 28 July 1967.<ref name="3A13" />
;182M Skylane
:Four-seat1969 lightmodel aircraftyear with fixedoptional landingelectroluminescent gear,instrument poweredpanel bylighting. a carburetedA {{convert|230|hp|kW|0|abbr=on}}turn Continentalcoordinator O-470-Rwas pistonadded engine,as grossstandard weightequipment {{convert|2800|lb|kg|0|abbr=on}}for the deluxe Skylane model. and certifiedCertified on 19 September 1968. 750 built.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" /> An experimental version of this model hadwas used to test a full cantilever wing originally intended for the [[Cessna 187|Cessna 343]] (later 187).<ref name="Phillips">Phillips, Edward H: ''Wings of Cessna, Model 120 to the Citation III'', Flying Books, 1986. {{ISBN|0-911139-05-2}}</ref>
;182N Skylane
:Introduced for the 1970 model year with a more streamlines cowling, conical camber wingtips, a revised instrument panel, and gross weight increased to {{convert|2950|lb|kg|0|abbr=on}}. The 1971 model year introduced shoulder harnesses for the front seats and improved cabin soundproofing. Certified on 17 September 1969. 770 total built; 390 (1970) and 380 (1971), plus 20 built by Argentina in 1972 as the '''A182N''' with the improvements of that year's 182P.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-R or O-470-S piston engine, gross weight {{convert|2950|lb|kg|0|abbr=on}} for takeoff and {{convert|2800|lb|kg|0|abbr=on}} for landing, certified on 17 September 1969<ref name="3A13" />
;{{visible anchor|182P Skylane}}
:Introduced for the 1972 model year with cowling-mounted landing/taxi lights, tubular steel main landing gear with increased track width, "Camber-Lift" withs with a new leading edge, a push-button annunciator panel, and redesigned control wheels. The 1973 model year introduced bonded cowl and cabin doors, a shock-mounted cowling, and an extended dorsal fairing. 1974 introduced tighter door/window seals, new engine cooling baffle seals, a [[Variable-pitch propeller (aeronautics)|constant-speed propeller]], and optional {{convert|84|gal|L||abbr=on}} fuel tanks and oxygen system. 1975 introduced new wheel/break fairings and the '''Skylane II''' with improved avionics. 1976 introduced a new {{convert|230|hp|kW|0|abbr=on}} Continental O-470-S engine, as well as improved wing root fairings. Certified on 8 October 1971. 4,371 total built; 621 (1972), 1,040 (1973), 1,010 (1974), 820 (1975), and 880 (1976), plus 25 built in France by [[Reims Aviation]] in 1976 as the '''F182P'''.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" /> In 1976, Cessna stopped offering the baseline 182, and all subsequent models carried the "Skylane" name.<ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-R or O-470-S piston engine, gross weight {{convert|2950|lb|kg|0|abbr=on}} and certified on 8 October 1971.<ref name="3A13" />
;182Q Skylane
:Introduced for the 1977 model year with a new {{convert|230|hp|kW|0|abbr=on}} Continental O-470-U engine and instrument panel fasteners, as well as minor changes to the instrument panel. The 1978 model year introduced a new 28V electrical system, molded plastic control wheels, and an avionics master switch. 1979 saw the replacement of the fuel bladders with a {{convert|88|gal|L||abbr=on}} [[wet wing]] as well as the introduction of a redesigned brake master cylinder and an alternator control unit (ACU). 1980 introduced a redesigned audio panel, marker beacon, flap position control indicator, and flap system circuitry as well as an optional writing table behind the pilots' seats. Certified on 28 July 1976. 2,537 total built; 790 (1977), 624 (1978), 709 (1979), and 414 (1980), plus 39 built by Reims in 1977 as the '''F182Q'''.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-U piston engine, gross weight {{convert|2950|lb|kg|0|abbr=on}} and certified on 28 July 1976<ref name="3A13" /> Significant changes were a change to a 24-V electrical system in model year 1978 at s/n 18265966 and a change from bladder to wet-wing fuel tanks in model year 1979 at s/n 18266591.{{Citation needed|date=February 2021}}
;182R/T182R Skylane
:Introduced for the 1981 model year with an increased gross takeoff weight of {{convert|3100|lb|kg|0|abbr=on}} (landing remained at {{convert|2950|lb|kg|0|abbr=on}}), a new door latch system, and wing root vents. A new model, the '''T182R''', was also introduced with a {{convert|235|hp|kW|0|abbr=on}} [[Lycoming O-540|Lycoming O-540-L3C5D]] piston engine. The 1982 model year featured only minor changes. 1983 introduced an improved O-470-U, increased flap extension speed, a low vacuum warning light, an improved avionics cooling fan, improved rear seat ventilation, and an optional split-switch electric elevator trim system. Certified on 29 August 1980. 895 total built; 339 (1981), 237 (1982), 74 (1983), 65 (1984), 106 (1985), and 74 (1986) before all 182 production stopped.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a carbureted {{convert|230|hp|kW|0|abbr=on}} Continental O-470-U piston engine, gross weight of {{convert|3100|lb|kg|0|abbr=on}} for takeoff and {{convert|2950|lb|kg|0|abbr=on}} for landing. Certified on 29 August 1980.<ref name="3A13" /> This variant, along with the 182Q, can alternatively be equipped with the [[jet fuel]] burning [[SMA SR305-230]] Diesel engine.
;182S Skylane
:Skylane production resumed in 1997 with the 182S, with Cessna dropping the model year system used on previous models. The 182S was powered by a fuel-injected {{convert|230|hp|kW|0|abbr=on}} Lycoming IO-540-AB1A5 and introduced multiple other improvements, such as new seats, cabin soundproofing, and corrosion proofing. Wheel fairings were no longer standard, though they were still an optional feature along with [[Instrument flight rules|IFR]] GPS and a two-axis autopilot. A "Millennium edition" was introduced in 2000 with special exterior and interior appointments. Certified on 3 October 1996. 941 built.<ref name="3A13" /><ref name=":0" />
:Four-seat light aircraft with fixed landing gear, powered by a [[Fuel injection|fuel-injected]] {{convert|230|hp|kW|0|abbr=on}} [[Lycoming O-540|Lycoming IO-540-AB1A5]] piston engine, gross weight of {{convert|3100|lb|kg|0|abbr=on}} for takeoff and {{convert|2950|lb|kg|0|abbr=on}} for landing, certified on 3 October 1996<ref name="3A13" />
;182T/T182T Skylane
:Four-seatImproved light182S aircraftintroduced in 2001 with fixeda landingredesigned cowling and wheel fairings, 12V power port, a smaller gear strut step, and other improvements. The '''T182T''' is powered by a turbocharged and fuel-injected {{convert|230235|hp|kW|0|abbr=on}} [[Lycoming OTIO-540|Lycoming IO-540-AB1A5]]AK1A piston engine, grossa weight4-place ofoxygen {{convert|3100|lb|kg|0|abbr=on}}system, and other improvements for takeoffhigh altitude flight. 2004 saw the introduction of the optional "Nav III" avionics package and {{convert|2950|lb|kg|0|abbr=on}}an foroptional leather interior. 2005 introduced redesigned wingtips, new landing lights, certifiedand onoptional 23[[AmSafe]] Februaryinflatable 2001restraints (which became standard in 2009). 2007 introduced the [[Garmin G1000]] instrument system as standard, andas well as ofmultiple Julyoptional 2015,additional itavionics ispackages. the onlyCertified varianton in23 productionFebruary 2001.<ref name="3A13" /><ref name=":0" /> The 182T was the only variant in production as of July 2015.<ref name="AOPA_news">{{cite news|last1=Marsh|first1=Alton|last2=Twombly|first2=Ian|title=Cessna halts orders for diesel Cessna 182|url=http://www.aopa.org/News-and-Video/All-News/2015/May/14/Cessna-not-accepting-182-JT-A-orders|website=AOPA.org|date=14 May 2015|access-date=18 July 2015}}</ref> The T182T was produced from 2001 to 2013, with production forecast to commence again in 2023.<ref name="O'Connor10Feb22">{{cite web |last=O'Connor |first=Kate |date=10 February 2022 |title=Turbo Skylane Returns To Textron Lineup |url=https://www.avweb.com/aviation-news/turbo-skylane-returns-to-textron-lineup/ |url-status=live |archive-url=https://archive.today/20220211184139/https://www.avweb.com/aviation-news/turbo-skylane-returns-to-textron-lineup/ |archive-date=11 February 2022 |access-date=11 February 2022 |work=AVweb}}</ref>
;{{visible anchor|R182 Skylane RG}} ▼===Special versions===
:Four-seat light aircraft with retractable landing gear, powered by a {{convert|235|hp|kW|0|abbr=on}} Lycoming O-540-J3C5D piston engine, gross weight {{convert|3100|lb|kg|0|abbr=on}} and certified on 7 July 1977.<ref name="3A13" />
▲;{{visible anchor|R182 Skylane RG/TR182 Turbo Skylane RG}}
;T182
:Four-seatIntroduced lightfor aircraftthe 1978 model year with fixedretractable landing gear, powered by a turbocharged {{convert|235|hp|kW|0|abbr=on}} Lycoming O-540-L3C5D,J3C5D piston engine, and a gross weight of {{convert|3100|lb|kg|0|abbr=on}}. for takeoffThe and1979 model year increased fuel capacity from {{convert|295075|lbgal|kgL||abbr=on}} to {{convert|88|gal|L||abbr=on}}. Certified on 7 July 1977. The '''TR182 Turbo Skylane RG''' was powered by turbocharged {{convert|235|hp|kW|0|abbr=on}} forLycoming landing,O-540-L3C5D and was certified on 1512 AugustSeptember 1978. At least 2,024 total built; 583 (1978), 729 (1979), 314 (1980), 169 (1981), 129 (1982), 44 (1983), 25 (1984), and 31 (1985), with production continuing into 1986. Reims also built a total of 69; 21 (1978), 24 (1979), and 24 (1980) as the '''FR182''' in France.<ref name="Phillips" /><ref name="3A13" /><ref name=":0" />
;T182TJ182T Turbo Skylane JT-A
: Four-seat light aircraft with fixed landing gear, poweredPowered by a {{convert|227|hp|kW|0|abbr=on}} [[SMA SR305-230]] diesel engine ,. itIt burns {{convert|11|u.s.gal}} per hour of Jet-A fuel and cruises at {{convert|156|kn|km/h|0|abbr=on}}. The model was first flown in May 2013, and as of July 2015, FAA certification is on hold indefinitely.<ref name="AOPA_news" /> Originally introduced as the '''Turbo Skylane NXT ''', Cessna changed the name to avoid confusion with the [[Remos GX|Remos NXT ]].<ref name="Grady22Jul12" /><ref name="JTA">{{cite web|url = http://textron.vo.llnwd.net/o25/CES/cessna_aircraft_docs/single_engine/skylane/TurboSkylaneJT-Aonesheet5.pdf|title = Cessna 182JT-A Sheet|access-date = 9 September 2012|last = Cessna|author-link = Cessna|date = n.d.|archive-url = https://web.archive.org/web/20120907010232/http://textron.vo.llnwd.net/o25/CES/cessna_aircraft_docs/single_engine/skylane/TurboSkylaneJT-Aonesheet5.pdf|archive-date = 2012-09-07|url-status = dead}}</ref><ref name="Pew22May13">{{cite news|url =http://www.avweb.com/avwebflash/news/cessna_jta_turbo_skylane_diesel_flight_208739-1.html|title = Cessna's Jet-A Skylane Flies|access-date = 23 May 2013|last = Pew|first = Glenn|date = 22 May 2013| work = AVweb }}</ref> Only 16 aircraft (one prototype and 15 production) had been built by 2014. A majority of orders for the Turbo Skylane JT-A had been canceled by 2017, and the aircraft was eventually discontinued.<ref name=":2">{{Cite book |title=[[Janes All the World's Aircraft|Janes All the World's Aircraft: Development & Production 2022–2023]] |year=2023 |isbn=978-0-7106-3396-5 |pages=913–915}}</ref> ▼:Four-seat light aircraft with fixed landing gear, powered by a turbocharged and fuel-injected {{convert|235|hp|kW|0|abbr=on}} Lycoming TIO-540-AK1A piston engine, gross weight of {{convert|3100|lb|kg|0|abbr=on}} for takeoff and {{convert|2950|lb|kg|0|abbr=on}} for landing, certified on 23 February 2001.<ref name="3A13" /> It was produced from 2001 to 2013, with production forecast to commence again in 2023.<ref name="O'Connor10Feb22">{{cite web|url= https://www.avweb.com/aviation-news/turbo-skylane-returns-to-textron-lineup/|title= Turbo Skylane Returns To Textron Lineup|access-date= 11 February 2022|last= O'Connor|first= Kate|work= AVweb|date= 10 February 2022|archive-url= https://archive.today/20220211184139/https://www.avweb.com/aviation-news/turbo-skylane-returns-to-textron-lineup/|archive-date= 11 February 2022|url-status= live}}</ref>
;TR182 Turbo Skylane RG
:Four-seat light aircraft with retractable landing gear, powered by a turbocharged {{convert|235|hp|kW|0|abbr=on}} Lycoming O-540-L3C5D piston engine, gross weight {{convert|3100|lb|kg|0|abbr=on}} and certified on 12 September 1978.<ref name="3A13" />
;T182JT-A Turbo Skylane JT-A
▲:Four-seat light aircraft with fixed landing gear, powered by a {{convert|227|hp|kW|0|abbr=on}} [[SMA SR305-230]] diesel engine, it burns {{convert|11|u.s.gal}} per hour of Jet-A fuel and cruises at {{convert|156|kn|km/h|0|abbr=on}}. The model was first flown in May 2013, and as of July 2015, FAA certification is on hold indefinitely.<ref name="AOPA_news" /> Originally introduced as the Turbo Skylane NXT, Cessna changed the name to avoid confusion with the Remos NXT.<ref name="Grady22Jul12" /><ref name="JTA">{{cite web|url = http://textron.vo.llnwd.net/o25/CES/cessna_aircraft_docs/single_engine/skylane/TurboSkylaneJT-Aonesheet5.pdf|title = Cessna 182JT-A Sheet|access-date = 9 September 2012|last = Cessna|author-link = Cessna|date = n.d.|archive-url = https://web.archive.org/web/20120907010232/http://textron.vo.llnwd.net/o25/CES/cessna_aircraft_docs/single_engine/skylane/TurboSkylaneJT-Aonesheet5.pdf|archive-date = 2012-09-07|url-status = dead}}</ref><ref name="Pew22May13">{{cite news|url =http://www.avweb.com/avwebflash/news/cessna_jta_turbo_skylane_diesel_flight_208739-1.html|title = Cessna's Jet-A Skylane Flies|access-date = 23 May 2013|last = Pew|first = Glenn|date = 22 May 2013| work = AVweb}}</ref>
;Robertson STOL 182
:An aftermarket 182 [[STOL]] conversion certified in 1967 that changes the [[leading edge]] shape and [[aileron]] controls and lowers the stall speed below {{convert|35|mph|km/h|0|abbr=on}}.<ref>{{cite journal|journal=Plane and Pilot|date=July 1967}}</ref>
{{Cessna 140 family}}
{{Cessna}}
{{Authority control}}
<!-- Categories -->
[[Category:Cessna aircraft|182]]
[[Category:High-wing aircraft]]
| 