Editing Piper PA-28 Cherokee (section)

==Variants==
=== Cherokee family ===
[[File:Piper PA-28 Cherokee Rafael Luiz (14687208168).jpg|thumb|A PA-28-140 Cherokee Cruiser with the constant-chord "Hershey Bar" wing of the Cherokee family.]]
;{{visible anchor|PA-10}}
:Unbuilt design study similar to the [[Thorp T-211|Thorp Sky Scooter]].  Was to have been powered by a {{convert|65|hp|kW|0|abbr=on}} engine.<ref name=":1">{{Cite book |last=Peperell |first=Roger W. |title=Piper Aircraft and their forerunners |last2=Smith |first2=Colin M. |publisher=Air-Britain (Historians) Limited |year=1987 |isbn=0-85130-149-5}}</ref>  Developed into the PA-28.<ref name=":0">{{Cite book |last=Simpson |first=R.W. |title=Airlife's General Aviation |publisher=Airlife Publishing |year=1995 |isbn=1853105775 |edition=2nd}}</ref>
;{{visible anchor|PA-28-140 Cherokee}}
:Two-place, fixed landing gear landplane, [[Lycoming O-320|Lycoming O-320-E2A or -E3D]] engine of {{convert|150|hp|kW|0|abbr=on}}, gross weight {{convert|1950|lb|kg|0|abbr=on}}. First certified on 14 February 1964. Approved as a {{convert|2150|lb|kg|0|abbr=on}} gross weight four place aircraft on 17 June 1965.<ref name="2A13" />  Built in the following variants:
:*'''PA-26-140 Cherokee''', initial version.<ref name=":0" />
:*'''PA-28-140-4 Cherokee''', four-seat version of the PA-28-140.  Introduced in 1965.<ref name=":0" /><ref name=":1" />
:*'''PA-28-140B Cherokee B''', as PA-28-140 with new engine mount and instrument panel as well as minor detail changes.  Introduced in 1969.<ref name=":0" /><ref name=":1" />
:*'''PA-28-140C Cherokee C''', as PA-28-140B with minor cosmetic changes.  Introduced in 1970.<ref name=":0" /><ref name=":1" />
:*'''PA-28-140D Cherokee D''', as PA-28-140C with new cabin heat system and minor changes.  Introduced in 1971.<ref name=":0" /><ref name=":1" />
:*'''PA-28-140E Cherokee E''', as PA-28-140D with minor cosmetic changes.  Introduced in 1972.<ref name=":0" /><ref name=":1" />
:*'''PA-28-140F Cherokee F''', as PA-28-140E with tail fillet, new instrument panel and front seats, and minor cosmetic changes.  Air conditioning was added as an option on this variant.  Introduced in 1973.<ref name=":0" /><ref name=":1" />
:*'''PA-28-140 Cruiser 2+2''', PA-28-140B/C/D/E/F with four-seat interior and baggage area.<ref name=":0" />  Renamed to '''Cruiser''' in 1974.
:*'''PA-28-140 Flite Liner''' (alternatively '''Fliteliner'''), two-seat trainer variant of the PA-28-140E/F with full instrumentation.<ref name=":0" />  Introduced in 1971.<ref>{{Cite book |last=Clarke |first=Bill |title=The Piper Indians |publisher=TAB Books |year=1988 |isbn=0-8306-0232-1 |edition=1st}}</ref>
;{{visible anchor|PA-28-150 Cherokee}}
:Four-place, fixed landing gear landplane, [[Lycoming O-320|Lycoming O-320-A2B or -E2A]] engine of {{convert|150|hp|kW|0|abbr=on}}, gross weight {{convert|2150|lb|kg|0|abbr=on}}. First certified on 2 June 1961.<ref name="2A13" />  Built in the following variants:
:*'''PA-28-150 Cherokee''', initial version.<ref name=":0" />
:*'''PA-28-150B Cherokee B''', as PA-28-150 with minor detail changes.  Introduced in 1963.<ref name=":0" /><ref name=":1" />
:*'''PA-28-150C Cherokee C''', as PA-28-150B with minor detail changes.  Introduced in 1965.<ref name=":0" /><ref name=":1" />
;{{visible anchor|PA-28-160 Cherokee}}
:Four-place, fixed landing gear landplane, [[Lycoming O-320|Lycoming O-320-B2B or -D2A]] engine of {{convert|160|hp|kW|0|abbr=on}}, gross weight {{convert|2200|lb|kg|0|abbr=on}}. First certified on 31 October 1960.<ref name="2A13" />  Built in the following variants:
:*'''PA-28-160 Cherokee''', initial version.<ref name=":0" />
:*'''PA-28-160B Cherokee B''', as PA-28-160 with minor detail changes.  Introduced in 1963.<ref name=":0" /><ref name=":1" />
:*'''PA-28-160C Cherokee C''', as PA-28-160B with minor detail changes.  Introduced in 1965.<ref name=":0" /><ref name=":1" />
;{{visible anchor|PA-28S-160 Cherokee}}
:Four-place, fixed landing gear seaplane, [[Lycoming O-320|Lycoming O-320-D2A]] engine of {{convert|160|hp|kW|0|abbr=on}}, gross weight {{convert|2140|lb|kg|0|abbr=on}}. First certified on 25 February 1963.<ref name="2A13" />  Built in the following variants:
:*'''PA-28S-160B Cherokee B''', PA-28-160B with [[Edo Aircraft Corporation|EDO 2000]] floats.<ref name=":1" />
:*'''PA-28S-160C Cherokee C''', PA-28-160C with EDO 2000 floats.<ref name=":1" />
;{{visible anchor|PA-28-180 Cherokee}}
:Four-place, fixed landing gear landplane, [[Lycoming O-360|Lycoming O-360-A3A or -A4A]] engine of {{convert|180|hp|kW|0|abbr=on}}, gross weight {{convert|2400|lb|kg|0|abbr=on}}. First certified on 3 August 1962.<ref name="2A13" />  Built in the following variants:
:*'''PA-28-180B Cherokee B''', initial version based on the PA-28-160B.  Introduced in 1963.<ref name=":0" /><ref name=":1" />
:*'''PA-28-180C Cherokee C''', as PA-28-180B with streamlined engine cowling, new spinner, and minor detail changes.  Introduced in 1965.<ref name=":0" /><ref name=":1" />
:*'''PA-28-180D Cherokee D''', as PA-28-180C with a third window on each side and a new instrument panel, engine control console, and control column.  Introduced in 1968.<ref name=":0" /><ref name=":1" />
:*'''PA-28-180E Cherokee E''', as PA-28-180D with an improved engine mount and new instrument lighting.  Introduced in 1970.<ref name=":0" /><ref name=":1" />
:*'''PA-28-180F Cherokee F''', as PA-28-180E with rear bench seat replaced by separate seats, new fuel selector system, and minor detail changes.  Air conditioning was added as an option on this variant.  Introduced in 1971.<ref name=":0" /><ref name=":1" />
:*'''PA-28-180G Cherokee G''', as PA-28-180F with improved instrument panel.  Introduced in 1972.<ref name=":1" />
;{{visible anchor|PA-28S-180 Cherokee}}
:Four-place, fixed landing gear seaplane, [[Lycoming O-360|Lycoming O-360-A3A or -A4A]] engine of {{convert|180|hp|kW|0|abbr=on}}, gross weight {{convert|2222|lb|kg|0|abbr=on}}. First certified on 10 May 1963.<ref name="2A13" />  Built in the following variants:
:*'''PA-28S-180B Cherokee B''', PA-28-180B with EDO 2000 floats.<ref name=":1" />
:*'''PA-28S-180C Cherokee C''', PA-28-180C with EDO 2000 floats.<ref name=":1" />
;{{visible anchor|PA-28-235 Cherokee 235}}
:Four-place, fixed landing gear landplane, [[Lycoming O-540|Lycoming O-540-B1B5, -B2B5, or -B4B5]] engine of {{convert|235|hp|kW|0|abbr=on}}, gross weight {{convert|2900|lb|kg|0|abbr=on}}. First certified on 15 July 1963 and introduced in 1964.<ref name="2A13" /><ref name="Cherokee235">{{Cite web |date=2009-09-22 |title=Piper Cherokee 235 |url=https://www.aopa.org/go-fly/aircraft-and-ownership/aircraft-fact-sheets/piper-cherokee-235 |access-date=2023-11-18 |website=www.aopa.org |language=en}}</ref>  Built in the following variants:
:*'''PA-28-235 Cherokee 235''', initial version.<ref name=":0" />
:*'''PA-28-235B Cherokee B''', as PA-28-235 with minor detail changes.  Introduced in 1966.<ref name=":0" /><ref name=":1" />
:*'''PA-28-235C Cherokee C''', as PA-28-235B with a third window on each side and a new engine control console.  Introduced in 1968.<ref name=":0" /><ref name=":1" />
:*'''PA-28-235D Cherokee D''', as PA-28-235C with minor cosmetic changes.  Introduced in 1970.<ref name=":0" /><ref name=":1" />
:*'''PA-28-235E Cherokee E''', as PA-28-235D with rear bench seat replaced by separate seats and improved soundproofing.  Air conditioning was added as an option on this variant.  Introduced in 1971.<ref name=":0" /><ref name=":1" />
:*'''PA-28-235F Cherokee F''', as PA-28-235E with tail fillet, a new instrument panel, and minor changes.  Introduced in 1972.<ref name=":0" /><ref name=":1" />
:*'''PA-28-235 Cherokee Charger''', four-place, fixed landing gear landplane, [[Lycoming O-540|Lycoming O-540-B4B5]] engine of {{convert|235|hp|kW|0|abbr=on}}, gross weight {{convert|3000|lb|kg|0|abbr=on}}. First certified on 9 June 1972 and introduced in 1973. Changes from the 1963 certified PA-28-235 Cherokee 235 include a five inch fuselage extension, wing span increase, larger horizontal tail, gross weight increase and other minor changes.<ref name="2A13" /><ref name="Cherokee235" />
:*'''PA-28-235 Cherokee Pathfinder''', four-place, fixed landing gear landplane, as Cherokee Charger but with noise reduction changes including redesigned windows.  Introduced in 1974.<ref name="Cherokee235" />
;{{visible anchor|EMB-710C Carioca}}
:PA-28-235 built by [[Indústria Aeronáutica Neiva|Neiva]] (a subsidiary of [[Embraer]]) in Brazil from kits supplied by Piper.<ref name=":1" />
;{{visible anchor|EMB-712 Tupi}}
:PA-28-180 built by Neiva in Brazil from kits supplied by Piper.<ref name=":0" />  Also known as the '''Carioquinha'''.<ref name=":1" /><ref>{{Cite web |date=June 5, 2023 |title=Comercialização pela H8 ALS de certas partes fabricadas sem a devida autorização. |trans-title=Commercialization by H8 ALS of certain manufactured parts without proper authorization. |url=https://www.gov.br/anac/pt-br/assuntos/regulados/aeronaves/arquivos/APS202206REV0.docx |access-date=July 23, 2024 |website=[[National Civil Aviation Agency of Brazil]] |language=pt, en |format=PDF}}</ref><ref name="ICAO DOC 8643 - Aircraft Type Designators">{{cite web |date= |title=DOC 8643 - Aircraft Type Designators: Part 1 — Aircraft Types by Manufacturer |url=https://cfapps.icao.int/doc8643/reports/Part1-By%20Manufacturer%20(Encode).pdf |accessdate=July 23, 2024 |website=ICAO Publications |publisher=International Civil Aviation Organization |authorlink1=ICAO}}</ref>

=== Warrior family ===
[[File:Piper PA-28 Cherokee - nice piper on a nice day (540786133).jpg|thumb|Warrior family aircraft, such as this PA-28-161 Warrior II, feature a tapered wing.]]
;{{visible anchor|PA-28-151 Cherokee Warrior}}
:Four-place, fixed landing gear landplane, [[Lycoming O-320|Lycoming O-320-E3D]] engine of {{convert|150|hp|kW|0|abbr=on}}, gross weight {{convert|2325|lb|kg|0|abbr=on}}. First certified on 9 August 1973. Changes from the PA-28-150 include a tapered wing.<ref name="2A13" /><ref>{{Cite web |date=2009-09-23 |title=Piper Warrior |url=https://www.aopa.org/go-fly/aircraft-and-ownership/aircraft-fact-sheets/piper-warrior |access-date=2023-11-18 |website=www.aopa.org |language=en}}</ref>
;{{visible anchor|PA-28-161 Warrior II}}
:Four-place, fixed landing gear landplane, [[Lycoming O-320|Lycoming O-320-D2A or -D3G]] engine of {{convert|160|hp|kW|0|abbr=on}}, gross weight {{convert|2325|lb|kg|0|abbr=on}}. First certified on 2 November 1976. Changes from the PA-28-160 include a tapered wing. Certified on 1 July 1982 for gross weight of {{convert|2440|lb|kg|0|abbr=on}}.<ref name="2A13" />
;{{visible anchor|PA-28-161 Warrior III}}
:Four-place, fixed landing gear landplane, [[Lycoming O-320|Lycoming O-320-D3G]] engine of {{convert|160|hp|kW|0|abbr=on}}, gross weight {{convert|2440|lb|kg|0|abbr=on}}. First certified on 1 July 1994.<ref name="2A13" />
;{{visible anchor|PA-28-161 Cadet}}
:Two-place, fixed landing gear landplane, [[Lycoming O-320|Lycoming O-320-D2A or -D3G]] engine of {{convert|160|hp|kW|0|abbr=on}}, gross weight {{convert|2325|lb|kg|0|abbr=on}}. Replaced the [[Piper PA-38 Tomahawk|PA-38 Tomahawk]] trainer in the late 1980s. Features the older Cherokee "2 side window" fuselage with the later tapered wing.<ref>{{cite web|url=http://www.planeandpilotmag.com/article/piper-cherokee-cruiser-cadet-warrior/|title=Piper "Cherokee"/"Cruiser"/"Cadet"/"Warrior"|publisher=Plane&Pilot Magazine|date=30 November 1999|access-date=15 February 2017}}</ref><ref>{{cite web|url=http://wayman.net/files/PiperCadet-PA28161.pdf|title=Piper Cadet Information Manual|publisher=Piper Aircraft Corporation|date=9 September 1988|access-date=15 February 2017}}</ref>
[[File:polly in flight riat2008 arp.jpg|thumb|[[Polly Vacher]], a record-breaking UK pilot, in her PA-28-236 Dakota]]
;{{visible anchor|PA-28-201T Turbo Dakota}}
:Four-place, fixed landing gear landplane, turbocharged [[Continental IO-360|Continental TSIO-360-FB]], engine of {{convert|200|hp|kW|0|abbr=on}}, gross weight {{convert|2900|lb|kg|0|abbr=on}}. First certified on 14 December 1978.<ref name="2A13" /><ref name="Dakota">{{Cite web |author=Staff Report |date=2001-03-06 |title=Piper PA-28 Cherokee 235/Dakota |url=https://www.aviationconsumer.com/aircraftreviews/piper-pa-28-cherokee-235-dakota/ |access-date=2023-11-18 |website=Aviation Consumer |language=en-US}}</ref>
;{{visible anchor|PA-28-236 Dakota}}
:Four-place, fixed landing gear landplane, [[Lycoming O-540|Lycoming O-540-J3A5D]] engine of {{convert|235|hp|kW|0|abbr=on}}, gross weight {{convert|3000|lb|kg|0|abbr=on}}. First certified on 1 June 1978. Changes from the 1972 certified PA-28-235 Cherokee Pathfinder include tapered wing.<ref name="2A13" /><ref name="Dakota" />
;{{visible anchor|EMB-710D Carioca}}
:PA-28-236 built by Neiva in Brazil from kits supplied by Piper.<ref name=":1" />

=== Archer family ===
;{{visible anchor|PA-28-180 Challenger}}
:Four-place, fixed landing gear landplane, [[Lycoming O-360|Lycoming O-360-A4A or -A4M]] engine of {{convert|180|hp|kW|0|abbr=on}}, gross weight {{convert|2450|lb|kg|0|abbr=on}}. First certified on 22 May 1972. Changes from the PA-28-180 Cherokee include a five inch fuselage extension, wing span increase, larger horizontal tail, gross weight increase and other minor changes.<ref name="2A13" /><ref name="Archer1">{{Cite web |date=2020-10-09 |title=Piper Archer |url=https://www.aopa.org/go-fly/aircraft-and-ownership/aircraft-guide/aircraft/piper-archer |access-date=2023-11-18 |website=www.aopa.org |language=en}}</ref>  Renamed to '''Archer''' after minor detail changes.<ref name=":0" />
;{{visible anchor|PA-28-181 Archer II}}
:Four-place, fixed landing gear landplane, [[Lycoming O-360|Lycoming O-360-A4A or -A4M]] engine of {{convert|180|hp|kW|0|abbr=on}}, gross weight {{convert|2550|lb|kg|0|abbr=on}}. First certified on 8 July 1975. Changes from the PA-28-180 Archer include a tapered wing.<ref name="2A13" /><ref name="Archer1" />
;{{visible anchor|PA-28-181 Archer III}}
:Four-place, fixed landing gear landplane, [[Lycoming O-360|Lycoming O-360-A4M]] engine of {{convert|180|hp|kW|0|abbr=on}}, gross weight {{convert|2550|lb|kg|0|abbr=on}}. First certified on 30 August 1994.<ref name="2A13" /><ref>{{Cite web |date=1998-05-11 |title=The New Piper's Archer III |url=https://www.aopa.org/news-and-media/all-news/1998/november/pilot/the-new-pipers-archer-iii |access-date=2023-11-18 |website=www.aopa.org |language=en}}</ref>
[[File:Piper PA-28-181 Archer LX (N563DF, cn 2881563) (10-20-2022).jpg|thumb|PA-28-181 Archer LX at 2022 [[National Business Aviation Association#NBAA conventions|NBAA-BACE]]]]
;{{visible anchor|PA-28-181 Archer TX and LX}}
:Four-place, fixed landing gear landplane, [[Lycoming O-360|Lycoming O-360-B4A]] engine of {{convert|180|hp|kW|0|abbr=on}}, maximum takeoff weight {{convert|2550|lb|kg|0|abbr=on}}.  Produced in Archer TX trainer and Archer LX personal aircraft variants, both with [[Garmin G1000|Garmin G1000 NXi]] avionics.<ref>{{Cite web |title=2023 Archer LX brochure |url=https://www.piper.com/wp-content/uploads/2023/01/2023_Archer-LX-Single-Sheet.pdf |access-date=November 18, 2023 |website=[[Piper Aircraft]]}}</ref><ref>{{Cite web |title=2023 Archer TX brochure |url=https://www.piper.com/wp-content/uploads/2023/01/2023_Archer-TX-Single-Spec-Sheet_no-pricing.pdf |access-date=November 18, 2023 |website=[[Piper Aircraft]]}}</ref>
[[File:Piper Archer DX PA-28 Indonesian Navy.jpg|thumb|PA-28-181 Archer DX of the [[Indonesian Navy]]]]
;{{visible anchor|PA-28-181 Archer DX and DLX}}
:Four-place, fixed landing gear landplane, turbocharged [[Thielert Centurion 2.0|Continental CD-155]] diesel engine of {{convert|155|hp|kW|0|abbr=on}}. Introduced at [[AERO Friedrichshafen]] in April 2014.<ref>{{cite web|last=Bertorelli |first=Paul |url=http://www.avweb.com/blogs/insider/Pipers-Archer-DX-Diesel-221915-1.html |title=Piper's Archer DX Diesel |publisher=Avweb |date=24 April 2014 |access-date=28 April 2014}}</ref><ref>{{cite web|url=http://www.avweb.com/avwebflash/news/Pipers-Diesel-Archer-Receives-FAA-Validation-223930-1.html|title=Piper's Diesel Archer Receives FAA Validation|access-date=21 April 2015|date=2015-04-21}}</ref> The [[compression-ignition engine]] is simpler to operate, avoiding starting difficulties, [[carburetor icing]] or propeller and [[mixture control]]s, and the [[liquid cooling]] does not suffer [[shock cooling]] in a rapid descent.<!--<ref name=AIN21nov2018>--> The [[turbocharger]] maintains full power up to over {{cvt|10,000|feet}} to climbs at {{cvt|700 to 500|ft/min|m/s}} at {{cvt|86|knots|km/h}}, and cruise fuel flow is {{cvt|4.2 to 6.3|USgal}}/h at 50 to 75% power and a {{cvt|100 to 117|kn|km/h}} [[Indicated airspeed|IAS]].<!--<ref name=AIN21nov2018>--> The engine must be replaced every 2,100 hours.<ref name=AIN21nov2018>{{cite news |url= https://www.ainonline.com/aviation-news/general-aviation/2018-11-21/pilot-report-piper-diesel-archer |title= Pilot Report: Piper Diesel Archer |author= Matt Thurber |date= November 21, 2018 |work= AIN online}}</ref> Produced in Archer DX trainer and Archer DLX personal aircraft variants.<ref name=":2">{{Cite web |title=2023 Archer DX brochure |url=https://www.piper.com/wp-content/uploads/2023/01/2023_Archer-DX-Single-Spec-Sheet_no-pricing.pdf |access-date=November 18, 2023 |website=[[Piper Aircraft]]}}</ref><ref name=":3">{{Cite web |title=2023 Archer DLX brochure |url=https://www.piper.com/wp-content/uploads/2023/01/2023_Archer-DLX-Single-Spec-Sheet.pdf |access-date=November 18, 2023 |website=[[Piper Aircraft]]}}</ref>
;{{visible anchor|PA-28-181 Pilot 100 and Pilot 100i}}
:New versions introduced in 2019 intended as low cost VFR and IFR trainers respectively, for the [[flight training]] market.<ref name=Pilot100>{{cite web|url = https://www.avweb.com/air-shows-events/piper-introduces-pilot-100-100i-trainer/|title = Piper Introduces Pilot 100/100i Trainer|access-date = 4 April 2019|last = O'Connor |first = Kate|work = AVweb|date = 2 April 2019}}</ref> Fixed landing gear, 180 hp [[Lycoming IO-360|Lycoming IO-360-B4A]], Garmin G3X Touch Certified avionics. IFR version includes GFC500 autopilot.<ref>{{cite magazine|url=https://www.flyingmag.com/piper-introduces-pilot-100-100i-trainers|title= Piper Introduces Pilot 100 and Pilot 100i Trainers|magazine=Flying Magazine|first=Rob|last=Mark|date=April 2, 2019|access-date=2019-04-04}}</ref> Features the 2-side-window fuselage with the later tapered wing, no baggage door, no air conditioning, no instruments on right-hand panel, all-white paint with decals, two-place seating standard on 100, rear third seat with push-to-talk and [[Bluetooth]] functions standard on 100i and optional on 100.<ref>{{cite journal | title = Piper Pilot 100: Smooth moves | journal = [[AOPA Pilot]] | date = December 1, 2019 | first = Jill W. | last = Tallman | url = https://www.aopa.org/news-and-media/all-news/2019/december/pilot/piper-pilot-100-smooth-moves | access-date = November 19, 2019}}</ref> These new versions were [[type certified]] in the US in December 2020 and in Europe in August 2021.<ref name="Cook15Dec20">{{cite web|url= https://www.avweb.com/aviation-news/piper-pilot-100-certified/|title= Piper Pilot 100 Certified|access-date= 16 December 2020|last= Cook|first= Marc|work= AVweb|date= 15 December 2020|archive-url= https://web.archive.org/web/20201216131030/https://www.avweb.com/aviation-news/piper-pilot-100-certified/|archive-date= 16 December 2020|url-status= live}}</ref><ref name="OConnor27Aug21">{{cite web|url= https://www.avweb.com/flight-safety/flight-training/piper-pilot-100i-earns-easa-approval/|title= Piper Pilot 100i Earns EASA Approval|access-date= 30 August 2021|last= O'Connor|first= Kate|work= AVweb|date= 27 August 2021|archive-url= https://archive.today/20220507183333/https://www.avweb.com/flight-safety/flight-training/piper-pilot-100i-earns-easa-approval/|archive-date= 7 May 2022|url-status= live}}</ref>

=== Arrow family ===
[[File:Piper PA-28R-200 Cherokee Arrow 3-view line drawing.png|thumb|A 3-view drawing of a Piper PA-28R-200 Cherokee Arrow]]

;{{visible anchor|PA-28R-180 Cherokee Arrow}}
:Four-place, retractable landing gear landplane, [[Lycoming O-360|Lycoming IO-360-B1E]] engine of {{convert|180|hp|kW|0|abbr=on}}, gross weight {{convert|2500|lb|kg|0|abbr=on}}. First certified on 8 June 1967.<ref name="2A13" />  Built in the following variants:
:*'''PA-28R-180 Cherokee Arrow''', initial version.<ref name=":1" />
:*'''PA-28R-180B Cherokee Arrow B''', as PA-28R-180 with minor changes.  Introduced in 1970.<ref name=":1" />
;{{visible anchor|PA-28R-200 Cherokee Arrow}}
:Four-place, retractable landing gear landplane, [[Lycoming O-360|Lycoming IO-360-C1C]] engine of {{convert|200|hp|kW|0|abbr=on}}, gross weight {{convert|2600|lb|kg|0|abbr=on}}. First certified on 16 January 1969.<ref name="2A13" />  Built in the following variants:
:*'''PA-28R-200 Cherokee Arrow''', initial version.<ref name=":0" />
:*'''PA-28R-200B Cherokee Arrow B''', as PA-28R-200 with improved fuel system and ventilation.  Autopilot added as an option on this variant.  Introduced in 1970.<ref name=":0" /><ref name=":1" />
;{{visible anchor|PA-28R-200 Cherokee Arrow II}}
:Four-place, retractable landing gear landplane, [[Lycoming O-360|Lycoming IO-360-C1C or -C1C6]] engine of {{convert|200|hp|kW|0|abbr=on}}, gross weight {{convert|2650|lb|kg|0|abbr=on}}. First certified on 2 December 1971. Changes from the 1969 certified PA-28R-200 Arrow include a five inch fuselage extension, wing span increase, larger horizontal tail, gross weight increase and other minor changes.<ref name="2A13" />
;{{visible anchor|PA-28R-201 Arrow III}}
:Four-place, retractable landing gear landplane, [[Lycoming O-360|Lycoming IO-360-C1C6]] engine of {{convert|200|hp|kW|0|abbr=on}}, gross weight {{convert|2750|lb|kg|0|abbr=on}}. First certified on 2 November 1976.<ref name="2A13" />
;{{visible anchor|PA-28R-201T Turbo Arrow III}}
:Four-place, retractable landing gear landplane, turbocharged [[Continental IO-360|Continental TSIO-360-F or -FB]] engine of {{convert|200|hp|kW|0|abbr=on}}, gross weight {{convert|2900|lb|kg|0|abbr=on}}. First certified on 2 November 1976.<ref name="2A13" />
[[File:PA 28 ARROW (cropped).jpg|thumb|A PA-28RT-201 Arrow IV over [[A Coruña Airport]]]]
;{{visible anchor|PA-28RT-201 Arrow IV}}
:Four-place, retractable landing gear landplane, [[Lycoming O-360|Lycoming IO-360-C1C6]] engine of {{convert|200|hp|kW|0|abbr=on}}, gross weight {{convert|2750|lb|kg|0|abbr=on}}. First certified on 13 November 1978. Features a [[T tail]].<ref name="2A13" />
;{{visible anchor|PA-28RT-201T Turbo Arrow IV}}
:Four-place, retractable landing gear landplane, turbocharged [[Continental IO-360|Continental TSIO-360-FB]] engine of {{convert|200|hp|kW|0|abbr=on}}, gross weight {{convert|2900|lb|kg|0|abbr=on}}. First certified on 13 November 1978. Features a T tail.<ref name="2A13" />
;{{visible anchor|PA-A-28R-260T Cherokee Arrow III}}<!-- PA-A-28 is not a typo -->
:Prototype armed military variant developed by [[Chincul]] in Argentina with a side-by-side two-seat cockpit and a sliding canopy.  Powered by a {{convert|260|hp|kW|0|abbr=on}} [[Lycoming O-540|Lycoming AEIO-540]] engine and armed with a 7.62 mm gun.  Intended for service in the [[Armed Forces of the Argentine Republic|Argentine armed forces]] but not accepted.<ref name=":1" />
[[File:YBT Enaer T-35 Pillan (8185362751).jpg|thumb|The second PA-28R-300 Pillán, designated YBT, at [[Museo Nacional Aeronáutico y del Espacio]].]]
;{{visible anchor|PA-28R-300 Pillán}}
:Two Piper-built prototypes of the [[ENAER T-35 Pillán]].  Military trainer with a cut-down [[Piper PA-32R|PA-32R Saratoga]] fuselage with a two-seat tandem cockpit and a PA-28R Arrow wing.  Powered by a {{convert|300|hp|kW|0|abbr=on}} [[Lycoming O-540|Lycoming IO-540-K]] engine.  First flown on 6 March 1981, and production aircraft were sent in kit form to be built by [[ENAER]].<ref name=":0" />  The first and second prototypes were designated '''XBT''' and '''YBT''', respectively.<ref name=":1" />
;{{visible anchor|EMB-711B Corisco}}
:PA-28R-201 Arrow III built by Neiva in Brazil from kits supplied by Piper.<ref name=":1" />
;{{visible anchor|EMB-711C Corisco}}
:PA-28R-200 Arrow II built by Neiva in Brazil from kits supplied by Piper.<ref name=":1" />
;{{visible anchor|EMB-711S Corisco II}}
:PA-28RT-201 Arrow IV built by Neiva in Brazil from kits supplied by Piper.<ref name=":1" />
;{{visible anchor|EMB-711ST Corisco II}}
:PA-28RT-201T Turbo Arrow IV built by Neiva in Brazil from kits supplied by Piper.<ref name=":1" />  Also known as the '''Corisco Turbo'''.<ref name=":0" />