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Antonov An-38
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{{short description|Regional airliner by Antonov}} <!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> {{Infobox aircraft |name=An-38 |image=Vostok Antonov An-38 Galkin.jpg |caption=Antonov An-38-100 of [[Vostok Aviation Company]] |type=[[Turboprop]] [[regional airliner]] |manufacturer=[[Novosibirsk Aircraft Production Association]] |designer=[[Antonov]] |first_flight=23 June 1994 |introduction=[[2000 in aviation|2000]] |retired= |status= In limited service |primary_user=[[ALROSA (airline)|ALROSA]] |more_users= |produced= |number_built=11 (2 operational) |unit cost= |developed_from = [[Antonov An-28]] |variants= }} The '''Antonov An-38''' is a stretched and upgraded version of Antonov's earlier [[Antonov An-28|An-28]]. It is a twin-engined [[turboprop]] transport aircraft, designed by the [[Antonov Design Bureau]] in [[Kyiv]], [[Ukraine]]. Production is in [[Novosibirsk]], [[Russia]], but some crucial parts are also made in Ukraine and [[Belarus]]. It first flew in [[1994 in aviation|1994]], and received international flight certification in April [[2000 in aviation|2000]]. A total of 11 were built and 2 remain in airline service as of August 2019.<ref name="FI">[[Flight International]], 3β9 October 2006</ref> A recent documentary says that only one remains in service with [[ALROSA_(airline)|ALROSA Airlines]] in 2021.<ref name=":0">Archived at [https://ghostarchive.org/varchive/youtube/20211206/ARPj3zzw1oI Ghostarchive]{{cbignore}} and the [https://web.archive.org/web/20210123130802/https://www.youtube.com/watch?v=ARPj3zzw1oI Wayback Machine]{{cbignore}}: {{cite web| url = https://www.youtube.com/watch?v=ARPj3zzw1oI| title = Flying on Exotic Antonovs - World's Only An-22, An-38 and An-140 | website=[[YouTube]]| date = 23 January 2021 }}{{cbignore}}</ref>{{Unreliable source?|date=January 2024|reason=Per [[WP:RSP]], YouTube is not a reliable source|certain=yes}} ==Development== Impetus for a stretch of the [[Antonov An-28]] design began with a [[1989 in aviation|1989]] sales tour in India, where it became clear that a significant market existed for an aircraft similar to the An-28, but with seating in the 25β30 seat range. The design was approved a year later, and was displayed at the [[1991 in aviation|1991]] [[Paris Air Show]] as a model. [[File:An-38-100-1999a.jpg|thumb|left|Antonov An-38-100 at [[MAKS airshow|MAKS 1999]].]] The An-38 is of a similar design to the older An-28, featuring the same wings and tail; but it has a longer fuselage and includes several enhancements, such as higher fuel efficiency, increased comfort (cabin and cockpit), and decreased internal noise, coupled with better sound insulation. Other improvements include an increase in passengers to 27, thanks to an increase in maximum payload to 2,500 kg (5,500 lbs), as well as a maximum speed of 405 km/h (250 mph). Its design also enables it to operate in adverse conditions—it is equipped with weather radar, sophisticated navigational systems, and low pressure tires that allow it to operate from primitive, unpaved and icy airfields. Furthermore, the aircraft is more resistant to [[Stall (flight)|stalling]] at high angles of attack and is stable and maneuverable with ice on the wing and tail assembly. ==Civil operators== As of August 2019, 2 Antonov An-38 aircraft remain in airline service with [[ALROSA (airline)|ALROSA]].<ref>{{Cite web|url=https://russianplanes.net/planelist/Antonov/An-38|title=β russianplanes.net β Π½Π°ΡΠ° Π°Π²ΠΈΠ°ΡΠΈΡ|website=russianplanes.net|access-date=2019-08-21}}</ref> Recent reviews suggest only one remains in service in 2021.<ref name=":0" />{{Unreliable source?|date=January 2024|reason=Per [[WP:RSP]], YouTube is not a reliable source|certain=yes}} '''Former operators''' '''{{RUS}}''' * [[Vostok Aviation Company]] ==Specifications (An-38-100)== {{Aircraft specs |ref=Jane's All The World's Aircraft 2003β2004,<ref name="JAWA 03 p467-8">Jackson 2003, pp. 467β468.</ref> Jane's All The World's Aircraft 2000β2001<ref name="JAWA2000-2001">{{cite book |title=Jane's all the World's Aircraft 2000β01 |editor1-last=Jackson |editor1-first=Paul|year=2000 |publisher=Jane's Information Group |location=Coulsdon, Surrey, United Kingdom |isbn=978-0710620118 |edition=91st |pages=513β514}}</ref> |prime units?=met <!-- General characteristics --> |crew=2 |capacity=26-27 passengers / {{cvt|2500|kg|0}} max payload |length m=15.67 |length note= |span m=22.06 |span note= |height m=4.6 |height note= |wing area sqm= |wing area note= |aspect ratio=<!-- sailplanes --> |airfoil=[[TsAGI]] R-II-14 (14%)<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |accessdate=16 April 2019}}</ref> |empty weight kg=5300 |empty weight note= |gross weight kg= |gross weight note= |max takeoff weight kg=8800 |max takeoff weight note= |fuel capacity={{cvt|2210|kg|0}} |more general= <!-- Powerplant --> |eng1 number=2 |eng1 name=[[Honeywell TPE331-14GR-801E]] |eng1 type=[[turboprop]] engines |eng1 kw=1118 |eng1 note=<br/> ::::(or 2x {{cvt|1029|kW|shp}} [[Omsk MKB Mars TVD-20]] turboprop engines driving [[AV-36]] propellers) |prop blade number=5 |prop name=[[Hartzell Propeller]] HC-B5MA |prop dia m=2.85 |prop dia note=constant-speed fully-feathering reversible-pitch propellers <!-- Performance --> |max speed kmh=405 |max speed note= |cruise speed kmh=380 |cruise speed note=at {{cvt|4200|m}} |stall speed kmh= |stall speed note= |never exceed speed kmh= |never exceed speed note= |minimum control speed kmh= |minimum control speed note= |range km=1650 |range note=with 9 passengers + 45 minutes reserve ::::{{cvt|1450|km|mi nmi}} with 17 passengers + 45 minutes reserve ::::{{cvt|600|km|mi nmi}} with 27 passengers + 45 minutes reserve |ferry range km= |ferry range note= |endurance=<!-- if range unknown --> |ceiling m= |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |climb rate ms= |climb rate note= |time to altitude= |wing loading kg/m2= |wing loading note= |fuel consumption kg/km= |power/mass= |thrust/weight= |more performance=<br/> *'''Take-off run:''' {{cvt|350|m}} *'''Landing run:''' {{cvt|270|m}} *'''Balanced field length:''' {{cvt|900|m}} |avionics= }} ==See also== {{Portal|Aviation}} {{Aircontent |related= * [[Antonov An-28]] |similar aircraft= |sequence= |lists= * [[List of airliners]] |see also= }} ==References== {{reflist}} == Further reading == {{commons category|Antonov An-38}} * {{cite web|url=http://www.antonov.com/aircraft/passenger-aircraft/an-38|title=AN-38|work=Antonov.com|publisher=Antonov ASTC|accessdate=2006-07-02|year=2004|archiveurl=https://timetravel.mementoweb.org/memento/2011/http://www.antonov.com/aircraft/passenger-aircraft/an-38|archivedate=23 January 2018|url-status=bot: unknown}} *{{cite book |last=Jackson |first=Paul |title=Jane's All The World's Aircraft 2003β2004 |year=2003 |publisher= Jane's Information Group|location=Coulsdon, UK |isbn=978-0-7106-2537-3 }} {{Antonov aircraft}} [[Category:Antonov aircraft|An-038]] [[Category:1990s Ukrainian airliners|Antonov An-038]] [[Category:Aircraft first flown in 1994]] [[Category:Twin-turboprop tractor aircraft]] [[Category:Twin-tail aircraft]] [[Category:Aircraft with fixed tricycle landing gear]] [[Category:High-wing aircraft]]
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