Editing Antonov An-12 (section)

==Specifications (An-12)==
[[File:Antonov An-12 Cub two-view silhouette.png|thumb|Antonov An-12]]
{{Aircraft specs
|ref=Global Aircraft,<ref name=global>{{cite web | title=An-12 Cub | work=Global Aircraft | url=http://www.globalaircraft.org/planes/an-12_cub.pl | access-date=9 March 2006 | archive-url= https://web.archive.org/web/20060219100727/http://www.globalaircraft.org/planes/an-12_cub.pl| archive-date= 19 February 2006 | url-status= live}}</ref> Airliners.net<ref name=airliners.net>{{cite web | title=The Antonov An-12 & Shaanxi Y8 | work=Airliners.net | url=http://www.airliners.net/info/stats.main?id=35 | access-date=9 March 2006 | archive-url= https://web.archive.org/web/20060219080507/http://www.airliners.net/info/stats.main?id=35| archive-date= 19 February 2006 | url-status= live}}</ref>
|prime units?=met
<!--
        General characteristics
-->
|crew=5 (two pilots, flight engineer, navigator, radio operator)
|capacity={{cvt|20000|kg|lb}} payload / 60 paratroopers / 2x [[BMD-1]] armoured vehicles
|length m=33.1
|length note=
|span m=38
|span note=
|height m=10.53
|height note=
|wing area sqm=121.7
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=<!--'''root:''' [[NACA airfoil|NACA ]]; '''tip:''' [[NACA airfoil|NACA ]]<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 |access-date=16 April 2019}}</ref>-->
|empty weight kg=28000
|empty weight note=
|gross weight kg=
|gross weight note=
|max takeoff weight kg=61000
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=4
|eng1 name=[[Ivchenko AI-20L]] or AI-20M
|eng1 type=[[turboprop]] engines
|eng1 shp=4000
|eng1 note=equivalent

|prop blade number=4
|prop name=constant-speed reversible-pitch propellers
|prop dia m=<!-- propeller aircraft -->
|prop dia note=
<!--
        Performance
-->
|max speed kmh=660
|max speed note=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=570
|cruise speed note=
|stall speed kmh=
|stall speed note=
|never exceed speed kmh=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed note=
|range km=5700
|range note=with maximum fuel
:::: {{cvt|3600|km|mi nmi}} with maximum payload
|combat range km=
|combat range note=
|ferry range km=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=10200
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=10.2
|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||m|0}}
*'''Take-off run to {{cvt|15|m|0}}:''' {{cvt||m|0}}
*'''Landing run:''' {{cvt||m|0}}
*'''Landing run from {{cvt|15|m|0}}:''' {{cvt||m|0}}-->
<!--
        Armament
-->
|guns=2× 23 mm (0.906 in) [[Nudelman-Rikhter NR-23]] [[autocannon|cannons]] in a tail turret (some aircraft)

|avionics=
}}