Editing Antonov An-8 (section)

==Specifications==
{{Aircraft specs
|ref=Airlife's World Aircraft<ref name="Simpson p.46"/>
|prime units?=met
<!--
        General characteristics
-->
|crew=6 (pilot, copilot, navigator, flight engineer, tail gunner, wireless operator)<ref name="Gunruss p23"/>
|capacity=48 persons / {{cvt|11000|kg|-3}} max payload
|length m=26
|length note=
|span m=30
|span note=
|height m=9.7
|height note=
|wing area sqm=117.2
|wing area note=<ref name="Gunruss p23">Gunston 1995, p. 23.</ref> 
|aspect ratio=11.7<ref name="Gunruss p23"/>
|airfoil=
|empty weight kg=21250
|empty weight note=<ref name="Gunruss p23"/>
|gross weight kg=
|gross weight note=
|max takeoff weight kg=40000
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=2
|eng1 name= [[Ivchenko AI-20D]]
|eng1 type=[[turboprop]] engines
|eng1 shp=5180
|eng1 note=
|prop blade number=4
|prop name=constant-speed propellers
|prop dia m=<!-- propeller aircraft -->
|prop dia note=
<!--
        Performance
-->
|max speed kmh=610
|max speed note=
|cruise speed kmh=480
|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=2780
|range note=
|combat range km=
|combat range note=
|ferry range km=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=9600
|ceiling note=<ref name="alex p31">Alexander 1975, p. 31.</ref>
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=7.12
|climb rate note=
|time to altitude=
|wing loading kg/m2=
|wing loading note=
|fuel consumption kg/km=
|power/mass=
|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= One 23 mm cannon in the tail turret.
|avionics=
}}