Editing Antonov An-10 (section)

==Specifications (An-10A)==
[[File:Antonov An-10 Cat two-view silhouette.png|thumb]]
{{Aircraft specs
|ref=Soviet Transport Aircraft since 1945,<ref name="Stroud">{{cite book |last1=Stroud |first1=John |title=Soviet transport aircraft since 1945 |date=1968 |publisher=Putnam |location=London |isbn=0-370-00126-5 |page=63}}</ref> Jane's all the World's Aircraft 1970–71<ref name="JAWA70-71">{{cite book |title=Jane's all the World's Aircraft 1970–71 |year=1970 |publisher=Sampson Low, Marston & Company |location=London |isbn=978-0-354-00067-3 |editor1-last=Taylor |editor1-first=John W.R. |page=480}}</ref>
|prime units?=met
<!--
        General characteristics
-->
|crew=4 flight crew +cabin crew
|capacity=100 or 130 pax / {{cvt|14500|kg}}
|length m=34
|span m=38
|upper span m=
|mid span m=
|lower span m=
|width m=
|height m=9.83
|volume m3=222
|volume note=cabin volume
*'''Underfloor hold volume:''' {{cvt|32|m3}}

|wing area sqm=120
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=
|gross weight kg=
|max takeoff weight kg=55100
|fuel capacity={{cvt|13000|L|USgal impgal}} ({{cvt|10250|kg}})
|more general=
<!--
        Powerplant
-->
|eng1 number=4
|eng1 name=[[Ivchenko AI-20K]]
|eng1 type=[[turboprop]] engines
|eng1 hp=4000
|eng1 note= (equivalent)

|prop blade number=4
|prop name=AV-68 reversible-pitch constant-speed propellers
|prop dia m=4.5
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=
<!--
        Performance
-->
|max speed kmh=715
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=680
|cruise speed note=maximum at {{cvt|10000|m}}
*'''Economical cruise speed:''' {{cvt|630|km/h|mph kn}} at {{cvt|10000|m}}
*'''Take-off speed:''' {{cvt|190|-|210|km/h|mph kn}}
|stall speed kmh=
|never exceed speed kmh=
|minimum control speed kmh=
|range km=1200
|range note=with max payload + 60 minutes reserve fuel<br />
::::{{cvt|4075|km}} with max fuel {{cvt|8440|kg}} payload and no reserves
|combat range km=
|ferry range km=
|endurance=<!-- if range unknown -->
|ceiling m=10200
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=
|time to altitude=
|wing loading kg/m2=430
|fuel consumption kg/km=
|power/mass={{cvt|7.2|lb/hp|kg/kW|order=flip}}
|thrust/weight=
|more performance=
*'''Landing run:''' {{cvt|500|-|650|m}} with reverse pitch
}}