Editing Polikarpov I-15 (section)

==Specifications (I-15 M-25)==
[[File:Polikarpov I-15.svg|thumb|Polikarpov I-15 drawing]]
{{Aircraft specs
|ref=Of Chaika and Chato…<ref name="Chaika p12">Green and Swanborough 1979, p. 12.</ref>
|prime units?=met
<!--General characteristics-->
|crew=One
|length m=6.10
|length note=(tail up)
|upper span m=9.75
|lower span m=7.50
|height m=2.20
|height note=(tail down)
|wing area sqm=21.90
|aspect ratio=<!-- sailplanes -->
|airfoil=[[Clark YH ]]<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=1012
|gross weight kg=1385
|max takeoff weight kg=1689
|fuel capacity={{cvt|260|L|impgal USgal}}
<!--Powerplant-->
|eng1 number=1
|eng1 name=[[Shvetsov M-25]]
|eng1 type=9-cylinder air-cooled radial piston engine
|eng1 kw=<!-- prop engines -->
|eng1 hp=700<!-- prop engines -->
|eng1 note=at {{cvt|2300|m|}}

|prop blade number=2
|prop name=variable-pitch propeller
|prop dia m=<!-- propeller aircraft -->
<!--
        Performance
-->
|max speed kmh=367
|max speed note=at {{convert|3000|m|ft|abbr=on}}
|cruise speed kmh=285
|cruise speed note=at {{convert|2000|m|ft|abbr=on}} (max. continuous cruise)
|stall speed kmh=
|stall speed note=
|never exceed speed kmh=
|range km=510
|endurance=<!-- if range unknown -->
|ceiling m=9800
|climb rate ms=
|climb rate note=
|time to altitude=<br/>
**1.1 min to {{convert|1000|m|ft|-2|abbr=on}}
**6.1 min to {{convert|5000|m|ft|-2|abbr=on}}
<!--Armament-->
|armament=
* 4 x[[7.62×54mmR]] [[PV-1 machine gun]]s 
* Up to 100 kg (220 lb) of bombs 
}}