Editing Macchi C.202 Folgore (section)

==Specifications (C.202CB Serie IV-VIII)==
[[File:Macchi MC.202.svg|thumb|3-view drawing of Macchi MC.202]]
{{Aircraft specs
|ref=''The Macchi C.202 and The Complete Book of Fighters'' <ref name="Cattaneo p. 10.">Cattaneo 1966, p. 10.</ref><ref name="Green">{{cite book |last1=Green |first1=William |title=The Complete Book of Fighters |year=1994 |publisher=Salamander |location=London |isbn=1-85833-777-1 |last2=Swanborough |first2=Gordon |page=360}}</ref>
|prime units?=met
<!--
        General characteristics
-->
|crew=1
|length m=8.85
|span m=10.58
|height m=3.49
|wing area sqm=16.82
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' [[NACA airfoil|NACA 23018 (modified)]]; '''tip:''' [[NACA airfoil|NACA 23009 (modified)]]<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=2491
|gross weight kg=
|max takeoff weight kg=2930
|fuel capacity=
|more general=
*'''Drop tanks:''' 2 × {{Convert|100|L|usgal impgal|1|abbr=on}} drop tanks<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Alfa Romeo RA.1000 R.C.41-I Monsone]]
|eng1 type=V-12 inverted liquid-cooled piston engine
|eng1 kw=864
|eng1 note=at 2,500 rpm for takeoff

|prop blade number=3
|prop name=constant-speed propeller
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=
<!--
        Performance
-->
|max speed kmh=600
|max speed note=at {{cvt|5600|m}}
|cruise speed kmh=
|stall speed kmh=
|never exceed speed kmh=
|range km=765
|combat range km=
|ferry range km=
|endurance=<!-- if range unknown -->
|ceiling m=11500
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=18.1
|time to altitude=
|wing loading kg/m2=174.2
|fuel consumption kg/km=
|power/mass=
|thrust/weight=

|more performance=
<!--
        Armament
-->
|armament=
* 2 × {{cvt|12.7|mm|3}} [[Breda-SAFAT]] machine guns in the engine cowling, 360/400 rpg
* 2 × {{cvt|7.7|mm|3}} Breda-SAFAT machine guns in the wings, 500 rpg
* 2 × {{cvt|50|kg}}, {{cvt|100|kg}} or {{cvt|160|kg}} bombs
|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=

|avionics=
|power/mass note={{cvt|0.21| hp/lb|kW/kg|order=flip}} This is using empty weight for the calculation, gross weight should be used instead which is currently not given, so this incorrect ratio shouldn't be displayed.}}