Editing Convair XC-99 (section)

==Specifications (XC-99)==
[[File:Convair XC-99 3-view line drawing.png|thumb|3-view line drawing of the Convair XC-99]]
{{Aircraft specs
|ref=''General Dynamics Aircraft and their Predecessors''<ref name="Wegg p98">Wegg 1990, p. 98.</ref>
|prime units?=imp
<!--
        General characteristics
-->
|crew=5 (with a relief crew of 5)
|capacity= up to 400 troops / {{cvt|100000|lb}} cargo
|length ft=182
|length in=6
|length note=
|span ft=230
|span in=0
|span note=
|height ft=57
|height in=6
|height note=
|wing area sqft=4772
|wing area note=
|swept area sqft=<!-- swing-wings -->
|swept area note=
|volume ft3=<!-- lighter-than-air -->
|volume note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' [[NACA airfoil|NACA 63(420)-422]]; '''tip:''' [[NACA airfoil|NACA 63(420)-517]]<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 lb=135232
|empty weight note=
|gross weight lb=265000
|gross weight note=
|max takeoff weight lb=320000
|max takeoff weight note=
|fuel capacity={{cvt|19112|USgal|impgal l}}
|more general=
<!--
        Powerplant
-->
|eng1 number=6
|eng1 name=[[Pratt & Whitney R-4360-41 Wasp Major]]
|eng1 type=28-cylinder air-cooled radial piston engine
|eng1 hp=3500

|prop blade number=3
|prop name=Curtiss-Electric constant-speed fully-feathering pusher propellers
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=
<!--
        Performance
-->
|max speed mph=307
|max speed note=
|cruise speed mph=
|cruise speed note=
|stall speed mph=
|stall speed note=
|never exceed speed mph=
|never exceed speed note=
|minimum control speed mph=
|minimum control speed note=
|range miles=8100
|range note= with {{cvt|19112|USgal|impgal l}} and {{cvt|10000|lb}} payload
|combat range miles=
|combat range note=
|ferry range miles=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ftmin=
|climb rate note=
|time to altitude=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption lb/mi=
|power/mass=

|more performance=
|avionics=* Weather radar
}}