Editing Grumman C-1 Trader (section)

==Specifications (C-1A)==
[[File:C-1A CVA-43 1967.jpg|thumb|C-1A on board [[USS Coral Sea (CV-43)|USS ''Coral Sea'']], with its wings folded.]]
{{Aircraft specs
|ref=''Grumman aircraft since 1929.''<ref name=Francilon>{{cite book |last1=Francillon |first1=René Jacquet |title=Grumman aircraft since 1929 |date=1989 |publisher=Putnam |location=London |isbn=0851778356 |pages=387–393 |edition=1st}}</ref>
|prime units?=imp
<!--
        General characteristics
-->
|crew=3
|capacity=9 pax / {{cvt|8500|lb|0}} payload
|length ft=42
|length in=
|length note=
|span ft=69
|span in=8
|span note=
|height ft=16
|height in=3.5
|height sigfig=3
|height note=
|wing area sqft=485
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' [[NACA airfoil|NACA 63A420]]; '''tip:''' [[NACA airfoil|NACA 63A415]]<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=16631
|empty weight note=
|gross weight lb=23031
|gross weight note=
|max takeoff weight lb=24600
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=2
|eng1 name=[[Wright R-1820-82WA Cyclone]]
|eng1 type=9-cylinder air-cooled radial piston engines
|eng1 hp=1525
|eng1 note=

|prop blade number=3
|prop name=constant-speed fully-feathering reversible-pitch propellers
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=
<!--
        Performance
-->
|max speed mph=280
|max speed note=at {{cvt|4000|ft}}
|max speed mach=<!-- supersonic aircraft -->
|cruise speed mph=167
|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=1110
|range note=
|ferry range miles=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=24800
|ceiling note=
|climb rate ftmin=1950
|climb rate sigfig=1
|climb rate note=
|time to altitude=
|wing loading lb/sqft=47.5
|wing loading note=
|fuel consumption lb/mi=
|power/mass={{cvt|0.13|hp/lb}}

|more performance=

|avionics=
}}