Editing Globe GC-1 Swift (section)

==Specifications (GC-1B)==
[[File:Globe GC-1A Swift 3-view silhouette drawing.png|frameless|right|3-view silhouette drawing of the Globe GC-1A Swift]]

{{Aircraft specs
|ref=Jane's All the World's Aircraft 1948<ref name="jawa48p323">Bridgman 1948, p. 323c</ref>  
|prime units?=kts<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--
        General characteristics
-->
|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=20
|length in=10
|length note=
|span m=
|span ft=29
|span in=4
|span note=
|height m=
|height ft=6
|height in=2
|height note=
|wing area sqm=
|wing area sqft=131.63
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=Root NACA 23015, Tip NACA 23009
|empty weight kg=
|empty weight lb=1125
|empty weight note=
|gross weight kg=
|gross weight lb=1710
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|26|USgal|impgal L|abbr=on}}
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Continental C125]]
|eng1 type=six cylinder, four-stroke aircraft engine
|eng1 kw=<!-- prop engines -->
|eng1 hp=125<!-- prop engines -->
|eng1 shp=<!-- prop engines -->
|eng1 kn=<!-- jet/rocket engines -->
|eng1 lbf=<!-- jet/rocket engines -->
|eng1 note=
|power original=
|prop blade number=<!-- propeller aircraft -->
|prop name=
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop note=

<!--
        Performance
-->
|perfhide=
|max speed kmh=
|max speed mph=150
|max speed kts=
|max speed note=at sea level
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=
|cruise speed mph=140
|cruise speed kts=
|cruise speed note=
|stall speed kmh=<!-- aerobatic -->
|stall speed mph=43<!-- aerobatic -->
|stall speed kts=
|stall speed note=(with flaps)
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=161
|never exceed speed note=<ref name="airweb.faa.gov">[https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/2a2d9d3dc18e0372862583080047620d/$FILE/A-766_Rev_19.pdf "Type Certificate Data Sheet No. A-766."] ''airweb.faa.gov''. Retrieved: April 8, 2021.</ref>
|range km=
|range miles=420
|range nmi=
|range note=
|endurance=<!-- if range unknown -->
|ceiling m=
|ceiling ft=16000
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ms=
|climb rate ftmin=1000
|climb rate note=
|time to altitude=
|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}