Editing Abrams P-1 Explorer (section)

==Specifications==
[[File:Abrams_Explorer_3-view_L'Aerophile_March_1938.jpg|thumb|Abrams Explorer 3-view drawing from L'Aerophile March 1938]]
{{Aircraft specs
|ref=Jane's all the World's Aircraft 1938<ref name=JAWA1938>{{cite book |title=Jane's all the World's Aircraft 1938 |editor1-last=Grey |editor1-first=C.G. |year=1938 |publisher=Sampson Low, Marston & company, ltd |location=London |editor2-last=Bridgman|editor2-first=Leonard |page=242c}}</ref>
|prime units?=imp
<!--
        General characteristics
-->
|crew=2
|capacity=
|length ft=26
|length in=6
|length note=
|span ft=36
|span in=8
|span note=
|height ft=6
|height in=4
|height note=
|wing area sqft=200
|wing area note=
|aspect ratio= 6.58
|airfoil='''root:''' [[NACA airfoil|NACA 23018]]; '''tip:''' [[NACA airfoil|NACA 23009]]<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 |accessdate=16 April 2019}}</ref>
|empty weight lb=2100
|empty weight note=
|gross weight lb=3400
|gross weight note=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Wright R-975E-1 Whirlwind]]
|eng1 type=9-cylinder air-cooled radial piston engine
|eng1 hp=365

|prop blade number=2
|prop name=[[Hamilton-Standard]] variable-pitch pusher propeller
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=
<!--
        Performance
-->
|max speed mph=200
|max speed note=at {{cvt|10000|ft}}
|cruise speed mph=175
|cruise speed note=at {{cvt|10000|ft}}<br/>
*'''Landing speed:''' {{cvt|60|mph|kn km/h}} with flaps extended
|stall speed mph=
|stall speed note=
|never exceed speed mph=
|never exceed speed note=
|range miles=1200
|range note=
|combat range miles=
|combat range note=
|ferry range miles=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=20000
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ftmin=1400
|climb rate note=
|time to altitude=
|wing loading lb/sqft=17
|wing loading note=
|fuel consumption lb/mi=
|power/mass={{cvt|9.3|lb/hp}}
|more performance=
}}