Editing Douglas DC-3 (section)

==Specifications (DC-3A-S1C3G)==
[[File:Douglas DC-3 3-view line drawing.svg|frameless|right|300px|3-view line drawing of the Douglas DC-3]]
[[File:N34---Douglas-DC3-Cockpit.jpg|thumb|DC-3 cockpit]]
{{multiple image|align = right |direction = vertical |width = 220 |image1 =Douglas DC-3C cold start.jpg |image2 =DC-3 spinning props.JPG |caption2 =A 1944 Douglas DC-3C starting its engines and taxiing with its tail wheel unlocked}}

{{Aircraft specs
|ref=''McDonnell Douglas Aircraft since 1920''<ref name="Franc"/><!-- for giving the reference for the data -->
|prime units?=kts
|crew=two
|capacity=21–32 passengers
|length m=19.7
|length ft=64
|length in=5
|length note=
|span m=29.0
|airfoil=NACA2215 / NACA2206
|span ft=95
|span in=
|span note=
|height m=5.16
|height ft=16
|height in=9
|height note=(level attitude) 23 ft 6 in
|wing area sqm=
|wing area sqft=987
|wing area note=
|aspect ratio=9.17
|empty weight kg=
|empty weight lb=16,865
|empty weight note=
|gross weight kg=
|gross weight lb=25,200
|gross weight note=payload w/full fuel, 3,446 lb
|fuel capacity={{convert|822|USgal|L|1|abbr=on}}
|eng1 number=2
|eng1 name=[[Pratt & Whitney R-1830-S1C3G Twin Wasp]]
|eng1 type=14-cyl. air-cooled two row radial piston engine
|eng1 kw=
|eng1 hp=1,200
|eng1 note=
|power original=
|prop blade number=3
|prop name=[[Hamilton Standard 23E50]] series
|prop dia m=3.5
|prop dia ft=11
|prop dia in=6
|prop dia note=hydraulically controlled constant speed, feathering
|max speed kmh=
|max speed mph=
|max speed kts=223
|max speed note=at 8,500 ft (2,590 m)
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=183
|cruise speed note=
|stall speed kmh=125.9
|stall speed mph=78.2
|stall speed kts=68.0
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=223
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=77
|minimum control speed note= with one engine inoperative
|range nmi= 1,370
|range note=(maximum fuel, 3500 lb payload)
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=, cruise speed/range at 10,000 ft ASL, cruise fuel consumption of 94 gph at 50% power, 157kt IAS, 1,740 nm
|endurance=<!-- if range unknown -->
|ceiling m=
|ceiling ft=23,200
|ceiling note=, with one engine operative, 9,000 ft
|climb rate ms=
|climb rate ftmin=1,140
|climb rate note=, rate of climb at sea level with one engine operative, 200 fpm
|time to altitude=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=25.5
|wing loading note=
|power/mass=0.0952 hp/lb (156.5 W/kg)
|thrust/weight=
}}<ref>Accessed 6 October 2023, https://www.aopa.org/news-and-media/all-news/1994/june/pilot/flying-the-dc-3 </ref>