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Antonov An-3
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== Specifications (An-3T) == [[File:An-3 prototype and An-3V silhouettes.png|thumb|Antonov An-3 side elevation drawings]] [[File:Марка России 2006г №1063-Ан-3Т.jpg|thumb|Antonov An-3T]] {{Aircraft specs | ref=Antonov An-2<ref name="An-2">{{cite book|last=Gordon|first=Yefim|title=Antonov An-2|publisher=Midland publishing|location=Hinkley|date=2004|series=Red Star|volume=15|isbn=1-85780-162-8}}</ref> | prime units?=met<!-- 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=two | capacity=Useful load {{cvt|1800|kg|lb}} | length m=14 | length note= | span m=18.176 | span note= | height m=4.235 | height note= | wing area sqm=71.51 | wing area note= | aspect ratio=<!-- give where relevant eg sailplanes --> | airfoil= | empty weight kg= | empty weight note= | gross weight kg= | gross weight note= | max takeoff weight kg=5,800 | max takeoff weight note= | fuel capacity= | lift kg=<!-- lighter-than-air --> | lift lb=<!-- lighter-than-air --> | lift note= | more general= <!-- Powerplant --> | eng1 number=1 | eng1 name=[[Glushenkov TVD-20-03]] | eng1 type=Turboprop | eng1 kw=<!-- prop engines -->1,010 | eng1 hp=<!-- prop engines --> | eng1 kn=<!-- jet/rocket engines --> | eng1 lbf=<!-- jet/rocket engines --> | eng1 note= | power original= | thrust original= | eng1 kn-ab=<!-- afterburners --> | eng1 lbf-ab=<!-- afterburners --> | eng2 number=<!-- for different engine types --> | eng2 name= | eng2 type= | eng2 kw=<!-- prop engines --> | eng2 hp=<!-- prop engines --> | eng2 kn=<!-- jet/rocket engines --> | eng2 lbf=<!-- jet/rocket engines --> | eng2 note= | eng2 kn-ab=<!-- afterburners --> | eng2 lbf-ab=<!-- afterburners --> | eng3 number=<!-- for different engine types --> | eng3 name= | eng3 type= | eng3 kw=<!-- prop engines --> | eng3 hp=<!-- prop engines --> | eng3 kn=<!-- jet/rocket engines --> | eng3 lbf=<!-- jet/rocket engines --> | eng3 note= | eng3 kn-ab=<!-- afterburners --> | eng3 lbf-ab=<!-- afterburners --> | more power= | prop blade number=<!-- propeller aircraft --> | prop name= | prop dia m=<!-- propeller aircraft --> | prop dia ft=<!-- propeller aircraft --> | prop dia in=<!-- propeller aircraft --> | prop note= | rot number=<!-- helicopters --> | rot dia m=<!-- helicopters --> | rot dia ft=<!-- helicopters --> | rot dia in=<!-- helicopters --> | rot area sqm=<!-- helicopters --> | rot area sqft=<!-- helicopters --> | rot area note= <!-- Performance --> | perfhide= | max speed kmh=260 | max speed mph= | max speed kts= | max speed note= | max speed mach=<!-- supersonic aircraft --> | cruise speed kmh=220 | cruise speed mph= | cruise speed kts= | cruise speed note=at {{cvt|2000|m|ft}} | stall speed kmh=<!-- aerobatic --> | stall speed mph=<!-- aerobatic --> | stall speed kts= | stall speed note= | never exceed speed kmh= | never exceed speed mph= | never exceed speed kts= | never exceed speed note= | minimum control speed kmh= | minimum control speed mph= | minimum control speed kts= | minimum control speed note= | range km=550 | range miles= | range nmi= | range note=with a {{cvt|1500|kg|lb}} payload | combat range km= | combat range miles= | combat range nmi= | combat range note= | ferry range km= | ferry range miles= | ferry range nmi= | ferry range note= | endurance=<!-- if range unknown --> | ceiling m=4,400 | ceiling ft= | ceiling note= | g limits=<!-- aerobatic --> | roll rate=<!-- aerobatic --> | glide ratio=<!-- sailplanes --> | climb rate ms=5 | climb rate ftmin= | climb rate note= | time to altitude= | sink rate ms=<!-- sailplanes --> | sink rate ftmin=<!-- sailplanes --> | sink rate note= | lift to drag= | wing loading kg/m2=81 | wing loading lb/sqft= | wing loading note= | disk loading kg/m2= | disk loading lb/sqft= | disk loading note= | power/mass=0.174 kW/kg | thrust/weight= | more performance= <!-- Armament --> | guns= | bombs= | avionics= }}
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