ANTONOV AN-2 Civil Aircraft Model Details

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General Information of ANTONOV AN-2

Designer : Oleg Antonov

First Flight : 31 August 1947[2]

Manufacturer : Antonov; Hongdu Aviation Industry Group; WSK PZL-Mielec; Shijiazhuang[1]

Number Built : 18,000+[1]

Primary Users : Soviet Union; North Korea; China; Many others

Produced : 1947–2001

Role : Agricultural and utility aircraft

Status : Series production may still continue in China as the Shijiazhuang Y-5;[3]engine refitting project underway[4]

Variants : Antonov An-3

General characteristics of ANTONOV AN-2

Capacity : 12 passengers

Crew : 1–2

Empty Weight : 3,300 kg (7,300 lb)

Height : 4.1 m (13 ft)

Length : 12.4 m (40 ft 8 in)

Loaded_Weight : 5,440 kg (12,000 lb)

Powerplant : 1 × Shvetsov ASh-62IR 9-cylinder supercharged radial engine, 750 kW (1,000 hp)

Useful Load : 2,140 kg (4,700 lb)

Wing Area : 71.52 m² (769.8 ft²)

Wingspan : ** Upper wing : 18.2 m (59 ft 8 in)

Performance of ANTONOV AN-2

Cruise Speed : 190 km/h (100 kn, 120 mph)

Maximum Speed : 258 km/h (139 kn, 160 mph)

Power/Mass : 0.136 kW/kg (0.083 hp/lb)

Range : 845 km (456 nmi, 525 mi)

Rate Of Climb : 3.5 m/s (700 ft/min)

Service Ceiling : 4,500 m (14,750 ft)

Stall Speed : 50 km/h (26 knots, 30 mph)

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