Antonov An-2

1st Flight 1947

Military Users-

Afghan Air Force, Albanian Air Force, People’s Air and Air Defense Force of Angola, Armenian Air Force, Azerbaijan Air Force, Belarusian Air Force, Bulgarian Air Force, Royal Cambodian Air Force, People’s Liberation Army Navy Air Force, Croatian Air Force, Cuban Air Force, Czechoslovakian Air Force, Egyptian Air Force, Estonian Air Force, Georgian Air Force, Luftwaffe, Military of Guinea-Bissau, Hungarian Air Force, Iraqi Air Force, Kyrgyzstan, Khmer Air Force, Royal Lao Air Force, Lao People’s Liberation Army Air Force, Transnistrian Air force, Latvian Air Force, Latvian National Guard, Lithuanian Air Force, Macedonian Air Force, Air Force of Mali, Moldovan Air Force, Mongolian People’s Air Force, Nicaraguan Air Force, Escuadrón de Transporte, North Yemen Air Force, North Korea, Polish Air Force, Polish Navy, Republic of Korea Air Force, Romanian Air Force, Russian Air Force, Russian Naval Aviation, Russian Airborne Troops, Serbian Air Force, Soviet Air Force, Soviet Naval Aviation, Sudanese Air Force, Syrian Air Force, Tajikistan, Tanzania, Tunisia, Turkmenistan, Ukrainian Air Force, Ukrainian Naval Aviation, Uzbekistan, Vietnam People’s Air Force, Yemen Air Force, Yugoslav Air Force.

Antonov An-2

The Antonov An-2 was designed to meet a 1947 Soviet Ministry of Forestry requirement for a replacement for the much lighter, largely wooden air framed Polikarpov Po-2, which was used in large numbers in both agricultural and utility roles.

Antonov designed a large single bay biplane of all-metal construction, with an enclosed cockpit and a cabin with seats for twelve passengers.

Antonov An-2

The first prototype, designated SKh-1 and powered by a Shvetsov ASh-21 radial engine, flew on 31 August 1947.

The second prototype was fitted with a more powerful Shvetsov ASh-62 engine, which allowed the aircraft’s payload to be significantly increased from 1,300 to 2,140 kg, and in this form it was ordered into production.

Antonov An-2

Initial Soviet production was at State Factory 473 in Kiev, Ukrainian SSR, where the bulk of up to 5,000 units had been produced by 1960.

Later Soviet production was at State Factory 464 at Dolgoprudniy, Russian SFSR.

Antonov An-2

After 1960, however, most An-2s were constructed at Poland’s WSK factory in Mielec, it is believed that over 13,000 aircraft were built in Poland before principal manufacturing activity ended during 1991.However, up until 2001, limited production was undertaken using remaining stocks of components, spares and maintenance coverage, such as a small batch of four aircraft that were produced for Vietnam.

China also builds the An-2 under licence as the Shijiazhuang Y-5.

Antonov An-2

It has been occasionally and erroneously reported that there was East German production of the An-2, however, while An-2s often underwent extensive refurbishment in East German facilities, no new aircraft were constructed there.

The An-2 is commonly used as a light utility transport, parachute drop aircraft, agricultural work and other tasks suited to a large slow biplane. Its slow flight and good short field performance make it suited for short, unimproved fields, and some specialized variants have also been built for cold weather and other extreme environments.

Antonov An-2

The Guinness Book of World Records states that the 45-year production run for the An-2 was for a time the longest ever for any aircraft and challenged the well over two decades-long run of the much lighter, late-1920s origin Polikarpov Po-2 biplane it was intended to replace.

But the An-2’s production duration run record was exceeded by the four-turboprop, 1954-origin, Lockheed C-130 Hercules military transport.

Antonov An-2

Specifications-

Crew: 1–2

Capacity: 12 passengers / 2,140 kg (4,718 lb)

Length: 12.4 m (40 ft 8 in)

Upper wingspan: 18.2 m (59 ft 9 in)

Lower wingspan: 14.2 m (46 ft 7 in)

Height: 4.1 m (13 ft 5 in)

Wing area: 71.52 m2 (769.8 sq ft)

Airfoil: TsAGI R-11 (14%)

Empty weight: 3,300 kg (7,275 lb)

Gross weight: 5,440 kg (11,993 lb)

Fuel capacity: 1,200 l (320 US gal; 260 imp gal)

Antonov An-2

Power plant: 1 × Shvetsov ASh-62IR 9-cylinder air-cooled supercharge radial piston engine, 750 kW (1,010 hp)

Propellers: 4-bladed constant-speed propeller

Performance

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

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

Stall speed: 50 km/h (31 mph, 27 kn) circa

Range: 845 km (525 mi, 456 nmi)

Service ceiling: 4,500 m (14,800 ft)

Rate of climb: 3.5 m/s (690 ft/min)

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

Fuel consumption: 185–200 l/h (49–53 gal/h; 41–44 imp gal/h)

Antonov An-2

Credits-

https://www.antonov.com/

Wikipedia.

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