The appearance of a biplane in 1947 was widely misread; instead of being an obsolete anachronism it lead to a record post war production exceeding 18,500 built (upto 1995) The first task assigned to the re-formed Antonov OKB was to design an aircraft to replace the the aging Po-2, the requirement was issued by the Ministry of Agricultural and Forestry in May 1946. In the Soviet environment it never occurred to Antonov that others might think a biplane passé; it was the smallest and lightest solution to the task, which as a result grew to a machine that was much larger and alot more capable than the Po-2.
Two prototypes were built designated SKh-1's (Rural Economy 1's) first having the ASh-21 and then the ASh-621R engines fitted. In each case the propeller had 4 scimitar shaped blades of 3.6 m diameter. 6 fabric tanks in the upper wing housed 1200 litres of fuel (91 octane). The engine was fitted with a 27V generator and an air compressor for charging a tank used for pressurizing the landing gear, locking the tail wheel and brakes. Normal equipment includes: blind flying equipment,gyrocompass, radio compass,2 radios, radioaltimeter and intercom. The side by side cockpit can have dual controls and it's side windows oversail the fuselage to give a good view rearwards and downwards. The centre and left windscreens are deiced electrically whilst the right windscreen uses engine heated air - which also heats the cabin - there is no airframe ice protection.
Variants
An-2TStandard Utility aircraft for the Military (10 equipped troops) and Aeroflot (1948) An-2TPFor scheduled Aeroflot routes - fitted with comfortable seating for 12 passengers (1949) An-2P14 lightweight seats and a soundproof cabin. An-2SFlying Ambulance with 6 stretchers. An-2TDParachute training and operational missions - 12 + equipment. An-2SKhAgricultural version with 1400 litre tank and spray bars or centre line duct. An-2LFire fighter. An-2VUtility aircraft fitted with dural floats. An-2PPFire fighter fitted with dural floats (1961). An-2ZAAtmospheric sampling - compartment for a scientist faired into the fin. An-2FGlazed rear fuselage, twin finned tail carrying UBT or NS-23 cannon - few built (1955) An-2NRKNight Artillery Correction An-2KAs above. An-2MUpdated An-2T with 290 engineering changes (1960) Y-5License built Chinese An-2. (1957) Y-5BUpgraded Y-5 with corrosion resistant airframe and specialist role equipment. (1992)
From 1959 production of the An-2 was moved to PZL-Mielec in Poland, where 12,000+ were produced (10,427 for USSR). Polish designations often differ from the Russian ones. In the late 1950's about 100 An-2's, often with rectangular cabin windows, were produced at the DDR factory in Dresden. In 1957, China began producing the An-2 under license at Nanchang as the Y-5, 727 delivered by 1968. Production was then moved to Shijiazhuang where over 288 were built by early 1992. Mid 1992 the Chinese produced the Y-5B with corrosion resistant airframe and specialist role equipment of which 150+ were delivered by mid 1993.
Role Light-transport (10 equipped troops), general utility Wing Span 59 ft, 8 in (18.19 m)Length 41 ft, 9 in (12.75 m) Height 4.1 m Weight 3330 kg - empty
5500 kg - maximum takeoff
1500 kg - maximum payloadEngine 1xASh-62 IR, 985 hp Maximum speed 250 km/h Range 1025 km - with maximum fuel
300 km - with maximum loadService Ceiling 5000 m Runway 650 m - dirt takeoff-landing strip
400 m - surfaced takeoff-landingArmament Usually none Crew Two