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An-12 (Cub) Russian Transport Aircraft

An-12

Twin-Engine Utility Aircraft
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Basic Information
Name
An-12 (Cub) Russian Transport Aircraft
Designation
An-12
Alternate Designation
An-12; NATO: Cub
Equipment Type
Twin-Engine Utility Aircraft
Manufacturer
Former Soviet government factories in Rostov and Ulan-Ude, Russia
Date of Introduction
1959
Description

The Antonov An-12 (Russian: Антонов Ан-12; NATO reporting name: Cub) is a four-engined turboprop transport aircraft designed in the Soviet Union. It is the military version of the Antonov An-10 and has many variants. For more than three decades the An-12 was the standard medium-range cargo and paratroop transport aircraft of the Soviet air forces. A total of 1,234 were eventually built. Developed from the Antonov An-8, the An-12 was a military version of the An-10 passenger transport. The first prototype An-12 flew in December 1957 and entered Soviet military service in 1959. Initially, the aircraft was produced at the State Aviation Factory in Irkutsk. From 1962, production was transferred to Tashkent, where 830 were built. Later, production moved to Voronezh and Kazan. In military use, the An-12 has the capacity for up to 100 fully equipped paratroopers or 20,000 kg (44,090 lb) of cargo, which is loaded through the rear loading ramp/door. In terms of configuration, size, and capability, the aircraft is similar to the United States-built Lockheed C-130 Hercules. Soviet military and former-Soviet An-12s have a defensive tail gun turret. In the 1960s, China purchased several An-12 aircraft from the Soviet Union, along with a license to assemble the aircraft locally. Due to the Sino-Soviet split, the Soviet Union withdrew its technical assistance and the first flight of a Chinese-assembled An-12 was delayed until 1974. After USSR ceased production in 1973, the Xi'an Aircraft Company and Xi'an Aircraft Design Institute reverse-engineered the An-12 for local production. In 1981, the Chinese version of the An-12, designated Y-8, entered production. Since then, the Y-8 has become one of China's most popular military and civilian transport/cargo aircraft, with many variants produced and exported. A Tu-16/H-6 bomber navigator cockpit design was chosen for the Y-8 instead of the original An-12 shorter navigator cockpit design, as the H-6 bomber had been in serial production for some time. Although the An-12 is no longer in use either in Russia or in Ukraine, the Y-8 is upgraded and produced in China. The latest Y8-F600 is a joint venture between the Shaanxi Aircraft Company, Antonov Aeronautical Scientific-Technical Complex (ASTC), and Pratt & Whitney Canada. The Y8-F600 has a redesigned fuselage, western avionics, PW150B turboprop engines with an R-408 propeller system, and a two-crew glass cockpit.

Air & Air Defense Specifications
Crew 6
Engine turboprop w/AV-28 4-blade reversible-pitch propellers (4000 hp)
Max Speed 777.0 km/h
Cruise Speed 670.0 km/h
Wingspan 38.00 m
Variants
An-12BP Cub This is the standard transport/cargo version; several electronics blister fairings are fitted.
Cub-A The Cub-A is the electronic intelligence (ELINT) version; blade aerials are fitted on the front of fuselage, aft of the flight deck.
Cub-B The Cub-B is the naval ELINT variant. Blister fairings are under the forward and center fuselage, and other antennas are added.
Cub-C The Cub-C is the ECM version. Ventral antenna housings, jammers on pallets and other features indicate the capability of "ferreting" ELINT information; the tail-gun position is replaced with an ogival tail cone.
AN-12PPS Cub-D This variant is an upgraded Cub-C with additional ECM equipment.
Shaanxi Y-8 This is the Chinese-manufactured variant.
System
Alternate Designation An-12; NATO: Cub
Type Transport Aircraft
Manufacturer Former Soviet government factories in Rostov and Ulan-Ude, Russia
Crew 6 (including tail gunner)
Troop Capacity 90 ea
Maximum Payload Capacity 20,000 kg
Dimensions
Length 33.10 m
Height 10.53 m
Wingspan 38.00 m
Wing Area 121.70 sq m
Hatch Opening, Length 7.70 m
Hatch Opening, Width 2.95 m
Cargo Hold, Length 13.50 m
Cargo Hold, Width 3.50 m
Cargo Hold, Height 2.60 m
Cargo Hold, Volume 97 cu m
Weight, Empty 28,000 kg
Maximum Takeoff Weight 61,000 kg
Normal Takeoff Weight 55,100 kg
Automotive
Engine Name 4 x Ivchenko AI-20K
Engine Type turboprop w/AV-28 4-blade reversible-pitch propellers
Engine Power 4,000 shaft hp each
Maximum Internal Fuel Capacity 18,100 liters
Normal Internal Fuel Capacity 13,900 liters
Maximum Speed 777 km/h
Cruise Speed 670 km/h
Economical Speed 580 km/h
Landing Speed 200 km/h
Minimum Speed 163 km/h
Range with Maximum Payload 1,400 km
Ceiling 10,200 m
Climb Rate 600 m/min
Takeoff Run 700 m
Landing Run 500 m
Main Weapon System
Note 2 x 23-mm NR-23 cannon in tail turret
Fire Control /Avionics
Navigation Radar 1 x Toadstool navigation
Protection
Stealth Properties No
Heat Signature Reduction No
Add on Armor INA
NBC Protection INA
EW Counter Measures INA
Chaffs/Flares INA
Details
Country of Origin Russia
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
A
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
33.1 m
Width
Height
10.53 m
Weight
61000 kg
Operators (22)
Russia
China
France
Ukraine
Poland
Serbia
Belarus
Angola
Armenia
Cameroon
Central African Republic
Chad
Congo, Republic of the
Egypt
Equatorial Guinea
Gabon
Ghana
Guinea
Iraq
Mexico
Philippines
Thailand
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