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General Info

Antonov
AN-24 Coke

Role Strategic airlifter
National origin Soviet Union
Manufacturer Antonov
First flight 29 October 1959
Introduction 1962
Status Active service Primary users UTair Cargo Angara Airlines IrAero Yakutia Airlines Air Koryo
Produced 1959–1979
Number built 1,367 (including the Chinese Y-7)
Variants Antonov An-26 Antonov An-30 Antonov An-32Developed into Xian Y-7

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History Antonov Company Antonov Design Bureau
Antonov An-24 "Coke"

The Antonov An-24 (Russian/Ukrainian: Антонов Ан-24) (NATO reporting name: Coke) is a 44-seat twin turboprop transport/passenger aircraft designed in 1957 in the Soviet Union by the Antonov Design Bureau[1] and manufactured by Kyiv, Irkutsk and Ulan-Ude Aviation Factories.

First flown in 1959, the An-24 was produced in some 1,000 units of various versions; in 2023 there are 93 still in service worldwide, mostly in the CIS and Africa. It was designed to replace the veteran piston Ilyushin Il-14 transport on short to medium haul trips, optimised for operating from rough strips and unprepared airports in remote locations. The high-wing layout protects engines and blades from debris, the power-to-weight ratio is higher than that of many comparable aircraft and the machine is rugged, requiring minimal ground support equipment..

Design and development

An-24RV of PLAAF at China Aviation Museum, Beijing
SAT Airlines' Antonov An-24RV

Operators

Military operators

Antonov An 24PB of Bangladesh Air Force,displayed at Bangladesh Air Force muserm
North Korea
Korean People's Army Air Force - 1 (converted to a rudimentary airborne early warning aircraft)
Russia
Syria
Syrian Air Force – 1
Ukraine
 

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Aircraft Speed

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Gallery

Photo Gallery
Antonov Company Antonov Design Bureau
Antonov An-24 "Coke"

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Antonov Company Antonov Design Bureau

Antonov Company Antonov Design Bureau
Antonov An-24 "Coke"

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General Info

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      • Crew: 3
      • Capacity: 50 passengers
      • Length: 23.53 m (77 ft 2 in)
      • Wingspan: 29.20 m (95 ft 10 in)
      • Height: 8.32 m (27 ft 4 in)
      • Wing area: 74.98 m2 (807.1 sq ft)
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Powerplant


      • Empty weight: 13,300 kg (29,321 lb)
      • Max takeoff weight: 21,000 kg (46,297 lb)
      • Fuel capacity: 5,550 L (1,470 US gal; 1,220 imp gal)
      • Powerplant: 2 × Ivchenko AI-24A turboprop engines, 1,900 kW (2,550 shp) each (eshp)
      • Propellers: 4-bladed AV-72 constant-speed propellers, 3.90 m (12 ft 10 in) diameter
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Performance

  • Cruise speed: 450 km/h (280 mph, 240 kn) at 6,000 m (20,000 ft)
  • Range: 2,400 km (1,500 mi, 1,300 nmi) with maximum fuel; 550 km (340 mi; 300 nmi) with maximum payload
  • Service ceiling: 8,400 m (27,600 ft)
  • Rate of climb: 1.91 m/s (375 ft/min)
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Related development

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Special Links Antonov Company Antonov Design Bureau

Links to Youtube & Others

Due to its rugged airframe and good performance, the An-24 was adapted to perform many secondary missions such as ice reconnaissance and engine/propeller test-bed,.

Antonov Bureau
An-24 "Coke"

Production continues at China's Xi'an Aircraft Industrial Corporation which makes licensed,

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Youtube Link

The main production line was at the Kyiv-Svyatoshino (later renamed "Aviant") aircraft production plant which built 985

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Antonov Design Bureau 

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