Wikipedia:

Antonov An-32



An-32 "Cline"
32-photo-4_©_ANTONOV_ASTC_2004.jpg
Antonov An-32P © ANTONOV ASTC
Type Transport
Manufacturer Antonov
Maiden flight July 9 1976[1]
Status Operational
Primary users Indian Air Force
Ukrainian Air Force
Others
Number built 357
Unit cost US$ 6-9 mil (2000)[1]
Developed from Antonov An-26

The Antonov An-32 (NATO reporting name: "Cline") is a twin-engined turboprop military transport aircraft.

General characteristics

The An-32 is basically a re-engined An-26. The An-32 is brought in to withstand adverse weather conditions better than the standard An-26. The high placement of the engine nacelles above the wing allowed for larger diameter airscrews, which are driven by 5100 hp rated AI-20 turboprop engines, almost twice as powerful as the An-26's AI-24 powerplants. The An-32 therefore enjoys excellent take-off characteristics under tropical and mountainous (high-altitude) conditions, where hot or thin air hampers the powerplants' tractive effort. The price for a newly built An-32 was quoted as being 6-9 million dollars in 2000. [1]

  • First flight: 1976
  • Production total: 357
  • Propulsion: 2 turboprop engines
  • Max passengers: 55

Operators

An-32 operators (countries with only airline operators are in green)
Enlarge
An-32 operators (countries with only airline operators are in green)

Military operators

The An-32 is still operated by some air forces. At present more than 240 of the An-32 aircraft are being operated in the countries around the world. Most of these nations have adverse weather conditions which stands as indication to the durability of the An-32.

Civil operators

In August 2006 a total of 56 Antonov An-32 aircraft remain in airline service. Major operators include: Air Pass (4), Alada (3), Libyan Arab Air Cargo (4), Million Air Charter (3), AERCARIBE LTDA (2), Trans-Charter (3) and Selva (4). Some 29 other airlines operate smaller numbers of the type.[4]

Specifications (An-32)

Orthographic projection of the Antonov An-32.

Data from {Jane's All The World's Aircraft 1988-89}[5]

General characteristics

  • Crew: 3
  • Capacity: 42 paratroopers/50 passengers/24 Casualties on stretcher with 3 medical personnel
  • Length: 23.78 m (78 ft 0¾ in)
  • Wingspan: 29.20 m (95 ft 9½ in)
  • Height: 8.75m (28 ft 8½ in)
  • Wing area: 75 m² (807 ft²)
  • Empty weight: 16,800 kg (37,038 lb)
  • Loaded weight: kg (lb)
  • Useful load: 6700 kg (kg)
  • Max takeoff weight: 27,000 kg (59,525 lb)
  • Powerplant: 2× ZMKB Progress AI-20DM turboprop, 3,812 kW (5,112 ehp) each
  • * Cargo hold dimensions: 12.48 (11 metres flat) x 2.30 x 1.84 metres
  • Cargo door size: 2.40 x 1.91 metres, closed by rear loading ramp
  • Maximum hold volume: 30 cubic metres

Performance

References

  1. ^ a b c AeroWorldNet - Renewed AN-32 in Flight Tests (October 16, 2000)
  2. ^ "", Aerospace Source Book 2007, Aviation Week & Space Technology, January 15 2007.
  3. ^ GAO
  4. ^ Flight International, 3-9 October 2006
  5. ^ (1988) in J W R Taylor: Jane's All The World's Aircraft,1988-89. Jane's Information Group. ISBN 0-7106-0867-5. 

Related content

Related development

Designation sequence

An-26 - An-28 - An-30 - An-32 - An-38 - An-70 - An-71

See also


 
 
 

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