Antonov An-32

1st Flight 1976

Military Users-

Afghan Air Force, Armenian Air Force, Bangladesh Air Force, Colombian Army, Croatian Air Force, Military of Ivory Coast, Air Force of Equatorial Guinea, Ethiopian Air Force, Indian Air Force, Iraqi Air Force, Jordanian Air Force, Libyan Air Force, Mexican air Force, Mexican Navy, Military of Rwanda, People’s Air and Air Defence Force of Angola, Peruvian Air Force, Peruvian Army, Peruvian Naval Aviation, Sri Lanka Air Force, Sudanese Air Force, Tanzania.


The Antonov An-32 is a turboprop twin-engine military transport aircraft.

The An-32 is essentially a re-engined An-26.


It is designed to withstand adverse weather conditions better than the standard An-26.

Announced at the May 1977 Paris Air Show, the An-32 is distinguished from its predecessor by engines raised 1.5 m above the wing in order to avoid foreign object damage on rough, unprepared air strips.


The type features high-lift wings with automatic leading-edge slats, large triple-slotted trailing edge flaps and an enlarged tail plane and a very large increase in power, giving improved take-off performance and service ceiling.


The high placement of the engine nacelles above the wing allowed for larger diameter propellers, which are driven by 5,100 hp rated Ivchenko AI-20 turboprop engines, providing almost twice the power of the An-26’s AI-24 powerplants.

Production from the Government Aircraft Factory in Kyiv, has included 123 aircraft for the Indian Air Force, which ordered the aircraft under strong foreign relations between then USSR leader Leonid Brezhnev and then India leader Indira Gandhi.


The majority of production has been for the Russian and Ukrainian Air Forces, with around 40 per year being built during the late 1980s to early 1990s.

The estimated price for a modernized An-32 version is 15 million US dollars.



Crew: 4

Length: 23.78 m (78 ft 0 in)

Wingspan: 29.2 m (95 ft 10 in)

Height: 8.75 m (28 ft 8 in)

Wing area: 75 m2 (810 sq ft)

Empty weight: 16,800 kg (37,038 lb)

Max takeoff weight: 27,000 kg (59,525 lb)


Power plant: 2 × ZMKB Progress AI-20DM turboprop engines, 3,812 kW (5,112 hp) each

Propellers: 4-bladed constant speed propellers


Maximum speed: 530 km/h (330 mph, 290 kn)

Cruise speed: 470 km/h (290 mph, 250 kn)

Range: 2,500 km (1,600 mi, 1,300 nmi) with 3,700 kg (8,160 lb) payload, no reserves

Service ceiling: 9,500 m (31,200 ft)




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