ANTONOV AN-32
The 'Antonov An-32' (NATO reporting name: "Cline") is a twin-engined turboprop military transport aircraft.
| Contents |
| General characteristics |
| Operators |
| Military operators |
| Civil operators |
| Specifications (An-32) |
| References |
| Related content |
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 mountanious (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
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.
★ : At least 6 were delivered to the Afghan Air Force from 1987. 2 remain operational[2].
★
★
★
★
★ 2 units operational, modernized in 2004
★ Equatorial Guinea
★
★
★ : The Indian Air Force operates 119
★ : Mexican Air Force, Mexican Navy,To be retired or are retired.
★
★
★
★
★
★ : Used by the 6th Special Operations Squadron for training[3]
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)
{{aircraft specifications
|plane or copter?=plane
|jet or prop?=prop
|ref={Jane's All The World's Aircraft 1988-89}[5]
|crew=3
|capacity=42 paratroopers/50 passengers/24 Casualties on stretcher with 3 medical personnel
|length main= 23.78 m
|length alt= 78 ft 0¾ in
|span main= 29.20 m
|span alt= 95 ft 9½ in
|height main= 8.75m
|height alt= 28 ft 8½ in
|area main= 75 m²
|area alt= 807 ft²
|airfoil=
|empty weight main= 16,800 kg
|empty weight alt= 37,038 lb
|loaded weight main= kg
|loaded weight alt= lb
|useful load main=6700 kg
|useful load alt= kg
|max takeoff weight main= 27,000 kg
|max takeoff weight alt= 59,525 lb
|more general=
★ 'Cargo hold dimensions': 12.48 (11 metres flat) x 2.30 x 1.84 metres
|engine (jet)=
|type of jet=
|number of jets=
|thrust main= kN
|thrust alt= lbf
|thrust original=
|afterburning thrust main= kN
|afterburning thrust alt= lbf
|engine (prop)=ZMKB Progress AI-20DM
|type of prop= turboprop
|number of props=2
|power main= 3,812 kW
|power alt= 5,112 ehp
|power original=
|max speed main= 540 km/h
|max speed alt= 286 knots, 329 mph
|cruise speed main= 480 km/h
|cruise speed alt= 254 knots, 292 mph
|stall speed main= km/h
|stall speed alt= knots, mph
|never exceed speed main= km/h
|never exceed speed alt= knots, mph
|range main= 2,500 km
|range alt= 1,350 nm, 1,553 mi
|more range= with 3700 kg payload, no reserves
|ceiling main= 9,500m
|ceiling alt= 31,165 ft
|climb rate main=640 m/s
|climb rate alt= ft/min
|loading main= kg/m²
|loading alt= lb/ft²
|thrust/weight=
|power/mass main= W/kg
|power/mass alt= hp/lb
|more performance=
★ 'Takeoff run': 1360 metres for max takeoff weight
|armament=
|avionics=
}}
References
1. 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. Jane's All The World's Aircraft,1988-89, , , , Jane's Information Group, 1988, ISBN 0-7106-0867-5
★ Official Page
★ Bangladesh Air Force AN-32 Image Gallery
★ Indian Air Force AN-32 Image Gallery
Related content
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