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At a glance
Measured figures
An-28 · Length
Single source13.10 m (43 ft 0 in)[source]
An-72 · Length
Single sourceConfiguration
| Specification | Antonov An-28 | Antonov An-72 |
|---|---|---|
| Type | Short-range airliner , utility aircraft[source] | Transport aircraft[source] |
| Designer | Antonov[source] | — |
| Built by | WSK PZL Mielec[source] | — |
| Status | In service[source] | In service[source] |
| Primary user | Aeroflot (former)[source] |
28.07 m (92 ft 1 in)[source]
Cruise; An-28 · at 3,000 m (9,800 ft)
Single sourceMaximum; An-28 · at 3,000 m (9,800 ft)
Single source350 km/h (220 mph, 190 kn) at 3,000 m (9,800 ft)[source]
335 km/h (208 mph, 181 kn) at 3,000 m (9,800 ft)[source]
Maximum; An-72 · Maximum speed
Single source700 km/h (435 mph, 378 kn)[source]
An-28 · 2 × Glushenkov TVD-10B turboprop engines (960 shp) each
Single source2 × Glushenkov TVD-10B turboprop engines, 720 kW (960 shp) each[source]
An-72 · 2 × Lotarev D-36 series 1A Turbofan thrust each
Single source2 × Lotarev D-36 series 1A Turbofan, 63.9 kN (14,330 lbf) thrust each[source]
An-28 · 1,640 ft/min
Single source8.3 m/s (1,640 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 191[source] | 133[source] |
|---|
| Manufactured | 1975–1993[source] | 1977–2002[source] |
|---|
| Introduction date | 1986[source] | — |
|---|
| First flight | September 1969[source] | 31 August 1977 ( 1977-08-31 )[source] |
|---|
| Developed from | Antonov An-14[source] | — |
|---|
| Variant | PZL M28 Skytruck[source] | — |
|---|
| Developed into | Antonov An-38[source] | Antonov An-71 Antonov An-74[source] |
|---|
| Capacity | 17 passengers or 1,750 kg (3,860 lb)[source] | up to 52 passengers or 10 tonnes of cargo[source] |
|---|
| Aspect ratio | 12.3[source] | — |
|---|
| Airfoil | TsAGI R-II-14 (14% thickness)[source] | — |
|---|
| Fuel capacity | 1,960 L (430 imp gal; 520 US gal)[source] | — |
|---|
| Propellers | 3-bladed AW-24AN, 2.80 m (9 ft 2 in) diameter[source] | — |
|---|
| Never exceed speed | 390 km/h (240 mph, 210 kn)[source] | — |
|---|
| g limits | +3[source] | — |
|---|
| Take-off run to 10.7 m (35 ft) | 410 m (1,350 ft)[source] | — |
|---|
| Landing run from 15 m (50 ft) | 315 m (1,033 ft)[source] | — |
|---|
| National origin | — | Soviet Union[source] |
|---|
| Manufacturer | — | Antonov[source] |
|---|
| Primary users | — | Russian Aerospace Forces Russian Navy Angolan Air Force Soviet Air Force (historical)[source] |
|---|
| Reported operators | — |
|
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