Credit
Kirill Naumenko - Moscow City Spotters · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
An-72 · Length
Single source28.07 m (92 ft 1 in)[source]
L-410 UVP-E20 · Length
Single sourceConfiguration
| Specification | Antonov An-72 | Let L-410 Turbolet |
|---|---|---|
| Type | Transport aircraft[source] | Regional airliner , cargo aircraft[source] |
| National origin | Soviet Union[source] | — |
| Manufacturer | Antonov[source] | Let Kunovice[source] |
| Status | In service[source] | In service[source] |
| Primary users |
14.42 m (47 ft 4 in)[source]
L-410 UVP-E20 · 2 × General Electric H80-200 turboprop engines each
Single source2 × General Electric H80-200 turboprop engines, 597 kW (801 hp) 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]
L-410 UVP-E20 · 1,670 ft/min
Single source8.5 m/s (1,670 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Russian Aerospace Forces Russian Navy Angolan Air Force Soviet Air Force (historical)[source] |
Russian Air Force Slovak Air Force Searca Aeroflot (historical)[source] |
| Number built | 133[source] | 1,200[source] |
|---|
| Manufactured | 1977–2002[source] | 1971–present[source] |
|---|
| First flight | 31 August 1977 ( 1977-08-31 )[source] | 16 April 1969[source] |
|---|
| Developed into | Antonov An-71 Antonov An-74[source] | Let L-610[source] |
|---|
| Capacity | up to 52 passengers or 10 tonnes of cargo[source] | 19 passengers / 1,800 kg (3,968 lb) payload[source] |
|---|
| Introduction date | — | 1970[source] |
|---|
| Variant | — | Aircraft Industries L 410 NG[source] |
|---|
| Fuel capacity | — | 1,300 kg (2,866 lb)[source] |
|---|
| Endurance | — | Five hours and six minutes[source] |
|---|
| Aspect ratio | — | 11.45[source] |
|---|
| Airfoil | — | root: NACA 63A418 ; tip: NACA 63A412[source] |
|---|
| Propellers | — | 5-bladed Avia AV 725, 2.3 m (7 ft 7 in) diameter[source] |
|---|
| Fuel consumption | — | 240 kg/h (529 lb/h)[source] |
|---|
| Take-off run | — | 510 m (1,670 ft) (ISA, SL, MTOW)[source] |
|---|
| Landing run | — | 500 m (1,600 ft) (ISA, SL, MTOW)[source] |
|---|
| Alternative designation | — | L-410 Turbolet[source] |
|---|
| Country of origin | — | Czechoslovakia[source] |
|---|
| Reported operators |
| — |
|---|