Credit
Kirill Naumenko - Moscow City Spotters · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
An-72 · Length
Single source28.07 m (92 ft 1 in)[source]
360-300 · Length
Single sourceConfiguration
| Specification | Antonov An-72 | Short 360 |
|---|---|---|
| Crew | five[source] | Three (Two pilots plus one cabin crew)[source] |
| Type | Transport aircraft[source] | Transport aircraft[source] |
| National origin | Soviet Union[source] | United Kingdom[source] |
| Manufacturer | Antonov[source] | Short Brothers |
21.58 m (70 ft 10 in)[source]
Maximum; An-72 · Maximum speed
Single source700 km/h (435 mph, 378 kn)[source]
360-300 · 2 × Pratt & Whitney Canada PT6 A-65AR turboprop (1,424 shp) each
Single source2 × Pratt & Whitney Canada PT6 A-65AR turboprop , 1,062 kW (1,424 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]
360-300 · 952 ft/min
Single source4.84 m/s (952 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In limited service[source] |
|---|
| Primary users | Russian Aerospace Forces Russian Navy Angolan Air Force Soviet Air Force (historical)[source] | Air Cargo Carriers TransAir Skyway Enterprises Air Flamenco[source] |
|---|
| Number built | 133[source] | 165[source] |
|---|
| Manufactured | 1977–2002[source] | 1981–1991[source] |
|---|
| First flight | 31 August 1977 ( 1977-08-31 )[source] | 1 June 1981[source] |
|---|
| Developed into | Antonov An-71 Antonov An-74[source] | — |
|---|
| Capacity | up to 52 passengers or 10 tonnes of cargo[source] | 36 passengers[source] |
|---|
| Introduction date | — | November 1982[source] |
|---|
| Developed from | — | Short 330[source] |
|---|
| Variant | — | Short C-23B/C Sherpa[source] |
|---|
| Airfoil | — | NACA 63A modified[source] |
|---|
| Fuel capacity | — | 2,182 L (480 imp gal; 576 US gal)[source] |
|---|
| Fuel consumption | — | 1.01 kg/km (3.57 lb/mi) 820 lb (370 kg)/h at 200 kn (370 km/h) TAS[source] |
|---|
| Reported operators |
| — |
|---|