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]
402C Businessliner · Length
Single sourceConfiguration
| Specification | Antonov An-72 | Cessna 402 |
|---|---|---|
| Crew | five[source] | Two pilots[source] |
| Type | Transport aircraft[source] | Corporate transport and airliner[source] |
| National origin | Soviet Union[source] | United States[source] |
| Manufacturer | Antonov[source] | Cessna |
36 ft 4 + 1 ⁄ 2 in (11.09 m)[source]
Maximum; An-72 · Maximum speed
Single source700 km/h (435 mph, 378 kn)[source]
402C Businessliner · 2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines each
Single source2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines, 325 hp (242 kW) 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]
402C Businessliner · 1,450 ft/min (
Single source1,450 ft/min (7.4 m/s)[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 service[source] |
|---|
| Primary users | Russian Aerospace Forces Russian Navy Angolan Air Force Soviet Air Force (historical)[source] | — |
|---|
| Number built | 133[source] | 2,000+[source] |
|---|
| Manufactured | 1977–2002[source] | 1966–1985[source] |
|---|
| First flight | 31 August 1977 ( 1977-08-31 )[source] | August 26, 1965[source] |
|---|
| Developed into | Antonov An-71 Antonov An-74[source] | Cessna 404 Titan Cessna 414[source] |
|---|
| Capacity | up to 52 passengers or 10 tonnes of cargo[source] | Six passengers[source] |
|---|
| Primary user | — | Cape Air[source] |
|---|
| Introduction date | — | 1967[source] |
|---|
| Developed from | — | Cessna 411[source] |
|---|
| Airfoil | — | NACA 23018 (root) NACA 23015 (tip)[source] |
|---|
| Fuel capacity | — | 206 US gal (172 imp gal; 780 L) usable fuel[source] |
|---|
| Propellers | — | 3-bladed McCauley 0850334-34 constant speed propeller[source] |
|---|
| Stall speed | — | 68 kn (78 mph, 126 km/h) (flaps down, power off) (CAS)[source] |
|---|
| Never exceed speed | — | 231 kn (266 mph, 428 km/h) ( CAS )[source] |
|---|
| Takeoff distance to 50 ft (15m) | — | 2,195 ft (669 m)[source] |
|---|
| Landing distance from 50 ft (15m) | — | 2,485 ft (757 m)[source] |
|---|
| Reported operators |
| — |
|---|