| Manufacturer |
Antonov |
Antonov |
| Description |
AI-24VT |
projected VTOL military transport |
| ICAO Code |
AN26 |
AN32 |
| EASA TCDSN |
EASA.IM.A.351 |
|
| First Flight |
1969-05-21 |
1976-07-09 |
| Entry Into service |
1972-01-01 |
|
| Production End |
|
2012-01-01 |
| Designer |
|
Antonov |
| Type |
Transport aircraft / regional airliner |
Military transport aircraft |
| Length (m) |
23.8 |
23.78 |
| Height (m) |
8.58 |
8.75 |
| Cockpit Crew |
|
4 |
| Max Seating |
40 |
42 |
| Max Speed (km/h) |
|
530 |
| Cruise Speed (km/h) |
440 |
470 |
| Max Ceiling (m) |
7500 |
9500 |
| Rate of Climb (m/s) |
8 |
|
| Capacity Description |
40 passengers / 5500 kg |
42 paratroopers/50 passengers/24 Casualties on stretcher with three medical personnel / 6700 kg max payload |
| National Origin |
Soviet Union |
Soviet Union |
| Number Built |
1403 |
373 |
| Powerplant Description |
2 × Progress AI-24VT Turboprop engines, 2103 kW (2820 hp) each |
2 × ZMKB Progress AI-20DM turboprop engines, 3812 kW (5112 hp) each |
| Primary Users |
Soviet Air Forces (former), Russian Aerospace Forces , Ukrainian Air Force , People's Liberation Army Air Force |
Indian Air Force, National Air Force of Angola, Sri Lanka Air Force, Ukrainian Air Force |
| Status |
In service |
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Antonov_An-26 |
en.wikipedia.org/wiki/Antonov_An-32 |
| Flat Wing Span (m) |
29.3 |
29.2 |
| Flat Wing Area (m²) |
74.98 |
75 |
| Flat Wing Aspect Ratio |
11.7 |
|
| Wake Category |
M |
M |
| Number of Engines |
2 |
2 |