| Manufacturer |
Airbus |
Antonov |
| Family |
A380 |
|
| Model |
A380-800 |
|
| Description |
|
The Antonov An-124 Ruslan (; ; NATO reporting name: Condor) is a large, strategic airlift, four-engined aircraft that was designed in the 1980s by the Antonov Design Bureau in the Ukrainian SSR of the Soviet Union (USSR). |
| ICAO Code |
|
A124 |
| First Flight |
|
1982-12-24 |
| Entry Into service |
|
1986-01-01 |
| Production End |
|
2004-01-01 |
| Designer |
|
Antonov |
| Type |
|
Heavy transport aircraft |
| Length (m) |
72.72 |
69.1 |
| Height (m) |
24.09 |
21.08 |
| Cockpit Crew |
2 |
|
| Max Seating |
853 |
88 |
| Three Class Typical Seating |
525 |
|
| Cruise Speed (km/h) |
|
865 |
| Max Ceiling (m) |
|
12000 |
| Capacity Description |
|
88 passengers in upper aft fuselage, or the hold can take an additional 350 pax on a palletised seating system / 120000 kg |
| Max Mach (Mach) |
0.89 |
|
| National Origin |
|
Soviet Union |
| Number Built |
|
57 |
| Powerplant Description |
|
4 × Progress D-18T (D-18 Series 4 on -150 models) high-bypass turbofan engines, 226.8 kN thrust each |
| Primary Users |
|
Russian Aerospace Forces, Volga-Dnepr Airlines , Antonov Airlines , Maximus Air |
| Status |
|
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Airbus_A380 |
en.wikipedia.org/wiki/Antonov_An-124_Ruslan |
| Flat Wing Span (m) |
79.75 |
73.3 |
| Flat Wing Area (m²) |
845 |
628 |
| Flat Wing Aspect Ratio |
|
8.6 |
| Wing Sweepback (°) |
33.5 |
|
| Fuselage Diameter (m) |
7.14 |
|
| Wake Category |
|
H |
| Aircraft Engine |
GP7270 |
Progress D-18T |
| Number of Engines |
4 |
4 |