| Manufacturer | Lockheed |
| Model | L-1011-200 Tristar |
| Modification | L-1011-200 |
| Country | USA |
| Years | 1976 |
| Type | Passenger aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 47.34 m |
| Length | 54.17 m |
| Height | 16.87 m |
| Wing area | 321.00 m2 |
| Zero fuel weight | - |
| Empty weight | 111200 kg |
| Maximum takeoff weight | 211370 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 3 Rolls-Royce RB211-524B (524B4) |
| Power | - |
| Thrust | 3 x 21770 (22700) kN |
| Maximum speed | - |
| Cruising speed | 982 km/h |
| Rate of climb | - |
| Practical range | 8520 km |
| Service ceiling | 12800 m |
| Hovering ceiling | - |
| Crew | 3-4 |
