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Attribute | Value |
General |
Manufacturer | Tupolev |
Model | Tupolev Tu-124 |
Country | Russia |
Manufactured from | 1960 year |
Manufactured to | 1965 year |
Type | Light Passenger Jets |
Icao | T124 |
Performance |
Engine | 2x Soloviev D-20P |
Power, hp | Add |
Power, lbf | 11,900 lbf |
Avionics | Add |
Max cruise speed | 963 km/h |
Approach speed | 222 km/h |
Travel range | 2,037 km |
Fuel economy | Add |
Service ceiling | 11,704 m |
Rate of climb | 12.19 m/sec |
Take off distance | Add |
Landing distance | Add |
Weights |
Max take off weight | 38,000 kg |
Max landing weight | Add |
Max payload | 6,000 kg |
Fuel tank capacity | 13,249 l |
Baggage volume | Add |
Dimensions |
Seats | 56 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | Add |
Cabin width | Add |
Cabin length | Add |
Exterior length | 30.58 m |
Tail height | 8.08 m |
Fuselage diameter | 2.9 m |
Wing span | 25.55 m |
Wing tips | No Winglets |
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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 26, 2021 (38 fields were changed)