Attribute | ![]() McDonnell Douglas DC-9-20 × | ![]() Tupolev Tu-134 × |
---|---|---|
General | ||
Manufacturer | McDonnell Douglas | Tupolev |
Model | McDonnell Douglas DC-9-20 | Tupolev Tu-134 |
Country | United States | Russia |
Manufactured from (year) | 1965 | 1966 |
Manufactured to (year) | 1982 | 1989 |
Type | Mid Size Passenger Jets | Light Passenger Jets |
Icao | DC92 | T134 |
Performance | ||
Engine | 2x JT8D-11 | 2x Soloviev D-30-II |
Power, lbf (lbf) | 15,000 | 14,990 |
Max cruise speed (km/h) | 898 | 898 |
Approach speed (km/h) | 235 | 232 |
Travel range (km) | 2,778 | 3,204 |
Service ceiling (m) | 10,668 | 12,101 |
Rate of climb (m/sec) | 12.7 | 14 |
Take off distance (m) | 1,600 | 2,440 |
Landing distance (m) | 1,500 | 1,340 |
Weights | ||
Max take off weight (kg) | 45,359 | 47,600 |
Max landing weight (kg) | 43,227 | 43,000 |
Max payload (kg) | 11,501 | 8,200 |
Fuel tank capacity (l) | 13,926 | 13,249 |
Baggage volume (m³) | 17 | 14.5 |
Dimensions | ||
Seats | 9 | 84 |
Cabin height (m) | 2.05 | 1.96 |
Cabin width (m) | 3.12 | 2.71 |
Cabin length (m) | 18.29 | 15.93 |
Exterior length (m) | 31.82 | 37.3 |
Tail height (m) | 8.4 | 9.14 |
Fuselage diameter (m) | 3.35 | 2.9 |
Wing span (m) | 28.44 | 29.01 |
Wing tips | No Winglets | No Winglets |