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Tupolev Tu-134
First flight year — 1963
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Tupolev Tu-134 Specifications
| Tu-134A | Tu-134B | |
| Dimensions | ||
| Length (m) | 37.1 | 37.1 |
| Wingspan (m) | 29.0 | 29.0 |
| Height (m) | 9.0 | 9.0 |
| Wing area (m2) | 127.3 | 127.3 |
| Weight | ||
| Maximum take-off weight (kg) | 47 600 | 47 600 |
| Maximum landing weight (kg) | 43 000 | 43 000 |
| Operating empty weight (kg) | 29 000 | 29 000 |
| Maximum payload (kg) | 8 200 | 2 000 |
| Max stock of fuel (kg) | 13 200 | 13 200 - 14 000 |
| Performance | ||
| Maximum range (km) | 2 770 | 3 340 |
| Range with max payload (km) | 1 750 | 1 830 |
| Maximum cruise speed (km/h) | 850 | 880 |
| Maximum operating altitude (km) | 12 100 | 10 100 |
| Take-off field length (m) | 2 400 | 2 500 |
| Engines | D-30-II, 2 x 15000 lb | D-30-III, 2 x 15300 lb |
| Fuel efficiency (g/pass*km) | 45.0 | 45.2 |
| Fuel flow rate (kg/h) | 2 500 | |
| Cabin Data | ||
| Passengers (1-class) | 76 | 76-80 |
| Passengers (2-class) | 68 | 68 |
| Economy seat pitch (cm) | 75 | 75 |
| Cabin width (m) | 2.9 | 2.9 |
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