Commercial Aircraft Directory - Aircraft Specification
Tupolev - Tu-234
View specification units in: METRIC | IMPERIAL
SPECIFICATION
| First Flight date: | Jul 2000 | |
| Certification date: |
PRINCIPAL DIMENSIONS
| Fuselage width: | ||
| Fuselage height: | 13.9 m | |
| Fuselage length: | 40 m | |
| Cabin length: | 30.18 m | |
| Cabin width: | 3.8 m | |
| Cabin height: | 4.1 m | |
| Cabin volume: | ||
| Hold volume: | 28 m3 |
WEIGHTS
| Empty operating: | 56,000 kg | |
| Max zero fuel: | ||
| MTOW: | 107,500 kg | |
| MLW: | 88,000 kg | |
| Standard fuel capacity: | ||
| Max fuel capacity: |
SPEEDS
| Normal cruise: | 808 km/h | |
| Max cruise: | 458 km/h |
PERFORMANCE
| Long Range Cruise alt: | ||
| Max ceiling: | 12,101 m | |
| Take off field length: | ||
| Landing field length: | ||
| Max Payload Range: | 5,800 m | |
| Range notes: | ||
| Max passengers: | 157 | |
| Typical passengers: | 157 |
POWERPLANT
| Category: | Turbofan | |
| Manufacturer: | Perm / Aviadvigatel | |
| Model/Submodel: | PS-90 | |
| Thrust: | 158 kN |
POWERPLANT
| Category: | Turbofan | |
| Manufacturer: | Perm / Aviadvigatel | |
| Model/Submodel: | PS-90 | |
| Thrust: | 158 kN |
