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TU-334 aircraft - is a Russian short-range turbojet aircraft designed for 102 passengers which flight range is equal to 3150 km with designed payload. TU-334 -100 a/c first flight was performed 8 February, 1999. |
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TU-334 a/c was manufactured on the base of advanced developments in dynamics, design, materials science, airborne equipment and is provided with high efficient engines. This allowed to obtain high aerodynamic characteristics and low operational costs. |
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CONCEPT • High comfort level • Passenger cabin arrangement as per customer request • Low noise level in passenger cabin and cockpit • State-of-the-art cabin design • Increased volume of overhead bins • Possibility of installation of audio/video systems • Possibility of installation of SATCOM satellite communcation systems |
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EFFICIENCY • Commonality with TU-204 a/c by components, systems and units • Modifications of different passenger capacity, flight range and comfort level to meet customer request • Performance of flights under visual and instrument meteorological conditions, on any airways, over water areas, non-reference terrain and Arctic area • Low specific fuel consumption • Simple operation and low maintenance labor content • Compliance with Chapter IV, ICAO regarding noise level • Assigned service life of airframe, engine and systems comply with current requirements of Operators • Decreased time period for flight preparation |
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SAFETY • Certification to AP-25 , JAR, FAR • State-of-the-art integrated flight and navigation complex • Availability of emergency avoidance systems • Conputerized built-in test of airborne systems • Use of fire safe masks for passengers and crew members |
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TU-334-100 AIRCRAFT DIMENSIONS Aircraft length, m 31,26 Aircraft height, m 9,38 Wing span, m 29,77 Wing area, sq.m 83,226 Wing sweep, grad. 24,0 Fuselage section 3,4 x 4,1 |
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WEIGHTS MAX takeoff weight, t 47,9 Operating empty weight, t 38,360 Max payload, t 9,69 Fuel reserve, t 10,1 Max landing weight, t 43,5 |
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Flight rangeat max payload, km 2040 Flight range with 102 passengers, km 3150 Cruise speed, km/h 8200 Runway length, m 1960 Passenger capacity (Tourist class) 102 |
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PASSENGER CABIN DIMENSIONS |
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PANEL MODEL Abacus Custom Panel Designer Version 3.0 |
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ENGINES Turbofan D-436T-1 engine with reversers (2x73.6 kN, 2x7500 kgf) produced by Zaporozhie Engine Manufacturing Design Bureau provided . Engine was certified in 2000. Low fuel consumption, high ecological data, low operational costs at long life. |
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Engine is produced in co-operation with “Motor Sich” JSC (Ukrain), “Moscow Engineering Manufacturing Corporation”Salut” JSC (Russia), “Ufa Engine Manufacturing Corporation” JSC (Russia). TU-334 a/c modifications are supposed to be provided with turbofan D-436T-2 engines with thrust of 80.4-83.4 kN (8200 kgf) each. |
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COCKPIT
Cockpit is in commonality with TU-204 a/c. Cockpit was designed on the base of state-of-the-art ergonomic standards and new designers approaches associated with electronic displays and means of computerized aircrfat control. “Dark” cockpit concept was applied with illumination of certain areas. Link |
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JRLucariny TU-334 Model |
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DRAWINGS “Aerosite Tupolev Tu-334" |
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< The Real "TUPOLEV" |