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TU-334 AIRCRAFT FAMILY

    “TU-334” AIRCRAFT PROGRAM

    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.

    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.

    TU-334 /ac first flight 08 February, 1999
    TU-334 /ac first flight 08 February, 1999

    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


    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


    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


    GENERAL VIEW OF TU-334-100 AIRCRAFT
    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
    WEIGHTS
    MAX takeoff weight, t 47,9
    Operating empty weight, t 38,360
    Max payload, t 12
    Fuel reserve, t 10,1
    Max landing weight, t 43,5
    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

    TU-334-100 A/C PAYLOAD VS.RANGE DIAGRAM


    PASSENGER CABIN DIMENSIONS

    • Length

    • Max width

    • Max height

    • Volume

    Passenger cabin layout can be designed as per customer desire Decorative finishing is made of incombustible materials. In passenger cabin overhead bins volume is increased. Noise level is low within cabin. Audio/video entertainment systems are provided and SATCOM satellite communication system is provided.

    Cabin
    Cabin

    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. 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.


    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.

    TU-334 a/c cockpit
    TU-334 a/c cockpit

    TU-334 a/c modifications
    100 100D 120D 200 220
    WING AREA, SQ.M 83,2 100 100 100 100
    ENGINES Ä436Ò1 D436-T2 BR715-56 D436-T2 BR715-56
    - takeoff thrust, kgf 2õ7500/8650 2õ8200/8650 2õ9074 2õ8200/8650 2õ9074
    - s.f.c.of engine kg/kgf*hour (max cruising mode. Í=11, Ì=0,75) 0,64 0,64 0,61 0,64 0,64
    PASSENGER CAPACITY
    single class layout 102 102 102 126 126
    wo class layout
    MAXIMAL TAKEOFF WEIGHT,t 47,9 54,42 53,75 54.47 54,8
    OPERATING EMPTY WEIGHT, t 28,95 31,92 32,32 33,975 34,325
    PAYLOAD, T
    Maximal 12 12 12 15 15
    passenger (1 pass - 95kg) 9,69 9,69 9,69 11,97 11,97
    OPEARATIONAL RANGE, km 2040 3020 2860 980 830
    with max payload, t 12 12 12 15 15
    OPERATIONAL RANGE, km 3150 4100 4100 2200 2200
    with designed payload, t 9,69 9,69 9,69 11,97 11,97
    CARGO COMPARTMENTS CAPACITY, m3 16,2 15,8 15,8 23,3 23,3
    FUEL TANKS CAPACITY, t 9,54 15,7 15,7 15,7 15,7
    VOLUME OF OVERHEAD BINS PER 1 PASS, L/PASS 53 56 56 56 56
    CABIN VOLUME PER 1 PASS, m3/pass. 1,16 1,22 1,22 1,23 1,23
    FUEL EFFICIENCY, g/pass*km 22,85 24,05 22,1 22,3 20,1
    WING LOAD, kg/m2 1575 1554 1537 1555 1548
    THRUST-TO-WEIGHT RATIO DURING TAKEOFF 0,313/0,181 0,301/0,159 0,338/0,169 0,296/0,156 0,331/0,166

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