Tupolev Tu-334-100

Public Joint Stock Company Tupolev

About

A twin-jet regional airliner Tupolev designed to replace the Tu-134, certificated by the Interstate Aviation Committee in 2003 and then built only in single figures before the programme was abandoned in favour of the Superjet. Its type certificate СТ231-Ту-334-100 gives a maximum take-off mass of 47,900 kg, a maximum landing mass of 43,500 kg, a maximum zero-fuel mass of 41,650 kg and a maximum payload of 12,000 kg, with a maximum operating Mach number of 0.80. Two D-436-T1 engines give 7,650 kgf of take-off thrust each, or 75.0 kN.

Weightscompared to Airbus A318

MRW (Maximum Ramp Weight)

48,180kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

47,900kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

43,500kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

41,650kg
0
25k
53k

Sources11 figures on this page

Engine Specifications

Engine Count

2×

Engine Model

Ivchenko-Progress D-436-T1

Thrust per Engine

75.0 kN(16861 lbf)

Fuel & Cargo

Fuel Capacity

12,949 L

Production & History

Production Status

Cancelled

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