Tupolev Tu-204-300

Public Joint Stock Company Tupolev

About

The shortened, longer-ranged Tu-204 — six metres out of the fuselage and the fuel kept, which turns a medium-haul airliner into one Vladivostok Avia flew non-stop to Moscow. Interstate Aviation Committee type certificate СТ238-Ту-204-300 gives a maximum take-off mass of 107,500 kg, higher than the full-length Tu-204-100, with a maximum ramp mass of 107,850 kg, a maximum landing mass of 88,000 kg, a maximum zero-fuel mass of 78,000 kg and a maximum payload of 18,000 kg. It cruises to a maximum operating Mach of 0.83 and a maximum altitude of 12,100 m, carries up to 157 passengers, and — like the Tu-204 and the Tu-214 — is certificated for a crew of three including a flight engineer. Two PS-90A engines give 16,000 kgf of take-off thrust each, or 156.9 kN, rising to 17,500 kgf on the one-shot contingency rating.

Weightscompared to Boeing 757-300

MRW (Maximum Ramp Weight)

107,850kg
0
50k
100k
124k

MTOW (Maximum Takeoff Weight)

107,500kg
0
50k
100k
124k

MLW (Maximum Landing Weight)

88,000kg
0
50k
102k

MZFW (Maximum Zero Fuel Weight)

78,000kg
0
50k
95k

Capacitycompared to Boeing 757-300

Passenger Capacity

157passengers
0
100
200
295

53% of 757-300 maximum capacity

Crew

Total
3
Cockpit
3

Sources13 figures on this page

Engine Specifications

Engine Count

2×

Engine Model

Aviadvigatel PS-90A

Thrust per Engine

156.9 kN(35273 lbf)

Fuel & Cargo

Fuel Capacity

45,551 L

Production & History

Production Status

Out of production

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