Tupolev Tu-204-120

Public Joint Stock Company Tupolev

About

The Tu-204 with Rolls-Royce engines and Western avionics, built for export and flown mainly by Egypt’s Cairo Aviation and by China. It shares type certificate 68-204 with the PS-90A models and shares their limits exactly — a maximum take-off mass of 103,000 kg, a maximum ramp mass of 103,350 kg, a maximum landing mass of 88,000 kg, a maximum payload of 21,000 kg, a maximum operating Mach of 0.83, a ceiling of 12,100 m and up to 210 passengers. What differs is the powerplant: two RB211-535E4-B-75s rated at 19,295 kgf, or 189.2 kN, against the PS-90A’s 16,000 kgf. Like every model on the sheet it is certificated for a crew of three, including a flight engineer.

Weightscompared to Boeing 757-300

MRW (Maximum Ramp Weight)

103,350kg
0
50k
100k
124k

MTOW (Maximum Takeoff Weight)

103,000kg
0
50k
100k
124k

MLW (Maximum Landing Weight)

88,000kg
0
50k
102k

Capacitycompared to Boeing 757-300

Passenger Capacity

210passengers
0
100
200
295

71% of 757-300 maximum capacity

Crew

Total
3
Cockpit
3

Sources11 figures on this page

Engine Specifications

Engine Count

2×

Engine Model

Rolls-Royce RB211-535E4-B-75

Thrust per Engine

189.2 kN(42534 lbf)

Production & History

Production Status

Out of production

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