Design features

Tu 204-120. Design features

Fuselage skin panels. Strengthened stringers (aluminum-lithium). Advanced lightweight structural materials. High surface smoothness.
6-ft winglet (composite)
Conventional 46 m length fuselage. New state-off-the-art interiors
Fin 2820 liters fuel tank. Auto C.G. management using fuel transfer
Broad use of composite structure: Rudder Elevator Wing parts
APU choice
Oval body cross section Width=149.5 in (3.8 m) Height=161.4 in (4.1 m)
Variable incidence horizontal tail
Container under-floor capacity
Most advanced wing design with 28 sweep and 42 m / 137.8 ft wing span with winglets
Full span leading edge stats
Engines RB211-535E4B
Fly-by-wire nose gear steering
Glass cockpit (dark environment) FMS, EFIS, EICAS, Cat IIIA VOR, DME, INS fly-by-wire FC (triplex analogue backup)
Combination of Russian and Western made avionics
Advanced 3 man crew flight deck