T204
TUPOLEV Tu-204
TUPOLEV Tu-204
Aircraft
Name
Tu-204
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing (winglets)
Tail
Regular tail, low set
WTC
M
APC
C
Type Code
L2J
Engine
Jet
Engine Count
Multi
Position
Underwing mounted
Landing gear
Tricycle retractable
Manufactured as
TUPOLEV Tu-204
TUPOLEV Tu-214
TUPOLEV Tu-224
TUPOLEV Tu-234
T204
Medium range airliner. In service since 1996. Developed in a few versions: TU-204C freighter version, TU-214 combi version, TU-204-120 and TU-204-220 Rolls Royce engine powered versions with Collins or Russian avionics. TU-224 Rolls Royce powered and TU-234 PS90 powered shorter versions for 166 passengers.
The freighter version, Tu-204-120CE, powered by RR 211 engines, with English-language flight deck and Operations documentation was the first Russian/CIS built aircraft to hold an EASA aircraft type certification.
Technical Data
Wing span (metric)
42.00 m
Length (metric)
46.00 m
Height (metric)
13.90 m
Powerplant
204-200: 2 x 157 KN Soloviev PS-90A turbofans.
Engine Model(s)
Rolls-Royce RB211
Soloviev PS-90
Indicative Performance Data
Take-Off
V2
160 kts
Distance
2050 m
MTOW
103000 kg
Initial Climb (to 5000 ft)
IAS
180 kts
ROC
2500 ft/min
Initial Climb (to FL150)
IAS
290 kts
ROC
2300
Initial Climb (to FL240)
IAS
290 kts
ROC
1500 ft/min
MACH Climb
MACH
0.72
ROC
1000 ft/min
Cruise
TAS
450 kts
MACH
0.79
Ceiling
390
Range
3600 NM
Initial Descent (to FL240)
MACH
0.72
ROD
800 ft/min
Descent (to FL100)
IAS
290 kts
ROD
3500 ft/min
Descent (FL100 & below)
IAS
250 kts
MCS
210 kts
ROD
1500 ft/min
Approach
Vapp (IAS)
140 kts
Distance
2100 m
