BASIC TECHNICAL DATA

 

 

Tu-204 passenger and cargo aircraft

 

 

 

 

 

Herewith we introduce to your attention the aircraft of Tu-204 type. They are manufactured by Ulyanovsk Aviation Industrial Complex Aviastar-SP and represent the family of modern twin-engine aircraft: passenger Tu-204-100 and cargo Tu-204C.

The aircraft are equipped with up-to-date, powerful and fuel-efficient Russian engines PS-90A, which support the on-condition maintenance concept. Engine is to be removed from the aircraft only if the service life is served out or the critical condition is detected by the engine monitoring and crew alert system.

The aircraft and engines are certified by Aviation Register of Interstate Aviation Committee and fully meet all international noise level and toxic emission requirements.

 

 

 

Up-to-date digital Integrated Flight and Navigation Complex with foreign laser gyro inertial navigation systems and radio communication equipment installed on the aircraft complies with all effective ICAO regulations for flights on international routes and provides the following:

•             vertical separation of 1000 ft (300 m) between flight levels 290-410 (RVSM);

•             RNP-5 requirements for BRNAV area navigation flights;

•             ICAO Category II automatic approach;

•             VHF/FM-immunity of short-range navigation and landing systems ILS, VOR.

The integrated flight and navigation complex may incorporate Honeywell (USA) traffic collision avoidance system TCAS-II with 07-version software and Mode S transponder.

To comply with ICAO requirements radio communication equipment includes VHF radio stations with 8,33/25kHz channel spacing, and also emergency locator transmitters of SARSAT system (one for automatic, another for manual operation) can be installed.

At the customers’ option, the aircraft can be equipped with Inertial Reference Systems Honeywell HG 1150BD02 (HG 1150BE01) or Litton (USA) LTN-101 integrated with GPS LTN-2001.

At an order from the customer the following can be installed on the aircraft:

•             main LG tires of Michelin;

•             accumulator batteries VARTA or SAFT;

•             Russian-manufactured refrigerator of 170/200-liter capacity “ΡΥΨ-170” (“ΡΥΨ-200”) in the centre galley.

Passenger aircraft Tu-204-100 provides the greater passenger capacity (up to 210 seats) compared with its domestic analogues resulting in the increased flight profitability.

The aircraft can be equipped with Russian and Western galley units, have various passenger cabin layouts arranged in economy-class version for 210 seats, two-class versions for 175 seats and 160 seats, or any other approved layout. Baggage compartments are equipped for carrying cargo in containers or in bulk.

 

Passenger Cabin Layouts

 

Cargo aircraft Tu-204C is equipped with ANCRA (USA) Cargo Handling System, which enables to use pallets and containers of four type sizes: 88’’x108’’, 88’’x125’’, 96’’x125’’, 53’’υ88’’. The system can be re-arranged to operate any of the above pallets or containers within 30 minutes reducing the period of time required for cargo loading/unloading operations and cutting the costs connected with the aircraft ground time.

 

Variants of standard pallet arrangement

 

 

 

 

Cargo cabin enables to carry cargoes in containers of up to 81’’ height of AAY-7000, AAY-7204 type or in super-large containers of AAY78577UPS type. The cargo cabin can include the equipment for transportation of long-size cargoes of up to 10 m length, which are installed on the main deck on two, three and four standard pallets latched to the floor. The portside cargo door measures 3408x2080 mm with the door sill of 3.89 m from the ground. Time required for complete loading/unloading of cargo cabin comes to about 18 minutes.

Cargo cabin complies with class ‘E’ fire safety requirements.

Product support of the aircraft is assured by the conditions to be agreed by the parties, inclusive of technical assistance, maintenance, performance of service bulletins, repair, supply of spare parts as within warranty period so as during post-warranty period.

 MAIN PERFORMANCE

OF TU-204 FAMILY AIRCRAFT

AIRCRAFT TYPE

TU-204-100

TU-204C

Aircraft length, m

46.14

Aircraft height, m

13.87

Wing span, m

40.88

Engine type

PS-90A

No. of engines ´ takeoff thrust, tf

2 ´ 16

Maximum takeoff weight, t

103.0

Maximum fuel quantity, t

32.8

Maximum payload, t

21.0

27.0

Maximum flight range, km

with maximum payload

with maximum fuel load and payload of
12 tons (Tu-204-100) and
13.5 tons (Tu-204C)

 

4300

 

6800

 

3120

 

7000

Volume of baggage/cargo cmpts arranged for ‘in bulk’ cargo carrying, m3

44.5

Cruising speed, km/hr

810-850

Cruising altitude range, km

10.1-12.1

Crew members

3

Outside air temperature at the ground, TH

±45°C

Friction factor, m

0.3

Aerodrome altitude, not more than

2000 m

Field length required, m

takeoff run

landing run

 

1760

2160

Landing category

II

Aerodrome code letter

Α

 

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