BASIC TECHNICAL DATA

Tu-204C cargo aircraft

Herewith we introduce to your attention the cargo aircraft Tu-204C, which is manufactured by Ulyanovsk Aviation Industrial Complex Aviastar-SP and represents the modern twin-engine aircraft equipped with PS-90A engines.

Up-to-date, powerful and fuel-efficient Russian engines PS-90A 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 of Tu-204 family and engines PS-90A 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.

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. The Cargo Handling System allows to move containers and pallets with cargo along the fuselage and fasten them.

Cargo cabin enables to carry cargoes in international-class 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 main cargo door is located on portside between frames 16-23, opens outside upward to angle of 73 degrees, measures 3408x2080 mm with the door sill of 3.89 m from the ground.

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

Baggage compartments are equipped for carrying cargo in containers or “in bulk”.

Variants of standard pallet arrangement

Variants of long-size cargo arrangement

MAIN PERFORMANCE OF TU-204 FAMILY AIRCRAFT

 

AIRCRAFT TYPE

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

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)

 

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

Periodicity of periodic maintenance checks, flying hrs:

§        F1 check

§        F2 check

 

600

3000

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.

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