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1993 Tupolev TU-154M
(AD PAUSED)
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1993 Tupolev TU-154M<br>(AD PAUSED)1993 Tupolev TU-154M<br>(AD PAUSED)1993 Tupolev TU-154M<br>(AD PAUSED)
1993 Tupolev TU-154M<br>(AD PAUSED)1993 Tupolev TU-154M<br>(AD PAUSED)
 
 
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 General information
Transaction
Sale
Last update
Feb. 01, 2011
Aircraft year
1993
Serial no.
TBA
Registration
RA
Specsheet
Airframe time
13 600
TSOH
5,400 h
Total cycles
5,400
Price
Availability
NOW
Engine(s)
D-30KU-154 D-30KU-154
 
Eng.1
Eng.2
Eng.3
S/N
0305931861244
0305931891244
5912881243
TT
14 576
11 452
17 411
TSOH
4 356
4 629
4 060
TBO
18 000
12 000
18 000
 
 Equipment
Avionics
The aircraft is fully equipped to perform international flights in compliance with European Union requirements, namely:
• Air data computer system for the purposes of assuring flights under Reduced Vertical Separation Minimum conditions (RVSM);
• Baklan-20 VHF communicator (2 sets). Frequency spacing of 8,33/25 кHz - one set;
• KLN-90B Global Positioning System (GPS);
• TCAS-II (CAS-67A) Traffic alert & Collision Avoidance System by Honeywell (USA);
• TTA-12S Enhanced Ground Proximity Warning System (EGPWS) with TDS-56D terrain variation display by Tranzas CJSC;
• Automatic stationary oxygen system for passengers and flight attendants (ASOS) with the chemical oxygen sources by Zvezda;
• АRМ-406АS1 and АRМ-406P Emergency Location Transmitters
Additional features
The external power supply sockets, waste systems, centralized fueling and oil-servicing systems do comply with international standards.
Passenger cabin furnishing.
• The information boards and placards available in the cabins are made in Russian and English.
• Condition and supervision of the furnishings do comply with regulatory documents.
• The fire extinguishing appliances do not create dangerous concentration of toxic gases inside the aircraft.
The aircraft is fitted up with:
• Onboard documentation.
• Feeder line diagrams.
• Recommendations on application of foreign aircraft-purpose POL and special liquids.
• List of documents required for flights.

Conclusion:
Configuration of communication, air navigation and domestic equipment of the aircraft does meet the requirements for aircraft used for operation at international airlines and abroad.
The aircraft has been admitted to operation at international airlines including airlines of Europe, India, Cyprus and Iran.
The aircraft has been admitted to operation at international airlines including the North Atlantic and European regions.
APU
ТА-6А, 2007, SN- 0136A020P
TTSN (hours / cycles) - 1 254 / 1 399
Assigned Life (hours / cycles) - 3 400 / 5 000

 
 Condition
Interior  - rating: 9/10 -
9/10
Exterior  - rating: 9/10 -
9/10
Weights & Performances
• Crew: 3-4
• Length: 48.0 m (157 ft)
• Wingspan: 37.55 m (123 ft 3 in)
• Height: 11.40 m (37 ft 5 in)
• Wing area: 201.5 m² (2,168 ft²)
• Empty weight: 55,300 kg (121,915 lb)
• Max takeoff weight: 102,000 - 104,000 kg (224,871 lb - 229,280 lb)
• Powerplant: 3Χ Soloviev D-30KU-154 turbofans, 103 kN (23,148 lbf) each

Performance
• Maximum speed: 950 km/h (510 kn, 590 mph)
• Range: ** With maximum payload: 3,900 km (5,200 km with 164 passengers and baggage) (2,100 nmi, 2,400 mi)
• With maximum fuel: 6,600 km (3,600 nmi, 4,100 mi)
• Service ceiling: 12,100 m (39,700 ft)
 
 Contact
CLOSED
 
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