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Tupolev Tu-154

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Tupolev Tu-154

Aeroflot Tupolev Tu-154M

Type Airliner
Manufacturer Tupolev/Aviakor
Designed by Aviakor
Maiden flight 4 October 1968
Introduced February, 1972
Status In Service
Primary users Aeroflot
Air Koryo
Produced 1968-2006[1]
Number built 935
Unit cost 45 Million USD 2008

The Tupolev Tu-154 (NATO reporting name: Careless) is a Soviet medium-range trijet airliner, similar to the Boeing 727 and of particularly rugged design. It remains the standard airliner for domestic routes in Russia and other states of the former Soviet Union and to a lesser extent in eastern Europe and Iran. The mainstay of Russian airlines for several decades, the Tu-154 has carried about half of all passengers flown by Aeroflot and its subsidiaries, or approximately 137 million passengers per year, and has been exported and operated by at least 17 foreign airlines. Designed to cope with unpaved and gravel airfields, the plane often operates in extreme Arctic conditions and although production has ceased, there have been requests for resumption of assembly. Despite a heavy and durable airframe capable of very long service life, the Tu-154 sometimes approaches Mach 1 speeds and is the fastest passenger jet in operation.[citation needed]

Contents

Design and development

Kavminvodyavia Tu-154M at Moscow airport
Kavminvodyavia Tu-154M at Moscow airport

The Tu-154 was developed to meet the Aeroflot requirement for a new aircraft to replace the jet-powered Tu-104, plus the Antonov An-10 'Ukraine' and Ilyushin Il-18 turboprops. It competed against the Ilyushin Il-74. The Soviet Ministry of Aircraft Industry picked the Tu-154 because it incorporated the latest in Soviet aircraft design and best met Aeroflot's anticipated requirements of the 1970s and 1980s. The aircraft was to transport a payload of 16 to 18 tons (35,270 to 39,680 lb) over a distance of 2,850 - 4,000 km (1,770 - 2,480 mi) while cruising at a speed of 900 km/h, or a payload of 5.8 tons (12,790 lb) over a distance of 5,800 - 7,000 km (3,600 - 4,350 mi) while cruising at 850 km/h (528 mph). It also had to be able to operate from airfields as short as 2,600 m (8,530 ft) at maximum take-off weight.[2]

The first project chief was Sergey M. Yerger. In 1964 Dimitriy S. Markov assumed that position. In 1975 he turned it over to Aleksandr S. Shengardt.[3]

Major design features

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