Tupolev Tu-154

The Gift

The Tupolev Tu-154 (Russian: Туполев Ту-154) (NATO reporting name: Careless) is a three-engine medium-range airliner designed in the mid 1960s and manufactured by Tupolev. As the mainstay 'workhorse' of Soviet and Russian airlines for several decades, it serviced over a sixth of the world's landmass and carried about half of all passengers flown by Aeroflot and its subsidiaries (137.5 million/year or 243.8 billion passenger km in 1990). Having been exported and operated by 17 non-Russian airlines and a number of air forces, it remained the standard domestic route airliner of Russia and former Soviet states until the mid 2000s.

With a cruising speed of 975 kilometres per hour (606 mph), the Tu-154 is one of the fastest civilian aircraft in operation and has a range of 5,280 kilometres (3,280 mi). Capable of operating from unpaved and gravel airfields, it is used in the extreme Arctic conditions of Russia's northern territories where facilities can be basic. With a service life of 45,000 hours (18,000 cycles) but capable of 80,000 hours with upgrades, it is expected to continue operations until 2016, although noise regulations have seen services to western Europe and other areas restricted. In January 2010, Russian flag carrier Aeroflot announced the retirement of its Tu-154 fleet after 40 years with the last flight operated being Aeroflot Flight 736 from Ekaterinburg to Moscow on 31 December 2009.

Since 1968 there have been 39 fatal incidents involving the Tu-154, most of which were caused by factors unrelated to the aircraft. This number is not considered unusual given its specifications, number in operation, years in service, and heavy use in demanding conditions.

 The Tu-154 was developed to meet Aeroflot's requirement to replace the jet-powered Tu-104, the Antonov An-10 'Ukraine' and the Ilyushin Il-18 turboprops. The requirements called for either a payload capacity of 16–18 tonnes (35,000–40,000 lb) with a range of 2,850–4,000 kilometres (1,770–2,500 mi) while cruising at a speed of 900 km/h (560 mph), or a payload of 5.8 tonnes (13,000 lb) with a range of 5,800–7,000 kilometres (3,600–4,300 mi) while cruising at 850 km/h (530 mph). A take-off distance of 2,600 metres (8,500 ft) at maximum take-off weight was also stipulated as a requirement. Conceptually similar to the British Hawker Siddeley Trident, which first flew in 1962, and the Boeing 727, which first flew in 1963, the medium-range Tu-154 would be marketed by Tupolev at the same time as Ilyushin was marketing the long-range Ilyushin Il-62. The Soviet Ministry of Aircraft Industry chose the Tu-154 as it incorporated the latest in Soviet aircraft design and best met Aeroflot's anticipated requirements for the 1970s and 1980s.

The first project chief was Sergey Yeger but in 1964, Dimitriy S. Markov assumed that position. In 1975 he turned it over to Aleksandr S. Shengardt.

The Tu-154 first flew on 4 October 1968. Commercial service began in February 1972, and there is still limited production of the 154M model as of January 2009, despite previous announcements of the end of production in 2006. 1015 Tu-154s have been built, 214 of which are still in service as of 14 December 2009.

 The Tu-154 is powered by three rear-mounted low-bypass turbofan engines arranged similarly to those of the Boeing 727, but is slightly larger than its American counterpart. Both the 727 and the Tu-154 use an S-duct for the middle (number 2) engine. The original model had Kuznetsov NK-8-2, while the Tu-154M has Soloviev D-30KU-154 engines. All Tu-154 aircraft models have a higher thrust-to-weight ratio than that of the 727 – this gives them superior performance, although at the expense of poorer fuel efficiency, which became an important factor in later decades as fuel costs grew.

The cabin of the Tu-154, although of the same six-abreast seating layout, gives the impression of an oval interior, with a lower ceiling than is common on Boeing and Airbus airliners. The passenger cabin accommodates 128 passengers in two-class layout and 164 passengers in single-class layout, and up to 180 passengers in high-density layout. The layout can be modified to what is called a winter version where some seats are taken out and a wardrobe is installed for passenger coats. The passenger doors are also smaller than on its Boeing and Airbus counterparts. Furthermore, luggage space in the overhead compartments is very limited.

Like the Tupolev Tu-134, the Tu-154 has a wing swept back at 35° at the quarter-chord line. The British Hawker Siddeley Trident has the same sweepback angle, while the Boeing 727 has a slightly smaller sweepback angle of 32°. The wing also has anhedral (downward sweep) which is distinguishing feature of Russian low-wing airliners designed during this era. Most Western low-wing airliners such as the contemporary Boeing 727 have Dihedral (upward sweep). The anhedral means that Russian airliners have poor lateral stability compared to Western ones, but also have weaker dutch roll tendencies, eliminating the need for a yaw damper.

Like many other Soviet-built airliners, the Tu-154 has an oversized landing gear enabling it to land on unpaved runways, once common in rural areas of the Soviet Union. The aircraft has two six-wheel main bogies fitted with large low-pressure tires that retract into pods extending from the trailing edges of the wings (a common Tupolev feature), plus a two-wheel nose gear unit. Soft oleo struts (shock absorbers) provide a much smoother ride on bumpy airfields than most airliners, which only very rarely operate on such poor surfaces.

The original requirement was to have a three-person flight crew – captain, first officer and flight engineer – as opposed to 4/5-person crew on other Soviet airliners. A fourth crew member, a navigator, is usually also present in the former Soviet Union, due to union rules. Navigators are no longer trained and this profession will become obsolete with the retirement of older Soviet planes.

The plane's avionics suite, for the first time in the Soviet Union, is built to American airworthiness standards. The latest variant (Tu-154M-100, introduced 1998) includes an NVU-B3 Doppler navigation system, a triple autopilot, which provides an automatic ILS approach according to ICAO category II weather minima, an autothrottle, a Doppler drift and speed measure system (DISS), "Kurs-MP" radio navigation suite and others. Modern upgrades normally include a TCAS, GPS and other modern systems, mostly American or EU-made.

Early versions of the Tu-154 cannot be modified to meet the current Stage III noise regulations and are banned from flying where those regulations are in force, such as Europe. The Tu-154M may use hush kits to meet Stage III and theoretically Stage IV. However current European Union regulations forbid the use of hush kits to meet Stage IV. The Tu-154M would need to be re-engined to meet Stage IV within the EU, an extensive and potentially expensive upgrade.

On January 2, 2011, Russia's Federal Transport Oversight Agency advised airlines to stop using the Tu-154 (B variant) until the fatal fire incident in Surgut had been investigated.