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Tupolev Tu 124

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Top speed
  
970 km/h

Length
  
31 m

First flight
  
March 29, 1960

Number of seats
  
56

Wingspan
  
26 m

Engine type
  
Soloviev D-20

Manufacturer
  
Tupolev

Tupolev Tu-124 Tupolev Tu124 Wikiwand

Fs2004 tupolev tu 124 engine start up and take off at stockholm arlanda


The Tupolev Tu-124 (NATO reporting name: Cookpot) was a 56-passenger short-range twinjet airliner built in the Soviet Union.

Contents

Design and development

Tupolev Tu-124 Tupolew Tupolev Tu124 Specifications Technical Data Description

Developed from the medium-range Tupolev Tu-104, the Tu-124 was meant to meet Aeroflot's requirement for a regional airliner to replace the Ilyushin Il-14 on domestic routes. Resembling a 75% scaled-down Tu-104, the two were hard to tell apart at a distance but it was not a complete copy of the Tu-104. The Tu-124 had a number of refinements, including double-slotted flaps, a large centre-section airbrake and automatic spoilers. Unlike the Tu-104, the wing trailing edge inboard of the undercarriage was unswept.

Tupolev Tu-124 tu124jpg

The Tu-124 retained a drogue parachute to be used in an emergency landing or landing on a slippery surface and had low pressure tires to aid operation from unpaved airfields. As on the Tu-104 the engines were integrated into the wings, but the turbofan engines were more fuel efficient. The placement of the engines amplified vibrations, which affected the comfort of the passenger cabin, and also the fatigue lifetime of the wing assembly.

The standard seating of the basic version was 44 seats. The first of two prototype, SSSR-45000 (C/N 0350101) made its first flight from Zhukovsky airfield on 24 March 1960. The second prototype, SSSR-45001 (C/N 0350102), followed in June 1960. Two other airframes served as a static test cells. Testing was successful, and the aircraft entered production at Factory 135 at Kharkov, Ukraine, replacing the Tu-104 in production. Deliveries to Aeroflot began in August 1962, with the type operating its first scheduled passenger service, between Moscow and Tallinn in Estonia, on 2 October 1962.

Operational history

Tupolev Tu-124 httpsuploadwikimediaorgwikipediacommonsthu

Aeroflot was impressed with the flight performance of the Tu-124 and used it on domestic routes from the end of 1962.

Tupolev Tu-124 Tupolev Tu124 Wikipedia

The improved Tu-124V, which could seat 56 passengers instead of the 44 of the original model, and which had increased range and maximum take-off weight, came into service in 1964. An Aeroflot Tu-124V was exhibited at the 1965 Paris Air Show. Despite the aircraft's low purchase price (stated as $1.45 million in 1965) and low operating costs, few were exported, with Československé Státní Aerolinie (ČSA) and the East German airline Interflug being the only airlines other than Aeroflot that bought the Tu-124 new, although ČSA sold its surviving Tu-124s to Iraqi Airways for use on VIP flights in 1973. Interflug used its three Tu-124s as an alternative to the Ilyushin Il-62, when the Il-62s were grounded due to mechanical issues. All three were sold back to the Soviet Union in 1975.

Tupolev Tu-124 1000 images about Tupolev TU154 TU204214 and TU104110124134

Three airframes were completed in 1966 in a VIP configuration, and designated Tu-124K. However, Aeroflot never placed them into service, and they were purchased by the Indian Air Force.

Tupolev Tu-124 FileCSA Tupolev Tu124 Soderstrom2jpg Wikimedia Commons

A number were also sold to military users, including the Soviet Air Force, which used them as navigational trainers, and to the Chinese Air Force.

A total of 164 Tu-124s were built. Issues with the safety of the Tu-104 affected the fate of the Tu-124, although the reliability of the Tu-124 was slightly better. Production ended in 1965 and Aeroflot decommissioned its last twelve Tu-124s on 21 January 1980. The Tu-124 continued in operation for some years with the Soviet Air Force and in Iraq, but all aircraft were withdrawn before and at 1990, The ones in Iraq military and Iraqi Airways were destroyed in early 1990s during a war.

Several Tu-124s have been preserved. One is in the museum of Kharkiv State Aircraft Manufacturing Company (formerly the Tu-124 manufacturer Factory 135), another is in China's Datangshan aviation museum in Beijing and a third is at the Central Air Force Museum at Monino outside Moscow. A Tu-124K is on display at New Delhi Airport.

Competition within the COMECON

The German Democratic Republic attempted to compete within the COMECON trading bloc with its own four-engined design called the Baade 152. The design was unsuccessful, leading Interflug to buy a rear-engined development of the Tu-124, the Tupolev Tu-134.

Variants

Tu-124/Tu-124V
The first production variant. International demand was small, as most foreign airlines were waiting to buy the improved Tupolev Tu-134
Tu-124B
Three prototypes with D-20P-125 engines, built in 1963
Tu-124K/Tu-124K2
VIP configuration operated by the militaries of Iraq and the Peoples' Republic of China, and by the Indian Air Force
Tu-124Sh-1
Military version used as navigator trainer
Tu-124Sh-2
Military version used as navigator trainer
Tu-127
Proposed military transport version, not built.

Civil operators

 Czechoslovakia
  • ČSA
  •  East Germany
  • Interflug (operated in Interflug colours, but owned by the East German Air Force)
  •  Iraq
  • Iraqi Airways
  •  Soviet Union
  • Aeroflot
  • Military operators

     People's Republic of China
  • People's Liberation Army Air Force
  •  Czechoslovakia
  • Czechoslovakian Air Force
  •  East Germany
  • East German Air Force
  •  India
  • Indian Air Force [three Tu-124K VIP variants]
  •  Iraq
  • Iraqi Air Force
  •  Soviet Union
  • Soviet Air Force
  • Accidents and incidents

    A total of fourteen Tu-124s were written off in crashes during the type's operational career; another two aircraft of Iraqi Airways were destroyed on the ground during the Gulf War.

    Specifications (Tu-124V)

    Data from Soviet Transport Aircraft since 1945

    General characteristics

  • Crew: three
  • Capacity: 56 passengers
  • Length: 30.58 m (100 ft 4 in)
  • Wingspan: 25.55 m (83 ft 10 in)
  • Height: 8.08 m (26 ft 6 in)
  • Wing area: 119.4 m² (1,284 ft²)
  • Empty weight: 22,900 kg (50,486 lb)
  • Max. takeoff weight: 37,500 kg (82,673 lb)
  • Powerplant: 2 × Soloviev D-20P turbofans, 53.1 kN (11,905 lbf) each
  • Performance

  • Maximum speed: 970 km/h (523 knots, 602 mph) at 8,000 m (26,000 ft)
  • Cruise speed: 800–870 km/h (432–469 knots, 497–540 mph)
  • Range: 2,100 km (1,133 nmi, 1,304 mi) (maximum fuel, 3,000 kg (6,600 lb) payload)
  • Service ceiling: 11,700 m (38,385 ft)
  • Rate of climb: 12.0 m/s (2,360 ft/min)
  • References

    Tupolev Tu-124 Wikipedia