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Airbus A310 for sale

 

Airbus A310 for sale information

In parallel with the development of the A300 aircraft company Airbus designed and less capacious option. So there was an aircraft A310. Its fuselage was considerably shorter than the plane A300. High-tech company BAe with Wing reduced scale and area and horizontal tail were new. Cabin crew, designed for two people, was located in the nose of the aircraft and was equipped with modern aircraft digital electronic equipment.

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Airbus A310 for sale

Year • 1988

Price on request

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More about Airbus A310 for sale

Airbus A310 for sale

Aircraft A310, housed in the salons of the middle class from 210 to 250 passengers, was formally launched in July 1978, and made its first flight April 3, 1982 and March 11 next year, the aircraft has passed certification in France and West Germany. In April, the first company-Lufthansa and Swissair-began operation of these aircraft. Main production version received the designation of the A310-200. in May 1986, these aircraft were originally established at the ends of the wings are aerodynamic ridged, reducing drag. Aircraft A310-200 and A310-200F were, respectively, convertible and commercial versions. The first major version became the aircraft with long-range A310-300 taking off July 8, 1985 he had a standard aerodynamic ridges at the ends of the wings and an additional fuel tank in the tail. In addition, the cargo hold can be placed the central fuel tank. The first customer is the company Swissair, and airplanes owned by companies such as Uordjejr, regularly commit flying across the Atlantic Ocean.

 SPECIFICATIONS:

 

Modification A310
Wingspan, m 43.90
Aircraft length, m 46.66
Aircraft height, m 15.80
Wing area m2 219.00
Mass, kg
empty equipped aircraft 113000
Max takeoff 150900
Engine type 2 BY-PASS TURBOJET ENGINE General Electric CF6-80C2A2 (Pratt Whitney PW4000)
Thrust, kgf 2 x 23586 (26761)
Maximum speed, km/h 898
Cruising speed, km/h 872
Economic speed, km/h 821
Range, km 9600
Service ceiling, m
Crew, pers 2
Payload 210-250 passengers or 26700 kg of cargo

 

Airbus A310-300 for sale

At the beginning of 1982 g. Consortium Airbus Industry announced the development of a variant of the aircraft A310-300 for operation on routes of greater length than the A310-200 plane. The development officially began in March 1983, after deliveries began aircraft A310-200. The main difference between aircraft A310-300 from the original is the optional fuel tank capacity 6100 l horizontal plumage and application of automated system for swapping fuel for maintaining optimal balancing of aircraft in flight. At the ends of the wings were installed small arrow-shaped aerodynamic surfaces (“puck”), which became later installed and on aircraft A310-200.

The first flight of the prototype A310-300 with Pratt & Whitney JT9D-7R4 July 8, 1985 took place, and the first flight of an airplane with General Electric CF6-80c2s-in September 1985, aircraft certification was completed in December 1985, and in the same month, the Swiss airline “Svissjer” received the first plane. In October 1991, A310-300 aircraft was certified “Aviaregistrom” of the Russian Federation, as a result of which he received the right to operate in the Russian airlines. Currently, the airline “Aeroflot-Russian international airlines has 10 aircraft A310-300, two of which are leased from Yakut Diamond Sakha Airlines”. Several aircraft A310-200 and-300 used in the AIR FORCES of a number of countries (Canada, Germany, France and Thailand) for transporting VIPs, as well as a military transport. In 1995 one A310-300 aircraft was converted into a transport tanker aircraft MRTT. MRTT aircraft can carry various goods for military purposes, as well as the extra fuel weight 28 t designed for one or two refueling aircraft in flight.

The aircraft is equipped with digital avionics EFIS complex, comprising four multifunctional display for the necessary information about the flight, and a digital control system for work onboard systems and preventing failures ESAM. Radio navigational equipment complies with ARINC 700. It is presented in 1985, only to the beginning of 1997, it was sold to 176 aircraft of this modification, is 167. The total number of aircraft sold A310 by mid-1997, amounts to 261, of which 249 aircraft were in operation.

 SPECIFICATIONS:

 

Modification A310-300
Wingspan, m 43.90
Aircraft length, m 46.66
Aircraft height, m 15.81
Wing area m2 219.00
Mass, kg
empty equipped aircraft 82600
Max takeoff 1641000
Engine type 2 BY-PASS TURBOJET ENGINE General Electric CF6-80C2A8 (Pratt Whitney PW4156)
Thrust, kgf 2 x 25420 (26780)
Maximum speed, km/h 940
Cruising speed, km/h 895
Range, km 9540
Service ceiling, m 11300
Crew, pers 2
Payload 191 passengers in three classes or cabin 220 passengers in two-class cabin or 255 passengers in economy class or maximum 280 or 32100 kg of cargo (e.g. 14:15 standard LD3 containers or three pallets and 6 ≈ 7 containers LD3)

 

Airbus A310-200 for sale

In mid-1975, the Consortium Airbus Industry began to develop project A300V10 aircraft, representing a A300V4 version with shortened fuselage. In July 1978, the Consortium officially launched aircraft programme, which received the designation of the A310, which was offered in two variants: airlines A310-100 with a flight range of 3700 km, to which virtually no one showed interest, and A310-200 with a range of 5500 km, which became the original model.

The first flight of the prototype A310-200 engines Pratt & Whitney JT9D-7R4 April 3, 1982 took place, and the first flight of an aircraft with General Electric CF6-80A ≈ in August 1982, March 1983 was completed certification in France and Germany in January 1984 g. ≈ in the UK, and in February 1985 g. ≈ in the United States. Regular operation started in April 1983, in the spring of 1986, the design of aircraft A310-200 has several enhancements aimed at further improving fuel efficiency: a small arrow-shaped aerodynamic surfaces (“puck”) at the ends of the wing, the vertical tail unit of carbon brakes and wheels are made of composite materials based on carbon fibers. On the basis of passenger aircraft designed by Combi variant equipped with a-200s A310 side cargo door and designed for transportation of cargoes in weight up to 40.3 tons, and A310-200F cargo aircraft with payload of 43 t. in March 1983, the Consortium began to develop a version of the A310-300 for long airlines.

The aircraft is equipped with digital avionics EFIS complex, comprising four multifunctional display for the necessary information about the flight of the plane, and a digital control system for work onboard systems and preventing failures ESAM. 1983 serially produced ≈ 1988 d. total 85 aircraft were sold to the modification. By the end of 1996, there were 64 aircraft operation.

 SPECIFICATIONS:

 

Modification A310-200
Wingspan, m 43.90
Aircraft length, m 46.66
Aircraft height, m 15.81
Wing area m2 219.00
Mass, kg
empty equipped aircraft 80600
Max takeoff 142000
Engine type 2 BY-PASS TURBOJET ENGINE General Electric CF6-80C2A8 (Pratt Whitney PW4156)
Thrust, kgf 2 x 25420 (26780)
Maximum speed, km/h 940
Cruising speed, km/h 895
Range, km 4070-6670
Service ceiling, m 11300
Crew, pers 2
Payload 191 passengers in three classes or cabin 220 passengers in two-class cabin or 255 passengers in economy class or maximum 280 or 34200 kg of cargo (e.g. 14:15 standard LD3 containers or three pallets and 6 ≈ 7 containers LD3)

 

Airbus A310 prices:

Airbus A 310 for sale – 115 000000 USD;

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