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Airbus A310 wide-body "1983"

The Airbus A350 is a long-range, wide-body jet airliner developed by Airbus. The first A350 design proposed by Airbus in 2004, in response to the Boeing 787 Dreamliner, would have been a development of the A330 with composite wings and new engines. As market support was inadequate, in 2006, Airbus switched to a clean-sheet "XWB" (eXtra Wide Body) design, powered by Rolls-Royce Trent XWB turbofan engines. The prototype first flew on 14 June 2013 from Toulouse in France

Airbus A310 wide-body "1983"

Role Wide-body aircraft
National origin Multinational
Manufacturer Airbus Industrie
Designer Airbus Industrie
First flight 3 April 1982; 39 years ago
Introduction April 1983 with Swissair
Status In limited service
Primary users Mahan Air / Iran Air / Royal Jordanian / 
Produced 1981–1998
Number built 255
Developed from Airbus A300
Variants Airbus A310 MRTT / Airbus CC-150 Polaris

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Airbus A310 wide-body "1983"

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Airbus A310 "1983"

The Airbus A310 is a wide-body aircraft; designed and manufactured by Airbus Industrie, then a consortium of European aerospace manufacturers. Airbus had demand for an aircraft smaller than the A300, the first twin-jet wide-body. On 7 July 1978, the A310 (initially the A300B10) was launched with orders from Swissair and Lufthansa. On 3 April 1982, the first prototype conducted its maiden flight, and it received its type certification on 11 March 1983.

Keeping the same eight-abreast cross-section, the A310 is 6.95 m (22.8 ft) shorter than the initial A300 variants, and has a smaller wing, down from 260 to 219 m2 (2,800 to 2,360 sq ft). The A310 introduced a two-crew glass cockpit, later adopted for the A300-600 with a common type rating. It was powered by the same General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan jet engines

A310 Airliner Design

The Airbus A310 was a medium- to long-range twin-engined wide-body jet airliner. Initially a derivative of the A300, the aircraft had originally been designated the A300B10. It was essentially a shortened variant of the earlier aircraft; however, there were considerable differences between the two aircraft.[20] Specifically, the fuselage possessed the same cross-section, but being shorter than the A300, it provided capacity for a typical maximum of 200 passengers. The rear fuselage was heavily re-designed, featuring altered tapering, while involved a move aft of the rear bulkhead to create additional capacity; this same design change was later transferred back to later variants of the A300, such as the A300-600 and A330/A340 fuselages.[20] The A310 also had a different emergency exit configuration, consisting of four main doors (two at the front and two at the rear of the aircraft), and two smaller doors over the wings

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Airbus A310 Wide-body (1983)

The A300 provided Airbus the experience of manufacturing and selling airliners competitively. The basic fuselage of the A300 was later stretched (A330 and A340), shortened (A310), or modified into derivatives (A300-600ST Beluga Super Transporter). In 2006, unit cost of an -600F was $105 million. In March 2006, Airbus announced the impending closure of the A300/A310 final assembly line, making them the first Airbus aircraft to be discontinued. The final production A300, an A300F freighter, performed its initial flight on 18 April 2007, and was delivered to FedEx Express on 12 July 2007. Airbus has announced a support package to keep A300s flying commercially. Airbus offers the A330-200F freighter as a replacement for the A300 cargo variants

Specifications

Crew 2 Passengers 266 / 345
Propulsion 2 Turbofan Engines
Engine Model General Electric CF6-80C2A5
Engine Power (each) 267,3 kN 60100 lbf

Wing Span 44,84 m 147 ft 1 in
Wing Area 260,0 m˛ 2799 ft˛
Length 54,08 m 177 ft 5 in
Height 16,54 m 54 ft 3 in
First Flight 28.10.1972 / 08.07.83 (-600R)

Speed 891 km/h 481 kts 554 mph
Mmo (max. Mach) Mach 0.82
Service Ceiling 12.192 m 40.000 ft
Range 6.667 km 3.600 NM 4.143 mi.
Empty Weight 78.201 kg 172.404 lbs
max. Takeoff Weight 170.500 kg 375.888 lbs
max. Landing Weight 140.000 kg 308.647 lbs

  • First Flight 28.10.1972 / 08.07.83 (-600R)
    Production Status out of production
    Production Range 1974-2007
    Total Production 561

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Only two A300B1s were built: the first prototype, registered F-WUAB, then F-OCAZ, and a second aircraft, F-WUAC, which was leased in November 1974 to Trans European Airways (TEA) and re-registered OO-TEF. TEA instantly subleased the aircraft for six weeks to Air Algérie, but continued to operate the aircraft until 1990. It had accommodation for 300 passengers (TEA) or 323 passengers (Air Algérie) with a maximum weight of 132 t and two General Electric CF6-50A engines of 220 kN thrust. The A300B1 was five frames shorter than the later production versions, being only 50.97 m (167.2 ft) in length.

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