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Airbus A400M - Wikipedia, the free encyclopedia

Airbus A400M

From Wikipedia, the free encyclopedia

Airbus A400M

Artist's impression of the A400M

Type Long-range military transport
Manufacturer Airbus Military
Status Early assembly
Number built 0
Unit cost €100 million

The Airbus A400M is a four-engine turboprop military transport & tanker, designed by Airbus Military.

Contents

[edit] Development

The project began as the Future International Military Airlifter (FIMA) group, set up in 1982 by Aerospatiale, British Aerospace, Lockheed, and MBB to develop a replacement for the C-130 Hercules and C-160 Transall. Varying requirements and the complications of international politics caused slow progress. In 1989 Lockheed left the grouping and went on to develop an upgraded Hercules, the C-130J. With the addition of Alenia and CASA the FIMA group became Euroflag.

The partner nations, France, Germany, Italy, Spain, the United Kingdom, Turkey, Belgium, and Luxembourg, signed an agreement in May 2003 to buy 212 aircraft. These nations decided to charge OCCAR with the management of the acquisition of the A400M.

Following the withdrawal of Italy and revision of procurement totals the revised requirement was for 180 aircraft, with first flight in 2008 and first delivery in 2009. On 28 April 2005, South Africa joined the partnership programme with the state owned Denel Aerospace Systems receiving a contract for fuselage components.

[edit] Design

Model of the A400M showing the turboprop engines
Model of the A400M showing the turboprop engines
A400M landing gear
A400M landing gear

The Airbus A400M will increase the airlift capacity and range compared to the aircraft it was originally set to replace, the older versions of the Hercules and Transall. Cargo capacity is expected to double over existing aircraft, both in payload and volume, and range is increased substantially as well. Like Airbus' other aircraft, the A400M will have a full glass cockpit (all information accessed through large colour screens) and fly-by-wire and as such will represent a technological leap compared to the older C-130s and C-160s that many countries now operate.

The Airbus A400M will operate in many configurations including cargo transport, troop transport, MEDEVAC, aerial refuelling, and electronic surveillance.

Originally the SNECMA M138 turboprop (based on the M88 core) was selected to power the A400M. Airbus Military issued a new Request for Proposal in April 2002 which Pratt & Whitney Canada and Europrop answered. Although industry sources indicated the P&WC proposal was the winning bid Airbus Military announced, after evaluating both designs, the selection of the Europrop TP400-D6 in May 2003.

The A400M's wings are primarily carbon fibre reinforced plastic. The cockpit features a fly-by-wire flight control system with sidestick controllers and flight envelope protection. High performance turboprop engines will allow operation in a civil air traffic control environment.[1]

[edit] Production

The A400M assembly at the Seville plant of EADS Spain started in Q1 2007. Airbus plans to manufacture thirty aircraft per year.[2] The major assemblies arrive by Airbus Beluga transporters. The four EuroProp TP400-D6 flight test engines have been delivered in late February 2008 for the first Airbus A400M.[3] According to EADS the first "static tests" of a dedicated A400M complete structure were started on 14th March in Spain.[4]

The first test flight, scheduled until recently for Q1 2008, has been postponed due to repeated program delays, schedule adjustments and mounting financial pressures. EADS announced in early January 2008 that continued development problems with the engines has resulted in a delay to Q2 2008 before the first engine test flights on a C130 testbed aircraft. The first flight of the aircraft, previously scheduled for July 2008 timeframe is now TBD, but a best estimate would be late 2008. There are also stories in the international Aviation Press, denied by Airbus Executives, that the aircraft faces other design and or development issues related to wings and fuselage components.[5] Civil certification under EASA CS-25 will be followed later by certification for military purposes.

[edit] Sales

On 9 December 2004, the South African Air Force announced it was to purchase eight A400Ms at the total cost of €837 million, and had options on 6 more, with South Africa therefore joining the Airbus Military team as an industrial partner. Deliveries are expected from 2010 to 2014.

On 18 July 2005, the Chilean Air Force signed a MOU for 3 aircraft to be delivered between 2018 and 2022,[6] although the deal was later cancelled.[citation needed]

On 8 December 2005 the Royal Malaysian Air Force ordered four A400M, to replace its ageing fleet of C-130s.

Canada issued a tender on 5 July 2006 for 17 new tactical airlifters to replace their old CC-130E models.[7] The A400M would be competing for the order with the Lockheed C-130J Super Hercules. Airbus has proposed the A400Ms would serve as the Canadian Force's mid-range transports. Instead, the government has purchased 4 Boeing C-17s as long-range transports, the first of which was delivered into CF inventory on August 12th 2007 [1] and on June 29th 2007 issued the RFP to Lockheed Martin for procurement of the C-130J,[2] This effectively eliminates the A400M from any hope EADS/Airbus entertained about Canada purchasing the A400M when it finally becomes available. [8] On 16 January 2008, Defence Minister Peter MacKay announced a 1.4 billion deal with Lockheed-Martin to acquire 17 Hercules.[9]

[edit] Orders

Date Country EIS Orders
May 27, 2003 Germany 2010 60
May 27, 2003 France 2009 50
May 27, 2003 Spain 2011 27
May 27, 2003 UK 2010 25
May 27, 2003 Turkey 2009 10
May 27, 2003 Belgium 2018 7
May 27, 2003 Luxembourg 2017 1
December 15, 2004 South Africa 2010 8
December 8, 2005 Malaysia 2013 4
Total: 192

[edit] Specifications

General characteristics

  • Crew: 3-4 (2 pilots, 3rd optional, 1 loadmaster)
  • Capacity: 37,000 kg (82,000 lb), 116 fully equipped troops / paratroops, up to 66 stretchers accompanied by 25 medical personnel
  • Length: 43.8 m (143 ft 8 in)
  • Wingspan: 42.4 m (139 ft 1 in)
  • Height: 14.6 m (47 ft 11 in)
  • Empty weight: 70 tonnes (154,000 lb)
  • Max takeoff weight: 130 tonnes (287,000 lb)
  • Total Internal Fuel: 46.7 tonnes (103,000 lb)
  • Max. Landing Weight: 114 tonnes (251,000 lb)
  • Max. Payload: 37 tonnes (82,000 lb))

Performance

  • Initial Cruise Altitude: at MTOW: 9,000 m (29,000 ft)
  • Range: at Max. payload: 3,300 km (1,782 nmi) (long range cruise speed; reserves as per MIL-C-5011A)
    • Range at 30-tonne payload: 4,800 km (2,592 nmi)
    • Range at 20-tonne payload: 6,950 km (3,753 nmi))
  • Ferry range: 9,300 km (5,022 nmi)
  • Service ceiling 11,300 m (37,000 ft)
  • Tactical Takeoff Distance: 940 m (3 080 ft) (aircraft weight 100 tonnes, soft field, ISA, sea level)
  • Tactical Landing Distance: 625 m (2 050 ft) (see above)
  • Turning Radius (Ground): 28.6 m

[edit] References

[edit] External links

[edit] See also

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