30 Eylül 2012 Pazar

Airbus A340-500

The Airbus A340-500 is a four-engined ultra-long-range widebody airliner with a capacity of maximum 375 passengers produced by the European manufacturer <I>Airbus S.A.S.</I>.

Crew

2

Passengers

typ. 313, max. 375

Propulsion

4 Turbofan Engines

Engine Model

Rolls-Royce Trent 553-61

Engine Power (each)

248,1 kN

55780 lbf

Speed

915 km/h

494 kts
<I>  568 mph</I>

Mmo (max. Mach)

Mach 0.86

Service Ceiling

12.634 m

41.450 ft

Range

16.699 km

9.017 NM
<I>10.377 mi.</I>

Empty Weight

222.000 kg

489.426 lbs

max. Takeoff Weight

368.000 kg

811.300 lbs

max. Landing Weight

240.000 kg

529.109 lbs

Wing Span

63,45 m

208,2 ft

Wing Area

439,4 m²

4730 ft²

Length

67,90 m

222,8 ft

Height

17,10 m

56,1 ft

First Flight

11.02.2002

Production Status

out of production

Production Range

2002-2011

Total Production

32

Developed from

Airbus A340-300

ICAO Code

A345

IATA Code

345

FAA TCDS

A43NM

EASA TCDS

A.015

Data for (Version)

Airbus A340-541

Variants

A340-541, A340-542

</DIV>

Remarks
The Airbus A340-500 is a development of the Airbus A340-200 resp. A340-300. The fuselage is stretched by 3,2 meters (10ft 6in) and the wing by 3,15 meters (10ft 4in) compared to the A340-300. It has the longest range of the A340-Family.

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