Airbus A350 for sale
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Information about Airbus A350
Airbus A350 is a new wide-body airliner for long-haul airlines being developed by the Airbus concern (EADS). Formally, the A350 project was launched on December 1, 2006 in order to replace the A330 and A340 aircraft. The main purpose of creating an airliner is to compete with the American company Boeing. The new Airbus A350 is a direct competitor to such aircraft as the Boeing 777 and Boeing 787 Dreamliner, also known as the Boeing 7E7.
Initially, the Airbus consortium wanted to use the A330 as the basis for a new aircraft. It was supposed to install new engines on the A330 and rework the aerodynamics of the aircraft. This project was named “A330-200 Lite”. But then this idea was abandoned, and the design of the A350 began as the development of a new aircraft. Although the fuselage of the first version of the A350 externally resembled the A330, nevertheless, it was a different aircraft with new wings made of new composite materials based on carbon fiber, with new engines and new flight stabilizers. The A350 also featured a modern layout and trim that seats up to nine seats in the same row. The new project of the aircraft received the name A350 XWB (Extra Wide Body).
August 31, 2010 began the first stage of construction of the aircraft. When it was built, new composite materials were widely used. They make up 52 percent of the total weight of the aircraft. According to the expectations of Airbus, the aircraft should be 10-15 percent cheaper to operate than its direct competitor Boeing 787. In early 2013, ground tests of the first Airbus A350 were conducted. The first flight of the new A350 took place on July 14, 2013. It was a model Airbus A350-900.
The new aircraft is equipped with two turbojet Trent XWB engines with a load of 374.5 kN each from Rolls & Royce. Negotiations are also underway with General Electric on the use of GEnx (General Electric Next-generation) engines. According to the Airbus corporation, the A350 with the new engines should increase fuel efficiency by 25 percent compared to the A330.
The airliner will be offered to air carriers in three versions. The first shortened version, 60.54 meters long, designated as A350-800. It is designed to carry 245 passengers in three classes at a distance of 15,900 kilometers. The estimated time for commissioning of this modification is at the end of 2014 or at the beginning of 2015.
The second version, it’s the base version – А350-900. This version will fly over a distance of 15,000 kilometers. And it can accommodate 314 passenger seats in a three-class configuration, or 366 seats in a two-class one. The length of the aircraft is 66.89 meters. This version will be put into operation in the second half of 2014.
The third modification of the aircraft, the A350-1000, is the largest aircraft in the Airbus A350 family. Its length is 73.88 meters. He will start entering the airline from mid-2015. This version is capable of carrying up to 412 passengers in two classes or 350 passengers in a three-class configuration. The range of this model will be 14,900 kilometers.
At present, the Airbus consortium, from its customers, has already received about 580 orders for the supply of А350 of various modifications.
Airbus A350 modifications:
- Airbus A350 XWB
- Airbus A350-800
- Airbus A350-900
- Airbus A350-900ULR
- Airbus A350 Regional
- Airbus A350-1000
- Airbus ACJ350
|Exit limit||160 / 150|
|1-class max. seating||156 at 28–30 in (71–76 cm) pitch|
|1-class, typical||134 at 32 in (81 cm) pitch|
|2-class, typical||124 (8F @ 38 in, 116Y @ 32 in)|
|Cargo capacity||27.7 m3 (980 cu ft)|
|Unit load devices||4× LD3-45|
|Length||33.84 m (111 ft 0 in)|
|Wheelbase||11.04 m (36 ft 3 in)|
|Track||7.59 m (24 ft 11 in)|
|Wingspan||35.8 m (117 ft 5 in)|
|Wing area||122.4 m2 (1,318 sq ft)|
|Wing sweepback||25 degrees|
|Tail height||11.76 m (38 ft 7 in)|
|Cabin width||3.70 m (12 ft 2 in)|
|Fuselage width||3.95 m (13 ft 0 in)|
|Fuselage height||4.14 m (13 ft 7 in)|
|Operating empty weight (OEW)||40.8 t (90,000 lb)|
|Maximum zero-fuel weight (MZFW)||58.5 t (129,000 lb)|
|Maximum landing weight (MLW)||62.5 t (138,000 lb)|
|Maximum takeoff weight (MTOW)||75.5 t (166,000 lb)|
|Cruising speed||Mach 0.78 (829 km/h; 515 mph)|
|Maximum speed||Mach 0.82 (871 km/h; 541 mph)|
|Range, typical payload[d]||3,750 nmi, 6,950 km|
|ACJ range||6,000 nmi, 11,100 km|
|Takeoff (MTOW, SL, ISA)||1,850 m (6,070 ft)|
|Landing (MLW, SL, ISA)||1,360 m (4,460 ft)|
|Fuel capacity||24,210–30,190 L (6,400–7,980 US gal)|
|Service ceiling||39,100–41,000 ft (11,900–12,500 m)|
|Engines (×2)||CFM56-5B, 68.3 in (1.73 m) fan|
|IAE V2500A5, 63.5 in (1.61 m) fan|
|Thrust (×2)||98–120 kN (22,000–27,000 lbf)|
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