Commercial Aircraft Directory - Aircraft Specification

Airbus - A350-900

The A350-900 will be the initial version of the new Airbus family when it enters service in mid-2013. As Airbus SAS works to refine the shape and structure of the A350 XWB, it is currently working on a "four-shell concept", which uses four composite sections of differing thicknesses which are joined by lap-joints. The manufacturer is considering offering up to 10-abreast seating. The anticipated composition of the A350 XWB structure has been set at 52% (by weight) carbonfibre, 20% aluminium, 7% steel, and 7% other materials. Launch customer, with the first firm order for six A350-900 on 21 November 2005, was lessor International Lease Finance Corp (ILFC). The first firm order from an airline was made by TAM Brasil, for ten aircraft on 20 December 2005. This order was converted to 22 A350XWB-900s in June 2007. In June 2008 the MTOW's of all three A350 XWB variants were raised by 3 tonnes so as to ensure that the aircraft can achieve its payload/range targets.

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date:  
Certification date: 13 2013  
Launch customer(s): TAM Linhas Aéreas
 

PRINCIPAL DIMENSIONS

Fuselage width: 5.96 m 
Fuselage height: 16.9 m 
Fuselage length: 65.2 m 
Cabin length:  
Cabin width: 5.61 m 
Cabin height:  
Cabin volume:  
Hold volume:  

WEIGHTS

Empty operating:  
Max zero fuel: 189,500 kg 
MTOW: 268,000 kg 
MLW: 202,500 kg 
Standard fuel capacity: 138,000 kg 
Max fuel capacity: 288,000 kg 

SPEEDS

Normal cruise:  
Max cruise: 919 km/h 

PERFORMANCE

Long Range Cruise alt:  
Max ceiling:  
Take off field length:  
Landing field length:  
Max Payload Range:  
Range notes:  
Max passengers: 0  
Typical passengers: 315  

POWERPLANT

Category: Turbofan  
Manufacturer: Rolls-Royce  
Model/Submodel: Trent XWB-83  
Thrust: 369 kN