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Dimensions & key data

The A350-900 is sized to seat more than 300 passengers comfortably over routes as long as 7,750 nautical miles.

The use of the most modern design and manufacturing techniques results in exceptional fuel economy. Outstanding operating efficiency is further enhanced when the commonality advantages of operation with other A350 XWB models are included.

A350-900 specs

Key figures

  Range 7 750 nm 14 350 km
Typical seating x 315
  Max payload - lb x 1 000 - tonnes
A350-900 Wing span Wing span 212 ft 5 in 64.75 m
A350-900 Overall length Overall length 219 ft 5 in 66.8 m
A350-900 Height Height 55 ft 11 in 17.05 m

Dimensions

Overall length 219 ft 5 in 66.8 m
Cabin length - - -
Fuselage width 19 ft 7 in 5.96 m
Max cabin width 18 ft 5 in 5.61 m
Wing span (geometric) 212 ft 5 in 64.75 m
Height 55 ft 11 in 17.05 m
Track 34 ft 9 in 10.60 m
Wheelbase 94 ft 1 in 28.67 m

New-generation design

The A350 XWB has an entirely new, uncompromised, 21st century design with a wider and taller fuselage for extra space and enhanced passenger comfort. Three A350 XWB models are available – with the A350-900 offering a typical passenger capacity of 315 seats (in a two-class layout) and operating range 7,750 nautical miles.  

Capacity

Pax
Typical seating 315
Max -
Freight
LD3 capacity underfloor 36 36
Max pallet number underfloor 11 11
Bulk hold volume 400 ft³ 11.3 m³
Total volume (Bulk loading) 6 088 ft³ 172.4 m³

Performance

Range 7 750 nm 14 350 km
Mmo M0.89
Max ramp weight 592.8 lb x 1000 268.9 tonnes
Max take-off weight 592.9 lb x 1000 268.0 tonnes
Max landing weight 451.9 lb x 1000 205.0 tonnes
Max zero fuel weight 423.3 lb x 1000 192.0 tonnes
Max fuel capacity 36 456 USG 138 000 litres

Engines x2

RR Trent XWB
Thrust range 84 000 lb slst 374 kN
Aircraft weights and capabilities shown are the highest values
Ranges shown are for typical passenger load

For more on technical specifications

Information required operating and supporting Airbus aircraft and airport planning, can be downloaded in Adobe PDF format, from the Aircraft Characteristics page.

Further specialised documents are in the on-line Technical Data library.