A350-1000
A critical component of the all-new airliner are the engines. Rather than the bleedless configuration used on the Boeing 787, Airbus has confirmed that it will further develop a full bleed air system on the engines. Rolls-Royce has agreed with Airbus to supply a new variant of the Trent engine for the A350 XWB, currently called the Trent XWB. After the low-speed wind tunnel test, Airbus froze the static thrust at sea level for all three proposed variants in the 330–420 kN (74,000–94,000 lbf) range. In June 2007, Rolls-Royce announced that it had signed its biggest ever contract with Qatar Airways for the Trent XWB to power 80 A350 XWBs on order from Airbus worth $5.6 billion at list prices.
| Model | A350-800 | A350-900 | A350-900R | A350-900F | A350-1000 |
| Cockpit crew | Two |
| Seating, typical | 270 (3-class)
276–312 (2-class)
440 (maximum) | 314 (3-class)
315–366 (2-class)
475 (maximum) | - | 350 (3-class)
369–412 (2-class)
550 (maximum) |
| Overall length | 60.54 m (198.6 ft) | 66.89 m (219.5 ft) | 73.88 m (242.4 ft) |
| Wingspan | 64.8 m (213 ft) |
| Wing area | 443 m2 (4,770 sq ft) | ~460 m2 (5,000 sq ft) |
| Wing sweepback | 31.9° |
| Overall height | 17.05 m (55.9 ft) |
| Fuselage width | 5.96 m (19.6 ft) |
| Fuselage height | 6.09 m (20.0 ft) |
| Cabin width | 5.61 m (18.4 ft) |
| Maximum takeoff weight | 259 t(571,000 lb) | 268 t (591,000 lb) | 298 t (657,000 lb) | 308 t (679,000 lb) |
| Maximum landing weight | 193 t (425,000 lb) | 205 t (452,000 lb) | 233 t (514,000 lb) |
| Maximum zero fuel weight | 181 t (399,000 lb) | 192 t (423,000 lb) | 220 t (485,000 lb) |
| Manufacturer's empty weight | | 115.7 t (255,100 lb) | | | |
| Maximum cargo capacity | 28 LD3 or 9 pallets | 36 LD3 or 11 pallets | 90 t (198,000 lb) | 44 LD3 or 14 pallets |
| Cruise speed | Mach 0.85 (903 km/h, 561 mph, 487 knots, at 40,000 ft or 12.19 km) |
| Maximum cruise speed | Mach 0.89 (945 km/h, 587 mph, 510 knots, at 40,000 ft or 12.19 km) |
Maximum range
(with passengers and baggage) | 15,700 km (8,480 nmi) | 15,000 km (8,100 nmi) | 19,100 km (10,300 nmi) | 9,250 km (4,990 nmi)
Maximum cargo payload | 15,600 km (8,420 nmi) |
| Maximum fuel capacity | 129,000 l (34,100 USgal) | 138,000 l (36,500 US gal) | 156,000 l (41,200 US gal) |
| Service ceiling | 43,100 ft (13.1 km) |
| Engines (2×) | RR Trent XWB |
| Maximum thrust capability | 79,000 lbf (351 kN) | 84,000 lbf (374 kN) | 93,000 lbf (414 kN) | 97,000 lbf (431 kN) |
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