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| AIRCRAFT DIMENSIONS |
| | metric |  | imperial | |
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| Overall length | | 58.8 m. | | 192 ft. 9 in. | |
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| Height | | 17.40 m. | | 58 ft. 1 in. | |
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| Fuselage diameter | | 5.64 m. | | 18 ft. 6 in. | |
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| Maximum cabin width | | 5.28 m. | | 17 ft. 4 in. | |
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| Cabin length | | 45.0 m. | | 147 ft. 8 in. | |
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| Wingspan (geometric) | | 60.3 m. | | 197 ft. 10 in. | |
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| Wing area (reference) | | 362 m2 | | 3,890 ft2. | |
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| Wing sweep (25% chord) | | 30 degrees | | 30 degrees | |
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| Wheelbase | | 22.2 m. | | 72 ft. 10 in. | |
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| Wheel track | | 10.69 m. | | 35 ft. 1 in. | |
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| BASIC OPERATING DATA |
| | metric | | imperial | |
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| Engines | | two CF6-80E1 or PW4000 or RR Trent 700 | | two CF6-80E1 or PW4000 or RR Trent 700 | |
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| Engine thrust range | | 303-320 kN | | 68,000-72,000 lb. slst | |
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| Typical passenger seating | | 253 (3-class) 293 (2-class) | | 253 (3-class) 293 (2-class) | |
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| Range (w/max. passengers) | | 13,400 km. | | 7,250 nm. | |
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| Max. operating Mach number (Mmo) | | 0.86 Mo. | | 0.86 Mo. | |
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| Bulk hold volume - Standard/option | | 19.7 / 13.76 m3 | | 695 / 486 ft3 | |
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| DESIGN WEIGHTS |
| | metric | | imperial | |
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| Maximum ramp weight | | 230.9 (233.9 ) tonnes | | 509 (515.7) lbs. x 1000 | |
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| Maximum takeoff weight | | 230 (238) tonnes | | 507 (524.7) lbs. x 1000 | |
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| Maximum landing weight | | 180 (182) tonnes | | 396.8 (401.2) lbs. x 1000 | |
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| Maximum zero fuel weight | | 168 (170) tonnes | | 370.3 (374.7) lbs. x 1000 | |
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| Maximum fuel capacity | | 139,090 Litres | | 36,750 US gal. | |
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| Typical volumetric payload | | 36.4 tonnes | | 80.2 lbs. x 1000 | |
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