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| AIRCRAFT DIMENSIONS |
| | metric |  | imperial | |
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| Overall length | | 59.4 m. | | 195 ft. | |
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| Height | | 16.8 m. | | 55 ft. 3 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 | | 46.06 m. | | 151 ft. 1 in. | |
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| Wingspan (geometric) | | 60.3 m. | | 197 ft. 1 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 | | 23.24 m. | | 76 ft. 3 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 | | four CFM56-5C4 | | four CFM56-5C4 | |
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| Engine thrust range | | 151 kN | | 34,000 lb. slst | |
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| Typical passenger seating | | 261 | | 261 | |
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| Range (w/max. passengers) | | 12,400 km. | | 6,700 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 | | 275 tonnes | | 606.3 lbs. x 1000 | |
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| Maximum takeoff weight | | 275 tonnes | | 606.3 lbs. x 1000 | |
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| Maximum landing weight | | 181 tonnes | | 399 lbs. x 1000 | |
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| Maximum zero fuel weight | | 169 tonnes | | 372.5 lbs. x 1000 | |
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| Maximum fuel capacity | | 155,040 Litres | | 36,678 US gal. | |
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| Typical volumetric payload | | 30.8 tonnes | | 67.9 lbs. x 1000 | |
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