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The first A320 jetliner built at the Airbus Final Assembly Line China completed its maiden flight on 18 May from Tianjin |
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| AIRCRAFT DIMENSIONS |
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| Overall length | | 37.57 m. | | 123 ft. 3 in. | |
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| Height | | 11.76 m. | | 38 ft. 7 in. | |
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| Fuselage diameter | | 3.95 m. | | 13 ft. | |
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| Maximum cabin width | | 3.70 m. | | 12 ft. 1 in. | |
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| Cabin length | | 27.51 m. | | 90 ft. 3 in. | |
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| Wingspan (geometric) | | 34.10 m. | | 111 ft. 10 in. | |
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| Wing area (reference) | | 122.6 m2 | | 1,320 ft2 | |
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| Wing sweep (25% chord) | | 25 degrees | | 25 degrees | |
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| Wheelbase | | 12.64 m. | | 41 ft. 5 in. | |
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| Wheel track | | 7.59 m. | | 24 ft. 11 in. | |
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| BASIC OPERATING DATA |
| | metric | | imperial | |
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| Engines | | two CFM56-5 or IAE V2500 | | two CFM56-5 or IAE V2500 | |
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| Engine thrust range | | 111-120 kN | | 22,000-27,000 lb. slst | |
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| Typical passenger seating | | 150 | | 150 | |
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| Range (w/max. passengers) | | 4,800 (5,700) km. | | 2,600 (3,000) nm. | |
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| Max. operating Mach number (Mmo) | | 0.82 Mo. | | 0.82 Mo. | |
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| Bulk hold volume - Standard/option | | 37.41 m3 | | 1,322 ft3 | |
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| DESIGN WEIGHTS |
| | metric | | imperial | |
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| Maximum ramp weight | | 73.9 (77.4) tonnes | | 162.9 (170.6) lbs. x 1000 | |
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| Maximum takeoff weight | | 73.5 (77) tonnes | | 162 (169.8) lbs. x 1000 | |
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| Maximum landing weight | | 64.5 (66) tonnes | | 142.2 (145.5) lbs. x 1000 | |
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| Maximum zero fuel weight | | 61 (62.5) tonnes | | 134.5 (137.8) lbs. x 1000 | |
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| Maximum fuel capacity | | 23,860 (29,840) Litres | | 6,300 (7,885) US gal. | |
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| Typical operating weight empty | | 42.4 tonnes | | 93.5 lbs. x 1000 | |
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| Typical volumetric payload | | 16.6 tonnes | | 36.59 lbs. x 1000 | |
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