| A300-600 | A300-600F | A300-600F Beluga
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Overall length | 177 ft. 5 in. | 177 ft. 5 in. | 184 ft. 3 in.
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Height | 54 ft. 3 in. | 54 ft. 3 in. | 56 ft. 7 in.
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Fuselage diameter | 18 ft. 5 in. | 18 ft. 6 in. | 13 ft.
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Maximum cabin width | 17 ft. 4 in. | 17 ft. 4 in. | 12 ft. 2 in.
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Cabin length | 133 ft. 6 in. | 133 ft. 6 in. | 123 ft. 8 in.
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Wingspan (geometric) | 147 ft. 1 in. | 147 ft. 1 in. | 147 ft. 2 in.
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Wing area (reference) | 2,800 ft² | 2,800 ft2 | 1,317 ft2
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Wing sweep (25% chord) | 28º | 28 degrees | 25 degrees
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Wheelbase | 61 ft. 1 in. | 61 ft. 1 in. | 36.25 ft.
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Wheel track | 31 ft. 6 in. | 31 ft. 6 in. | 25 ft.
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| BASIC OPERATING DATA
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Engines | two CF6-80C2 or PW4000 | two CF6-80C2 or PW4000 | GE CF6-80C2A8
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Engine thrust range | 56,000-61,500 lbs | 56,000-61,500 lb. slst | 26,752-26,977 lb. slst
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Typical passenger seating | 266 | 22 (23) | 15 (21) pallets
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Range (w/max. passengers) | 1,950 (2,650) nm. | 39.3-tons payload: 1,500 nm. / 25.6-tons payload: 2,500 nm.
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Max. operating Mach number (Mmo) | 0.82 | 0.82 Mo. | 0.82 Mo.
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Bulk hold volume - Standard/option | 361.0 | 398 ft3 |
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DESIGN WEIGHTS
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Maximum ramp weight | 380.5 lbs. X 1000 | 377.9 (366) lbs. X 1000
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Maximum takeoff weight | 378.5 lbs. X 1000 | 375.9 (370.4) lbs. X 1000 | 341,713 lb.
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Maximum landing weight | 308.6 lbs. X 1000 | 308.6 (315.5) lbs. X 1000 | 308,644 lb.
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Maximum zero fuel weight | 286.6 lbs. X 1000 | 286.6 (300.9) lbs. X 1000 | 294,314 lb.
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Maximum fuel capacity | 18,000 US gal. | 18,000 (11,730) US gal. | 6,303 (8,520)(9,095) US gal.
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Typical operating weight empty | 200.4 lbs. X 1000 | 180.7 lbs. X 1000 |
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Typical volumetric payload | 76.9 lbs. X 1000 | 105.9 / 120.2 lbs. X 1000 | 103,616 lb.
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