Airbus A300B4-622R JAS Japan Air System "1990s" Colors. JA8735  on Taxiway D

 
Measurement A300B4 A300-600R A300-600F
Typical capacity 220 passengers (three-class)
266 passengers (two-class)
375 passengers (one-class)
Max payload 48.1 / 54.6 tonnes
(cargo)
Cargo capacity + 22/23 LD3 containers in the lower cargo compartment 15 (21) pallets on the main deck
+ 22/23 LD3 containers
Fuselage length 52.79 meters (173.2 ft) 53.30 meters (174.9 ft)
Overall length 53.62 meters (175.9 ft) 54.08 meters (177.4 ft)
Wingspan 44.84 meters (147.1 ft) 44.85 meters (147.1 ft) (with wing fences)
Wing area 260 square meters (2,800 sq ft)
Overall height 16.62 meters (54.5 ft)
Max cabin width 5.28 meters (17.3 ft)
Fuselage diameter 5.64 meters (18.5 ft)
Operating empty weight typical 88,500 kilograms (195,100 lb) 90,900 kilograms (200,400 lb) 81,900 kilograms (180,600 lb)
MTOW 165,000 kilograms (364,000 lb) 171,700 kilograms (378,500 lb) 170,500 kilograms (375,900 lb)
Takeoff field length (MTOW, SL, ISA) N/A 2,324 meters (7,625 ft)
Cruising speed mach 0.78 (833 km/h, 518 mph, 450 knots at 35,000 ft)
Maximum speed mach 0.86 mach 0.82 (876 km/h, 544 mph, 473 knots at 35,000 ft)
Range fully loaded   6,670 kilometers (3,600 nmi) 7,540 kilometers (4,070 nmi) 4,850 kilometers (2,620 nmi)
Maximum fuel capacity   62,900 liters (16,600 US gal) 68,150 liters (18,000 US gal)
Engines CF6-50C2 or JT9D-59A CF6-80C2 or PW4158
Cockpit crew Three Two

 

 

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