Airbus A300

Information about Airbus A300

Airbus A300 modifications:

  • Airbus A300 +
  • Airbus A300B2/B4
  • Airbus A300-600R
Model A300B4-200
Cockpit crew Three
Main deck 281 (2-4-2 Y @ 34in)
309 (2-4-2 Y @ 31in)
max 345
Lower deck 20 LD3 + bulk
Length 53.61 m (175.9 ft)
Overall height 16.72 m (54.9 ft)
Wingspan 44.83 m (147.1 ft)
Wing area 260 m2 (2,800 sq ft)
Max cabin width 5.287 m (17.35 ft)
Fuselage diameter 5.64 m (18.5 ft)
Pressurized Volume 542 m³ / 19 140 cu ft
MTOW 165,000 kg (363,763 lb)
MLW 136,000 kg (299,829 lb)
MZFW 126,000 kg (277,782 lb)
Max Payload 37,495 kg (82,662 lb)
Maximum fuel capacity (d=0.785) 48,470 kg (106,858 lb) 
62,000 L (16,000 US gal)
Operating empty weight typical 88,505 kg (195,120 lb)
Engines CF6-50C2 or JT9D-59A
Takeoff thrust 230.15–230.5 kN (51,740–51,820 lbf)
Takeoff field length (MTOW, SL, ISA) 2,300 m (7,500 ft)
Cruise speed Mach 0.78 (450 kn; 833 km/h; 518 mph) at FL350
Range 5,375 km / 2,900 nm

Source: //en.wikipedia.org/wiki/Airbus_A300

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