Airbus A400M Atlas - Specifications

Specifications

Data from Airbus Military specifications

General characteristics

  • Crew: 3 or 4 (2 pilots, 3rd optional, 1 loadmaster)
  • Capacity: 37,000 kg (81,600 lb)
    • 116 fully equipped troops / paratroops,
    • up to 66 stretchers accompanied by 25 medical personnel
  • Length: 45.1 m (148 ft 0 in)
  • Wingspan: 42.4 m (139 ft 1 in)
  • Height: 14.7 m (48 ft 3 in)
  • Empty weight: 76,500 kg (168,654 lb) ; operating weight
  • Max takeoff weight: 141,000 kg (310,852 lb)
  • Fuel capacity: 50,500 kg (111,330 lb) internal fuel
  • Max landing weight: 122,000 kg (268,963 lb)
  • Powerplant: 4 × Europrop TP400-D6 turboprop, 8,250 kW (11,060 hp) each
  • Propellers: 8-bladed, 5.3 m (17 ft 5 in) diameter

Performance

  • Cruising speed: 780 km/h (485 mph; 421 kn) (Mach 0.68-0.72)
  • Initial cruise altitude: at MTOW: 9,000 m (29,000 ft)
  • Range: 3,298 km (2,049 mi; 1,781 nmi) at max payload
    • Range at 30-tonne payload: 4,540 km (2,450 nmi)
    • Range at 20-tonne payload: 6,390 km (3,450 nmi)
  • Ferry range: 8,710 km (5,412 mi; 4,703 nmi)
  • Service ceiling: 11,300 m (37,073 ft)
  • Tactical takeoff distance: 980 m (3,215 ft) (aircraft weight 100 tonnes, soft field, ISA, sea level)
  • Tactical landing distance: 770 m (2,526 ft) (as above)
  • Turning radius (ground): 28.6 m

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