Airbus A319

Information about Airbus A319 

Airbus A319 modifications:

  • Airbus A319-111
  • Airbus A319-112
  • Airbus A319-113
  • Airbus A319-114
  • Airbus A319-115
  • Airbus A319-131
  • Airbus A319-132
  • Airbus A319-133
  • Airbus ACJ319
  • Airbus A319LR
Cockpit crew Two
Exit limit 160 / 150
1-class max. seating 156 at 28–30 in (71–76 cm) pitch
1-class, typical 134 at 32 in (81 cm) pitch
2-class, typical 124 (8F @ 38 in, 116Y @ 32 in)
Cargo capacity 27.7 m3 (980 cu ft)
Unit load devices 4× LD3-45
Length 33.84 m (111 ft 0 in)
Wheelbase 11.04 m (36 ft 3 in)
Track 7.59 m (24 ft 11 in)
Wingspan 35.8 m (117 ft 5 in) 
Wing area 122.4 m2 (1,318 sq ft)
Wing sweepback 25 degrees
Tail height 11.76 m (38 ft 7 in)
Cabin width 3.70 m (12 ft 2 in)
Fuselage width 3.95 m (13 ft 0 in)
Fuselage height 4.14 m (13 ft 7 in)
Operating empty weight (OEW) 40.8 t (90,000 lb)
Maximum zero-fuel weight (MZFW) 58.5 t (129,000 lb)
Maximum landing weight (MLW) 62.5 t (138,000 lb)
Maximum takeoff weight (MTOW) 75.5 t (166,000 lb)
Cruising speed Mach 0.78 (829 km/h; 515 mph)
Maximum speed Mach 0.82 (871 km/h; 541 mph)
Range, typical payload[d] 3,750 nmi, 6,950 km
ACJ range 6,000 nmi, 11,100 km
Takeoff (MTOW, SL, ISA) 1,850 m (6,070 ft)
Landing (MLW, SL, ISA) 1,360 m (4,460 ft)
Fuel capacity 24,210–30,190 L (6,400–7,980 US gal)
Service ceiling 39,100–41,000 ft (11,900–12,500 m)
Engines (×2) CFM56-5B, 68.3 in (1.73 m) fan
IAE V2500A5, 63.5 in (1.61 m) fan
Thrust (×2) 98–120 kN (22,000–27,000 lbf)

Source: https://en.wikipedia.org/wiki/Airbus_A319

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