Airbus A321-112 Alitalia  Ready for getting towed in to the hangar

 
Airbus A320 family
  A318-100 A319-100 / A319LR / A319CJ A320-200 A321-200
Cockpit crew Two
Seating capacity 132 (1-class, maximum)
117 (1-class, typical)
107 (2-class, typical)
156 (1-class, maximum)
134 (1-class, typical)
124 (2-class, typical)
180 (1-class, maximum)
164 (1-class, typical)
150 (2-class, typical)
220 (1-class, maximum)
199 (1-class, typical)
185 (2-class, typical)
Seat Pitch 29 in (74 cm) & 30 in (76 cm) (1-class, maximum)
32 in (81 cm) (1-class, typical)
38 in (97 cm) & 32 in (81 cm) (2-class, typical)
28 in (71 cm) & 30 in (76 cm) (1-class, maximum)
32 in (81 cm) (1-class, typical)
36 in (91 cm) & 32 in (81 cm) (2-class, typical)
28 in (71 cm) & 29 in (74 cm) (1-class, maximum)
32 in (81 cm) (1-class, typical)
36 in (91 cm) & 32 in (81 cm) (2-class, typical)
Cargo capacity 21.21 m3 (749 cu ft) 27.62 m3 (975 cu ft)
4 LD3-46
37.41 m3 (1,321 cu ft)
7 LD3-46
51.73 m3 (1,827 cu ft)
10 LD3-46
Length 31.44 m (103 ft 2 in) 33.84 m (111 ft 0 in) 37.57 m (123 ft 3 in) 44.51 m (146 ft 0 in)
Wingspan 34.10 m (111 ft 11 in)
Wing area 122.6 m2 (1,320 sq ft)
Wing sweepback 25 degrees
Tail height 12.51 m (41 ft 1 in) 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) 39,500 kg (87,100 lb) 40,800 kg (89,900 lb) 42,600 kg (93,900 lb) 48,500 kg (106,900 lb)
Maximum zero-fuel weight (MZFW) 54,500 kg (120,200 lb) 58,500 kg (129,000 lb) 62,500 kg (137,800 lb) 73,800 kg (162,700 lb)
Maximum landing weight (MLW) 57.5 t (127,000 lb) 62.5 t (138,000 lb) 66 t (146,000 lb) 77.8 t (172,000 lb)
Maximum take-off weight (MTOW) 68 t (150,000 lb) 75.5 t (166,000 lb) 78 t (172,000 lb) 93.5 t (206,000 lb)
Cruising speed Mach 0.78 (828 km/h/511 mph at 11,000 m/36,000 ft)
Maximum speed Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft)
Maximum range, fully loaded 3,100 nmi (5,700 km; 3,600 mi),
3,200 nmi (5,900 km; 3,700 mi) with sharklets
3,600 nmi (6,700 km; 4,100 mi),
3,700 nmi (6,900 km; 4,300 mi) with sharklets
LR: 5,600 nmi (10,400 km; 6,400 mi)
CJ: 6,500 nmi (12,000 km; 7,500 mi)
3,100 nmi (5,700 km; 3,600 mi),
3,300 nmi (6,100 km; 3,800 mi) with sharklets
3,000 nmi (5,600 km; 3,500 mi),
3,200 nmi (5,900 km; 3,700 mi) with sharklets
Takeoff distance at MTOW
(sea level, ISA)
1,828 m (5,997 ft) 2,164 m (7,100 ft) 2,090 m (6,860 ft) 2,560 m (8,400 ft)
Maximum fuel capacity 24,210 L (5,330 imp gal; 6,400 US gal) 24,210 L (5,330 imp gal; 6,400 US gal) standard
30,190 L (6,640 imp gal; 7,980 US gal) optional
24,050 L (5,290 imp gal; 6,350 US gal) standard
30,030 L (6,610 imp gal; 7,930 US gal) optional
Service ceiling 12,000 m (39,000 ft)
A319 CJ and A321: 12,500 m (41,000 ft)
Engines (2) CFM International CFM56-5 series
Pratt & Whitney PW6000 series IAE V2500 series
Thrust (2) 96106 kN (22,00024,000 lbf) 98120 kN (22,00027,000 lbf) 111120 kN (25,00027,000 lbf) 133147 kN (30,00033,000 lbf)

 

 

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