Airbus A320-233 Wizzair "2004s Colors". "WIZZ Wizzair.com" Titles. HA-LPA Turning away from the runway
Airbus A320-233 Wizzair "2004s Colors". "WIZZ Wizzair.com" Titles. HA-LPA At the holding point Taxiway L1 ready for departure
| 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) | 96–106 kN (22,000–24,000 lbf) | 98–120 kN (22,000–27,000 lbf) | 111–120 kN (25,000–27,000 lbf) | 133–147 kN (30,000–33,000 lbf) |
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