Airbus A321-111 Austrian Airlines "Pinzgau". "1000 Years" Colors. OE-LBB at Gate C04 Terminal 3
Airbus A321-111 Austrian Airlines "Pinzgau". "1000 Years" Colors. OE-LBB at Gate A06 Terminal 1
| 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) |
© 2004-2024 Aeronautic pictures. This website, the content, the design and the pictures and are intended for public non commercial use, and may be redistributed, freely printed, or electronically reproduced in its complete and unaltered form provided distribution is for private use only. Partial and other distribution means require the permission of Aeronautic Pictures. All rights reserved.