Specifications

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)
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 12.56 metres (41 ft 2 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)
Cargo capacity 21.21 m3 (749 cu ft) 27.62 m3 (975 cu ft)
4× LD3
37.41 m3 (1,321 cu ft)
7× LD3
51.73 m3 (1,827 cu ft)
10× LD3
Empty weight, typical 39,500 kg (87,000 lb) 40,800 kg (90,000 lb) 42,600 kg (94,000 lb) 48,500 kg (107,000 lb)
Maximum take-off weight (MTOW) 68,000 kg (150,000 lb) 75,500 kg (166,000 lb) 78,000 kg (170,000 lb) 93,500 kg (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 nautical miles (5,700 km; 3,600 mi) 3,600 nautical miles (6,700 km; 4,100 mi)
LR: 5,600 nmi (10,400 km; 6,400 mi)
CJ: 6,500 nmi (12,000 km; 7,500 mi)
3,200 nautical miles (5,900 km; 3,700 mi) 3,000 nautical miles (5,600 km; 3,500 mi)
Take off run at MTOW (at Sea Level, ISA) 1,355 m (4,446 ft) 1,950 m (6,400 ft) 2,090 m (6,860 ft) 2,180 m (7,150 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 litres (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)
Engines (×2) Pratt & Whitney PW6000 series
CFM International CFM56-5 series
IAE V2500 series
CFM International CFM56-5 series
Thrust (×2) 96–106 kilonewtons (22,000–24,000 lbf) 98–120 kilonewtons (22,000–27,000 lbf) 111–120 kilonewtons (25,000–27,000 lbf) 133–147 kilonewtons (30,000–33,000 lbf)

 Engines

Model     Date   Engines  
A318-111 2003 CFM56-5B8/P
A318-112 2003 CFM56-5B9/P
A318-121 2007 PW6122A
A318-122 2007 PW6124A
A319-111 1996 CFM56-5B5 or 5B5/P
A319-112 1997 CFM56-5B6 or 5B6/P or 5B6/2P
A319-113 1997 CFM56-5A4 or 5A4/F
A319-114 1997 CFM56-5A5 or 5A5/F
A319-115 2002 CFM56-5B7 or 5B7/P
A319-131 1997 IAE Model V2522-A5
A319-132 1997 IAE Model V2524-A5
A319-133 2002 IAE Model V2527M-A5
A320-111 1988 CFM56-5A1 or 5A1/F
A320-211 1988 CFM56-5A4 or 5A4/F
A320-212 1990 CFM56-5A3
A320-214 1996 CFM56-5B4 or 5B4/P or 5B4/2P
A320-216 2005 CFM56-5B6
A320-231 1989 IAE Model V2500-A1
A320-232 1993 IAE Model V2527-A5
A320-233 1995 IAE Model V2527E-A5
A321-111 1995 CFM56-5B1 or 5B1/P or 5B1/2P
A321-112 1995 CFM56-5B2 or 5B2/P
A321-131 1995 IAE Model V2350-A5
A321-211 1997 CFM56-5B3 or 5B3/P or 5B3/2P
A321-212 2005 CFM56-5B1 or 5B1/P or 5B1/2P
A321-213 2005 CFM56-5B2 or 5B2/P
A321-231 1997 IAE Model V2533-A5
A321-232 2005 IAE Model V2530-A5

 

 
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