Airbus A320 family |
The A320 is the most popular of all Airbus families with at least 10,798 produced units of different kinds. The base model is the narrow-body airplane A320, which had a maiden flight on 22 February 1987. Very soon after that, in 1988, the “stretch variant” A321 was launched. The family expanded with the first “shrink variant”, A319 in the early 1990s. The second “shrink variant”, A318 flew its maiden flight on 15 of January 2002. The A320 family was given a new and more efficient engines in 2010s. Around 2015 the suffix “neo” (new engine options) was added to all models with an engine-refresh and the old variants become known as “ceo” (current engine option). Side-by-side comparison of most variants of the A320 family is present in the following table. Some important technical characteristics are also given for a reference. |
Modification ▾ | Dimensions ▾ | Engine type ▾ | Engine | Capacity ▾ | Performance ▾ |
---|---|---|---|---|---|
A319-111 | Overall length: 33.84 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 11.04 m; | CFM56-5B5 or 5B5/P or 5B6/2P Thrust: 98 kN; Bypass ratio: 6.0; OPR: 32.6; Weight: 2,380 kg; | Typical seating: 124; Max. seating: 156; Load: 4xLD3-45W + 1xLD3/40-45W; Max. cargo: 27.00 m³; | Range: 6,950 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 75.50 t; Max. landing weight: 62.50 t; Max. fuel capaity: 30,190 L; | |
A319-112 | Overall length: 33.84 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 11.04 m; | CFM56-5B6 or 5B6/P Thrust: 100 kN; Bypass ratio: 5.9; OPR: 32.6; Weight: 2,380 kg; | Typical seating: 124; Max. seating: 156; Load: 4xLD3-45W + 1xLD3/40-45W; Max. cargo: 27.00 m³; | Range: 6,950 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 75.50 t; Max. landing weight: 62.50 t; Max. fuel capaity: 30,190 L; | |
A319-132 | Overall length: 33.84 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 11.04 m; | IAE Model V2524-A5 Thrust: 102.5 kN; Bypass ratio: 4.9; OPR: 32.8; Weight: 2,404 kg; | Typical seating: 124; Max. seating: 156; Load: 4xLD3-45W + 1xLD3/40-45W; Max. cargo: 27.00 m³; | Range: 6,950 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 75.50 t; Max. landing weight: 62.50 t; Max. fuel capaity: 30,190 L; | |
A320-211 | Overall length: 37.57 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 12.64 m; | CFM56-5A1 or 5A1/F Thrust: 111 kN; Bypass ratio: 6.0; OPR: 31.3; Weight: 2,270 kg; | Typical seating: 150; Max. seating: 180; Load: 7xLD3-45W; Max. cargo: 37.00 m³; | Range: 6,200 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 78.00 t; Max. landing weight: 66.00 t; Max. fuel capaity: 27,200 L; | |
A320-214 | Overall length: 37.57 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 12.64 m; | CFM56-5B4 or 5B4/P or 5B4/2P Thrust: 120 kN; Bypass ratio: 5.7; OPR: 32.6; Weight: 2,380 kg; | Typical seating: 150; Max. seating: 180; Load: 7xLD3-45W; Max. cargo: 37.00 m³; | Range: 6,200 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 78.00 t; Max. landing weight: 66.00 t; Max. fuel capaity: 27,200 L; | |
A320-216 | Overall length: 37.57 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 12.64 m; | CFM56-5B6 Thrust: 100 kN; Bypass ratio: 5.9; OPR: 32.6; Weight: 2,380 kg; | Typical seating: 150; Max. seating: 180; Load: 7xLD3-45W; Max. cargo: 37.00 m³; | Range: 6,200 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 78.00 t; Max. landing weight: 66.00 t; Max. fuel capaity: 27,200 L; | |
A320-232 | Overall length: 37.57 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 12.64 m; | IAE Model V2527-A5 Thrust: 108.9 kN; Bypass ratio: 4.8; OPR: 32.8; Weight: 2,404 kg; | Typical seating: 150; Max. seating: 180; Load: 7xLD3-45W; Max. cargo: 37.00 m³; | Range: 6,200 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 78.00 t; Max. landing weight: 66.00 t; Max. fuel capaity: 27,200 L; | |
A320-233 | Overall length: 37.57 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 12.64 m; | IAE Model V2527E-A5 Thrust: 110.3 kN; Bypass ratio: 4.8; OPR: 32.8; Weight: 2,404 kg; | Typical seating: 150; Max. seating: 180; Load: 7xLD3-45W; Max. cargo: 37.00 m³; | Range: 6,200 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 78.00 t; Max. landing weight: 66.00 t; Max. fuel capaity: 27,200 L; | |
A320-251N | Overall length: 37.57 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 12.64 m; | CFM LEAP-1A Thrust: 143.05 kN; Bypass ratio: 11.0; OPR: 40.0; Weight: 2,990-3,153 kg; | Typical seating: 165; Max. seating: 194; Load: 7xLD3-45W; Max. cargo: 37.00 m³; | Range: 6,300 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 79.00 t; Max. landing weight: 64.30 t; Max. fuel capaity: 26,730 L; | |
A320-271N | Overall length: 37.57 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 12.64 m; | PW1100G Thrust: 107.82 - 147.28 kN; Bypass ratio: 12.5; OPR: ?; Weight: 2,858 kg; | Typical seating: 165; Max. seating: 194; Load: 7xLD3-45W; Max. cargo: 37.00 m³; | Range: 6,300 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 79.00 t; Max. landing weight: 64.30 t; Max. fuel capaity: 26,730 L; | |
A321-131 | Overall length: 44.51 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 16.90 m; | IAE Model V2530-A5 Thrust: 140.6 kN; Bypass ratio: 4.6; OPR: 35.2; Weight: 2,404 kg; | Typical seating: 185; Max. seating: 220; Load: 10xLD3-45W; Max. cargo: 51.00 m³; | Range: 5,950 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 93.50 t; Max. landing weight: 77.80 t; Max. fuel capaity: 30,030 L; | |
A321-211 | Overall length: 44.51 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 16.90 m; | CFM56-5B3 or 5B3/P or 5B3/2P Thrust: 150 kN; Bypass ratio: 5.4; OPR: 35.5; Weight: 2,380 kg; | Typical seating: 185; Max. seating: 220; Load: 10xLD3-45W; Max. cargo: 51.00 m³; | Range: 5,950 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 93.50 t; Max. landing weight: 77.80 t; Max. fuel capaity: 30,030 L; | |
A321-212 | Overall length: 44.51 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 16.90 m; | CFM56-5B1 or 5B1/P or 5B1/2P Thrust: 130 kN; Bypass ratio: 5.5; OPR: 35.4; Weight: 2,380 kg; | Typical seating: 185; Max. seating: 220; Load: 10xLD3-45W; Max. cargo: 51.00 m³; | Range: 5,950 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 93.50 t; Max. landing weight: 77.80 t; Max. fuel capaity: 30,030 L; | |
A321-231 | Overall length: 44.51 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 16.90 m; | IAE Model V2533-A5 Thrust: 140.6 kN; Bypass ratio: 4.5; OPR: 35.2; Weight: 2,404 kg; | Typical seating: 185; Max. seating: 220; Load: 10xLD3-45W; Max. cargo: 51.00 m³; | Range: 5,950 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 93.50 t; Max. landing weight: 77.80 t; Max. fuel capaity: 30,030 L; | |
A321-232 | Overall length: 44.51 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 16.90 m; | IAE Model V2530-A5 Thrust: 140.6 kN; Bypass ratio: 4.6; OPR: 35.2; Weight: 2,404 kg; | Typical seating: 185; Max. seating: 220; Load: 10xLD3-45W; Max. cargo: 51.00 m³; | Range: 5,950 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 93.50 t; Max. landing weight: 77.80 t; Max. fuel capaity: 30,030 L; | |
A321-251N | Overall length: 44.51 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 16.90 m; | CFM LEAP-1A Thrust: 143.05 kN; Bypass ratio: 11.0; OPR: 40.0; Weight: 2,990-3,153 kg; | Typical seating: 206; Max. seating: 244; Load: 10xLD3-45W; Max. cargo: 51.00 m³; | Range: 7,400 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 97.00 t; Max. landing weight: 79.20 t; Max. fuel capaity: 32,940 L; | |
A321-251NX | Overall length: 44.51 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 16.90 m; | CFM LEAP-1A Thrust: 143.05 kN; Bypass ratio: 11.0; OPR: 40.0; Weight: 2,990-3,153 kg; | Typical seating: 206; Max. seating: 244; Load: 10xLD3-45W; Max. cargo: 51.00 m³; | Range: 7,400 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 97.00 t; Max. landing weight: 79.20 t; Max. fuel capaity: 32,940 L; | |
A321-271N | Overall length: 44.51 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 16.90 m; | PW1100G Thrust: 107.82 - 147.28 kN; Bypass ratio: 12.5; OPR: ?; Weight: 2,858 kg; | Typical seating: 206; Max. seating: 244; Load: 10xLD3-45W; Max. cargo: 51.00 m³; | Range: 7,400 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 97.00 t; Max. landing weight: 79.20 t; Max. fuel capaity: 32,940 L; | |
A321-271NX | Overall length: 44.51 m; Fuselage width: 3.95 m; Wingspan: 35.80 m (with sharklets); Height: 11.76 m; Track: 7.59 m; Wheelbase: 16.90 m; | PW1100G Thrust: 107.82 - 147.28 kN; Bypass ratio: 12.5; OPR: ?; Weight: 2,858 kg; | Typical seating: 206; Max. seating: 244; Load: 10xLD3-45W; Max. cargo: 51.00 m³; | Range: 7,400 km (with sharklets); Ceiling: 11.9-12,5 km; Cruise speed: Mach 0.78 (446 kn; 829 km/h); MMO speed: Mach 0.82 (470 kn; 871 km/h); Max. take-off weight: 97.00 t; Max. landing weight: 79.20 t; Max. fuel capaity: 32,940 L; |