Technical Data Airbus A321
Aircraft Dimensions
| ft | m | |
| Overall length | 146ft. | 44.51 |
| Height | 38ft. 7in. | 11.76 |
| Fuselage diameter | 13ft. | 3.95 |
| Maximum cabin width | 12ft. 1in. | 3.70 |
| Cabin length | 113ft. | 34.44 |
| Wing span (geometric) | 111ft. 10in. | 34.10 |
| Wing area (reference) | 1,320 ft2 | 122.6 m2 |
| Wing sweep (25% chord) | 25 degrees | 25 degrees |
| Wheelbase | 55ft. 48in. | 16.91 |
| Wheel track | 24ft. 11in. | 7.59 |
Basic Operation Data
| imperial | metric | |
| Engines | two CFM56-5 or IAE V2500 | two CFM56-5 or IAE V2500 |
| Engine thrust range | 27 000-33 000 lb. slst | 133 (138) (147) kN |
| Typical passenger seating | 185 | 185 |
| Range (max. pax) | 2 350 (3 050) nm | 4,400 (5,600) km |
| Max. operating Mach number (Mmo) | 0.82 Mo. | 0.82 Mo. |
| Bulk hold volume - Standard/option | 1,829 ft3 | 51.76 m3 |
Design Weights
| imperial | metric | |
| Max. ramp weight | 183.9 (207) lbs. x 1000 | 83.4 (93.9) t |
| Max. take-off weight | 183 (206.1) lbs. x 1000 | 83 (93.5) t |
| Max. landing weight | 166.5 (171.5) lbs. x 1000 | 71.5 (77.8) t |
| Max. zero fuel weight | 157.6 (162.7) lbs. x 1000 | 67.2 (73.8) t |
| Maximum fuel capacity | 6 260 (6 850) US gal. | 23,700 (29,680) l |
| Typical operating weight empty | 106.3 lbs. x 1000 | 48.2 t |
| Typical volumetric payload | 46.74 lbs. x 1000 | 21.2 t |
