A321-100 - Choice of two 133.4kN (30,000lb) International Aero Engines V-2530-A5 or CFM International CFM-56-5B1 turbofans. CFM-56-5B2s of 139.7kN (31,000lb) available as an option.
A321-200 - As above or 142.3kN (32,000lb) CFM-56-5B3s or 146.8kN (33,000lb) V-2533-A5s.
A321-100 - Max cruising speed 903km/h (488kt), economical cruising speed 828km/h (447kt). Range with 186 passengers and reserves 4352km (2350nm) with V-2530s, 4260km (2300nm) with CFM-56s.
A321-200 - Range 4907km (2650nm).
A321-100 - Operating empty 47,776kg (105,330lb) with V-2530s, 47,900kg (105,605lb) with CFM-56s. Max takeoff (with either engine option) 83,000kg (183,000lb) or 85,000kg (187,390lb).
A321-200 - Operating empty 48,024kg (105,875lb) with CFM-56-5B3s, 48,139kg (106,130lb) with V-2533-A5s, max takeoff 89,000kg (196,210lb) or 93,000kg (205,000lb).
Wing span 34.09m (111ft 10in), length 44.51m (146ft 0in), height 11.76m (38ft 7in). Wing area 123.0m2 (1320sq ft).
Flightcrew of two. Maximum passenger accommodation in a high density layout of 220 passengers. Passenger accommodation in a typical two class arrangement consists of 16 passengers at four abreast, and 170 passengers at six abreast.
250 A321s ordered by late 1998 with 104 delivered.
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