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Aircraft type: Commercial airplane
Manufacturer: Airbus
Maiden flight year: 1993
A321-100/200 | |
Dimensions | |
---|---|
Length (m) | 44.5 |
Wingspan (m) | 34.1 - 35.8 |
Height (m) | 11.8 |
Wing area (m2) | 122.4 |
Weight | |
Maximum take-off weight (kg) | 89 000 - 93 500 |
Maximum landing weight (kg) | 75 500 - 77 800 |
Operating empty weight (kg) | 48 100 |
Maximum zero fuel weight (kg) | 71 500 - 73 800 |
Maximum payload (kg) | 21 200 |
Standard fuel capacity (litres) | 24 050 - 30 030 |
Performance | |
Range with max payload (km) | 5 000 - 5 900 |
Cruise speed (km/h) | 840 |
Maximum speed (km/h) | 890 |
Maximum operating altitude (m) | 11 900 |
Take-off field length (m) | 2 180 |
Landing field length (m) | 1 580 |
Engines | CFMI CFM56-5A/5B, 2 x 30000-33000 lbIAE V2500-A5, 2 x 30000-33000 lb |
Fuel efficiency (g/pass*km) | 18.2 |
Fuel flow rate (kg/h) | 3 200 |
Cabin Data | |
Passengers (1-class) | 220 - 236 |
Passengers (2-class) | 185 |
Cabin length (m) | 34.4 |
Cabin width (m) | 3.7 |
61% | 17% | 22% |