Crew | 2 | |
Passengers | 107 / 117 | |
Propulsion | 2 Turbofan Engines | |
Engine Model | CFM Intl. (Pratt & Whitney) CFM56-5 (PW6000) | |
Engine Power (each) | 96,1 kN | 21600 lbf |
Speed | 900 km/h | 486 kts 559 mph |
Mmo (max. Mach) | Mach 0.82 | |
Service Ceiling | 12.131 m | 39.800 ft |
Range | 5.950 km | 3.213 NM 3.697 mi. |
Empty Weight | 34.500 kg | 76.059lbs |
max. Takeoff Weight | 59.000 kg | 130.073lbs |
max. Landing Weight | 56.000 kg | 123.459lbs |
Wing Span | 34,10 m | 111,9 ft |
Wing Area | 122,6 m² | 1320 ft² |
Length | 31,44 m | 103,1 ft |
Height | 12,56 m | 41,2 ft |
First Flight | 15.01.2002 | |
Production Status | in production | |
Developed from | Airbus A320 | |
ICAO Code | A318 | |
IATA Code | 318 | |
FAA TCDS | A28NM | |
EASA TCDS | A.064 | |
Data for (Version) | Airbus A318 | |
Variants | A318–111, A318–112, A318–121, A318–122 |
RemarksThe Airbus A318 is a shortened (minus 6 meters / 20 ft) development of the A320. It is powered by either Pratt & Whitney PW6000 or CFM International CFM56-5 engines.
AIRBUS A318 ELITE
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