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The Airbus A318 is a short-to-medium range commercial passenger aircraft manufactured by Airbus. It is the smallest member of the Airbus A320 family, which also includes the A319, A320, and A321. The A318 was designed to cater to the needs of airlines operating in smaller markets or airports with limited runway lengths.
One of the notable features of the Airbus A318 is its size. It has a length of approximately 31 meters and can accommodate up to 132 passengers in a typical two-class configuration. This makes it suitable for regional flights or routes with lower passenger demand.
The A318 is powered by two engines, typically either CFM International CFM56 or Pratt & Whitney PW6000 engines. These engines provide the necessary thrust for the aircraft to take off and maintain its flight. The A318 also incorporates advanced avionics and systems, ensuring a safe and efficient flying experience.
In terms of performance, the Airbus A318 has a maximum range of around 3,100 nautical miles (5,700 kilometers) and a cruising speed of approximately 450 knots (833 kilometers per hour). This allows it to operate on both short-haul and medium-haul routes, connecting smaller cities and airports.
The A318 has been well-received by airlines around the world. It offers operational flexibility, allowing airlines to serve markets that may not be economically viable with larger aircraft. Additionally, its smaller size enables it to operate in airports with shorter runways, expanding the number of destinations it can serve.
Overall, the Airbus A318 is a versatile and efficient aircraft that meets the needs of airlines operating in smaller markets or airports with limited infrastructure. Its compact size, range, and performance make it a popular choice for regional flights, connecting passengers to their destinations efficiently and comfortably.
| Cockpit crew | Two |
|---|---|
| Exit Limit | 136 |
| 1-class max. seating | 132 at 29–30 in (74–76 cm) pitch |
| 1-class, typical | 117 at 32 in (81 cm) pitch |
| 2-class, typical | 107 (8F at 38 in (97 cm) pitch, 99F at 32 in (81 cm)) |
| Cargo capacity | 21.2 m3 (750 cu ft) |
| Length | 31.44 m (103 ft 2 in) |
| Wingspan | 34.10 m (111 ft 11 in) |
| Wing area | 122.4 m2 (1,318 sq ft) |
| Wing sweepback | 25° |
| Tail height | 12.56 m (41 ft 2 in) |
| Cabin width | 3.70 m (12 ft 2 in) |
| Fuselage width | 3.95 m (13 ft) |
| Operating empty weight | 39,500 kg (87,100 lb) |
| Maximum zero-fuel weight (MZFW) | 54,500 kg (120,200 lb) |
| Maximum landing weight (MLW) | 57,500 kg (126,800 lb) |
| Maximum take-off weight (MTOW) | 68,000 kg (150,000 lb) |
| Cruising speed | Mach 0.78 (829 km/h; 447 kn; 515 mph) |
| Maximum speed | Mach 0.82 (871 km/h; 470 kn; 541 mph) |
| Range (typical payload) | 3,100 nmi (5,740 km; 3,570 mi) |
| ACJ range | 4,200 nmi (7,780 km; 4,830 mi) |
| Takeoff (MTOW, SL, ISA) | 1,780 m (5,840 ft) |
| Landing (MLW, SL, ISA) | 1,230 m (4,040 ft) |
| Fuel capacity | 24,210 L (6,400 US gal) |
| Ceiling | 39,100–41,000 ft (11,900–12,500 m) |
| Engines (×2) | CFM56-5B 68.3 in (1.73 m) fan PW6000 56.5 in (1.44 m) fan |
| Thrust (×2) | 96–106 kN (22,000–24,000 lbf) |
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