Airbus A318 Single-Aisle Medium-Range Airliner, Europe

Airbus A318 Single-Aisle Medium-Range Airliner, Europe
The Airbus A318 single-aisle medium range-airliner is a short bodied version of the A319.
"The Airbus A318 single aisle medium-range airliner is a short-bodied version of the A319."
The development program was launched in the spring of 1999 and the aircraft took its maiden flight, with Pratt and Whitney PW6000 engines, in January 2002. The first flight with CFM International CFM56-5 engines took place in August 2002.
The A318 with CFM engines received European Join Aviation Authorities (JAA) certification in May 2003. Deliveries began in July 2003 to launch customer Frontier Airlines.
Certification of the aircraft with PW6000A engines was received in December 2005 and the first A318 powered by these engines will enter service with LAN Airlines of Chile in June 2007.
A318 ORDERS AND DELIVERIES
100 A318s have been ordered and 42 delivered. Orders include: Air France (18), America West (15), CIT Aerospace (four), Comlux Aviation (three), Frontier Airlines (nine), GECAS (12), Iberia (ten), International Lease Finance Corporation (ten), LAN (20), Mexicana (ten) and TAROM (four).
Airbus Industrie is a consortium formed by EADS and BAE Systems. EADS, the European Aeronautic Defence and Space Company, was formed by a merger of Aerospatiale-Matra of France, Daimler-Chrysler Aerospace of Germany and CASA of Spain (former members of Airbus). In October 2006, BAE Systems completed the sale of its shareholding to EADS, which is now the sole owner of Airbus.
In November 2007, the A318 fitted with the Thales D-HUDS digital head-up display system was certificated by the European Aviation Safety Agency (EASA). The HUD increases the pilot's situational awareness and allows take-off visibility minima to be lowered from 125m to 75m. The HUD approval will be extended to the other members of the A320 family of aircraft.
The A318, which has a very wide cabin for its class of airliner, has over 95% commonality with other members of the A320 fly-by-wire family of aircraft. The cabin width of 3.70m allows a high-density single-class seating for 129 passengers. A typical mixed class seating arrangement has eight first-class and 99 economy seats.
FLIGHT DECK
The aircraft, in common with the A320, has fly-by-wire controls designed and manufactured by Thales/SFENA. Instead of a control column, the pilot and co-pilot each have a sidestick controller. The digital fly-by-wire system is controlled by five dedicated computers and operates all the primary and secondary flight controls by a combination of electronic signalling and hydraulic jacks.
"The 23,860l-capacity fuel tanks give the A318 a range of 2,800km with the maximum number of passengers."
Very high safety standards have been built into the flight control systems, with system redundancy and flight envelope protection, which will not allow manoeuvres to exceed the aircraft's structural and aerodynamic limitations. It is, for example not possible for the aircraft to fly beyond the maximum operating speed for longer than a few seconds.
The aircraft's flight speed is maintained safely above the stall speed and the throttles are automatically opened to achieve a successful positive climb.
ENGINES
The aircraft is offered with two Pratt & Whitney PW6000 engines or two CFM International CFM 56-5B developing 98kN. The fuel tanks have a capacity of 23,860l giving the aircraft a range of 2,800km with the maximum number of passengers.
LAN Airlines became the launch customer for the PW6000 engine on the A318, in August 2005 and the first production engine was delivered in August 2006.
AVIONICS
The aircraft uses ARINC 700 digital avionics with a digital automatic flight control and flight management system. The advanced digital automatic flight control is integrated with the SFENA autopilot and the Honeywell flight management system.
Honeywell also supplied the aircraft's air data and inertial reference system.
FUSELAGE
The fuselage has been laser welded rather than riveted in order to reduce cost and weight. Large completed sections of the aircraft are built by EADS France (formerly Aerospatiale Matra), the Belgian Belairbus, BAE SYSTEMS, EADS Spain (formerly CASA), and EADS Germany (formerly Daimler Chrysler Aerospace Airbus). The completed aircraft sections are transported to Hamburg for assembly.
The main cabin has two passenger doors on the port side and service doors on the starboard side. The cargo hold has a capacity of 21.21m³. The small baggage doors do not allow pallets or cargo containers to be carried.
"The fuselage is laser welded rather than riveted in order to reduce cost and weight."
The aircraft's air conditioning system is supplied by Liebherr and ABG-Semca. Two Sundstrand constant frequency generators power the primary electrical systems. Another Sundstrand generator powered by the aircraft's auxiliary power unit, can be used during ground operations and in flight if required. The auxiliary power unit is either the Honeywell 131-9A or the Sundstrand APS32000.
LANDING GEAR
The aircraft is equipped with hydraulically retractable tricycle landing gear. The main landing gear units supplied by Dowty retract inwards into the wing and body fairings. The Messier Bugatti nose gear which is stearable, retracts forward. The wheels are fitted with carbon brakes.