Airbus ACJ Corporate Jetliner, Europe

Airbus has developed the ACJ business jet, that can easily be converted to commercial passenger service. The Airbus Corporate Jetliner is based on the airframe of the A319, a twin-engine, single-aisle, medium-range airliner. Airbus Industrie, headquartered in Toulouse, is owned jointly by EADS and BAE Systems.

The A319 airframe is a short-bodied version of the successful Airbus A320 family of aircraft. The main differences between the ACJ and the A320 are the length of usable cabin, two fewer fuselage plugs (shortening the length by nearly 4m), a modified rear cargo door and the deletion of a bulk hold door and forward overwing emergency exit.

In October 2002, the ACJ received FAA approval for scheduled and private operation in the USA.

In June 2003, Airbus increased the baggage capacity on new ACJ models from 3m³ to 10m³ by modifications to the auxiliary fuel tanks arrangement.

ACJ ORDERS AND DELIVERIES

More than 100 aircraft in the ACJ family have been ordered and over 50 ACJ delivered. It is operational with: launch customer Qatar Airways, based at Doha; EADS Deutschland GmbH in Stuttgart: Twinjet Aircraft with headquarters in Bedfordshire, UK; Aero Services in France; Al Kharafi group of Kuwait, DaimlerChrysler of Germany; Blue Moon in the US; PrivatAir of Switzerland; Air Luxor (Masterjet) of Portugal; Alpha Tours of Dubai; AZAL of Azerbaijan, UB Group of India and with a number of other governments and private customers

The ACJ is in service with the following governments: Italian Air Force (two), Venezuelan Air Force (two), French Air Force (two), United Arab Emirates (one), Royal Thai Air Force (one), Azerbaijan, Brazil and Qatar. In May 2004, National Air Services (NAS) of Saudi Arabia ordered two A319 Executive (an ACJ variant).

In November 2005, an order was placed for three ACJ by the first customer from China. In March 2006, the Czech government ordered two aircraft. In May 2006, Pharmair Corporation became the first US customer for the ACJ, with the delivery of one aircraft.

Other variants of the ACJ family are the A318 Elite and the A320 Prestige. Launch customer for the A318 Elite is Comlux of Switzerland with an order for three aircraft placed in November 2005 and an additional two ordered in February 2007. Flight testing began in October 2006 and first deliveries were in May 2007. Orders have been received for 30 aircraft.

The Airbus family of corporate jetliners also includes VIP variants of the A330 and A340 widebody airliners and the A380 Flying Palace, the VIP version of the double-deck airliner. The first order for the Flying Palace was placed in November 2007, by HRH Prince Alwaleed bin Talal bin Abdulaziz Alsaud.

FUSELAGE

The primary structures of the ACJ are of composite construction with Aramid Fibre (AFRP), Glass Fibre (GFRP) and Carbon Fibre (CFRP) Reinforced Plastics.

CABIN

The spacious 24m-long cabin has a floor area of nearly 80m². The cabin layout can include executive suites, equipped offices and meeting rooms, a bedroom, a family living room or sitting room area and bath or shower room according to the needs of the individual client or corporate customer.

The cabin can also be designed to allow public transport flights, so that the aircraft can be operated to allow private or commercial flights. In other words, the interior can be easily converted to provide seamless commercial passenger service.

The cabin environment gives an exceptionally quiet and comfortable flight. The air conditioning system provides a constant fresh air flow at low velocity as the air conditioning manifold is situated in the fuselage recess and maintains the cabin pressure at 8.33lb/in².

The ACJ is fitted with airstairs to allow self sufficiency at airfields with limited airport facilities.

FLIGHT DECK

The ACJ 17-hour flight deck has twice the volume of typical business jets and easily accommodates the pilot and copilot. The aircraft is fitted with Thales/SFENA fly-by-wire controls. The fly-by-wire system incorporates flight envelope protection, reduces costs and pilot workload as well as improving the aircraft's performance. The aircraft has CAT IIIB automatic landing capability.

Each pilot has a side-stick controller allowing single hand control. The fly-by-wire system incorporates many safety features including a high level of redundancy, use of dissimilar redundancy with different computers, different microprocessors, different vendors, division and separation of each computer, the segregation of power supplies and the maximum segregation in signalling lines.

The Thales / VDO Electronic Flight and Information System (EFIS) includes a set of primary flight and navigation displays for each pilot. The primary flight display provides speed, altitude and heading data. Two Thales / VDO Electronic Central Aircraft Monitoring (ECAM) displays are mounted in the centre section between the pilot's and co-pilot's instrument panels.

Rockwell Collins supplies the communications and navigations suite including: ACARS (Aircraft Communications Addressing and Reporting System), ADF (Automatic Direction Finding), VHF Omni-directional Radio range navigation aid with data from the Distance Measuring Equipment (VOR/DME), Multi-Mode Receivers (MMRs), TCAS ll collision avoidance system and weather radar, as well as optional items such as satellite communications and data-links.

ENGINES

The aircraft is offered with two IAE V2527M-A5 engines or two CFM International CFM 56-5B7 developing 111.9kN. The fuel tanks have a capacity of 6,260gal (23,860l) giving the aircraft a range of over 6,500km with eight passengers. The aircraft is approved for 180 minutes ETOPS operations (Extended-range Twin-engine Operations).

The total usable fuel capacity can be increased to 10,640gal by installing up to six auxiliary fuel tanks.

The aircraft is fitted with Full Authority Digital Engine Control (FADEC). FADEC increases engine life and lowers costs through providing fuel control thrust setting computation, engine limit protection, automatic start sequencing and monitoring, thrust reverse control and feedback, flight deck indications and engine health monitoring.

SAFETY STANDARDS

The Airbus Corporate Jetliner meets the FAR Amendment 56 standards for protection against sudden decompression, damage tolerant and fail safe structure, structural fatigue evaluation, bird strike damage protection, emergency exits and access doors and ice protection.