AIRBUS INDUSTRIE by A Bhattacharya AIRBUS INDUSTRIE GENESIS

AIRBUS INDUSTRIE by A Bhattacharya

AIRBUS INDUSTRIE GENESIS • Airbus was established in 1970 as a European consortium of French, German and later, Spanish and U. K companies. • Bring about cooperation among European Aircraft manufacturers and be able to compete effectively with the U. S. giants. • Overcome national divides, share development costs, collaborate in the interests of a greater market share, and even agree to a common set of measurements and a common language. • Airbus changed the face of the business, and brought airlines, passengers and crews the benefits of real competition

AIRBUS INDUSTRIE THE ENTITIES • The co-operation between the different entities that make up Airbus today goes back to the 1920 s. They are: Ø Daimler. Chrysler Aerospace AG (DASA) of Germany ( Original Founder) Ø Aerospatiale Matra S. A of France (Original Founder) Ø Hawker Siddley (Original Founder) Ø Fokker (Original Founder) Ø Construcciones Aeronauticas S. A. (CASA) of Spain ( Full Partner in 1971) Ø Bae ( Full Partner in 1979) HEADQUARTER Toulouse

ORGANISATION • A joint stock company operating as a wholly owned subsidiary of Airbus France, Airbus Deutschland, Airbus España and Airbus UK • An Executive Committee of ten members, led by Airbus President and Chief Executive Officer Noël Forgeard, and including the heads of each core business function, are responsible for managing all Airbus activities. • It employs directly some 46, 000 people of over 50 nationalities.

PRODUCTION THE MAIN MANUFACTURING UNITS ARE: • CABIN INTERIOR. • BUXTEHUDE - GERMANY • LAUPHEIM - GERMANY • FUSELAGE (FORWARD & AFT) • HAMBURG • BREMEN • VAREL • NORDENHAM • FUSELAGE (COCKPIT & CENTRE) • MEAULTE - FRANCE • St. NAZAIRE - FRANCE • NANTES - FRANCE

PRODUCTION • EMPENNAGE (VERT. TAILPLANE) • STADE - Germany • WINGS • BROUGHTON - UK • FILTON - UK • PYLON & NACELLE • TOULOUSE - FRANCE • EMPENNAGE (HOR. TAILPLANE) • PEURTO REAL - SPAIN • GETAFE - SPAIN • ILLESCAS - SPAIN • STADE - GERMANY

PRODUCTION FINAL ASSEMBLY LINES. • A 320/380 TOULOUSE , HAMBURG • A 300/310/330/340 TOULOUSE

OPERATIONS • More than 150 sites throughout the world, which includes • 16 development and manufacturing facilities in France, Germany, the U. K. and Spain. • Several subsidiaries, six regional offices, three training centres, five spare centres and 120 resident customer services offices • International network of some 1, 500 suppliers in more than 30 countries, including 800 suppliers in the United States • Three main operation hubs Airbus North America Airbus Japan Airbus China

PROCUREMENT • The largest single area of suppliers is the United States. • Over 800 companies produce hardware ranging from engines to window glass. • Host of excellent suppliers from all over Europe and in Asia, Africa and Australia, providing aero structure commodities, materials, equipment systems, propulsion systems as well as company consumables and services or product related services.

A 300 -600 PERFORMANCE • Optimized for maximum profitability in the demanding mid-size regional market. • The A 300 -600 seats 266 passengers in a typical two-class layout and has a range of 4, 000 nm/7, 700 km. PARIS NEW YORK BANGKOK 4150 nm/7700 km with full pax payload.

A 300 -600 CABIN LAYOUTS SINGLE CLASS- 298 SEATS TWO CLASS- 266 SEATS

A 300 -600 Aircraft Dimensions Overall Length 177 ft 5 in 54, 10 m Cabin Length 133 ft 6 in 40, 70 m Fuselage Diameter 18 ft 6 in 5, 64 m Max. Cabin Width 17 ft 4 in 5, 28 m Height 54 ft 4 in 16, 54 m Wheelbase 61 ft 1 in 18, 62 m Track 31 ft 6 in 9, 60 m

A 300 -600 Wing Dimensions Wing Span (geometric) 44, 84 m 147 ft 1 in Wing Area (reference) 2800 ft 2 / 260 m 2 Sweep (25% chord) 28 degrees

A 300 -600 Design Weights lbx 1000 tonnes Max. Ramp Weight 365, 8 (380, 5) 165, 9 (172, 6) Max. Take-off Weight 363, 8 (378, 6) 165, 0 (171, 7) Max. Landing Weight 304, 2 (308, 6) 138, 0 (140) Max. Zero fuel Weight 286, 6 130 Max. fuel Capacity 16 380 USg 62 000 Litres Operating Weight Empty 198, 6 90, 1 Typical Volumetric Payload 76, 9 34, 9

A 300 -600 Basic Operating Data Powerplants 2 x CF 6 -80 C 2 or PW 4000 Thrust Range 56 000 -61 500 lb Typical Seating (two class) 266 Range (max. pax) 4050 (4 150)nm, 7 500 (7 700)km Max. Operating Mach N°. (Mmo) 0, 82 Mo Containers Underfloor - Standard/Option 22/23 Pallets Underfloor 4 Bulk Hold Volume - Standard/Option 610 (318)ft 3 17, 3 (9, 0)m 3 Total Volume - Standard/Option 4 086 (3952)ft 3 115, 7 (1119)m 3

A 310 Performance • The A 310 has been designed for optimum operating efficiency in regional operations. • Optimized design range of up to 5200 nautical miles/9600 km

A 310 Cabin Layout Single class- 247 seats Two class- 240 seats

A 310 Aircraft Dimensions • Overall Length 153 ft 1 in/ 46, 66 m • Cabin Length 109 ft 1 in/ 33, 25 m • Fuselage Diameter 18 ft 6 in/ 5, 64 m • Max. Cabin Width 17 ft 4 in/ 5, 28 m • Height 51 ft 10 in/ 15, 80 m • Wheelbase 49 ft 11 in/ 15, 21 m • Track 31 ft 6 in/ 9, 60 m

A 310 Wing Dimensions Wing Span (geometric) 1440 in/ 43, 90 m Wing Area (reference) 2360 ft/ 2219 m 2 Sweep (25% chord) 28 degrees

A 310 DESIGN WEIGHTS lb X 1000 tonnes Max. Ramp Weight 332. 7 (363. 5) 150. 9 (164. 9) Max. Take-off Weight 330. 7 (361. 6) 150. 0 (164. 0) Max. Landing Weight 271. 2 (273. 4) 123. 0 (124. 0) Max. Zero fuel Weight 249, 1 (251, 3) 113. 0 (114. 0) Max. fuel Capacity 6 130 (19 940) 61070 Typical operating Weight Empty 178. 2 (182. 1) 80. 8 (82. 6) Typical Volumetric Payload 58. 9 (47. 6) 2 6. 7 (21. 6)

A 310 BASIC OPERATING DATA Powerplants 2 X CF 6 -80 C 2 or PW 4000 Thrust Range 52 000 -59 000 lb Typical Seating (two class) 220 Range (max. pax) Max. Operating Mach n° (Mmo) 4350 (5200)nm 8050 (9600)km 0, 84 Mo Containers Underfloor - Standard/option 14 (15) Pallets Underfloor 3 Bulk Hold Volume - Standard/Option 610 (318)ft 3/ 173 (90)m 3 Total Volume - Standard/Option 2 822 (2688) ft 3 799 (761) m 3

A 320 FAMILY A 319

A 318 A 319 • Launched 1999 1997 • Seat/ class 107/ 2 124/2* • Range 3200 nm/ 3700 nm/ 6000 km 6800 km • Engines 2 x. CFM 56 -5/ 2 x. IAE V 2500 PW 6000 • Thrust Range 21 600 -23 800 lb 22000 -27000 lb • Max. Operating Mach n° 0. 82 0. 82 • Wing Area (reference) 1320 ft/2 122. 6 m 2 1320 ft 2/122. 6 m 2 • Sweep (25% chord) 25 degrees * corporate jet liner

A 320 A 321 • Launched 1988 1989 • Seat/ class 150/ 2 185 -220/2 • Range 3000 nm/ 3000 nm 5500 km • Engines 2 x. CFM 56 -5/ 2 x. IAE V 2500 IAE V 2500 • Thrust Range 22000 -27000 lb 30000 -33000 lb • Max. Operating Mach n° 0. 82 0. 82 • Wing Area (reference) 1320 ft/2 122. 6 m 2 1320 ft 2/122. 6 m 2 • Sweep (25% chord) 25 degrees

A 330/340 FAMILY Four Engines for ETOPS Freedom

A 330 -300 • Launched 1993 A 340 -600 1993 • Seat/ class 295/3 380/3 335/2 • Range 5600 nm/ 7500 nm 10400 km 5500 km • Engines 2 x. CF 6 -80 E-1/ 4 x. RR Tent 556 PW 4000 • Thrust Range 22000 -27000 lb 56000 lb • Max. Operating Mach n° 0. 86 0. 86 • Wing Area (reference) 3892 ft² 4729 ft ² • Sweep (25% chord) 30 degrees 31. 1 degrees

A 340 CABIN SPACE UTILIZATION BY DIFFERENT AIRWAYS

A 340 IN AIRLINE AIRCRAFT IN OPERATION ON ORDER Air France A 340 -300 14 Austrian AL A 340 -200 2 Austrian AL A 340 -300 2 Iberia A 340 -300 18 18 Lufthansa A 340 -200 7 Lufthansa A 340 -300 32 Lufthansa A 340 -600 10 Olympic A 340 -300 4 DAT A 340 -200 3 DAT A 340 -300 2 SAS A 340 -300 4 3 TAP A 340 -300 4 THY A 340 -300 7 Virgin A 340 -300 10 Virgin A 340 -600 << Back to Map Close Window 10

A 340 IN Airline Aircraft Number On Order Air China 340 - 300 3 Cathay Pacific A 340 -300 11 China Airlines A 340 -300 7 China Eastern A 340 -300 5 China Eastern A 340 -600 5 Emirates Airlines A 340 -500 6 Emirates Airlines A 340 -600 8 Gulf Air A 340 -300 6 Kuwait Airlines A 340 -300 4 Philippine Airlines A 340 -200 4 Philippine Airlines A 340 -300 4 Singapore Airlines A 340 -300 16 0 Singapore Airlines A 340 -500 5 Sri Lanka Airlines A 340 -300 3 3 (ILFC)

A 340 IN Airline Aircraft Number On Order Aerolineas Argent. A 340 -200 4 Aerolineas Argent. A 340 -600 6 Air Jamaica A 340 -300 1 Lan Chile A 340 -300 4 3

PRODUCTION SCORE CARD BOEING AIRBUS 707/720 - 1010 (1958 -92) A 300 - 523 (1972) 717 -200 - 111+ (1998) A 310 -200/300 - 255 (1987) 727 - 1832 (1963 -84) A 319/320/321 - 1856+ (1987) 728737 -100/200 - 1144 (1967 -88) (1992) 729737 -300/500/600 A 330 -200/300 - 243+ - 1988 (1984) 730737 -600/700/800/900 - 1230+ (1997) 731747 -100/200/300/400 - 1317 (1961) A 340 -200/300/600 - 222+ (1993) 732757 -200/300 - 1022+ (1982) 733767 -200/300/400 - 889+ (1981) 734777 -200/300 - 420+ (1995) Aircraft Harms. Source: Commercial Jet Census by Bill

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