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AIRBUS INDUSTRIE

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.

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AIRBUS INDUSTRIE

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  1. AIRBUS INDUSTRIE by A Bhattacharya

  2. 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

  3. AIRBUS INDUSTRIE • THE ENTITIES • The co-operation between the different entities that make up Airbus today goes back to the 1920s. They are:- • DaimlerChrysler Aerospace AG (DASA) of Germany ( Original Founder) • Aerospatiale Matra S.A of France (Original Founder) • Hawker Siddley (Original Founder) • Fokker (Original Founder) • Construcciones Aeronauticas S.A. (CASA) of Spain ( Full Partner in1971) • Bae ( Full Partner in1979) • HEADQUARTER • Toulouse

  4. 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.

  5. 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

  6. 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

  7. PRODUCTION • FINAL ASSEMBLY LINES. • A320/380 TOULOUSE , HAMBURG • A300/310/330/340 TOULOUSE

  8. 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

  9. 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.

  10. AIRBUS FAMILY

  11. 4150nm/7700km with full pax payload. A300-600 PERFORMANCE • Optimized for maximum profitability in the demanding mid-size regional market. • The A300-600 seats 266 passengers in a typical two-class layout and has a range of 4,000 nm/7,700 km. PARIS NEW YORK BANGKOK

  12. A300-600 CABIN LAYOUTS SINGLE CLASS- 298 SEATS TWO CLASS- 266 SEATS

  13. A300-600 Aircraft Dimensions Overall Length 177ft 5in 54,10m Cabin Length 133ft 6in 40,70m Fuselage Diameter 18ft 6in 5,64m Max. Cabin Width 17ft 4in 5,28m Height 54ft 4in 16,54m Wheelbase 61ft 1in 18,62m Track 31ft 6in 9,60m

  14. A300-600 Wing Dimensions Wing Span (geometric) 147ft 1in 44,84m Wing Area (reference) 2800ft2 / 260m2 Sweep (25% chord) 28 degrees

  15. A300-600 Design Weights lbx1000 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

  16. A300-600 Basic Operating Data Powerplants 2x CF6-80C2 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) 0,82Mo Containers Underfloor - Standard/Option 22/23 Pallets Underfloor 4 Bulk Hold Volume - Standard/Option 610 (318)ft3 17,3 (9,0)m3 Total Volume - Standard/Option 4 086 (3952)ft3 115,7 (1119)m3

  17. A310 Performance • The A310 has been designed for optimum operating efficiency in regional operations. • Optimized design range of up to 5200 nautical miles/9600km

  18. A310 Cabin Layout Single class- 247 seats Two class- 240 seats

  19. A310 Aircraft Dimensions • Overall Length153ft 1in/ 46,66m • Cabin Length 109ft 1in/ 33,25m • Fuselage Diameter 18ft 6in/ 5,64m • Max. Cabin Width 17ft 4in/ 5,28m • Height 51ft 10in/ 15,80m • Wheelbase 49ft 11in/ 15,21m • Track 31ft 6in/ 9,60m

  20. A310 Wing Dimensions Wing Span (geometric) 1440in/ 43,90m Wing Area (reference) 2360ft/ 2219m2 Sweep (25% chord) 28 degrees

  21. A310 DESIGN WEIGHTS lb X 1000tonnes 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)

  22. A310 BASIC OPERATING DATA Powerplants 2X CF6-80C2 or PW 4000 Thrust Range 52 000-59 000 lb Typical Seating (two class) 220 Range (max. pax) 4350 (5200)nm 8050 (9600)kmMax. Operating Mach n° (Mmo) 0,84Mo Containers Underfloor - Standard/option 14 (15) Pallets Underfloor 3 Bulk Hold Volume - Standard/Option 610 (318)ft3/ 173 (90)m3 Total Volume - Standard/Option 2 822 (2688) ft3 799 (761) m3

  23. A320 FAMILY A319

  24. A319 A318 • Launched 1999 1997 • Seat/ class 107/ 2 124/2* • Range 3200nm/ 3700nm/ • 6000 km 6800km • Engines 2xCFM56-5/ 2xIAE V2500 • PW 6000 • Thrust Range 21 600-23 800 lb 22000-27000lb • Max. Operating Mach n° 0.82 0.82 • Wing Area (reference) 1320ft/2 122.6m2 1320ft2/122.6m2 • Sweep (25% chord) 25 degrees 25 degrees • * corporate jet liner

  25. A320 A321 • Launched 1988 1989 • Seat/ class 150/ 2 185-220/2 • Range 3000nm/ 3000nm • 5500km 5500km • Engines 2xCFM56-5/ 2xIAE V2500 • IAE V2500 • Thrust Range 22000-27000lb 30000-33000lb • Max. Operating Mach n° 0.82 0.82 • Wing Area (reference) 1320ft/2 122.6m2 1320ft2/122.6m2 • Sweep (25% chord) 25 degrees 25 degrees

  26. A330/340 FAMILY • Four Engines for ETOPS Freedom

  27. A330-300 A340-600 • Launched 1993 1993 • Seat/ class 295/3 380/3 • 335/2 • Range 5600nm/ 7500nm • 10400 km 5500km • Engines 2xCF6-80E-1/ 4xRR Tent 556 • PW 4000 • Thrust Range 22000-27000lb 56000lb • Max. Operating Mach n° 0.86 0.86 • Wing Area (reference) 3892ft² 4729ft ² • Sweep (25% chord) 30 degrees 31.1 degrees

  28. A340 CABIN SPACE UTILIZATION BY DIFFERENT AIRWAYS

  29. A340 IN AIRLINE AIRCRAFT IN OPERATION ON ORDER

  30. A340 IN

  31. A340 IN

  32. PRODUCTION SCORE CARD • BOEING AIRBUS • 707/720 - 1010 (1958-92) A300 - 523 (1972) • 717-200 - 111+ (1998) A310-200/300- 255 (1987) • - 1832 (1963-84) A319/320/321 - 1856+ (1987) • 737-100/200 - 1144 (1967-88) A330-200/300 - 243+ (1992) • 737-300/500/600 - 1988 (1984) • 737-600/700/800/900 - 1230+ (1997) • 747-100/200/300/400 - 1317 (1961) A340-200/300/600 - 222+ (1993) • 757-200/300 - 1022+ (1982) • 767-200/300/400 - 889+ (1981) • 777-200/300 - 420+ (1995) Source: Commercial Jet Aircraft Census by Bill Harms. • http://www.bird.ch/bharms/asrstart.htm

  33. Thank you

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