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Download File 6.28 MB JULY 2003 FLIGHT AIRWORTHINESS SUPPORT 32 TECHNOLOGY AIRBUS TECHNICAL DIGEST FAST 32 FAST 32 FLIGHT AIRWORTHINESS SUPPORT TECHNOLOGY JULY 2003 Just happened… Coming soon… 2 Advanced materials and technologies 3 for A380 structure Technology platform for future development AIRBUS TECHNICAL DIGEST Jérôme Pora PAGE Airbus Flight Operational Commonality 9 1 in action FAST 32 FAST Régine Vadrot Christian Aubry Gerrit van Dijk Revision of rules for Extended and 17 Long Range Operations Editor: Denis Dempster ETOPS & LROPS Art Director: Agnès Massol-Lacombe André Quet in association with Chandler Gooding Lithium thickened grease 25 London • Leeds • Toulouse Higher performance General Purpose grease Customer Services Marketing for Airbus aircraft Tel: +33 (0)5 61 93 39 29 Céline Normand Fax: +33 (0)5 61 93 27 67 E-mail: [email protected] From the archives... 31 Printer Escourbiac Extended Range Operations – The Beginning FAST may be read on Internet http://www.airbus.com under Customer Services/Publications Customer Services 32 ISSN 1293-5476 Around the clock… Around the world Airbus Customer Services © AIRBUS 2003. All rights reserved Cover photo: The articles herein may be reprinted without permission except where Lay-up of carbon fibre side panel for A380 vertical tail plane copyright source is indicated, but with acknowledgement to Airbus. Articles which may be subject to ongoing review must have their accuracy verified prior to reprint. The statements made herein do not constitute an offer. They are based on the assumptions shown and are expressed in good faith. Where the supporting grounds for these statements are not shown, This issue of FAST has been printed on paper the Company will be pleased to explain the basis thereof. produced without using chlorine, to reduce Computer graphics by I3M waste and help conserve natural resources. Photographs (cover/pages 3-8/pages 25-30) by Philippe Masclet & Hervé Bérenger Every little helps! JUST HAPPENED… COMING SOON… Just happened… 12TH PERFORMANCE & A318/A319/A320/A321 AIRBUS LEASING OPERATIONS CONFERENCE SYMPOSIUM CONFERENCE 7-11 April 2003 11-16 May 2003 10-12 June 2003 Rome, Italy Cancun, Mexico Madrid, Spain The 12th Performance and This year’s Single-aisle The fact that one-third Operations Conference was attended by 229 Symposium gathered 135 representatives of the Airbus in-service fleet (and 40% of representatives from 92 airlines and 21 repre- from 51 airlines and 67 vendor represen- ordered aircraft) are leased, underlines the sentatives from vendors, authorities and other tatives. importance of such a conference. About 65 organisations. representatives of leasing companies, finan- The programme included actual in- cial institutions and Airbus experts attended. Customers appreciated demonstrations at service issues covering structure, engine Airbus stands showing Less Paper Cockpit and systems for purely technical matters Key points covered included increased (LPC), Performance Engineering Programmes and general topic discussions on mainte- transparency for pricing of standard options, (PEP), Load & Trim Sheet software (LTS), nance economics, reliability enhancement retrofit modification offers, reduced lead- Line Operations & Monitoring Systems and others. 2 time for service bulletins and kits, and air- (LOMS), Line Operations Assessment System craft configuration tracking. (LOAS) and Airbus on-line system (AOLS). Awards for excellence in reliability were 3 given to All Nippon Airways, Jet Blue The increasing awareness that leasing During the conference,1 which has been held and TAM. companies play a full part in the Airbus cus- every two years since 1980, some 85 presenta- tomer community with their own specific tions were made in nine sessions covering top- requirements was a major benefit of the ics such as LPC Administration, Operations, conference. Performance, PEP, Cost Index, New Cockpit and Operations Information Management. It SECOND AIRBUS SPARES LOGISTICS CONFERENCE 2003 was concluded by presentations from different 17-18 June 2003 Hamburg, Germany airlines allowing operational experiences to be shared. The second Airbus Spares Logistics Conference in Hamburg was attended by more than 80 participants – including 26 from 17 customers. PAGE 2 On-time delivery of spare parts requires integration and management of flexible supply chains between supplier activities and customers’ requirements. Physical distribution FAST 32 FAST 17TH AIRBUS HUMAN FACTORS SYMPOSIUM qualified communication and IT-based monitoring systems are key to harmonising all 1-3 July 2003 Helsinki, Finland spares related processes. 4 The 17th Human Factors Symposium gathered Airbus Spares Support and Services presented the new Customised Spares Logistics together approximately 100 human factors and (CSL) concept that transfers the transport responsibility from the customer to Airbus. safety Airbusspecialists took fromits common more than design 20 Airbus Airbus Spares Support has a clear mandate to continue improving the Spares Logistics. operators.philosophy The symposium was organised in Also the vendors are being encouraged to offer similar support to the Airbus customers. co-operation with Finnair, which is celebrating its 80th anniversary.5 JAN 03 FEB 03 MAR 03 APR 03 MAY 03 JUN 03 JULY 03 I 2 3 4 5 Coming soon… 1 2 3 AUG 03 SEPT 03 OCT 03 NOV 03 DEC 03 2ND AIRBUS FLIGHT OPERATIONS MONITORING & 18TH AIRBUS HUMAN A300/A300-600/A310 SAFETY DEVELOPMENT CONFERENCE FACTORS SYMPOSIUM TECHNICAL SYMPOSIUM September 2003 New York City, USA Seville, Spain Rome, Italy October 2003 November 2003 As part of our commitment to increase safety In association with Jet Blue, Preparation for this technical symposium performance, Airbus plans to continue its Airbus is organising its next is already in progress. Operators are being invited constructive dialogue with all parties at this Human Factors Symposium to give their feedback and input before the pro- Rome conference. This gathering follows on in New York. gramme covering their needs is finalised. There from the first very successful conference held in will be presentations on actual in-service issues Hong Kong. In it, Airbus will continue affecting the A300/A310 programme as well as 1 the dialogue2 with its opera- subjects of more general interest. The programme will cover the integrated Airbus tors at a proven forum, dis- safety plan with tailored solutions, the evolution cussing human factors For information, contact3 your local resident cus- of Flight Operation Monitoring (FOM) package aspects with practical and tomer support manager. Agenda and participation and regulatory aspects. operational perspectives. form will be sent out in September. ADVANCED MATERIALS AND TECHNOLOGIES FOR A380 STRUCTURE Advanced materials and technologies for PAGE 3 A380 structure 32 FAST TECHNOLOGY PLATFORM FOR FUTURE DEVELOPMENTS A competitive new aircraft programme with a life span Results from manufacture and structural testing of of 40 to 50 years requires the introduction of advanced full-scale demonstrators supported the decision- and new materials – combined with new manufacturing making process for selection of structural design technologies – which allow for further optimisation as concepts, materials and manufacturing technologies the aircraft family evolves. Thus, the A380-800, the in order to ensure that only mature technologies and launch version of the A380 family, establishes a proven concepts were taken on board. “technology platform” for future developments. Design solutions and material applications envisaged An “Initial Set of Structural Design Drivers” was were also reviewed with structure and maintenance established in early 1997, giving guidance for a experts from airlines to get approval with respect to preliminary selection of possible materials for inspections and repairs. Workshops with airlines are different sub-components of the airframe. The regarded as a key element of the “technology materials choice results from a down-selection down-selection process”. process, which reviewed material performance, manufacture of components and associated costs at the same time. Jérôme Pora Deputy Director Structure A380 Programme ADVANCED MATERIALS AND TECHNOLOGIES FOR A380 STRUCTURE ADVANCED MATERIALS AND TECHNOLOGIES FOR A380 STRUCTURE THE A380 GENERAL STRUCTURAL DESIGN CRITERIA NEW AND ADVANCED METALLIC MATERIALS Materials distribution (weight breakdown) on A380 structure General structural design criteria for A380 fuselage & empennage The distribution of materials for the A380 shows that aluminium 2% surface protections makes up the largest proportion 2% miscellaneous Fin box with 61% share of airframe struc- 22% composite materials - Static strength - Compression ture weight (Figure 3). Upper fuselage Static strength & fatigue - Crack growth 3% GLARE (internal pressure) - Residual strength Performance improvement initiat- Bird strike Rudders ives must first address this large impact - Static strength proportion of airframe weight and - Shear search for improved materials. The 10% titanium Bird strike specific direction in which to go is impact & steel given by the “drivers for structural design”, e.g. high strength and/or damage tolerance, stability and corrosion resistance. So there was Horizontal stabiliser box - Static strength a strong demand for further improve- Strength & fatigue - Compression ments of primary aluminium struc- (ground load cases) Strength for Lower fuselage ture on the A380, in particular on jacking loads - Static strength
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