2009

ICAF 2009, Bridging the Gap between Theory and Operational Practice

Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, The Netherlands,27–29 May 2009

Editors:

ISBN: 978-90-481-2745-0 (Print) 978-90-481-2746-7 (Online)

Table of contents (76 chapters)

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  1. Front Matter

    Pages i-xviii

  2. Full-Scale Fatigue Testing of Aircraft and Aircraft Structural Components

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      Pages 3-14

      A Test Concept For Future Aircraft Fuselage Panels

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      Pages 15-54

      Marker Loads for Quantitative Fractography of Fatigue Cracks in Aerospace Alloys

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      Pages 55-58

      Substantiations of an Airborne Composite Radome Mounted on an Aircraft Dome

  3. Airworthiness Considerations

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      Pages 61-71

      Development of a “Low Stress Criterion” That Eliminate a Large Portion of the Aircraft from Damage Tolerance Based Maintenance Program for Structural Repairs Required by the New Part 26 Federal Regulation

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      Pages 73-90

      Damage Tolerance Philosophy for Bonded Aircraft Structures

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      Pages 91-107

      First Diamond

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      Pages 109-121

      Survey of Structural Repairs and Alterations in Transport Category Airplanes

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      Pages 123-142

      Enhanced Teardown of Ex-Service F/A-18A/B/C/D Centre Fuselages

  4. NDI, Inspections and Maintenance

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      Pages 145-167

      Glare Teardowns From the Megaliner Barrel (Mlb) Fatigue Test

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      Pages 169-186

      30 Years of Damage Tolerance – Have we Got it Right?

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      Pages 187-207

      Compilation Of Damage Findings From Multiple Recent Teardown Analysis Programs

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      Pages 209-221

      Detection Of Arrested Crack For Foam Core Sandwich Structures Using Optical Fiber Sensors Embedded In A Crack Arrester

  5. Life Extension and Management of Ageing Fleets

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      Pages 225-236

      Concept Of The New A320 Fatigue Test

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      Pages 237-244

      The Use Of Composite Material Strips To Extend The Damage-Tolerance Life Of Integrally Stiffened Aluminum Panels

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      Pages 245-261

      Structural Integrity Of A Wing Upper Skin With Exfoliation Corrosion

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      Pages 263-277

      Helicopter Structural Integrity Program Of Polish Mi-24 Hind Helicopters

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      Pages 279-299

      Airframe Life Extension By Optimised Shape Reworking — Overview Of Dsto Developments

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      Pages 301-327

      Evaluation, Modification And Damage Tolerance Of An In-Service Aircraft Critical Area

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      Pages 330-353

      Procedures For Aircraft Structural Teardown Analysis: Development Of A Best Practices Handbook

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      Pages 355-361

      Fatigue Lifetime Improvement Of Arrestment Hook Shanks By Application Of Laser Peening

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