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  • The paper addresses the assessment of detectable cracks by non-destructive inspection methods during the lifetime extension process of ageing metallic commuter aircrafts. Almost all of the ageing commuter aircrafts were certified in compliance with Safe-Life (SL) philosophy many years ago. The requirement for extending the lifetimes of these metallic airframes is topical; therefore, most of the airframes certified as SL structures are at the end of their lifetimes. The Damage Tolerance (DT) philosophy seems to be the only method for service lifetime extension of these ageing aircraft structures. However, application of the DT philosophy induces some relevant additional demands that have not been previously considered. This report describes a few basic approaches and problems associated with the application of the DT philosophy to ageing airframe structures and the work that has to be completed during the lifetime extension certification process from a non-destructive inspection point of view. Examples of teardown test results, including the initial manufacturing defects and detectable cracks, are presented. All procedures described in this report comply with aviation standards and regulations.
  • The paper addresses the assessment of detectable cracks by non-destructive inspection methods during the lifetime extension process of ageing metallic commuter aircrafts. Almost all of the ageing commuter aircrafts were certified in compliance with Safe-Life (SL) philosophy many years ago. The requirement for extending the lifetimes of these metallic airframes is topical; therefore, most of the airframes certified as SL structures are at the end of their lifetimes. The Damage Tolerance (DT) philosophy seems to be the only method for service lifetime extension of these ageing aircraft structures. However, application of the DT philosophy induces some relevant additional demands that have not been previously considered. This report describes a few basic approaches and problems associated with the application of the DT philosophy to ageing airframe structures and the work that has to be completed during the lifetime extension certification process from a non-destructive inspection point of view. Examples of teardown test results, including the initial manufacturing defects and detectable cracks, are presented. All procedures described in this report comply with aviation standards and regulations. (en)
Title
  • NDI aspects of aircraft lifetime extension by changing Safe Life to Damage Tolerance philosophy
  • NDI aspects of aircraft lifetime extension by changing Safe Life to Damage Tolerance philosophy (en)
skos:prefLabel
  • NDI aspects of aircraft lifetime extension by changing Safe Life to Damage Tolerance philosophy
  • NDI aspects of aircraft lifetime extension by changing Safe Life to Damage Tolerance philosophy (en)
skos:notation
  • RIV/00010669:_____/12:#0001505!RIV13-MPO-00010669
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • I
http://linked.open...iv/cisloPeriodika
  • Issue 1
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 153445
http://linked.open...ai/riv/idVysledku
  • RIV/00010669:_____/12:#0001505
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Metallic ageing airframe structure; Life extension; NDI; Teardown analysis; Probability of Detection (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • US - Spojené státy americké
http://linked.open...ontrolniKodProRIV
  • [CBD15D99E7B4]
http://linked.open...i/riv/nazevZdroje
  • International Journal of Terraspace Science and Engineering
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...v/svazekPeriodika
  • Volume 5
http://linked.open...iv/tvurceVysledku
  • Růžek, Roman
  • Boháčová, Marie
issn
  • 1943-3514
number of pages
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