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AD/SA-TP/23 Amdt 2 - Structural Components Fatigue Lives
British Aerospace (Scottish Aviation) TwBritish Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes
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British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes
| AD/SA-TP/23 Amdt 2 | Structural Components Fatigue Lives | 17/2012 |
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| Applicability: | All models. |
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| Requirement: | Action in accordance with the technical requirements of Scottish Aviation Service TNS No. 33 Issue 2.Note: Appendices refer to specific serial numbers; if no Appendix is specified then carryout the instructions of Appendix S of the requirement document. |
| Compliance: | As specified in the requirement document. |
| This Amendment becomes effective on 23 August 2012. | |
| Background: | Scottish Aviation Service promulgates fatigue lives of components based on full scale fatigue testing and the analysis of operator submitted flight plans. If no flight plans were submitted or operational role differs from that originally advised, the manufacturer specifies Appendix S to be appropriate. |
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Mike Higgins
Delegate of the Civil Aviation Safety Authority
17 August 2012