AMS2647F-2017

Fluorescent Penetrant Inspection Aircraft and Engine Component Maintenance

AMS2647F-2017 发布历史

Purpose This specification details requirements and procedures for the detection of defects in aircraft and engine components during maintenance and overhaul operations. This specification contains three appendices which provide additional guidance designed to supplement the information contained in the main body of the document. Because the guidance contained in the appendices is either subjective in nature or may have alternative acceptable approaches@ it is not intended to be binding unless specifically invoked by the Cognizant Engineering Organization (CEO)@ an Original Equipment Manufacturer (OEM)@ or other contractual agreement. Personnel performing inspections to this specification should be familiar with the guidance and exercise good judgment if variance from this guidance is necessary. The following appendices are included: Appendix A - Guidelines for Design@ Procurement and/or Fabrication of Penetrant Systems Appendix B - Guidelines for Assessment of Background Fluorescence Appendix C - Processing and Inspection of Drum Rotors/Deep Well Spools and Other Complex Parts w/Limited Accessibility Processing of parts and interpretation and evaluation of indications revealed by this inspection process shall be accomplished by qualified personnel having experience with fluorescent penetrant inspection. Qualification of personnel shall be in accordance with ATA 105@ NAS 410@ EN 4179@ or ASNT SNT-TC-1A. Basis of Application This process has been used typically by maintenance and overhaul facilities to inspect aircraft and engine components and associated accessories when fluorescent penetrant inspection is specified@ but usage is not limited to such applications.

AMS2647F-2017由SAE - SAE International 发布于 2017-09-01，并于 2017-10-04 实施。

AMS2647F-2017的历代版本如下：

• 2017年09月01日 AMS2647F-2017

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标准号

AMS2647F-2017

发布日期

2017年09月01日

实施日期

2017年10月04日

废止日期

无

中国标准分类号

/

国际标准分类号

/

发布单位

SAE - SAE International

引用标准

42

适用范围

Purpose This specification details requirements and procedures for the detection of defects in aircraft and engine components during maintenance and overhaul operations. This specification contains three appendices which provide additional guidance designed to supplement the information contained in the main body of the document. Because the guidance contained in the appendices is either subjective in nature or may have alternative acceptable approaches@ it is not intended to be binding unless specifically invoked by the Cognizant Engineering Organization (CEO)@ an Original Equipment Manufacturer (OEM)@ or other contractual agreement. Personnel performing inspections to this specification should be familiar with the guidance and exercise good judgment if variance from this guidance is necessary. The following appendices are included: Appendix A - Guidelines for Design@ Procurement and/or Fabrication of Penetrant Systems Appendix B - Guidelines for Assessment of Background Fluorescence Appendix C - Processing and Inspection of Drum Rotors/Deep Well Spools and Other Complex Parts w/Limited Accessibility Processing of parts and interpretation and evaluation of indications revealed by this inspection process shall be accomplished by qualified personnel having experience with fluorescent penetrant inspection. Qualification of personnel shall be in accordance with ATA 105@ NAS 410@ EN 4179@ or ASNT SNT-TC-1A. Basis of Application This process has been used typically by maintenance and overhaul facilities to inspect aircraft and engine components and associated accessories when fluorescent penetrant inspection is specified@ but usage is not limited to such applications.