Description
This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. This process has been used typically by maintenance and overhaul facilities personnel to inspect aluminum aircraft structures for service-induced cracks, but usage is not limited to such applications.
Product Details
- Published:
- 06/11/2013
- File Size:
- 1 file , 580 KB
- Note:
- This product is unavailable in Ukraine, Russia, Belarus
