In the aviation industry, we're heavily regulated by OEM & Federal "Acceptable Methods, Techniques and Practices". As such, I'd be interested in your input on the following hypothetical repair:
Problem: Pulled Threads in Aluminum Housing (2024-T4)
Proposed Repair: Threaded Insert (Heli-Coil)
Repair Dimensions: Remaining wall thickness after tapping for Heli-Coil = 0.070".
Per the OEM standard practice governing maintenance on this unit, the proposed repair would be considered unacceptable since the remaining wall thickness would fall below the 0.090" min requirement. Based on experience in your respective industries, would you be able to proceed with this repair?
Thanks in advance for your input.
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