Vidaman
Mechanical
- Jul 28, 2002
- 39
Hello All,
I'm building a kit plane that is taking longer than anticipated to complete. I have some AN470AD an AN426AD rivets that are over 4 years old. I have heard, but have been unsuccessful in confirming, that aluminum alloy 2117-T4 will age harden. My question is, if true, what is a legitimate working life for these rivets?
The reason I ask is that the rivets seem more difficult to buck than they have in the past. I'm not sure if this is true or all in my head. None of my engineering references provide the specific information of acceptable life.
Anyone with good experience or a real reference out there?
Thanks,
-Mike
I'm building a kit plane that is taking longer than anticipated to complete. I have some AN470AD an AN426AD rivets that are over 4 years old. I have heard, but have been unsuccessful in confirming, that aluminum alloy 2117-T4 will age harden. My question is, if true, what is a legitimate working life for these rivets?
The reason I ask is that the rivets seem more difficult to buck than they have in the past. I'm not sure if this is true or all in my head. None of my engineering references provide the specific information of acceptable life.
Anyone with good experience or a real reference out there?
Thanks,
-Mike